Power Plant Engineering by G.R.nagpal
Power Plant Engineering by G.R.nagpal
Power Plant Engineering by G.R.nagpal
MR Nagpal
?.Sr Engineering (Mechanical)
rech. (Mech. Engg.)
F 7. Mechanical Engineering Department
i.A., Institute of Engineering
ARIDAfiAD (Haryana)
me Drawing
me ToilJ'i- . ing
we Design
igineering arA lesign
Forming Process
Khanna Pub1ishe
Published by:
Romesh Chander Khanna
for KHANNA PUBLISHERS
2-B, Nath Market, Nai Sarak
Delhi- 110 006 Undia)
Fifteenth Edition
Fourth Reprint: 2006
Printed at:
3•.: . htP.-inters, Phari Bhoja,
Delhi 110006 .
DEDICATED
TO
MY LATE RESPECTED MOTHER
Preface
This book is quite suitable for degree and diploma engineering
students of many Universities and for A.M.I.E. (Sec. B). The book
has been revised and brought up-to-date to suit the requirements
of the students. More problems have been solved on steam power
plant and hydro-power plant. The overall objective is to present
the subject matter in more simple language. Objective type problems
have been added to make the subject matter more clear.
Although carefully prepared and reviewed the book may con-
thin some errors. The author will be thankful to the readers for
bringing them to his notice. Suggestions for improvement of the
book shall be gratefully received and appreciated.
The author is thankful to Sh. Romesh Chander Khanna for his
most co-operative and painstaking attitude for bringing out this
edition in a very short time.
—G.R. NAGPAL
Contents
Chapter
Pages
1. Sources of Energy
1-52
1.1. Power
1.2. Sources of Energy
1.2.1. Conventional and Non-Conventional.
Sources of Energy
1.3. Fuels
.
1.3.1. Solid Fuels
1.4. Calorific Value of Fuels
1.5. To Calculate Approximate Flue Gas Loss
... 10
1.6. Types of Coal
1.7. Liquid Fuels
1.7.1. Oil Properties
1.8. Advantages of Liquid Fuels over Solid Fuels
1.9. Gaseous Fuels
1.10. Advantages of Gaseous Fuels. over Solid Fuels
1.10.1. Composition of Liquid Fuels .
1.11. Comparison of Sources of Power
1.12. Sources of Energy in India
1.12.1. Conservation of Energy
1.13. Combustion of Fuels
1.14. Products of Combustion
1.15. Combustion Chemistry
1.16. Combustion of Gaseous Fuels
1.17. Weight of Air Required for Complete Combustion
of Fuel
1.18. Coal Selection
1.18.1. Ranking and grading of coal
1.19. Composition of Solid Fuels . ... 34
1:19.1. Ash
1.19.2. Volatile Matter
1.20. Weight of Excess Air Supplied
1.21. Requirements of Fuel
1.22. Principal Stages of Combustion
1.23. Complete Combustion
1.24. Incomplete Combustion
...38
1.24.1. Weight of Carbon in Flue Gases
1.24.2. Weight of Fuel Gas per kg of Fuel Burnt
1.25. Conditions for Proper Burning (combustion) of Fuel ...39
1.26. Temperature of Fuel Combustion
Problems
.. .50
(viii)
2. Power Plant Economics 53-139
2.1. Power Plant .53
2.2. Types of Power Plants
2.3. Requirement of Plant Design
2.4. Useful Life of a Power Plant
2.5. Comparison of Public Supply and Private
Generating Plant .0. 55
2.6. Prediction of Future Loads . . .56
2.7. Terms and Definitions .0. 57
2.8. Power Plant Capacity
2.8.1. Feasibility of Electric Power Plant
2.9. Principles of Power Plant Design . ..63
2.10. Economic Load Sharing between Base Load and
Peak Load Power Stations . ..64
2.11. Type of Loads ...65
2.12. Typical Load Curves
2.13. Cost of Electrical Energy .0. 66
2.14. Energy Rates (Tariffs)
2.14.1. Types of Tariffs ...69
2.15. Economics in Plant Selection ...72
2.16. Economic of Power Generation
2.17. Plant Performance and Operation Characteristics
2.18. Economic Load Sharing .0. 77
2.19. Condition for Maximum Efficiency .
2.20. Choice of Power Station ... 80
2.21. Effect of Variable Load on Power Plant Operation
and Design . . .82
Problems ...135
3. Steam Power Plant 140-315
3.0. Introduction ... 140
3.1. Essentials of Steam Power Pit. uipment ...140
3.1.1. Power Station Design ...142
3.1.2. Characteristics of Steam Power Plant ...142
3.2. Coal Handling 143
3.2.1. Dewatering of Coal
3.3. Fuel Burning Furnaces ...149
3.3.1. Types of Furnaces . ...149
3.4. Method of Fuel Firing ... 150
3.4.1. Hand Firing ...150
3.4.2. Mechanical Firing (Strokers) ... 153
3.4.3. Types of Stokers ...154
3.5. Automatic Boiler Control ...158
3.6. Pulverised Coal ... 159
3.6.1. Ball mill .0. 160
(ix)
3.6.2. Ball and race mill
3.6.3. Shaft Mill
3.7. Pulverised Coal Firing
3.8. Pulverised Coal Burners
16(
3.8.1. Cyclone Fired Boilers
3.9. Water Walls
3.10. Ash Disposal
3.10.1. Ash Handling Equipment
3.11. Smoke and Dust Removal
3.12. Types of Dust Collectors
3.12.1. Fly Ash Scrubber
18
3.12.2. Fluidised Bed Combustion (FBC)
18
3.12.3.Types of FBC Systems
3.13. Draught 1
3.13.1. Comparisons of Forced and Induced
Draughts
18'
3.13.2. Draught Measurement
3.14. Chimney
3.15. Calculation of Chimney Height
3.16. Methods of Burning Fuel Oil
...19E
3.16. (a) Fuel Oil and Gas Handling
3.16. (b) Gas Burners 19
3.17. Slag Removal ..20C
• . .20C
3.18. Economiser
...201
3.18.1. Soot Blower
.203
3.18.2. Air Preheater
• ..203
3.18.3. Heat Transfer in Economiser and Air
Preheater
.204
3.19. Super Heater
...205
3.19.1. Sugden Superheater
...209
3.20. Advantages of Super-heated Steam
...209
3.21. Super-heat Control
.209
3.22. Feed Water Treatment
...210
3.23. Methods of Feed Water Treatment
...212
3.24. To Determine Blow Down
...217
3.25. pH Value of Water
..218
3.26. Analysis of Water
...218
3.27. Feed Water Heaters
...219
3.28. Steam Condensers
...220
&29. Types of Steam Condensers
.220
3.29.1. Surface Condensers
...220
3.29.2. Jet Condensers
..222
3.29.3. Types of Jet Condensers
...224
3.30. Condenser Cooling Water Supply
.225
3.30.1. River or Sea
..226
3.30.2. Cooling Ponds
.226
(x)
3.30.3. Cooling Towers ...227
3.31. Maintenance of Cooling Towers • ..230
3.32. Condenser Efficiency .230
3.33. Vacuum Efficiency ...231
3.34. Condenser Pressure ... 231
3.35. To Calculate the Weight of Cooling Water ...232
3.36. Selection of a Condenser ..234
3.37. Sources of Air in a Condenser .234
3.37. (a) Effects of Air Leakage ...234
3.38. Air Extraction Pump ...235
3.39, Condenser Auxiliaries ...235
3.40. Condenser Performance ...236
3.41. Steam Separator ..236
3.42. Steam Trap ...238
3.43. Steam Turbines ...239
3.44. Advantages of Steam Turbine Over Steam Engine ...241
3.45. Steam Turbine Capacity .242
3.45.1. Nominal Rating ...242
3.45.2. Capability .242
1.46 Steam Turbine Governing ...243
.47 Steam Turbine Performance .244
3.47.1. Steam Turbine Testing ..245
3.47.2. Choice of Steam Turbine ...245
1.48. Steam Turbine Generators ...246
3.48.1; Steam Turbine Specifications ...246
1.49 Boilers ...246
1.50. ms of Boiler ...248
3.50. (a) Babcock and Wilcox Boiler .:.251
3.50. (b) Cochran Boiler ...251
3.51. Lancashire Boiler ...252
3.51. (a) Scotch marine bqiler ...253
3.51. (b) Cornish Boiler ..255
3.52. Boiler Mountings and Accessories ..255
3.53. Flue Gas and Water Flow .255
3.54. Causes of Heat Loss in Boilers .256
3.55. Thermal Efficiency of Boiler ...256
3.56. Boiler Performance .257
3.56.1. Selection of Fuel for Boiler ...257
3.56.2. Equivalent Evaporation ..258
3.57. Boiler Trial ...258
3.58. Boiler Maintenance ..259
3.59. Control and Measuring Instruments • ..260
3.59.1. Soot Blowers .260
3.60. Circulation of Water in Boilers ..260
3.61. Feed Water Regulators ...261
3.62. High Pressure Boiler .262
3.62.1 Unique Features of High Pressure Boilers ...262
(Xi)
3.62.2 Advantage
3.63. Types of High Pressure Boilers ...263
3.63.1. (a) Advantages of . .. 263
High Pressure Boilers
3.63.2. Selection of Boiler ...265
3.64. Modern Trends in Generating Steam ...266
3.65. Gas Fired Boilers . ..266
3.65.1. Selection of boiler (steam generator) . ..267
3.66. Piping System ...267
3.67. Types of Piping System
3.68. Size and Strength of Pipe ...268
3.69. Insulation
3.70. Material for P , ...269
3.71. E xpansion Bends ...269
3.72. Pipe Fittings ...270
3.73. Pipe Joints .. .270
3.74 Valves ...271
3.75. Principles of Steam Power Plant Design .. .272
3.76. Factors Affecting Steam Plant Design ...273
3.77. Site Selection . ..273
3.77.1 Controls at Steam Power Plant ...274
3.77.2. Feed Water Control- ...274
3.78. Industrial Steam Turbines ...275
3.79. Overall Thermal Efficiency ...275
3.80. heat Flow ...277
3.81. Cost of Steam Power Plant ...278
3.82. H eat Balance Sheet for Boiler ...280
3.83. Useful Life of Components ...281
3.83.1. Power Plant Pumps ...284
3.84. Plant Layout... 285
3.85. Terms and Definitions ...285
3.86. Modern Steam Power Station ...286
3.87. Ways of Increasing Thermal Efficiency of a Steam ...287
Power Plant
3.88. Indian Boiler Act
3.89. Thermal Power Stations in India ...290
3.90. Super Thermal Power Stations ...293
3.90. (a) Singrau ...293
Super Thermal Power Plant
3.91. Korba Super Thermal Power Station ...294
3.92. Thermal Power Plants Environmental Control ...294
3.93. Com missioning of Plants ...294
Problems .. .296
...312
1. Diesel Engine Power Plant
4.0. I ntroduction 316_-355
4.1. Classification of ...316
Engines Internal Combustion (I.C.)
4.2. Four Stroke Diesel Engine ...318
...321
(xii)
4.3. Two-stroke Diesel Engine ...322
4.4. Application of Internal Combustion Engines ...324
4.5. I.C. Engine Terminology .324
4.6. Engine Performance • .325
4.7. Heat Balance Sheet ...326
4.8. Diesel Engine Power Plant Auxiliaries ...331
4.9. Internal Combustion Engine Cooling Methods ...332
4.9.1. Cooling Methods ...333
4.10. Lubrication ...337
4.11. Engine Starting Methods ...338
4.12. Starting Procedure ...339
4.12.1. Stopping the Engine ...339
4.13 Starting Aids ...339
4.13.1. Warming up of Diesel Engine ...340
4.14. I.C. Engine Fuel ...340
4.15. Fuel Supply ...340
4.16. Diesel Engine Fuel Injection System ...341
4.17. Fuel Injection Nozzle • .343
4.18. Filter and Silencer Installation ...343
4.19. Advantages of Diesel Engine Poyer Plant ..344
4.20, Site Selection ...345
4.21. Layout •.345
4.22. Applications of Diesel Engine Plants • . .346
4.23. Cost of Diesel Power Plant ...346
4.24. Testing Diesel Power Plant Performance .346
4.25. Log Sheet .348
4.26. Advantages of I.C. Engine Over Steam Engine .348
4.27. Plant Maintenance ...348
4.28. Specific Fuel Consumption ...349
4.29. Comparison of a Diesel Engine and Petrol Engine ...349
4.30. Supercharging ...349
4.31. Advantages of Supercharging ...350
4.32. Factors Affecting Engine Performance ...351
4.33. Combustion Phenomenon in C.I. Engines ...351
4.34. Comparison of Gas Turbine with Reciprocating I.C.
Engine ... 351
Problems ... 354
8. Instrumentation 526-538
8.0. Introduction ...526
8.1. Classification of Instruments ...526
8.2. Measurement of Pressure ...5N
.2. Temperature Measurements
(Xi. • t i)
'xix)
11.16.1. Basic Components of a Wind Energy
Conversion System (WECS)
11.17. Site Selection for Wind Mill Units ...611
...613
11.17.1. Performance of Wind Machines
11.18, Bioniass ...613
11.19. Biomass Gasification ...614
11.20. Tidal Power ...615
11.20.1. Tidal Power Plants ...615
11.21. Classification ...616
...616
11.22. Advantages and Disadvantages of Tidal Power ...617
11.22.1. Regulation of Tidal Power Supply
11.23. Biogas ...618
11.24. Classification of Bio-gas Plants ...618
...618
11.24.1. Factors affecting Bio-digestion or
Generation of Gas
11.24.2. Thermionic Generation ..'.619
...620
11-24.3. Thermiorjc Converter
11.25. Types of M111)Generators ...620
... 621
11.25.1. Open cycle generator
11.25.2 Closed cycle systems ...622
11.25.3. Advantages of MHD Sys ... 622
tem ...623
11.25.4. Combination of MIlD power plant and
steam power plant
11.26. Fuel Cell ...623
11.27. Therm o-Electric Power ... 624
11.28. Therm ... 624
Thermo-electric Power Generator
11.29, Therm o-electric Materials ... 625
11.30. M . 626
Methods for Maintaining Biogas Production
Problems ..629
..630
12. Environment Pollution and its Control
12.1. Introduction 632-648
12.2. Steam Power Plant Pollutants ...632
12.3. Control of Pollutants ...633
.635
12.4. Control of Particulate Matter
12.5. Control of SO, ...636
12.5.1. Wet Scrubber .637
12.5.2. Catalytic Oxidation ...638
12.5.3. Magnesiun- Oxide Scrubbing ...639
12.6. Control of NO, ...639
...640
12,7. Control of Waste Waters from Steam Power Plant ...641
12.8, - '.11utants from Nuclear Power Plants their Effects
Z1110 Control
12.9. Pollution and Noise Control
12.10 St a11c13rdj . itio15 ... 644
for
Environmental Pollution ..644
12.11. Thermal Pollution
..644
12.12. Cleaning of Ventilation Air at Atomic Power
Stations .645
1213. Fuel econom y in furnaces of boilers .6 16
Problems .618
I-...
Introduction
The global energy crisis has attracted the attention of the de-
veloping and deelopecl countries to explore and find out new means
of energy sources to meet this ever-increasing demand of the man-
kind as the conventional main sources of energ y viz., coal and oil
would exhaust after certain period of time. Electrical energy is an
important index of country's economic and technological progress.
In India the installed power capacity has been increased by more
than 13 times during the last 30 years. i.e. from 2,300 to 31,000
MW in 1980. The power demand has also gone up steeply. If we
analyse this load growth, two factors will con out more promi-
nently apart from others.
• Growth of industries.
• Increase in domestic load due to nw and extensive urban
residential area and vertical growth in existing area with
increased and intensive use of electrical gadgets.
The acceleration of the process of industrialisation and urbani-
sat i on following the determined effort of the developing countries
like India to improve their economic well-being has inevitabl y lead
to larger and larger demands for energy. The central problem, there-
fore, is how a country like India can ensure adequate supplies of
energy of fuel, its economic growth into global environment of scar-
city of desired fuels and high costs.
In our country the main sources oferiergv are fossil fuels, hydel,
and nuclear power even though solar energy, wind power and tidal
power offer hopeful technological opportunities.
Coal will remain as main source of energy for severni decades
to some. While discovers' of more oil and gas is not ruled out, the
question is what production level can he reached and for how long
can it be sustained. A large untapped hydro-potential exists in our
country. It is found that total h ydro-potential could be equivalent
to 75,400 M\V at 6O'2 load factor of which about 10 1,' to 1 2'' has
been exploited so far. hydra power being a renewable sourL(-(f
energy nu.ist receive a high priority in our energ y development pro-
gramme.
The use ofIiio-gas for lighting and irrigation opens Uj) new pos-
sibilities for self-contained rural communities. In the long run over
energy economy would have to be built aroei !and-based hiojuass
fuels and the plentiful sunshine which we receive virtuall y tlirwgli-
out, the year. Uwe succeed in tapping solar energy oil n
(.rxu)
scale for lift irrigation purposes we may indeed achieve a break
through in our rural economy by successful utilising our coal, oil,
gas uranium and hydro are commonly called conventional energy
sources.
World over the trend has been towards utilising the existing
resources like hydle and coal and at the same time developing nu-
clear power generation capabilities. Developed countries have taken
a long term view of their power needs and have gone in for a judi-
cious mix of these sources.
The various Lources of power generation should be used to match
particular circumstances and needs. Nuclear power is a clean source
of energy and hazards can be minimised. Dams have longer life
than thermal power plants. While the demand for electrical power
is on the rise, the over all known resources of petroleum are on the
decline. It is therefore imperative that the consumption of petro-
leiim products in the field of power generation, transmission and
distribution is conserved to the maximum extent.
In India, the present petroleum may not last long. Alternative
sources of energy must therefore be found out so far the known
sources of unconventional energy are nuclear fusion, solar energy,
geo-thermal energy, wind power, tidal wave energy and biogas tech-
nical. In a tropical country with abundant solar energy. If we suc-
ced in tapping solar energy on a massive scale for lift irrigation
purposes, we may indeed achieve a break-through in our rural
economy by successfully utilising our under-ground water resources.
All efforts should be made to conserve conventional sources and to
develop non-conventional sources of energy.
In our country industrial sector consumes the maximum dcc-
rical power about 52% of the total power. Next of industrial sector
is the transport sector.
In our country the installed capacity was nearly 2300 MW in
1950 and will be about 65000 MW by 1991. Power sector proposes
to induct an additional capacity of about 38000 MW during eighth
five year plan which will need an investment of about Rs. 128000
crores. This is a very huge amount and therefore all efforts should
be made to conserve energy. There is a need to make best use of
our present capacity. Plants load factor must be increased. Efforts
should be made to reduce transmission and distribution losses. We
must also look into alternative sources of energy like solar, bio-
mass, photovoltaic energy and micro-hydel projects.
In our country the per capita energy production is ver y low.
For example the per capita annual average production of electricity
(Xxiii)
during 1986-88 in UK was 5300 KWH, France 6300 KWH, Ger-
maii•' 6800 KWH as against that India's generation was onl y 260
KWh. The peak power demand by the end of the ninth plan (2001-
02) will be 104000 MW. This would require an instafled capacity of
about 170000 M\V. As such about 100000 MW of additional gener-
ating capacity would need to be installed during the decade 1992-
2002.
Sources of Energy
1.1 Power
Power plays a great role wherever man lives and works--in
industry, agriculture transportation etc. Power provides our homes
with light and heat. The living standard and prosperity of a nation
var y directly with increase in use of power.
I::Jfle v
Generator
Low tide
_•:: .-TidoI bosn
-
= '
Turbinc - Gnerator
Fig. 1.1.
SOURCES OF ENERGY 7
CONDENSER
'T' - TE
C, :DENSA
CIRCULATING
PUMP
r!. flfl
Fig. 1.2
TLJRBINEJ..L1 GEN.
CONDENSER
VAPOR1 I-lEA T
EXCHANGER
PUMP
GEOTHERMAL
REGION
Fig 1.2(A)
8 POWER PLANT
The hot water closed (Binary) s ystem shown in Fig. 1.2 (A) is
also used where temperature and pressure of water are not suffi-
cient to produce flash steam. In this system heat in water is used in
a closed c y cle. In this system Freon or Iso butane is used as working
fluid which is continuously circulated. This system has the ad-
vantage that lower hot water temperature can be used. Such system
is under development in USA and USSR.
8. Thermo-electric Plant. When the two junctions of loop of
two dissimilar metals are kept at different temperatures, an
electromotive force is developed and current starts flowing in the
loop. This is known as Seebeck effect. By using suitable materials
this method call be used for the generation of electrical energy in
small amounts.
1.2.1. Conventional and Non-conventional sources of
energy. The sources of energy used for mass generation of power
called conventional sources ofénergy are as follows
(i) Thermal (ii) Hydro-power
(iii) Nuclear power.
The non-conventional sources of energy used for generating
power in lesser magnitude are as follows
(i) Solar energy (ii) Wind power
(iii) Tidal power (iv) Rio-gas
(v) Magneto-Ilydro-dynamiC plant
(vi) Geo-thermal energy.
1.3 Fuels
Fuel is defined as any material which when burnt will produce
heat. Various fuels commonly used are as follows
1.3.1. Solid Fuels. Natural solid fuels include wood, peat,
lignite, bituminous coal and anthracite coal. The prepared solid
fuels are charcoal, coke and pulverised coal, Peat, Lignite,
Bituminous coal and Anthracite, coal are various varieties of coal.
Coal havingrelatively high percentage of volatile matter is called
soft coal and with lower percentage of volatile matter is called hard
coal. Wood can be burnt easily and gives maximum intensity of heat
very quickly, but is not suitable for boilers etc. because the calorific
value of wood is low (3000-4000 cal/kg).
Coal. The vegetable matter which accumulated under the earth
millions of years ago was subjected to the action of pressure and
heat. This changed the physical and chemical properties of matter
and it got converted into what we call as coal. In India coal is the
primary source of energy and Coal India is the controlling body for
the coal industry. India has reserves of both oil and coal. While coal
reserves in the country are sufficient to last for some hundreds of
years, oil represents only a fraction of total coal reserves. The power
SOURCES OF ENERGY
_-1
POWER PLANT
10
where Cil.( ml represent the percentage by weight of Carbon,
h y drogen, ON -W11 iliI(l sulphur respectivelY.
The net )r I wer calorific value(L.C.V.) is obtained b y subtract-
ing from I IC V. the heat carried by the products of combustion
especially by stuani which call taken as 588.76 kcal/kg of water
vapours b.r:iwd due to burning of 1 kg of fuel.
L.C.V. - (11.(,'.V. - 588.76 x W) kcallkg.
where W is the amount of water vapours formed by the combustion
of 1 kg of hid.
The hiher calorific value at N.T.P. of various constituents of
fuek are a follows C = 8060 kcal/kg, S = 2220 kcal/kg,
ll . 3 1.500 kcallkg and CO 2430 kcal/kg.
1.5 To Calculate Approximate Flue Gas Loss
Percent age of net calorific value (Btu) lost in flue gas
(T1
=J1x
POWER PLANT
12
Table 1.1(B)
Proximate Analysis
d Ash C Jl N2 S Ash Dn
olatile
atter rarb- I I repor busts
h-el
I
26 11 6 23 to 1.55 6
28 31 6 42 L i 6 4000
volatile
Medium
3516TiTh5
3 24 62 11 77
Sit urn rw:e Cool
5
J 4.5
6s
h)Ojcfins
Aromatics 17
A
POWER PLANT
14
and nun poisonous. The calorific value of nat aral gas is 5,2.-)
k cii L'cu 1)1 c met cc.
16 POWER PLANT
Table 1.2
- Specific Composttioo bvu'ei/zt
- ity - .--.- - -
Table 1.2A
Electrical Energy Generation
1987-83 217.2
1999-2000
Projected Dernand- 424/465
7otal
SOURCES OF ENERGY 31
16 + 64 - 44 + 36
11 9
Table 1.4.
Substance (Oxygen Products of Combustion (kg).
(I kg) reqd. kg.)
CO CO2 1120 SO2
C 8/3 - 11/3 -
CO 4/7 - 11/7 -.
H2 8 - -. 9..
S 1 -•. .- 2.
CH 4 4 . - 11/4 . 9/4 .
POWER PLANT
34
1.19.1 Ash
• Ash is the combustion product of mineral matters presents in
the coal. It comprises mainly of silica (Si0 2 ), alumina (Al 203) and
ferric oxide with varying amounts of other oxides such as CaO, MgO,
NaO etc. High ash content in coai is undesirable in general.
A coal with high ash content has following properties:
(i) is harder and stronger
(ii) has lower calorific value
(iii) produces more slag (impurities) in the blast furnace when
coke made out of it is used therein.
Ash content of the coal is reduced by its washing.
1.19.2 Volatile Matter
Certain gases like CO, CO 2 , CH 4 H2, N2 , 02, hydrocarbons etc.
are present in the coal which conies out during its heating These
are called the volatile matter of the coal.
The coal with higher volatile matter content has following
properties
(i) ignites easily i.e. it has lower ignition temperature
(ii) burns with long smoky yellow flame
(iii) has lower calorific value
(iv) will give more quantity of coke oven gas when it is heated
in absence of air
Cu) will require larger furnace volume for its combustion
(ui) has a higher tendency ofcatching fire (due to low tempera-
ture exothermic oidation) when stored in open space.
1.20 Weight of Excess Air Supplied
The weight of excess air required during combustion of coal is
calculated from the weight ofunused oxygen in flue gases after CO
is present in flue gases is burnt to CO2.
POWER PLANT
36
COKE
ANTHRACITE
(02
I 08ITJMINOUS
NATURAL GAS -
0 50 100 150
- EXCESS AIR(/.
Fig. 1.3
The amount of CO2 in flue gases depends on type-of fuel and
excess air supplied to the furnace. Fig. 1.3 shows typical variation
SOURCES OF ENERGY
37
Of CO2 in flue gases (per cent by volume) and excess air (percent) for
complete combustion of various types of fuels.
The total amount of air needed for complete combustion of a fuel
depends on following factors:
(i) Type of fuel.
(ii) Furnace arrangements.
(iii) Heat transfer surface arrangement.
Typical values of excess air supplied, expressed as percentage
of the quantity theoretically required are as follows:
Hand fired boiler furnace : 100
Mechanically stokered furnace : 40
Petrol engine : 20
Oil engine : 20
1.21 Requirements of Fuel
A fuel should possess the following requirements:
(i) Calorific value. The fuel selected should have high calorific
value.
(ii) Price. It should be cheap. -
(iii) Operating efficiency. The fuel should burn n •ffectively.
It should produce minimum amount of dust, smoke, slagging and
clinkering. In case of coal a careful study should he de about
volatile matter, ash, sulphur, moisture, ash fusion te mperature ash
analysis and grinding and coking characteristics
(iv) Refuse disposal. The fuel should produce minimum ash on
burning. In general oil and gas, produce ash in very small quantities
and do not present any refuse disposal problem -whereas . coal
Produces sufficient amount of ash and, th.erefare, ash disposal
equipment is required where coal is used as fuel.
(u) Handling cost. The handling cost shoulcibe minimum. Han-
dling cost of coal at power station is maximum and gas requires
minimum handling cost whereas handling cost ofoil is intermediate.
(vi) Operating labour cost. The operating labour cost is maxi-
mum in coal fired plants whereas it is minimum where gas is used
as fuel.
1.22 Principal Stages of Combustion
The combustion of fuel is a complicated physical and chemical
process in which the combustible elements of the fuel combine with
the oxygen of air witH the evolution of heat attended by a sharp rise
in temperature and formation of flame. During the burning of any
fuel two stages are observed
(i) Ignition (ii) oxnbustion.
POWER PLANT
38
= 11 CO2 + 7CO
1.24.2 Weight of flue gas per kg of fuel burnt. The actual
weight of dry flue gases can be obtained by comparing the weight of
carbon present in flue gases with the weight of carbon in the fuel.
Let, 1V2 = weight of carbon in 1 kg of fuel
W = Weight of flue gas per kg of fuel burt
= w21w1
where W1 = Weight of carbon in 1 kg of flue gases.
POWER PLANT
40
0.03 8 0.03x8=0.24
H2
- 002
Ash i
9.10
0.02
L 4.40 0.146
28 0.56
0.13 32 _ 4.16 0.140
28 21.00 0.696
I W=30.12
POWER PLANT
42
= x 0.146 + x 0.018
11 7
= 004 + 0.008 = 0.048 kg.
•. Weight of flue gas per kg of coal
0.24 -
= -- = a kr'
0.048
Weight of excess oxygen per kg of flue gas
= Amount of oxygen in flue gas -- Oxygen
require(I to burn CO
Products of Combustion
C+O-4CO2 12=32 - 12+32
12=32 - 44
SOURCES OF ENERGY 43
1 kg of C + kg of 02 kg of CO2
v
2
2.13 kgof0 gi es CO2 r xx2.13 = 2.93 kg
1 kgofH2+8kgofO2=9kgofH2O
=
1120 X 16 1.8 kg/kg of fuel. Ans.
CO2 0.18 - -
L
CO
CU4
- 0.125
__ 1
2
0,062
N2 0.40 - -
SO2 0.02 64 -
= 0.0003 0.05%
SOURCES OF ENERGY 45
02 1.1 32 1.1
32
N2 12.8 28 12.8046 81.07%
28
Total 0.5673 100%
Example 1.6. The percentage composition by weight of a sample
of coal is given as below.
C=65.50%; 112=6.65%
02= 17.50%; S= 1.80%
Using Dulong formula, calculate the calorific value of coal.
Solution. According to Dulong's formula, the higher calorific
value (H.C.V.) is given by the following relation:
H.C.V. = ooc + 34,500 [H - + 2220 s}
1001
=x 65.50 + 34,500 (6.65- 17.50) + 2220 x 1.801
100 18080
100 J520,924 + 153,870 + .39961 = 6787.90 kcal/kg
=
Steam produced = 0.0665 x 9 = 0.5985 kg.
Lower calorific value (L.C.V.) = H.C.V. - 0.5989 x 588.76
= 6787.90 - 0.5985 x 588.76 = 6787.90 - 352.37
= 6435.53 kcal/kg. Ans.
Example 1.7. A boiler uses coal of the following composition
C=89%; 112=4%; 02=3.8%
If CO2 records read 10% calculate the percentage of excess air
supplied per kg of coal.
Substance per Mal. Weight Proportional vol. Oxygen reqd. Thy prod uct
kg of coal composition by vol. ofcombustion
by vol.
C=0.89 12 0.89 0.074 0.074
- -0O74
1
H2 = 0.04 2 0.01
-002
02 0.038 32 0.0380.012
i2- -OO12
J
(A)
IC
0.1.541 0.15 x 41
= 6.6 =21.56.
CO 0.01 28 0.01 X 28 0.28
-100
= 0 28
02 0.05 32 0.05 x 32
Li.-.----- -
100
--
N 2 079 28 0792S 2212
X 100
:i 12 =7229
.-'- L. 1=00
S = 0.02; Ash 0. 1.
SOURCES OF ENERGY
49
= 15.72 kg.
mi = Mass of CO 2 produced
= x C as 1 kg of carbon produced kg of CO2
3-
-
=
x 0.77
= 2.82 kg
P112 = Mass of 1-120 produced
77
x 15.72
=
12.1 kg
= Temp. of flue gases entering the chiiuiey = 324°C
T 2 = 16°C
II I = Heat carried away by CO2
= Mass x Specific heat x Rise in temperature
= mi x C, X (7' - 7'2)
= 2.82 x 1.05 x(324 - 16)
POWER PLAN
50
= 912 kJ/kg
112 = Heat carried away by S02
= fl13 X C, x (Ti - '2)
= 0.04 x 1.05 x (324 -. 16)
12.94 kJ/kg
Heat carried away by excess 02
= m4 x C,, x (Ti - T2)
= 1.2 x 1.007 x (324 - 16)
= 372 kJ/kg
11 4 Heat carried away by N2
= M5 Cp (Ti - T2)
= 12.1 x' 1.007 x (324- 16)
3753 kJlkg
Ks Heat carried away by moisture
=
= 2930 kJx fl12
=2930x0.45
= 1318.5 kJ
H = Total heat carried away be flue gas
=H1 +112+1131-1141-115
= 912 + 12.94 + 372 +3753 + 1318.5
= 6368.5 kJ/kg of coal.
PROBLEMS
1.1. Name and explain the various sources of energy. Compare the
various sources of energy.
1.2. What are the various types of solid fuels? Describe Bituminous,
Lignite and Anthracite varieties of coal.
1.3. What do you understand by higher calorific value (H.C.V.) and
lower calorific value (L.C.V.) of a fuel? Explain Dulong's formula
to find H.C.V.
1.4. What is meant by composition of fuel? Give percentage composi-
t ion of some of liquid fuels. Explain ultimate analysis to find
various constituents of a solid fuel.
1.5. What are the various advantages of liquid fuels and gaseous
fuels over solid fuels?
SOURCES OF ENERGY 51
1.6. Write short notes on the following: -
(i) Degrees A.P.I. of liquid fuel
(ii) Firing qualities of coal
(iii) Combustion of fuels
(iv) Types of gaseous fuels
(u) Ultimate analysis
(vi) Proximate analysis
(vii) Products of combustion
(viii) Requirements of a fuel.
1.7. A boiler uses an oil with a calorific value of 9000 kcaVkg. The
analysis of the oil is 85 percent carbon and 15 per cent hydrogen.
The air supplied is ible the theoretical mass required for the
complete combustion u .he oil. Calculate the mass of exhaust
gases per kg of oil burnt.
1.8. The percentage composition by weight of a sample ofcoal is given
below:
C=70%, H2=6%
02 = 22% 8=2%
Using Dulong formula, determine the calorific value of coal.
1.9. Explain the method to find the weigh-. ,.,f excess air required for
the combustion of a fuel.
1.10. Write short notes on the following:
(a) Principal stages of fuel combustiors.
(b) Theoretical temperature of combwion of a fuel.
1.11.A boiler uses fuel oil. Gravimetric analysis : Carbon 0.86 and
hydrogen 0.14 at the rate of consumption is 500 kg/hour. The air
supplied is 25% in excess of theoretical minimum air required for
complete combustion. What is the total amount of air supplied
per hour? [Ans. 9250 kg/hI
1.12. The ultimate analysis of a sample of coal gives in percentage
composition by weight. C = 66%, H 2 6%. 0 = 19% and S =
Find the calorific value of coal using l)ulong's formula.
.13. Discuss the sources of energy in India.
1.14. Write short notes on the following:
(a) Conservation of energy
(b) Tidal power
(c) Solar energy
(d) Geothermal ..nergy.
1.15.A fuel contain- the following . rcentage of combustibles by
weight
Carbon 84%, and h ydrogen 4.1%.
If the air used for hirning of the coal in a boiler is 16.2 b y per kg
of fuel, fin- the tut heat carried awa y by dry flue gases and if
they escape at 300 C The specific heat of (.'O2_ 02, N2 are 0.213
and 0.219-050 respectivel y l'uul the minimum amount of air
required for the complete c()n'l 'tLstion of 1 kg of this fuel and the
excess oxygen supplied. 1A.M.1.E. I9711
1.16. Write short notes on the following:
(a) Liquid fuel properties
POWER PLANT
52
O/5TAI9UT,N
$V8-SrAr,o,.
r1i ii
CONSUMERS
1125ERVICE
MAIN
fu(rfl,b,,rnn
S../O4y
r 94 VSM/$ S/ON
MANSMISSiOlV 5C/8 -STA TION
Fig. 2.1
From the economic point of view it is desirable that when large
amount of electric potver is to be transmitted over long distance it
should be transmitted at a voltage higher than the distribution
voltage. The voltage for transmission should be so chosen that it
gives best efficiency, regulation and economy. Step up transformer
is used to step up the generation voltage to transmission voltage
which is usually 132 kV At the transmission sub station the voltage
is stepped down to ledi.imvoltage usually 33 or 3.3 kV. The feeders
carry the power to e dstrjbution sub-stations. Feeders should not
be tapped for direct supply. The function of transformers at
the distribution sub-station is to step down the voltage to low
POWER PLANT
54
distribution voltage which is usually 400 to 230 V. Distributors are
uscd to supply power to the consumers.
Transmission of electric power over long distances can be done
most economically by using extra high voltage (E.H.V.) lines. In the
world today many A.C. extra high voltage lines are in operation.
These E.H.V. lines operate at voltages higher than the high voltage
lines i.e. 230 kV. The E.H.V. lines are now in operation in Europe,
USA and Canada and oplrate at 330 kV, 400 kV, 500 kV and 700
W. Still higher voltage 1000 kV level are in the experimental stage.
In India there is no E.H.V. line so far but it is hoped that soon such
lines in the form of Super Grid will be developed.
2.2 Types of Power Plants
Based upon the various factors the power plants are classified
as follows
1. On the basis of fuel used
(i) Steam Power Plant
(a) condensing power plant
(b) non-condensin g power plant
(ii) Diesel power plant
(iii) Nuclear power plant
(iv) Hydro electric power plant
(o) Gas-turbine power plant
2. On the basis of nature of load
(i) Base load plant
(ii) Peak load power plant
3. On the basis of location
(i) Central power station
(ii) jolted power station
4. On the lasis of service rendered.
(j) Stationary
(ii) Locomotive.
9ilIIiIT15--20 T
and in.,trun_J_ 10-
2.5 Comparison of Public Supply and Private
Generating Plant
Industrial concerns ma y generate their own power or may
purchase power from public supply company. The two are compared
as f011QWs
(a) Public Supply
(i) Reliability of power is assured and over-load power
demand can be available at short notices.
(ii) It is cheaper to purchase power from public supply com-
pany.
POWER PLANT
56
—6
POWER PLANT
58
AiE RA
LOA u
..t
9AS LOAD
TM (SOURS
Load curves give full information about the incoming load and
help to decide the installed capacity of' the power station and to
decide the economical sizes of various generating units. They also
help to estimate the generating cost and to decide the operating
schedule of the power station i.e. the sequence in which different
generating units should be run. Fig. 2.2 shows a load curve.
(v) Load Factor. It is defined as the ratio of average load to
maximum demand. Load factors and demand factors are always less
than unity. Load factors play all part oil cosi of
generation per unit. The higher the load factor the lesser will he the
cost of generation per unit for the same maximum deniaiul.
Load factors for different types of consumers are as follows
(i) Residential load 10- 15
(ii) Commercial load 25-30%
(iii) Municipal load 25
(iv) Industrial load
(a) Small scale industries 30-50
(b) Medium size industries 55-60%
(c) Heavy Industries70-807
Base load plants run oil high load factor whereas the load
factor of peak load plants is usually low.
over I kW 0.50
Lghtirig coinincrctl Schools, Hostels, 0.50
Small Industry, Theatres 0.60
Restaurants, Offices, Stores 0.70
POWER PLANT ECONOMICS
61
General Power Service uptoionjJ
10 to 20 H.P. 0.65
20 to 100 H.P. 0.55
above 100 H.P. 0.50
Some typical diversity factors are mentioned in Table 2.3.
Table 2.3
jettnetors
Lighting !ightu G'ncral Poui'r
J
)I KW
2 I KW
xW
Fig. 2.3
The area under the load duration curve and the corresponding
chronological load curve is equal and epresents total energy
delivered by the generation station. Load duration curve gives a
clear analysis of generating power economically. Proper selection of
base load power plants and peak load power plants becomes easier.
POWER PLANT
62
dE 1 R1-R2
= ------ hours.
dM 1 P2-P1
E 1 the number of units generated by the base load station is
represented by area under straight line AB
POWER PLANT ECONOMICS
65
66 POWER PLANT
tT.i I t[I H
$2 6 72 6 12
A.M. 11.
.
12 6 12 6 72
All. RI-f.
1'
IkL
12 6 12 6 72
4.11. R.
TIME -
Fig. 2.6 Fig. 2.7 Fig. 2.8
rwi
12 6 $2 6 12 12 6 12 6 72 6 12 6 12 6 72 6 72
1W. A.M. An A.M. (7M. 4.11. Pd-I.
This curve varies with cities and season. For metropolitan areas
a typical daily load curve is shown in Fig. 2.10.
2.13 Cost of Electrical Energy
The total cost of electrical energy generated b y a power station
can be sub-divided as follows
1. Fixed cost. It includes the following cost:
(a) Capital cost of power plant.
(i) Cost of land
(ii) Cost of building;
(iii) Cost of equipment
(iv) Cost of Installation;
(t') Cost of designing and planning the station.
(b) Capital cost of primary distribution system which in-
cludes cost of sub-stations, cost of transmission lines etc.
Fixed cost consists of the following:
(i) Interest, taxes and insurance on the capital cost.
(ii) General management cost.
(iii) Depreciation cost.
= (P - S)
[(1 + r)' - 1
where r = rate of compound interest.
Fig. 2.11(b) shows the depreciation curve.
TOTAL
N.., EPREC/AT/ON rio....
I-1
e
VALVE
L/EIN YEAAS
STRAIGHT LFNE .4ETHoO J(flKIP1 b VP1Q M& 'MUO
Fig. 2.11
r = Rate of interest
A = Annual depreciation amount.
Then the amount A after earning interest for one year
=A +Ar =A (1 + r)
The amount A after earning interest for two years
=A(1+r)+Ax(1+r)xrA(1+r)2
The amount A set aside after one year will earn interest for
(n - 1) years.
Therefore, the sum of the amounts saved together with interest
earnings should be equal to (P - S)
(P-S)=A+A(1+r)+A(1+r)2A(1+r)n
(P-S)=AI1+(1+r)+(1+r)2 .... (1+r)'']
Multiplying both sides by(1 + r)
(1+r)(P-S)=Al(1+r)+(1+r)2+(1+r)3(1+r)'J ...(ii)
Substracting the two equations from each other, we get
[(1 + r)' - 1
2. Energy Cost. It consists of the following costs:
(i) Cost of fuel
(ii) Cost of operating labour;
(iii) Cost of maintenance labour and materials
(iv) Cost of supplies such as:
(a) water for feeding boilers, for condensers and for
generai use,
(b) lubricating oils;
(c) water treatment chemicals etc.
In power generation activities minimum annual costs are
achieved by a proper balance of the fixed and operating costs. The
fundamental way to compare alternate schemes of power generation
is to compare their total annual costs.
3. Customer Charges. The ccst utcluded in these charges
depend upon the number of customers. The various costs to be
considered are as follows:
(i) Capital cost of secondary distribution system and
depreciation cost, taxes and interest on this capital cost.
ii) Cost of inspection and maintenance of distribution lines
and the transformers.
POWER PLANT ECONOMICS
69
(iii) Cost of labour required for meter reading and office work.
(iv) CosL of publicity.
4. Investor's Profit. The investor expects a satisfactory return
on the capital investment. The rate of profit varies according to the
business conditions prevailing in different localities.
Cost of power generation can be reduced by adopting the follow-
ing economical meosures:
(i) By reducing initial investment in Jie power plant.
(ii) B y selecting generating units of adequate capacity.
(iii) the power plant at maximum possible load
factor.
(iv) By increasing efficiency offuel burning devices so that cost
of fuel used is reduced.
(v) By simplifying the operation of the power plant so that
fewer power operating men are required.
(vi) By installing the power plant as near the load centre as
possible.
(vii) By reducing transmission and distribution losses.
2.14 Energy Rates (Tariffs)
Energy rates are the different methods of charging the con-
sumers for the consumption of electricity. It is desirable to charge
the consumer according to his maximum demand (kW) and the
energy consumed (kWh). The tariff chosen should recover the fixed
cost, operating cost and profit etc. incurred in generating the electri-
cal energy.
Requirements of a Tariff. Tariff should satisfy the following
requirements
() It should be easier to understand.
(ii) It should provide low rates for high consumption.
(iii) It should enco-age the consumers having high load fac-
tors.
(iv) It should take into account maximum demand charges
and energy charges.
(v) It should provide less charges for power connections than
for lighting.
(vi) It should avoid the complication of separate wiring and
metering connections.
2.14.1 Types of Tariffs
The various types of tariffs are as follows
(a) Flat demand rate
(b) Straight line meter rate
(c) Step meter rate
70 POWER PLANT
"I
C
I.)
-I 2
4 X
0
4
(a) (H
Fig. 2.12 Flat demand rate.
(ii) Straight line meter rate. According to this energy rate the
amount to be charged from the consumer (kp(llds upon the energy
consumed in kWh which is recorded b y a means of a kilowatt hour
met 'r. It is expressed in the firiti
EZ
This rate suffers from a drawback that conswla'r using no
it
I
t N
It. a
0
C
'I.
C,
4
I-.
0
(iii) Step meter rate. According to this tariff the charge for
energy consumption goes down as the energy consumption becomes
more. This tariff is expressed as toltows (Fig. 2.14).
f
t
0 z
0
4
,.fl
0
5
'., C)
Fig. 2 15
IV
72 POWER PLANT
Y=EZ ifO5Z5A
Y=E 1 Z 1 ifAZ.!5B
Y=E2Z2 ifBZ2C
and so on. Where E, E 1 , E2 are ihe energy rate per kWh and A, B
and C are the limits of energy consumption.
(iv Block Rate Tariff. According to this tariff a certain price
per units (kWh) is charged for all or any part of block of each unit
succeeding blocks of energy the corresponding unit charges
decrease.
It is expressed by the expression
Y= EZ 1 + E 2Z2 E3Z3 + .......
where Ej, E2, E:3.... are unit energy charges for energy blocks of
magnitude Z i , Z2. Z3,.... respectively (Fig. 2.15).
(v) Two part Tariff (Hopkinson Drnand Rate). In this tariff
the total charges are based on the maximum demand and energy
consumed. It is expressed as
Y = D. X + EZ
A separate meter is required to record the maximum demand.
This tariff is used for industrial loads.
(vi) Three-part Tariff (Doherty Rate). According to this tariff
the customer pays some fixed amount in addition to the charges for
maximum demand and energy consumed. The fixed amount to be
charged depends upon the occasional increase in fuel price, rise in
wages of labour etc. It is expressed by the expression
Y = l)X + EZ + C.
2.15 Economics in Plant Selection
A power plant should be reliable. The capacit y ofa power plant
depends upon the power demand. The capacity of a power plant
should be more than predicted maximum demand. It is desirable
that the number ofgenerating units should be two or more than two.
The number of generating units should be so chosen that the plant
capacity is used efficiently. Generating cost for large size units
running at high load factor is substantially low. However, the unit
has to be operated near its point of maximum econom y for most of
the time through a proper load sharing programme. Too many stand
bys increase the capital investment and raise the overall cost of
generation.
The thermal efficienc y and operatingcost ofa steam power plant
depend upon the steam conditions such as throttle pressure and
temperature.
POWER PLANT ECONOMICS
73
respond to load variation as the control supply is only for the prime
mover. III steam power plant control is required for the boilers as
well as turbine. Boiler control ma y be manual or automatic for
feeding air, feed water fuel etc. Boiler control takes time to act and
therefore, steam powers plants cannot take up the variable load
quickly. Further to Cope with variable load operation it is necessary
for the power station to keep reserve plant ready to tnuntain
reliability and continuit.y of power supply at all times. To supply
variable load combined workingofpower stations is also economical.
For example to supply a load the base load may he supplied by
a steam pow?r plant and peak load ma y he supplied by a hydropower
plant or diesel power plant.
The size and number of generating units should be so chosen
that each will operate on about full load or the load at which it gives
maximum efficiency. The reserve required would onl y he one unit
of the largest size. In a power station neither there should be only
one generating unit nor should there he a large number of small sets
ofcliffercnt sizes. In steam power plant generating sets of80 to 500
MW are quite commonly used whereas the maximum size of (liesel
power plant generating sets is about 4000 kW. Hdro electric
generating sets up to a capacity of' 200 M\V are in use in U.S.A.
2.16 Economic of Power Generation
Economy is the main principle of design of'a power plo:it. Power
plant economics is important in controlling the total power costs to
the consumer. Power should be supplied to the consumer at the
lowest possible cost per kWh. The total cost of power generation is
made up of fixed cost and operating cost. Fixed cost consists of
interest on capital, taxes, insurance and management cost. Operat-
ing cost consists of cost of fuel labour, repairs, stores and super-
vision. The cost of power generation can he reduced by,
U) Selecting equipment of longer life and proper capacities.
(ii) Running the power station at high lad factor.
(iii) Increasing the efficiency of the power plant.
(ii Carrying out proper maintenance of power plant equip-
nient to avoid plant breakdowns.
(r) Keeping proper supervision as a good supervision is
reflected in lesser breakdowns and extended plant life.
(vi) Using a plant of simple design that (lees not need highly
skilled personnel.
Power plant selection depends upon the fixed cost and operating
cost. The fuel costs are relativel y low and fixed cost and operation
and maintenance charges are quite high in a case ofa nuclear power
plant. The fuel cost in quite high in a diesel power plant and for
hydro power plant the fixed charges are high of the order of 70 to
POWER PLANT ECONOMICS 75
Annuol
cost
—investment (efficiency)
(a)
0
Li
- Capacity
(b)
Fig. 2.15
76 POWER PLANT
Fig. 2.15 (b) shows the variation of various costs of power plant
versus its capacity.
Graph A shows variation of engineering and labour cost where
as graph B indicates material cost and graph C indicates total cost.
Unit Cost = Total cost
Capacity
2.17 Plant Performance and Operation Characteristics
Boilers, turbines, generators etc. of a power stations should
work efficiently. Some curves are plotted to observe their perfor-
mance. The various curves used are as follows
I. Input output curve. Performance of a power station is most
precisely described by the input-output curve which is a graphical
representation between the net energy output (L) and input M. The
input is generally expressed as millions of BTU/hr or kcal/hr and
load or output is expressed in megawatts. The input to hydroplant
is measured in cusecs or cubic metre per second of water.
INPUT - OUTPUT ahQvE EFFICIENCY CURVE
iz
10
0 OUTPUT 0 OUTPUT L
(W (bJ
0 OUTPUT
(c)
Fig. 2.16
POWER PLANT ECONOMICS 77
78 POWER PLANT
tdOC
8001
/ 12OO OPTIM(/Mt.OAO
OCUSFOR 4.',.t6
400 800
q200 ca Jo:
2 4 6 8 10 %.11 4 6 8 FO
Uv/T LOAD (LA OR L8) £0.40 0/i? VN/ A(LA)-F.4W
(t4EGA WA
i) (h)
Fig. 2.17
CILA - dLB
dL,4
1dLB
dL.. 3
Substituting in (2), we get
(11 11 (/Ij
dLA - dL
F'ron(1) and (4)
(11,4 - di
(ILA dLB
Therefore, to achieve best economy in load sharing, the slopes
Of the input-output curves for each unit must he equal at L.4 and
LB (Fig. 2.18). In other words, the incremental heat rates are equal.
(HR) = 0
dL
• d(
dLL
Ldi - JilL
0
Ldl = IdL
80 POWER PLANT
Output(L)
Fig. 2.18
I dL
L 1L
This shows that (t (iciency will be naximum at a load where heat
rate is equal to incremental heat rate.
2.20 Choice of Power Station
In a power station energy is converted from one form or another
electrical energy. The power plant should be able to meet power
demand efficiently.
The various factors to be considered while choosing the type of
wer plant are as follows
(i) Type of fuel available. If the site where power plant is to be
installed if near the coal mines then steam power plant is preferred
whereas a hydro power plant is chosen if water is available in larger
quantity. Nuclear power plants are located near river or sea so that
nuclear waste can be disposed off easily. Diesel power plant is used
for supplying smaller loads.
(ii) Power plant site. The power plant site should satisfy the
following requirements
(a) Cost of land as well as taxes on land should he low.
(b) It should be nearer to load centre so that cost of transmit-
ting energy is low.
(c) It should be accessible by road, rail or sea so that transpor-
tation of fuel etc. is easier.
POWER PLANT ECONOMICS 81
06 I688J2Jj21iFlJTh26f2224
t
I
L±.L_jL_L°
50 ...........
(a) Determine the load factors of power station.
• (Ii) What is the load factor of standby equipment rated at 25
MW that takes up all load in excess of 60 MW ? Also
calculate its use factor.
Solution. (a) Load curve is shown iii Fig. 2.19. Energy
generated (area under the load curve)
=40x6+50x2+60x4+ 50x2 *70x4
•1 8 x 4 +40 x 2
= 1360 M\Vh = 1360 x 10 kWh.
1300 x 103
Average load = = 56,666 kW.
Maxinu.imn demand = 80 x 10 3 M.
Averagjoad 56,666
Load Factor 0.71. Ans.
- Max. demand = 80,000 =
1
0C
0
4
TIME CHOURS
Fig. 2.19
Deter,nznL'
(a) Annual energy production
(b) Reserve capacity Over and above peak load
(c) flours per year not in service.
Solution.
4xI = 22,500kW
0.4 x 8760
Reserved capacit y = 22,500 - 15,000 = 7500 k\V.
(c) Use factor =
Cx ti
where ti = Actual number of hours of the year fbr which the plant
remains in Operation.
0.45 - 7884 x 106
22,500 x
78.84 x
ti-
= = 7786 hours.
22,500 x 0.15
Hours per y ear not in service = 6760- 7786 = 971 hours.
Example 2.5. For a power station the yearly load duration curve
is a straight line from 30,000 to 4,000 kW. To meet the load three
turbo-generator are installed. The capacity of two generators is
15,000 kW each and the third is rated at 5,000 kW. Determine the
following:
(a) Load factor,
(b) Capacity factor or plant factor,
(c) Maximum demand.
Solution. As shown in Fig. 2.20 the load curve is a straight line
from 30,000 to 4,000 kW
Average load
Load factor
- Maximum demand
From the given load duration curve.
30,000 kW
cl
0
-.
4000 kV
4 87601iours
Time__-
Fig. 2.20
POWER PLANT
88
Aver eload
Load factor =
Maximum demand
17,100 170 0.57
30x10003OO
Energygjrated
- plant x 8760
Capacity factors = Capacity of
Avcruage load
Annual load factor = --_
Maximum demand
1600 = x 100 = 10.7%
15,000 150
geratCd - 14x10
Capacity factor = Ener gycity x 8760- 18 x 1000 x 8760
—8
POWER PLANT
90
Example 2.16. A 500 kW electric power station cost Rs. 800 per
kW installed. The plant supplies 150 kWfor 5000 hours of the year,
400 kW for 1000 hours and 25 kW for the remaining period. Deter-
mine the cost of production per unit of electric energy. The fixed
charges are 10% and operating charges 7paise per kWh.
Solution. Energy supplied
= 5000 x 150 + 1000 x 400 + 2760 x 25
= 1,219,000 kWh
Example 2.17. (a) Compute the monthly bill and unit energy
cost for a total consumption of 1600 kWh and a maximum demand
of 10 kW using Hopkinson demand rate quoted as follows:
Demand Rates
First kilo-watts of maximum demand Rs. 75 per kW per month.
Next 5 kW of maximum demand at Rs. 12 per kWper month.
Excess over 6 kW of maximum demand at Rs. 10 per kW per
month.
Energy Rates
First 50 kWh at 15 paise per kWh.
Next 50 kWh at 12 paise per kWh.
Next 300 kWh at 8 paise per kWh.
Next 500 kWh at 6paise per kWh.
Excess over 900 kWh at 4 poise per kWh.
(b) Also find the lowest possible bill for a month for 3 days and
the unit energy cost on the given energy consumption.
Solution. (a) Demand charge = 15 + 5 x 12 + 4 x 10
= 15 + 60 + 40 = Rs. 115.
Energy charges = 50 x 0.15 + 50 x 0.12 + 300 x 0.08
+ 500 x 0.06 + 700 x 0.04
POWER PLANT ECONOMICS 95
= Rs. 95.50
Monthly bill = 115 + 95.50 = 210.50
Unit energy cost = 210,50
1600
= 13.15 paise per kWh.
(b) The lowest bill occurs when the demand is maximum
which is possible at 100% load factor.
Maximum demand = Average load
Efficiency Output
In -L
put -
1
11=
106(+8+0.4LJ
Now for maximum value efficiency
411 - 0
dL
Differentiating (1), we get
- 1o6(_+ 0.4 1
drl L2
dL
POWER PLANT ECONOMICS 99
_106[3+0.4]=0
or Lo
-i=O.4
L
10-0.4L2=0
L2==25
L =5 MW.
(b) When load L = 3 MW
Input 13=106110+8x3+0.4x321
= 106 [10 + 24 + 3.61 = 37.6 x 106 kcal/hour.
When load L=5MW
Input 15 = 106 [10 1+ 8 x 5 + 0.4 x 52]
= 106 110+40+101
= 60 x 106 kcal/hour:
Increase in input required = 1 - 13
= (60 - 37.6) x 10 6 = 22.4 x 106 kcal/hr.
From incremental rate curve
When load varies from 3 to 5 Mw, the incremental rate may be
considered to be straight line and the average height of area under
the curve between 3 MW and 5 MW would be a
= 4 MW
8L+0.4L2)
=f(0.07Pa+ 10)dP2
= [0.035 P1 + 10 Pa1
so = - Rs. 77.12 per hour.
This shows that in case of unit B there is decrease in cost.
Hence net increase in cost due departure from economic dis-
tribution = 78.75 - 77.12 = Rs. 1.63 per hour.
POWER PLANT ECONOMICS 101
== 0.06 kW
Maximum demand charge per hour
= 0.06.x 70 x 100 = 0.048 paise.
• Energy consumed per hour 0.06 x 1 = 0.06 kWh.
Energy charge per hour = 0.06 x 5 = 0.30 paise.
Total cost per hour = 0.4 + 0.048 + 0.3 = 0.748 paise.
Therefore, first lamp is economical.
Let x be the load factor at which both lamps become equally
advantageous. Only maximum demand charge changes with load
factor.
0.1+ 0' 08 0.5 = 0.4 + 0.048 +0 3
x x
x = 0.32 or 32%.
Example 2.24.A new factory having a minimum demand of 100
k Wanda load factor of25% is comparing two power supply agencies.
(a) Public supply tariff is Rs. 40 per kW of maximum demand
plus 2 paise per kWh.
Capital cost = Rs. 70,000
Interest and depreciation = 10%
(b) Private oil engine generating station.
Capital Cost = Rs. 250,000
Fuel consumption = 0.3 kg per kWh
Cost of fuel = Rs. 70 per tonne
Wages = 0.4 poise per kWh
Maintenance cost = 0.3 poise perk Wh
Interest and deprecjatjcn = 15%.
Solution.
Load factor = Average load
Maximum demand
Average load = 'oad factor x Maximum demand
POWER PLANT ECONOMICS 103
the fuel acquired fora month and overall efficiency ofthe plant. Plant
capacity factor = 40%.
Solution. Capacity factor = E
where c = capacity of the plant
=700+2x500= 1700 kW
t = time (hours) in the given period
= 30 x 24 = 720 hours.
E
- 2700 x 720
E = 0.4 x 1720 x 720 = 48,96,000 kWh.
Fuel oil consumption = 48,96,000 x 0.28 = 137,088 kg.
- Output
Overall efficiency
Input
Output = 48.96,000 kWh = (48,96,000 x 860) kcal
48,96,000 x 860
Overall efficiency = 0.3 or M. Ans.
137,088 10,200
Example 2.26. The incremental fuel costs of two generating
units A and B of a power station are given by the following expres-
sions:
dFA
^iPA =0.01 PA+2.25
dFB
=0.0J5Ps+1.5
dPB
where F is in rupees per hour and P it is MW. Determine incremental
fuel cost and loading schedule for minimum cost if the total load to
be supplied is to be 50 MW 175 MW and 200MW. Both units operate
at all times and maximum and minimum load on each unit is to be
100 MW and 15 MW respectively.
Solution. Let P = total load
PA = load supplied by unit A
RB = load supplied by unit B
P = PA I-PB
As the incremental fuel cost of unit A is higher than that of B so
for a total load of 50 MW the unit A should supply 15 MW.
POWER PLANT ECONOMICS
105
PA=15MW
PB=35MW
dFA
= 0.01 x 15 + 2.25 = Rs. 2.40 per MWII
dPA
dFB
^PB = 0.015x 35 + 1.5 = Rs. 2.025 per MWh
when the load increases the unit B will continue to supply the
additional load till = 2.40.
dP
PB9-6OMW
When P=75MW
PA = 15 MW and P8 60 MW
For total load P = 175 MW
PA+PB= 175
.(i)
and for economical loading
dFA - dF8
dPA - dP8
0.01 PA + 2.25 = 0.015 PB + 1.5
.(ii)
Solving (i) and (ii), we get
PA = 75 MW
P8 = 100 MW.
When the total load = 200 MW
PA = 100 MW
P8 = 100 MW.
dFA
= 0.01 x 100 = 2.25 Rs. 3.25 per IfWh
dFB
= 0.015 x 100 + 1.5 = Rs. 3 per MWh.
POWER PLANT
106
4
Solution. 1 square cm = 400 x 2 = 800 kWh.
(j)IORW,5H.P. (005
kW (i)10H.P.,5kW
e;;1.1 bW (ii20 kW (it) 15 H.P.
= 7 + 4 + 2.8 = 13.8 kW
Sum of individual maximum demand
Diversity factor = Simultaneous maximum demand
T IME (HOURS) -
Fig. 2.21
108 POWER PLANT
a
a
TIME (HOURS)
Solution.
Nuclear Power Plant
Capital cost = 2500 x 103 x 100 = Rs. 25 x
Interest = Rs. x 24 x iø
Depreciation = Rs.x 25 x iO
Hydropower Plant
Capital cost = 1800 x 100 x 10 3 = Rs. 18 x
Interest=_X18X107r9X106
As the overall cost per kWh is same for both the power stations.
234M 168Mx100
3+MFxl00=6+ MFx8
66Mx 1000
MFx8760
600
Fx87603
F=0.25
% Load factor = 25%. Ans.
Example 2.33. The input output curve of 100 MWpower station
is expressed as follows:
1= 10 (100+2L +0.00041!)
where I is in kcal/hr and L is in MW.
Determine (a) Input, heat rate and efficiency when load is 40
jlI%V
(b) Load at which efficiency is maximum.
Solution.
(a) 1= 106(100+2L+00004L3)
When L= Load =40MW
i = 106 (100 + 2 x40 + 0.0004 x 403)
= 106 x 205.6 kcal/hr.
Heat rate (I) = 106(100 +
2 + 0.0004 x L2)
+ 0.0004 L 2 = 0.00012 L2
= 0.0008 L2
L2 = 0.0008= 125,000
L = 50 MW. Ans.
=.jx96x106=Rs.1344x104
+25x O.735xx8760_J._1P. ] -
4 0.85 100
= Rs. (4471 + 14,203) = Rs. 18,674.
Annual maintenance cost = Rs. 400
Total cost = Rs. [237 + 250 4- 1,674 + 4001 = Rs. 19,561.
Motor B
Depreciation per year = 0.95 x 4200 Rs. 199
20
Interest -j-j x 4200 = Rs. 210
POWER PLANT
118
3 1 x r 5001
25 x 0.735 x 8760 x 4 x
0.82 100
Equating CA = GB, we get
r= 28 paise. Ans.
Annual Cost
102 x 80 = Rs. 14,016 x 102
(i) Cost of coal = 1752 x
POWER PLANT ECONOMICS 119
are 5 paise per kWh geerated. Plot the curve between cost of energy
per kWh and load factor.
Solution.
Load factor = 100%
C1 = Fixed cost per hour = 43,800 - 5 paise.
8760 -
1 kW plant is available at a cost of 5 paise per hour.
E Energy generated per hour at 100% load
factor
= 1 x 1 = 1 kWh.
C2 = Fuel and operating cost per hour
= E x 5 1 x 5 = 5 paise
C = Total cost per kWh produced per hour.
= C 1 + C2 = 5 + 5 = 10 paise.
Similarly the total costs per kWh at other load factors are as
follows:
Load fac. Energy Fixed Fuel and Total cost Cost per kWh
tor % Produced cost operating per hour produced per hour
per hour (Paise) cost per (Paise) (Paise)
(kWh) hour
100 1 5 5 10 10
'.-
CL
Cj
'1'
0
C-)
Fig. 2.24
POWER PLANT ECONOMICS 121
Fig. 2.24 shows the variation of cost of energy per kWh
generated with respect to load factor.
This shows that cost per kWh increases with decrease in load
factor.
Example 2.41. In a steam power plant the capital cost ofpower
generation equipment is Rs. 25 x io. The useful life of the plant is
30 years and salvage value of the plant to Rs. .1 x io. Determine by
sinking fund method the amount to be saved annually for replace-
ment if the rate of annual compound interest is 6%.
Solution. P = Capital cost = Rs. 20 x iO
S = Salvage value = Rs. 1 x
n = Useful life =30 years
r = Compound interest
A = Amount to be saved per year for replacement
A=(=(29x105_1x105)x0.06
(1+r)'-1 (1+0.06)°-1
= Rs. 24,000. Ans.
Example 2.42. A hydra power plant is to be used as peak load
plant at an annual load factor of 30%. The electrical energy obtained
during the year is 750 x 105 kWh. Determine the maximum demand.
lithe plant capacity factor is 24% find reserve capacity of the
plant.
Solution. E = Energy generated = 750 x 10 5 kWh
42 20
30 . 60
8 18
Total = 168 hours
(a) Calculate total energy that can be generated by hydrc
power plant.
(b) How the load shall be shared by the two power plants?
Solution.
(a) E 1 = Energy which can be generated in coming week.
= 3 x 168 = 504 MWh
As the hydro power plant has a provision to store 120 MWh.
E2 = Total energy that the hydro power plant can generate
=E+120=504+12Q=624MWh.
(b) The hydro power plant will be started when the load
exceeds 30 MW.
E = Energy generated by diesel engine
=8x 18+15x20+25x50+30x60
= 144 + 300 + 1250 + 1800 = 3494 MWh.
The hydro power plant will run at its full capacity of 12 MW for
20 hours. Energy generated by hydro power plant
= 12 x 20 = 240 MWh.
Example 2.44. A steam power plant is to supply load for 24
hours as follows:
Time SAM. to 10 10AM. to 5 5P.M. to 11 II P.M. to 5
- A.M. P.M. P.M.__- AM.
Load(AM) 1 50 100 35 15
POWER PLANT ECONOMICS 123
(a) The energy rate is 14paise per kWh and cost of input is 15
N.E. per 6000 kcal. The thermal efficiency of the plant is
35% at 100 MW, 30% at 59 MW, 28% at 35 MW and 20%
at 15 MW.
Determine the net revenue earned.
(b) lithe above load is supplied by a combination of steam
power plant and pump storage plant and steam power
plant runs at constant load with 35% efficiency. Calculate
the capacity of steam power plant and percentage increase
in revenue earned.
The overall efficiency of pump storage plant is 79% and cost of
energy input and cost of selling power is same as mentioned above.
Solution.
(a) E = Energy generated by steam power plant in 24 hours.
= 40 x 5 + 100 x 7 + 35 x 6 + 15 x 6
= 250 + 700 + 210 + 90 = 1250 MWh
= 1250 x 103 kWh
r = Energy rate = 14 paise per kWh
C 1 = Cost of selling power = E x r
=1250x10xj=175x10rup.s
C2 = Input to steam plant in 24 liouis
100x7 50x5 35x6 Yx
0.35 + 0.3 + 0.28 + 0.2
= 2000 + 833 + 750 + 450 = 4033 MWh.
= 4033 x 103 kWh = 4033 x 103 x 860 kcal.
= 3468 x 106 kcal.
(as 1 kWh = 860 kcal.)
S = Input rate = 15 paise per 6000 kcal.
= Cost of input energy
3116 x
= 86.7 x 103
= 6000 100
New revenue earned from steam power plant = C 1 - C2
= 175 x iø - 86.7 x 10
= 88.3 x 10 3 rupees per day.
Igo POWER PLAN1
O.65=h
L=0.65xM
E = Energy generated in one year
x 8760 = 0.65 xMx8760
Capacity factor =
CXt
0.65xMx8760
0.5..= 200x8760
M= 169 MW
Reserve capacity= C - M = 200 - 169
= 31 MW
0.69 x 169 x 8760
= 962 x 103 kWh = 962 x 10 6 kWh.
Now 4% of E is required to run the plant auxiliaries.
100 )
16 POWEP PLANT
=11+ I__)x962x1o6
-... .,
=lOOlxlO6kWh
C i - Interest per year
x 130 x 10 = Rs. 7 x 106.
=
C.Depreciation...per year
1Xi40x!o6=RS.S.4x 106
12,
.S0
2
Fig. 2.25
= (NK+R7) xNT+RTxRS
32 x 106 x 100
= 5.2 paise.
6 14.38 x 106
Example 2.47. A common load is to be shared by two power
plants. One power plant is a base load plant with 30 MW installed
capacity and other power plant is a standby plant with 20 MW
capacity. The yearly output of the base load plant is 130 x 10 kWh
and that of standby plant is 9 x 10 6 kWh. The peak load taken by the
standb y plant is 15 MW and this plant works for 2800 hours during
the year. The base load plant takes a peak 0125 MW. Determine the
following for both plants:
(a) Annual load factor
(h) Plant use factor
(c) Capacity factor.
Solution.
Standby Power Plant
C = Capacity of plant
= 20 MW
E = Energy generated per year
9 x 10 6 kWh
I = Hours of working per year
= 2800 hours
1 lours in y ear 8760
4130 POWER PLANT
M = Maximum demand
= 15MW
(a) Annual load factor
E 9x106
MxT 15x1000x8760
= 0.068 or 6.8%.
M
(b) Plant use factor = - = 15
= 0.75 or 75%.
(c) Capacity factor = Cxt
9 x 106
16 or 16%.
20000 x 2800 = 0.
Base Load Power Plane
C = Capacity of plant
= 30 MW
E = Energy generated per year
= 130 x 106 kWh
M = Maximum demand
= 25 MW.
(a) Annual load factor
E 130x106
M x T 25 x 1000 x 8760
= 0.593 or 59.3%.
M 25
(b) Plant use factor =-
= 0.83 or 831/(,.
E
(c) Capacity factor =
= - --- - = 0 49 49 44
30000 x 8760
Example 2.48. An t'leetricsnpp!y company has the /oIlouing
annual expenses
Generation Rs. 80 x to'
Transmission Rs. 25 x to'
Distribution Rs. 20 x 10
Fuel Rs. 30 x 10'
Repair etc. Rs. 3.5 x
POWER PLANT ECONOMICS 131
The number of units generated per year are 430 x 106 kWh. The
consumers have an aggregate ,naxi,num demand of 80 MW. The
fixed charges for generation. transmission, distribution, fuel, repair
etc. are 80%, 90%, 9%, 15% and 50% respectively. Losses in trans-
mission and distribution are 10%.
Determine a two part tariff to be charged from the consumers.
Solution. M = Maximum demand
=80 MW = 80 x 10'kW
E = Energy generated per year
= 430 x 106 kWh.
The fixed and running charges are calculated as follows:
Rem Total Fixed charges Ru
charges Amount 'Ye Amount
(Rs.) I (Rsi
-Generation 80 64 x 20 16X IO
Transmission -25 x 104 90 22.5 x iO 10 2.5'< io
Distribution 20 x 10 5 95 19 x le 5 1. 10 5
Fuel 30 x 105 15 4.5 x iø 85 Z5.5x
Repairs !f__ 3.5 50 1.75 x 10" 50 1.75 x
Total 339x 10 301 x
C1 = Fixed charges
= Rs. 339 x io
Fixed charges per kV of maximum demand
- C1 - 339 x iO
M 80x103
= Rs. 42.37
C2 = Running charges = Rs. 301 x 10
Transmission losses = 10%
Net energy supplied (E)
= 430 x 1 6 x 0.9
Running charges per unit
C2 301 x 10 x 100
- E - 430 x 101; x 0.9
= 0.77 paise.
I
J32 POWER PLANT
18 x 106
Average load = Maximum Demand x Load factor
=SOXO.S=4OMW4OX1000kW
E = Energy generated per year = Average loac
x Time in hours
= 40 x 1000 x 8760
= 3504 x 10 5 kWh
W = Weight of fuel consumed
= 1.3xE
= 1.3 X 3504 x
= 4555x 10 5 kg
= 4555 x 102 tonne
C2 = Cost of fuel
=Wx80
= 4555 x 10 2 x 80 = Rs. 3644 x io
C3 = Salaries, wages and maintenan
= Rs. 8x105
S = Total investment
=C1+C2+C3 •;
=18x106+3644x104+8x10
. S.
5'
= Rs. 55.24 x 106
0 •5 •
Cost of generation = S -
•
POWER PLANT
134
55.24 x 106
- 3504 x 105
= 15.76 paise per kWh.
Example 2.51. Two electrical units are used for same purpose.
Cost of first unit = Rs. 7000 and it takes 90 kW.
Cost of second unit = Rs. 18000 and it takes 50 kW.
Useful life of each unit =38 x 10 hours.
Energy rate = Rs. 100 per kWof maximum demand per year and
8 poise per kWh.
Find which unit will be economical if both units run at full load.
Solution. First Unit.
C 1 = Capital cost per hour
I
==7000Rs. 0.184
38 x io
Maximum demand = 90 kW
Rate for maximum demand = Rs. 100 per kW
C2 = Charge for maximum demand per hour
90 x 100
= 8760 = Rs. 1.028
= 90 x = Rs. 7.20
= (50 x 1) ><
= Rs. 4.0
C = Total charges per hour
= C1 + C2 + C3
= 0.47 + 0.57 + 4.0 = Rs. 5.04
Hence second unit is economical.
Example 2.52. The maximum (peak) load on a thermal power
plant of 60 MW capacity is 50 MW at an annual load factor of 50%.
The loads having maximum demands of25 MW, 20 MW, 8 MW and
5 M are connected to the power station.
Determine : (a) Average load on power station (b) Energy
generated per year (c) Demand factor (d) Diversity factor.
Solution.
(a) Load factor = _ A v era g e loa4
Maximum demand
Average load = 0.5 x 50 = 25 MW
(b) E = Energy generated per year
= Average load x 8760
= 25 x 1000 x 8760
= 219 x 106 kWh.
(c) Demand factor = Maximum demand
Connected load
=-
25 + 20 + 8 + 5
= = 0.86
A ., ... ..
'.,4 . .•..)_.
: -, . . I' •
C .
"I
f t'.' ,,
•i•'•'
C..
S
3.0 Introduction
Steam is an important medium of producing mechanical energy.
Steam has the advantage that it can be raised from water which is
available in abundance it does not react much with the materials of
the equipment of power plant and is stable at the temperature
required in the plant. Steam is used to drive steam engines, steam
turbines etc. Steam power station is mbst suitable where coal is
available in abundance. Thermal electrical power generation is one
of the major method. Out of total power developed in India about
60% is thermal. For a thermal power plant the range of pressure
may vary from 10 kg/cm 2 to super critical pressures and the range
of temperature may be from 250' C to 650'C.
The average all India Plant load factor (P.L.F.) of thermal power
plants in 1987-88 has been worked out to be 56.4% which is the
highest P.L.F. recorded by thermal sector so far.
3.1. Essentials of Steam Power Plant Equipment
A steam power plant must'have following equipments
(VAt
RA6( L,.J
A".k
AR Wf -
$'4 Ifq
H P £ P CO1OfN5A If
14TfR kE41ER IXIRACIICN PW.1P
Fig. 3.1
UNLOADING
OIJTI)O011 STORAGE
(!)EAI) S7OIMGI.;
IN PL.4NT FIA.VI)I.I.VG
EIG ti/VU
AN!)
A1/.1SU/?f,V(;
b'tJI?VA(:E
Fig 32.
POWER PLANT
EVSC/IARGE END
Fig. 3.4 Screw conveyor.
GRAB
CRA N E
Fig. 3.5
Fig. 3.5 (a) shows a flight conveyor. Flight conveyors possess the
following advantages
(i) They can be used to transfer coal as well as ash.
(ii) The speed of conveyor can be regulated easily.
(iii) They have a rugged construction.
(iv) They need little operational care.
Disadvantages. Various disadvantages of flight couvevors are
as follows
(i) There is more wear clue to dragging action.
(ii) Power consumption is more.
STEAM POWER PLANT 147
Scrapper
RcPer -Chain
Coal
Fig. 3.5 (a).
ti
tation of coal or due to strikes in
coal mines. Also when the Prices
are low, the coal can be purchased
and stored for future use. The COAL/WZET
amount of coal to be stored
depends on the availabilit y of
space for storage, transportation
fci!iies, the amount of coal that
will whether away and nearness Fig. 3.6
to coal niines of the power station. -
Usuall y coal required for one month operation of power plant is
stored in case of power stations situated at longer distance from the
collieries whereas coal need for about 15 days is stored in case of
power station situated near to collieries. Storage of coal for longer
periods is not advantageous because it blocks the capital and results
in deterioration of the qualit y of coal.
The coal received at the power station is stored in dead storage
in the form of piles laid directl y on the ground.
The coat stored has the tendenc y to whether (to combine with
oxygen of air) and during this process coal toss some of its heating
value and- ignition qualit y . J)ue to low oxidation the coal ma y ignite
s>ttivuiisly. Thi s is avot(hI•cl by storing coal in the form of pilvs
148 POWER PLANT
tuna C -,
00 0
SAWDUST. GRATE
Fig. 3.8
-
Lever
'. •%'•:..
'• Grate bars
. .
GRAT( ______
I 1 11
RIMARYAR
Fig. 3. 10
boiler consist of N2, CO2 , 02 and 1120 and also CO if the combustion
is not complete.
T1AME5 QYAIR
AS
(E(N COAL -
PRIMARY AIR
Fg. 3.11
Overfeed Underfeed
-
Conveyor Spreader Single Retort Multi-Retort
Stoker Stoker Stoker Stoker
AIR FOR
I /
• Ai
I'VI E TS
I!
Fig. 3.12.
The chain travels over two sprocket wheels, one at the front and
one at the rear of furnace. The travelling chain receives coal at its
front end through a hopper and carries it into the furnace. The ash
is tipped from the rear end of chain. The speed of grate (chain) can
be adjusted to suit the firing condition. The air required for combus-
tion enters through the air inlets situated below the grate. Stokers
are used for burning non-coking free burning high volatile high ash
coals. Although initial cost of this stoker is high but operation and
maintenance cost is low.
The travelling grate stoker also uses an endless chain but differs
in that it carries small grate bars which actuall rt the fuel
fed. It is used to burn lignite, very small sizes ul an rac'. coke
breeze etc.
The stokers are suitable for low ratings .. must
be burnt before it reaches the rear of the furnace. With forced
draught, rate of combustion is nearly 30 to 50 lb of coal per square
foot of grate area per hour, for bituminous 20 to 35 pounds per
square foot per hour for anthracite.
CA1
HOPPER
OVER
cc c
AIR
r
Fig. 3.13.
I5 POWER PLANT
COAL
-kr-
Trbø II
AIR DUCT
Fig. 3.14.
5TAMp,Ec5IJFE'1
,4V ANc c.uE S ..
/ TO FAN HAND
I
I' P15 Tc'R
BOfER I
r SECOND4RY
T/0N5 I AIR FAN
N rOMSLJS T/OAI.
-f Cl/4/I8ER
- - ITOIZI
MOTOR
I/AND RF6LJLATOR
_____---%-, StIPPLY
;!R 5U"PY
FAN
V# Nt
I
Fig. 3.15.
Fig. 3.16.
160 POWER PLANT
PULVERISED COAL
TO BURNERS
RAWCOAL FEED
ROTATING •
I • •
CLASSIFIER
• •I
SPRING
UPPER
RACE
GRINDING
ELEMENTS
4.
-lOT PRIMARy I
AIR SUPPLY BALL 1101 PRIMARY
AIR SUPPLY
LOWER-1
RACE I rGLAR
WORM
Fig. 3.16(a)
BUNKER
AUTOMATIC
BALANCE
FEEDER
The air fed to the ball mill is heated in the air heater. In the
separator dust (fine pulverised coal) is separated from large coal
particles which are returned to the ball mill for regrinding. The dust
moves to the cyclone. Most of the dust (about 90%) from cyclone
moves to bunker. The remaining dust is mixed with air and fed to
the burner.
Coal is generlIy ground in low speed ball tube mill. It is filled
to 20-35% of its volume. With steel balls having diameter varying
from 30-60 mm. The steel balls crush and ground the lumps of coal.
The average speed ofrotation of tube or drum is about 18-2.0 R.P.M.
[Fig. 3.17 (b)].
FUEL IN
.I1IIj1uIi
HOTAIR
1
ARMOUR
Advantages
The advantages of using pulverised coal are as follows
1. It becomes easy to burn wide variety of coal. Low grade
coal can be burnt easily.
2. Powdered coal has more heating surface area. They per-
mits rapids and high rates of combustion.
3. Pulverised coal firing requires low percentage of excess air.
4. By using pulverised coat, rate of combustion can be ad-
justed easily to meet the varying toad.
5. The system is free from clinker troubles.
6. It can utilise highly preheated air (of the order of 700F)
successfully which promotes rapid flame propagation.
7. As the fuel pulverising equipment is located outside the
furnace, therefore it can be repaired without cooling the
unit down.
8. High temperature can be produced in furnace.
Disadvantages
1. It requires additional equipment to pulverise the coal. The
initial and maintenance cost of the equipment is high.
STEAM POWER PLANT 163
Auk
bQ
Fe
164 POWER PLANT
The pulverised fuel is dried up and then blown into shaft by hot
r.ir. Secondary air is delivered into the furnace through holes to burn
the fuel completely.
3.7 Pulverised Coal Firing
Pulverised coal firing is done by two system:
(i) Unit System or Direct System.
(ii) Bin or Central System.
Unit System. In this system (Fig. 3.18) the raw coal from the
coal bunker drops on to the feeder.
Fig. 3.18
Hot air is passed through coal in the feeder to dry the coal. The
coal is then transferred to the pulverising mill where it is pulverised.
Primary air is supplied to the mill, by the fan. The mixture of
pulverised coal and primary air then flows to burner where secon-
dary air is added. The unit system is so called from the fact that
each burner or a burner group and pulveriser constitute a unit.
R(TuRl AID
, ran—,
WENT I ,.i I
PL' VER/SED (O.4 8I.'Q
PR,MARr AIR
SE(QO4Rv.N
Fig. 3.19.
STEAM POWER PLANT
165
Advantages
I. The system is simple and cheaper than the central system.
2. There is direct control of combustion from the pulverising
mill.
3. Coal transportation system is simple.
Advantages
I. The pulverising mill grinds the coal at a steady rate
irrespective of boiler feed.
2. There is always some coal in reserve. Thus any occasional
breakdown in the coal supply will not effect the coal feed
to the burner.
3. For a given boiler capacity pulverising mill " mall
capacity will be required as compared to unit sy ;tem.
Disadvantages
I. The initial cost of the system is high.
2. Coal transportation system is quite complicated.
3. The system requires more space.
To a large extent the performance of pulverised fuel system
depends upon the mill performance. The pulverised mill should
satisfy the following requirements:
1. It should deliver the rated tonnage of coal.
2. Pulverised coal produced by it should be of satisfactory
fineness over a wide range of capacities.
3. It should be quiet in operation.
4. Its power consumption should be low.
5. Maintenance cost of the mill should be low.
Fig. 3.19 (a) shows the equipments for unit and central sS'stem
of pulverised coal handling plant.
POWER PLANT
16
RAW COAL
PRIMARY CRUSHER
MAGNETIC SEPARATOR
COAL DRIER
COAL BUNKERS
SCALE
SCALE
PULVERISER
PULVE RISER
CENTRAL BIN
7 Is
BURNERS FEEDER
FURNACE
FURNACE ,
BURNERS
and control flame shape and travel in the furnace. The flame shape
is controlled by the secondary air vanes and other control adjust-
ments incorporated into the burner. Secondary air if supplied in too
much quantity may cool the mixture and prevent its heating to
ignition temperature.
RAW COAL
BUNKER
_7 PULVERIZED FUEL
BURNERS
BURNER WINDBOX
EEDER
\ PULVERIZED FUEL
CONTROL AND AIR PIPING
DAMPER
PULVERIZER
- PRIMARY
AIR FAN
(iii) Coal air mixture should move away from 4' ,rner at a
rate equal to flame front travel in order to avL.I, iash back
into the burner.
The various types of burners are as follows
1. Long Flame Burner (U-Flame Burner). In this burner air
and coal mixture travels a considerable distance thus providing
sufficient time for complete combustion [Fig. 3.20 (a)].
2. Short Flame Burner (Turbulent Burner). It is shown in
Fig. 3.20 W. The burner is fitted iii the furnace will and the flame
enters the furnace horizontally.
3. Tangential Burner. A tangential burner is shown in Fig.
3.20 (c). In this s ystem one burner is fitted attach corner of the
furnace. The inclination of the burner is so made that the flame
produced are tangential to an imaginary circle at the centre.
4. Cyclone Burner. It is shown in Fig. 3.20 (d). This burner
uses crushed coal intend of pulverised coal. Its advantages are as
follows
S
168 POWER PLANT
Pr
Z. Secondary
air
huh
Secondary
'I
air
(a) (b)
Coal and
Primary air Cool and
primary
Sec air air
sec.—"
air
ec
Furnace
-.1 SECTION AT A-A
A
(c)
Fig. 3.20
BOILER DRUM
CONVECTION
SUPER HEATER
ECONOMIZER._
-
•o.
I I'll
AIR
PREHEATER 7WATER WALL
:7
BOILER
TUBES
Ill P ULVERISED COAL
BURNER
TO STACK ULJ
STEAM POWER PLANT 169
RAW COAL
BUNKER
FEEDER
CONVEYOR
PRIMARY
AIR
Rota
IICRUSHER J I—'-1
BREAKER VALVE
______ d It C
T CYCLONE
FURNACE
f .
COAL PIPE
41,121
CONVEYOR
Fig. 3.21 (b) Shows a typical firing system fo r ., ,urnace.
IA'SULATING CONCRITE
rMANOED METAL LATH
NIGH TEMPPLASTIC/#15LATIOn
MAGNESIA BLOCK
CASING
Touching tubes.
CAST
L. .r...
BRICK
NSi'L A nON
BLANKET
4_^^ INSUtA''
CASING
Half radiant cast ief.ctoiy.
CHI-tEY
ASH DrSCHARGE
EQUIPMENT
Fig. 3.23
BOILERS
WATER_
SUMPS
BOILERS
Fig. 3.24
FURNACE
NOZZLE
STOKER
T.ROUGH___1
WATER JETTING
Fig. 3 25
rF
D. PIPE
HOPPER
H.P.P UMP
__ I ID
BT D S PUIP
JLR S.8.N.
A.F.N. ,LiI
-.
SCREE
Fig. 3.26
cc
ir
uJ
x
'U
cr
Fig. 3.27
3OILER
FU RNA CE S
ASH
U 6H
cII1 TRUCK
between them at high voltage (Fig. 3.30). The flue gases are made
to pass between these two sets ofelectrodes. The electric field ionises
the dust particles that pass through it attracting them to the
electrode of opposite charge. The other electrode is maintained at a
negative potential of 30,000 to 60,000 volts. The dust particles are
removed from the collecting electrode by rapping the electrode
periodically. The electrostatic precipitator is costly but has low
maintenance cost and is frequently employed with pulverised coal
fired power stations for its effectiveness on very fine ash particles
and is superior to that of any other type.
The principal characteristics of an ash collector is the degree of
collection.
il = Degree of collection
G1—G2
C'
- Cl - C2
Cl
where Gi = Quantity of ash entering an ash collector per unit
time (kgls)
G2 = Quantity of uncollected ash passing through the
collector per unit time (kg/s)
C, Concentration of ash in the gases at the inlet to the
=
ash collector (kg/m3)
C2 = Ash concentration at the exist (kg/rn3).
Depending on the type ot fuel and the power of boiler the ash
collection in industrial boilers and thermal power stations can be
effected by mechanical ash collectors, fly ash scrubbers and electros-
tatic precipitators.
For fly ash scrubbers of large importance is the content of free
lime (CaO) in the ash. With a high concentration of CaO the ash can
be cemented and impair the operation of a scrubber.
The efficiency of operation of gas cleaning devices depends
largely on the physico-chemical properties of the collected ash and
of the entering waste gases.
Following are the principal characteristics of the fly ash
(i) Density
(ii) Dispersity (Particle size)
(iii) Electric resistance (For electrostatic precipitators)
(iv) Coalescence of ash particles.
STEAM POWER PLANT 179
Due to increasing boiler size and low sulphur high ash content
coal the problem of collecting fly ash is becoming increasingly
complex. Fly ash can range from very fine to very coarse size
depending on the source. Particles colour varies from light tan to
grey to black. Tan colour indicates presence of ion oxide while dark
shades indicate presence of unburnt carbon. Fly ash particles size
varies between 1 micron (iji) to 300.t. Fly ash concentration in flue
gases depends upon mainly the following factors:
(i) Coal composition.
(ii) Boiler design and capacity.
Percentage of ash in coat directly contributes to fly ash emission
while boiler design and nr'ration determine the percentage
retained in the furnace as botiin ash and fly ash carried away by
flue gas. Fly ash concentration widely varies around 20-90 g/mm3
depending on coal and boiler design. Fly ash particle size distribu-
tion depends primarily on the type of boiler such as pulverised coal
fired boiler typically produces coarser particles then cyclone type
boilers. Electrostatic precipitator (ESP) is quite commonly used for
removal of fly ash from flue gases.
Purified gas
Houi
Inlet
ii
180 POWER PLANT
Dust
Ladden
IJ I
GasCIeari
li
1111111
U Gas
.1
Dust Hopper
Dust -
Fig. 3.28 (b).
3.12.2 Fluidised Bed Cbmbustion (FBC)
Burning of pulverised coal has some problems such as particle
size of coal used in pulverised firing is limited to 70-100 microns,
the pulverised fuel fired furnances designed to burn a particular can
not be used other type of coal with same efficiency, the generation
of high temp. about (1650 ' C) in the furnace creates number of
problems like slag formation on super heater, evaporation of alkali
metals in ash and its deposition on heat transfer surfaces, formation
Of SO2 and NO in large amount.
Fluidised Bed combustion system can burn any fuel including
low grade coals (even containing 70% ash), oil, gas or municipal
waste. Improved desuiphurisation and low NO emission are its
main characteristics. Fig. 3.28 (c) shows basic principle of Fluidised
S
182 POWER PLANT
SOLID I I I . - TART UP
FUELN H SBURNER
DEFLECTOR
WALL
Lid IT c
ii
MATTER —•
DISTRIBUTE - LIQUID
________ FUEL
L4 M4 AIR
AIR AIR
H4
ASH
AIRrORT
ASH
Fig. 3.28 (c
3.13 Draught
The purpose of draught is as follows:
(i) To supply required amount of air to the furnace for the
combustion of fuel. The amount of fuel that can be burnt
per square foot of grate area depends upon the quantity of
air circulated through fuel bed.
(ii) To remove the gaseous products of combustion.
STEAM POWER PLANT
183
Draught is defined as the difference between absolute gas pres-
sure at any point in a gas flow passage and the ambient (same
elevation) atmospheric pressure. Draught is plus if <Pgos and
it is minus Pat . > Pgas. Draught is achieved by small pressure
difference which causes the flow of air or gas to take place. It is
measured in millimetre (mm) of water.
kflpjr
"IS , B0 40-80 kV dc
Cleaned gas
Rectifie
Gas teal
Inlet H.4 Cu^rrent[ gas
Tr
Oust laden
gas - electr
jE,n,tt ing
Ilecting
electrode
Duet
Fig. 3.29.
Fig. 3.30.
cc
COAL CIWAINEY
MOURNACC
Fig. 3.31.
I,'
STEAM POWER PLANT
185
The fan sucks in gas from the boiler side and discharges it to the
chimney (stack).
The draught produced is independent of the temperature of the
hot gases an d, therefore, the gases may be discharged as cold as
possible after recovering as much heat possible in air preheater and
economiser.
In forced drauLc vstem [Fig. 3.32 (b)] the fan installed near
the boiler base supplies the air at a pressure above that of atmos-
phere and deIivers it through air duct to the furnace. Most high
rating combustion equipment employs forced draught fans for sup-
plying air to the furnace. Forced draught is used in under fed stokers
carrying a thick fuel bed.
t
Li
-,i
DRUM
LO. r.4,v
()
a
r1 cHflNey
(b)
GR4T
F 0 F,1N
/o\ - lOrAN
(c)
Fig. 3.32
—14
POWER PLANT
186
Forced
fan
I nduced
f.
u _!
Grote
conomiser
Air
Furnace pre-heciter
e
Atmosph ric
r pressure (mr
P,
4=-^
P5
Fig. 3.32 Balanced draft.
(0 S q*
[Various types of blade forms are shown in Fig. 3.331
Backward
cu,vzd
Forward
curved
Fig. 3.33.
Rod, al
STEAM POWER PLANT
187
The air leaving the tips of ackward curved blades possesses low
velocity. This makes them suitable for high rotor speed. Fans with
backward curved blades are used in forced Iraught system. Forward
and radial blades are used in induced draught fans.
3.13.1 Comparisons of forced and induced draughts
The forced draught system has tie following advantages as
compared to induced draught
i) The induced draught handles more volume of gases and
at elevated temperature. Therefore, the size and power
required for induced draught fan is more than forced fan.
iii) Improved route of burning of fuel is achieved by using
forced draught because there is more uniform flow of air
through the grate and furnace and also the air penetrates
better into the fire bed.
(iii) In case of induced draught when doors are opened for
firing there will be rush of cold air into the furnace and
this reduces the heat transmission
(iv) The induced dr:uight fan handles flue gases at high
temperature and us water cooled bearing are needed for
induced draught Ian.
Steam Jet Draught. Steam jet draught may be induced or
forced draught depending upon the location of steam jet producing
the draught.
Induced dra ight produced by steam jet is shov n Fig. 334 (a).
This system is used in locomotive boilers. Exhau i steam from the
engine enters the smoke box through a nozzle to ci te draught. The
air is induced through the flues, the grate and as. t to thy smoke
box.
STE.4M
A/R
SUCKCC, 111
5TE NCZZ(E
F 05FR
ST,. .,OLJcEQ OR4L6HT SYSTEM Jt T-FORCED 2RAt6H7 5Y5 TEl"
(a)
(b)
Fig. 3.34.
188 POWER PLANT
Pf + Ps = PA + P0 + PV
where PF = Total fan effect pressure
Ps = Net stack effect
(Chimney ± vertical passages)
PA = Draft pressure loss on air side.
= Sum of friction losses in following:
(i) Airducts, bends (ii) Air heaters
(iii) Stoker be
STEAM POWER PLANT 189
(iv) Secondary air pressure at fuel burner.
Po = Draft pressure loss on gas side.
This is sum of friction losses in the following:
(i) Gas ducts, bends (ii) Economiser
(iii) Air heater (iv) Super heater
(v) Boiler setting (vi) Chimney
Pv = Gas exit velocity pressure.
3.14 Chimney
Chimneys are made up or steel of bricks and concrete. Concrete
chimneys are more popular. The average life of concrete chimneys
is 50 years and that of steel chimneys is ah''. v':rs depending
upon the care taken to prevent corrosion. The net . .a of chimney
depends on the following factors:
(i) Volume of gases to be discharged when
at maximum rating.
tr
boilers operate
(ii) Draught to be produced.
Chimney generally denotes brick concrete construction whereas
stack means steel construction.
Fig. 3.36 (a) shows a brick chimney and Fig. 3.36 (b) shows
reinforced chimney. Chimney is provided with a lighting conductor,
aircraft warning lights, and various means of access and inspection.
The various advantages of steel chimneys over masonry chim-
neys are as follows
(i) Lower overall cost (ii) Slightly high efficiency
(iii) Easier construction (iv) Requires lesser space
(u) Lighter in weight.
R.C.C. chimneys are also becoming popular.
3.15 Calculation of Chimney Height
Air is required to burn coal or fuel in the furnace. We know
C + 02 = CO2
This shows that volume of chimney gases produced by the
complete combustion of 1 kg of coal or oil is same as that of air
required to support combustion if the temperatune of flue gases and
air is same. -
Let H = Height of chimney above grate level in metres.
W = Weight of air in kg required per kg of fuel.
T = Average absolute temperature of chimney gases in K.
T1 = Absolute temperature of air outside the chimney in K.
190 POWER PLANT
(IW4
(a) (b)
Fig. 3.36.
Weight of chimney gases produced
= (W x 1) kg of fuel burnt
rno Of chimney gases at 231K
= volume of 1 kg air at 273K
= 0.7734 x
STEAM POWER PLANT 191
T
0.7734 X
27
Volume of( IV' 1) kg of chimne y gases at T K
07731 x X W
1 '73
1.293 . xlIL
7'
1 Hi it
3:,.>!! . T km.
* H [[i (W+1 1
353
h' =
W+1 1
1.293 x 273 x1,— —x-
h'=H[1,i)x_
Example 3.2. A chimney is 28 metres high and the temperature
of hot gases inside the chimney is 320C. The ternperaiuie of outside
air is 27C and furnace as supplied with 15 kg of air per kg of coal
burnt. Calculate
(a) Draught in mm of water.
(b) Draught height in metres of hot gases.
Solution. We have
11=
P
Difference of pressure (1P)
= Height of chimney (H)
- Pi1u) kg/mm2.
A P = 22 mm of water = 22 kg/in'.
(As 1 kg/rn 2 = 1 mm of water)
= P
=I
1.033x104 3
= 29.26x(273+205 = 1.2 kg/rn
(P = Pressure = 760 mm of Hg = 1.033 kg/cm2)
1 P = 1.033 x 101
p, = = = 0.69 kg/rn
194 POWER PLANT
11 x 1.2 . 1 kg.
Mass of equal column of external air A x
Difference in masses = 1.24 All 0.65 All 0.59 A x 1 kg.
= 0.59 11 mm of water.
(As 1 kg/rn 2 = 1 mm of water)
0.5911=16
11 = 27.1 metres. Ans.
Example 3.4. (a) A chimney proc/aces a c/ru ugh t of 1.8 (-111 of
It, cite I, when temperature of /7ue gases is 280°C and anl/)tent tempera.
tare is 21°C. The flue gases formed per kg of fuel burnt are 21 kg.
Taking diameter of chirn nev as 1.77n c/etermi,u' the mass of/be gases
flowing through the c/urn ,iey.
Solution.
It Draught
1.8 cm -
IS mm of water
T - Temperature of flue gases
280° f 273
= 553°K
= Ambient Temperature
= 21 -i 273
= 294"K,
W = Mass of air reqd. per kg of fuel
=24-1
= 23 kg
h=353H[-(.-jx
18 = 353 H[- - x
23 553
^23-)
H = 34.1 in of air
ii' = Height of column of hot gases
r w ' T 1
=HLix 1J
I
[23 553
x
=
= 28.9 in of air
C = Velocity of gases
=
=
= 23.5 m/s
Wg = mass of flue gases
=AXCX
where A = Area of chimney
Tt
=-x(1.7) 2 fly)--
1
x
=
=33[__ x 1
= 0.67 kg/m 3
(17)2 x 23,5 x 0.67
= 35.7 kg/s.
3.16 Methods of Burning Fuel Oil
Fuel oil is burnt by means of burners. The function of a burner
is to atomise the fuel and mix it with proper amount of air for
combustion. The various types of burners used are as follows
CCIT
-
Fig. 3.37
. 196 ... POWER PLANT
AIR NOZZLE
SPARY OIL.
CONE
.A1ISNG1I
cup
AIR
Hg. 3.38 (a)
oil Out
Slewn
Fig. 3.38.1 Fig. 3.38.2
198 POWER PLANT
Low pressure burners use air pressure between 0.015 bar to 0.15
bar. They are simple in shape and are quite commonly used.
(i) Blast -atorn.jsation. In this method the oil is atoinised by
compressed air or steam. Steam atomising burners may he inside
burners or outside burners.
Ia the inside burners the steam and (0l oue in contact inside
the burner and atomisation of mixture tik place while passing
through the orifice of the burner. Fig. 3.37 (a) shows an injector
inside mixing burner. In outside burner, the oil is pumped to the oil
orifice and is picked up and atomised by jet of steam outside the
burner.
(ii) Mechanical atom isation. I n this method the fuel oil is
atoinised b y subjecting it to a high pressure and passing it through
an orifice. Fig. 3.38 (h) shows Babcock and Wilcox mechanical
atomising burner. The fuel oil flowing through the centre tube is
atomised and discharged through tangential slots in the sprayer
plate. The oil then passes a conical chamber with an orifice at its
apex and due to whirling action oil leaves the orifice in the form of
a hollw tone of minute particles.
Fig. 3.38 (c.) shows spring loaded piston type burner also called
oil pressure t y pe burner. The oil comes out of nozzle in the form of
spray
3.16 (a) Fuel oil and gas handling
Fuel handling system is designed depending on the type and
nature of ueI. I'i. 3.38d) shows liquid fuel handling arrangement-
Fuel storage tanks of concrete or steel are located near the power
plant. Underground tanks are usuall y preferred. A vent pipe open
to the atmosphere allows the storage tank to breathe. The level
indicator is used to record the level of oil in the tank. Oil pumped
from the tank is first passed through strainers, and then through
heaters to bring the liqi.iid fuel to the conditions necessary for the
burners. Man-hole is provided for cleaning the storage tank.
Pipes are used to handle the gas in power plants using gas as
fuel. The pipe line may divide into two parallel lines each fitted with
the following
(. 1) meters (ii) regulators
(lit) stop valves.
Plants call justify storing gas on their premises. However
underground storage proves feasible in some areas. ManY plants use
natural gas as fuel. For best econom y the pipe lines should be kept
flowing at full capacity.
Control
valve
I Burners
Excess Discharge
Boiler pressure
Strainers
relief line
(return)
Level
indicators ØPressure
j
Vent pipe
21 rr_ID. lanhole
Strainer
Oil
pumps
Heaters
Storage tank
Heating
cod
Fig. 3.38 (
Stag
-,
ii
Fig. 3.39
Fig. 3.40
Secondary Primary
furnace
Slog
.18 Economiser
In order to utilise the heat accompanying combustion gases
?aving the furnace, the gases are passed through the heat recovery
I1 ip111e11t such as economiser and air preheater.
.15
202
POWER PLANT I
b
Economiser. Economiser is a device intended for heating the
feed water by means of flue gases from boiler. There are steaming
economisers in which the water is raised to the boiling point and
partially (10-20%) evaporates and non-steaming economisers in
which the temperature of water is below the boiling point by
20 - 30°C. The advantages of an economiser are as follows:
TUBES
-WATER
WATER
Fig. 3.43
WATER
QUTLEr
WATER
/AIL ET
FLUE 645
Fig. 3.44
00000000 0000000
0 0000000 0000000
000000000000000
00000000 0000000
00000000 0000000.\
0000000
• 00000000 0000000
00000000 0000000
0001,0000
S gases
,__
,7; -7l I O77 I.-7,
- Lancashin
boiler
Fig. 3.44 (a)
travel in the opposite direction (counter flow). Fig. 3.46 (a) shows
the variation of temperature along the flow paths of the fluids.
oh0
OCj
Fig.3 16(a).
The heat transfer from the hot flue gases to water in case of
economiser and to air in case of air preheater is found as follows
Q = UA.0,,,
where Q = Quantity of heat transferred
U = Overall heat transfer coefficient
A = Area of heat transfer surface
= Log Mean temperature diticconce
- 0, -
log 0,
61,
Or,, = Outlet temperature of cold fluid
0,., = Inlet temperature of cold fluid
= Outlet temperature of hot fluid
Oh, = Inlet temperature of hot fluid
0, = Temperature difference at inlet = Oh, - 0,
0,, = Temperature difference at outlet = Oh, -
3.19 Super Heater
Thesteam produced in the boiler is nearly saturated. This steam
as such should not be used in the turbine because the dryness
fraction of the steam leaving boiler will be low. This results in the
presence of moisture which causes corrosion of turbine blades etc.
To raise the temperature of steam super-heater is used. It consists
Of several tube circuits in parallel with one or more return bends
connected between headers. Super-heater tubes range from 1 to 2
inch of diameter. Super-heater supplies steam at constant tempera-
206 POWER PLANT
Fig. 3.48
The final temperature of steam depends upon the gas flow rate,
quantity of gas flow and the temperature of the gases leaving the
Fig. 3.49
Fig. 3.50
b 208 POWER PLANT
1..
\\
E.2
\\'
()
E ma
I1__
3. -o
0. 0.
E-
E
0 ci
2 -i
(.0 -
C
C
(Al
I? 3
E
0
0 0
0
(0
E —0
0 u_ Q(
Desu per
heater
Steam
Drum
Super heater
sections
F(owmeter
Inlet
valve
Venturi Fine sand
nozzle
Backward Gravel
water to
Alum waste
pot Strainer
Raw water
Filtered
water
Backward outlet
supply
Filtered water
to waste
Fig. 354 (a).
form of uniform showers over the heating trays and air separating
trays and finally gets collected in the storage space. Steam enters
the heater through a nozzle fitted in the side of heater shell. The
entire space between the shell and tray compartment gets filled with
steam. The steam makes its way downwards through the perfora-
tions in the top plate of tray compartment. While flowing downward
the steam comes in contact with the falling water. Most of the steam
condenses in between the spray and heating trays. From the bottom
of heating trays, the remaining steam and separated gases such as
oxygen etc. flow to the vent condenser. The steam used for heating
may be the main turbine bled steam or may be from other sources.
Storage tank with controls helps to add make up water when needed
to maintain the feed water flow.
Closed Feed water heater
Fig. 3.55 (A) shows a closed feed water heater in which steam
bled from steam turbine is used for heating the feed water. This
process is also called regenerative process and increases the efficien-
cy of the generation cycle.
214 POWER PLANT
VENT WA7ER COA/TROI
VALVE
VENT __
CONDENSER
5PR4 y PIPE
uLJuijuuI
LJLJLJLJLJ I
HE.4TIWG TRAYS UUuIJL, UI .STEAAI
.4/P 5EPARAT/N6— 4-J L3L_JL.I ,
TRAYS LJLJLLJ
TO 5ORAGE
• TA WI(
T9 FEED
WATER P1114P
Fig. 3.55
Turbine
ICondenser
Boiler
Heaters
Pump
"Condensate
Hot weii_- extraction pump
Fig. 3.55 (a) FOR
Row AirFloat
e f
water re control
storage
, Teolite -Gravel
Graded
gravel Brine tank
flow controller
1xc
BOILER
—16
Fig. 3.56 (b)
POWER PLANT
218
Fig.
3.56 (b) shows mass balance of impurities and treatment
chemical s, in boiler.
3.25 pH Value of Water
It is the logarithm of the recipuocal of hydrogen ion conceittra-
hon in water. in water either hydroxyl ions (011 - or h ydrogen ions
1)
8. Hardness as CaCO
9. Silica as SiO2
10. Iron as Fe-203
11. Sodium -
i2iii ie1ii1ii—It
13 . Calcium
................. -
14. Carbonates as CO3 -
15. Bicarbonates as llCOj
Ilvdroxide as
L_
17. Sulphate as SO4
Chloride as Cl
19. Nitride as NO:3
20. Carbon dioxide S --
STEAM POWER PLANT 219
Condensote Water
inlet
Fig. 3.56 (c).
Chemical tests are performed at frequent intervals on samples
of water to have information of some improtant items such as
variation in mineral characteristics of raw water suppl y , condition
of boiler water with respect to treatment adjustment and blow down
adjustment percentage ofcoridensate and make up in the feed water
220 POWER PLANT
b
steam purity and correction of feed water and boiler water for
corrosion control etc.
3.28 Steam Condensers
A steam condenser is meant to receive the exhaust steam from
the turbine or engine, condense it and maintain a pressure at the
exhaust lower than atmospheric. Some extra work is obtained due
to exhaust at a pressure lower than the atmospheric. This improves
the efficiency at a pressure lower than the atmospheric. This im-
proves the efficiency of the plant. Air inside the condenser should
be pumped out continuously in order to maintain the vacuum. The
condensation of steam occurs in the range of 25'C to 38'C.
Steam pressure in a condenser depends mainly on the flow rate
and temperature of the cooling water and on the effectiveness of air
removal equipment. Some of the advantages of a steam condenser
are as follows:
(i) It increases power output. Power plant cycle improves in
efficiency as the turbine exhaust pressure drops.
(ii) It recovers most of the feed water (in case of surface
condenser) which is available at 45'C to 50'C. This save
the amount of fuel to be burnt in boiler.
(iii) The use-of condenser, decreases the size of boiler installa-
tion.
The main disadvantage of condenser is that it adds to the initial
cost of power plant as the condenser requires additional equipment
such as cooling tower or cooling pond, vacuum pump, water circulat-
ing pump etc.
The vacuum obtainable in a condenser is governed by the outlet
water temperature which in turn varies with the amount ofcondens-
ing water used per kg of steam and its initial temperature. Air
entertainment in the condenser has its effect upon the vacuum. The
addition of air lowers the vacuum.
3.29 Types of Steam Condensers
Steam condensers are of two types:
(i) Surface condensers (ii) Jet condensers.
3.29.1 Surface Condensers
In surface condensers there is no direct contact between the
steam and cooling water and the condensate can be re-used in the
boiler. In such condenser even impure water can be used for cooling
purpose whereas the cooling water must be pure in jet condensers.
Although the capital cost and the space needed is more in surface
condensers but it is justified by the saving in running cost and
increase in efficiency of plant achieved by using this condenser.
Depending upon the position of condensate extraction pump, flow of
STEAM POWER PLANT
221
condensate and arrangement of tubes the surface condensers may
be classified as follows
(i) Down flow type. Fig. 3.56(d) shows a sectional
view of down
flow condenser. Steam enters at the top and flows downward. The
water flowing through the tubes in one direction lower half comes
out in the opposite direction in the upper half. Fig. 3.57 shows a
longitudinal section of a two pass down-flow condenser.
Steam and
Air
Air and
Steam
Exh(rst
Cover
Plate
Baffle
Wa t e, Plate
Box
onden.qa ;e
Fig. 3.58.
Steam
Air
(ati2'1 ate -
Fig. 3.59.
STEAM POWER PLANT 223
Condensate
- r— Outlet
Fig. 3.60.
(ii) High level or Barometric condenser. Fig. 3.61 shows a
high level jet condenser. The condenser shell is placed at a height
of 10.33 ni (barometric height) above the hot well. As compared to
low level jet condenser this condenser does not flood the engine if
the water extraction pump fails. A separate air pump is used to
remove the air.
(iii) Ejector Condenser. Fig. 3.62 shows an ejector condenser.
n this condenser cold water is discharged under a head of about 5
.0 6 m through a series of convergent nozzles. The steam and air
enter the condenser through a non-return valve. Steam gets con-
densed by mixing with water. Pressure energy is partly converted
into kinetic energy at the converging cones. In the diverging cone
the kinetic energy is partly converted into pressure energy and a
pressure higher than atmospheric pressure is achieved so as to
discharge the condensate to the hot well.
STEAM POWER PLANT
225
Air Pump
Suction
Tail
Pipe
Th.jcct ion
Pump
t er
In 1 et
Non Return
onvera1ng Va lye
Cones
Exhaust
Steam
Dierifl!1
Cone
vnioclyzrac to
hot Well
Fig. 3.62
water. The water coming out of the condenser is hot and is cooled in
order that it may be recirculated through the condenser.
There are two types of condensers namely surface condenser
and jet condenser. The surface condensers are preferred because the
cooling water and exhaust stem do not mix with each other. The
cooling water passes through the tubes and steam passes over the
outer surface of tubes. The steam leaves the condenser in the form
of condensate which is re-used as boiler feed water. The amount of
cooling water required is usually quite large such as in large steam
power plants millions of gallons of cooling water per hour is required
for the condenser. Therefore, the source of cooling water chosen
should be able to supply the required quantity of cooling water. The
coi:ling water supply is made by the following sources:
Ci) River or sea (ii) Cooling ponds (iii) Cooling towers.
3.30.1 River or sea
Large power stations require enough quantity of cooling water
per hour. Such plants are usually located near a river or sea. The
water is constantly drawn from the river by the pump, filtered and
circulated through the condenser: Hot coolant is discharged back
into the river (Fig. 3.63).
F/t TeR
PUMA
Fig. 363
PLAN
SECTIONAL ELEVATION
COOL fMI- PONO
Fig. 364
Air
rffLcuvers
Water—=='J_______
(n
water
out
Fig. 3.64 (a)
URBINE
&IRIH J) lUNJCI.ING UNIT
WATER
PUMP
kK
NO EN 5€ P
CIRCULATING
PUMP
Fig. 3.65
INICT
HURDLESS
Fig. 3.66
Cooling towers may be made up of timber, .concrete or steel. A
concrete hyperbolic cooling tower is shown in Fig. 3.66. Fig. 3.67
shows the water circulation from the cooling tower to the condenser.
Fig. 3.65 shows the cooling tower in which the position of turbine
has also been shown. The system consists of turbine, condenser.
Circulating pump, tank, additional water pump and sprinkling unit.
STEAM POWER PLANT
229
The air is delivered through the holes in the side walls of the tower.
The circulating water is delivered to the upper part of the watering
unit where it flows down and gives its heat to the surrounding air.
The cooled water flows into the tank and is circulated through the
condenser. Towers made up of the concrete are preferred because
they are stable against larger air pressure, their maintenance cost
is low and they have larger capacities.
WATER
Fig. 3.67
,PAY(LJA1FNATOR HdTA/R
SPRAY
- hT WAT!R
OW(Rft P/6 _______ :• ____
SLArS
Cool.o I k
CA rci,' 8AI
Fig. 3.68
Hot Air
on
Motor
Eliminator
I Hot
Nozzle
Water
Cold -
Water
Fig. 3.68 (a)
= P1
'2
where PI = Actual vacuum in condenser
P2 = Theoretical vacuum in condenser.
Theoretical vacuum in the condenser is the vacuum if no air is
present in it.
3.34 Condenser Pressure
The total condenser pressure (P) is given by the relation
P =P +P
where P. = Steam saturation pressure corresponding to steam
temperature
Pa = Air pressure.
Air must be removed constantly to keep P0 low.
Example 3.5. The vacizurn in a condenser is 68 cm. of Hg with
barometer reading 76 cm of Hg. lithe inlet and outlet temperatures
of cooling water to a condenser are 28'C and 42 C respectively,
calculate the condenser efficiency.
Solution. Ti = 28C
T2 =42'C
Rise in temperature = 42 - 28 = 14C
Absolute pressure in the condenser
= 76-68 8 c of Hg = 0.108 kg/cm2,
Saturation temperature corresponding to 0.108 kg/cm 2 = 47 C.
0
232 POWER PLANT
Condenser efficiency =
= x 100 = 73.6%.
7'2 - Tj
7'2 - T1
Now in place ofH, and d 1 the corresponding temperature Tand
T3 respectively can be substituted with sufficient accuracy.
• _________
-
STEAM POWER PLANT 233
- 1 (T + qLT3)
-
IV W
-
= 40(38 + 1
= 960 kg.
g.
To atmosphere steam
from turbine
....._Livt steam
t
Co nd enser
Steam jet Water
ejector gouge glass
Condensate Pump
CircutotnQ pump
Fig. 3.69 (a)
STEAM -- STEAM
INL E 7 CLI TLE 7
Fig. 3.70.
Water
gouge aBaffle
Water
r Q fl
C
238 POWER PLANT
Fig. 3.70 (a) shows baffle plate steam separator. Steam entering
the separator moves down and strikes the baffle plates and gets
deflected water particles fall to the bottom of separator and are
drained off. Steam leaving the separator is free from moisture.
(iii) Separator with screens. In this separator, the water
particles are separated by mechanical filtration.
3.42 Steam Trap
The water formed due to partial condensation of steam is pipe
line should be removed to avoid damage. It is done by locating a
steam trap. Traps are used on steam mains, headers, separator etc.
where they remove water formed due to condensation. Trap allows
automatic removal of water but permits now flow of steam. The
various types of steam traps in common use are as follows
(i) Ball float steam trap.
(ii) Inverted bucket type steam trap.
(iii) Thermostatic traps.
(iv) Expansion of orifice traps.
• CONDANSATE
I •i— INSET
8,1L L
FLOAT
W.4 T1/?
::::;Z?72')mrA CJTLET
Vt.
Fig. 3.71
STE.4M lE4rEO
(dU/PMENT
; f 'dGA7E VAcVE
57Q/4'EP
I.'
0 SC EL/NE CATE
Fig 3.72
Fig. 3.73
2. According to the direction of steam flow
(i) Axial (ii) Radial
(iii) Mixed.
3. According to pressure of exhaust
(t) Condensing (ii) Non-condensing
(iii) Bleeder.
4. According to pressure of entering steam
(i) Low pressure (ii) High pressure
(iii) Mixed pressure.
STEAM POWER PLANT 241
"VVIV6
& ADES CL E4Qt.'c
S :'E4/.1 .. ii u ii II I I
ENTRy L,1LJI II II I I EXHAUST
Fig. 3.74
Nozz le
Box
Throttle
Valve(V)
Stecor
lelt
(f;)
Fig. 3.75
Steam
Fig. 3.76
244 POWER PLANT
Bar Lift
Valve St
Valve Li ft Bar
3.49 Boilers
Boiler is an apparatus used to produce steam. Thermal energy
released by combustion of fuel is transferred to water which
vaporises and gets converted into steam at the desired pressure and
temperature. The steam produced is used for:
(i producing mechanical work by expanding it in steam
engine or steam turbine.
STEAM POWER PLANT 247
Boiler
Water
Fuel
Fig. 3.78 (a)
Stearn Control
err
Turbine
Insulation V
steam
Fig. 3.78 (b) Shows flow of steam through the steam turbine.
248 POWER PLANT
Turbine shatt
._..j_...To turbine
arm
4 / J 11- I1
DOUblQ__H
t
Steam
Fig. 3.78.
Fig. 3.79
2. Internal furnace
(1) Horizontal tubular
(ii) Short fire box (b) Locomotive (c) Compact (d) Scotch.
(ii) Vertical tubular
(a) Straight vertical shell, vertical tube
(b) Cochran (vertical shell) horizontal tube.
Various advantages of fire tube boilers are as follows
(i) Low cost
(ii) Fluctuations of steam demand can be met easily
(iii) It is compact in size.
5TgAM
FURNACE 8E0
AIR
Fig. 3.80
Furnacee'BIOwott
valve
h pit
Mud box
Cleaning
door
Fig. 3.8
STEAM POWER PLANT
251
CCW6U5 TON
CH4/IBER
SMOKE
",P.A' BOX
T .-._
Fig. 3.82
3.50 (b) Cochran Boiler
A brief outline of this boiler is shown in Fig. 3.82. The coal burns
on the grate inside the fire box. The flue gases after passing through
POWER PLANT
252
the combustion chamber make their way through the fire tubes. The
gases heat the water and convert it into steam hich collects in
steam space, and can be taken out through steam stop valve. The
flue gases escape to the atmosphere after passing through smoke
box and stack. Man-hole is provided to clean the boiler when neces-
sary. A fire brick lining is provided to prevent the shell from being
damaged. It is a vertical type boiler, requires lesser space and is
quite compact in design. In such boilers the ratio of heating surface
to great area ranges between 10 to about 25 and steam can be
produced upto a pressure of 10 kg/cm 2 . This boiler is made in size
upto about 2.743 metres diameter and 5.791 metres height and the
maximum evaporative capacity from and at 100C is 4730 kg per
hour.
2. According to position of furnace
(i) Internally fired (ii) Externally fired
In internally fired boilers the grate combustion chamber are
enclosed within the boiler shell whereas in case of extremely fired
boilers and furnace and grate are separated from the boiler shell.
3. According to the position of principle axis
(i) Vertical (ii) Horizontal
(iii) Inclined.
4. According to application
(i) Stationary (ii) Mobile, (Marine, Locomotive).
5. According to the circulating water
(i) Natural circulation (ii) Forced circulation.
6. According to steam pressure
(i) Low pressure (ii) Medium pressure
(iii) Higher pressure.
3.51 Lancashire Boiler
Fig. 3.83 shows a brief outline of this boiler. The coal is fed
through the fire hole on the gate (G) where its combustion takes
place. F.B. represents Fire-box. The flue gases move through the
entire length of the furnace tubes (T) upto the back end then move
downward and flow along the bottom flue and finally letive to the
atmosphere through a chimney. The surface tubes are nearly one
metre in diameter, the diameter being larger at the front end and
smaller at the rear end.
The two furnace tubes are surrounded by water on all sides. The
boiler shell is filled with substantial quantity and is supported over
the brickwork. The steam produced collects in the space above the
water level. Blow cock (B.C.) is provided to empty the boiler so that
repairing, inspection or cleaning can be carried out when desired.
Such boilers are gr'nerally constructed for working pressure upto
17.5 kg/cm 2 and evaporation capacity of 8300 kg hour.
STEAM POWER PLANT 253
JTT
L1 1tt
ii •
l'
1i:1 i1
ii
Fig. 383.
Smoke I--CombustIOn
box .. - chamber
_
--1
\ I--
L-
Furnace
Fire tube
Bottom
flu
I CASES AIR
TO PRE HEATER
COWNEY
tIorAIR
DRAFT
EOU,PiEN r
SLJPE1 HLA TL
H OrFLUE
GASES
STLAM
Fig. 384
Heat
Supply
17 't
Biier D:"a'
FCCd Water
1eci1 Water
Va
Fig, 3.85(b)
&A1 1/ STEAM
- I tiri7vER
I. 1jT .r.Eo
'o
')1' SE(T"2V
24 POWER PLANT
5 TEA . To
pRfMr.AIO vR
-1
ECO)V OM/5ER 1
I
CON V5C TON i
5L/PERHATR
-4 RADIANT I
.SUPERHEATER
STEAM
IRCuAT/NG
PUMP [HI
ORLJPI
Fig. 3.86
ECONOMISER
5rg4/.1
To
PR'#4EMOVER r
II
AEED POMp
1._
Fig. 3.87
STEAM To
PRIME MOYER
CONVECTION
SUPER YEA TER-
STEAM
54R4 TIMS .-
SEC TIC/V
Areo
PUMP
IWC
(i) The steam can be raised quickly to meet the variable load.
(ii) By using high pressure boilers the efficiency of steam
power plant is increased upto about 40%.
(iii) By using forced circulation, there is more freedom in the
arrangement of furnace, tubes and boiler components.
(iv) The space required is less.
(v) Light weight tubes with better heating surface arrange-
ment can be used.
(vi) The tendency of scale formation is eliminated clue to high
velocity of water through the tubes.
(vii) Various parts are uniformly heated. Therefore, the danger
of overheating is redqced and thermal stress problem is
simplified.
3.63.2 Selection of boiler
Selection of boiler depends upon the following factors
(1) Type of fuel
(ii) Space available
(iii) Cost of fuel
(it) Controls necessary to enable the load to be picked up
quickly
(t) Desireability of using heat recovery equipment such as air
preheater, economiser
(ti) Type of load to be supplied by the boiler.
3,64 Modern Trends in Generating Steam
Some of the special features used in generating steam using
high pressure boilers are as follows
(i) Use of forced circulation of water inside the boiler.
ii) Use of small tubes in large number in order to increase
the surface area of heat receiving surface.
(iii) Treating the feed water thoroughi .N before use.
(it') Use of multiple tubes circuits.
(u) Use of pressurised combustion.
(ti) Use of superheaters.
The process ofsteam generation can be divided into three stages
namely
(i) heating of water upto boiling point
(ii) evaporation of boilitg water and its conversion into dry
saturated steam,
(iii) transformation of dr y saturated steam into superheated
steam.
These stages are shown on temperature (T) and heat input
diagram (see Fig. 3.88 (a)). At point. I the ice is heated. As point 2,
ire starts melting. At point 3 entire ice has incited. Further heatiiit.
Temp.
Heat input—..
Fig. 3.88 (a)
1. Standard.
2. Extra heavy or extra strong.
3. Double extra heavy or double extra strong.
Pipes up to-12 inch (300 mm) diameter are designated by their
nominal inside diameter and pipes above 300 mm diameter are
specified by their outside diameter.
Various codes and standards specify minimum pipe diamen-
sions and materials to meet certain requirements. The codes should
be consulted for allowable stress values. They depend on tempera-
ture and vary for different types of steel. Pipe diameter affects the
fluid speed for a given mass flow rate. High temperature steam in
piping has the following effects:
(i) It decreases allowable stress.
(ii) It accelerates oxidation and corrosion.
(iii) It produces expansion.
. (iv) It makes the pipe material creep.
3.69 Insulation
The pipes carrying the fluids at high temperature should be
properly insulated to avoid heat loss to the sun ings. The
insulating material should have low co-efficient of t.iermal conduc-
tivity. It should not damage the pipe material and s;:rnild he able to
resist the temperature to which it is subjected. It s .i be easily
moulded and applied and have the requisite mechanical strength.
High temperature line can be effectively insulated by 85%
magnesia block in varying thickness depending upon the tempera-
ture. The various materials in common use 85% magnesia, asbestos
fibre, cork, hair felt, mineral wool, glass wool, expanded, mica etc.
85% magnesia contains 85% carbonate of magnesium and 15%
binder and is used for temperature upto 325C. Asbestos blankets
can be used upto 500'C. Mineral wool can be used up to tempera-
tures of 875°C. Mineral wool is made by blowing steam through
fused clay lime stone of furnace slag to fibrise it. Expanded mica,
hair felt and cork can be used up to 125C. Glass wool can be used
upto temperatures of 350C. It is made by blowing steam through
streams of molten glass.
3.70 Material for Pipes
The various materials used for the pipes are as follows:
(i) Cast Iron. Cast iron pipes are used underground for water
and drainage systems and in other places where problem of cor-
rosion is excessive. Cast iron pipes are used for water services upto
a pressure of 15 kg/cm2.
(ii) Wrought Iron. Pipes made up of wrought iron are used for
condensate, feed water and blow off lines. Such pipes are used . for
270 POWER PLANT
low and medium pressure range and should not be used when
pressure is more than 250 p.s.i.
(iii) Wrought Steel. Most of the pipes used in power station are
made up of wrought steel. Wrought steel pipes are cheaper.
(iv) Alloys Steel. For high temperature flows pipes are made
up of alloy steel.
Chromium steel pipes are used for temperature higher than
525CC. For temperatures between 400-525C carbon molybdenum
steel may be used.
(v) Copper and Brass. Pipes made up of copper and brass are
costly and are mostly used for oil lines. Brass pipes are used upto
pressure 20 kg/cm2.
3.71 Expansion Bends
In order to allow for the expansion in pipes due to temperature
changes, expansion bends are used in pipe lines. The various types
of expansion bends used are shown in Fig. 3.89.
I •'.
EXPANSION U-BEND
DeL/SuE o'F5E7 EXPANSION LOOP
BEND
Fig. 3.89
direction and having an outlet for a branch pipe. Plugs and caps are
used to close the ends of fittings and pipes. Reducers are used tojoin
pipes of different sizes.
Fittings made up of cast iron, malleable iron, steel, steel alloys
and brass are in common use. The materials used for fittings depend
on service as regards pressure and temperature.
2 3 4 5
ket End
End
Fig. 3.93
Fig. 3.94
3.74 Valves
Various types of valves used in the pipe line are gate valve, globe
valve, angle valve automatic stop valve, reducing valve, check valve
and back pressure valve. Out of these first four are called stop
valves. They are used to stop the flow of fluids. The function of
reducing valve is to change pressure in a steam lute. Check valve
permits flow in one direction only. Back pressure valve is used in
STEAM POWER PLANT 273
Dnum
Feed
Pe lay
SU Z,/
—44 Fig. 3.94 (a).
The pilot valve (C) can be automatically reset and this makes it
possible to hold boiler drum level constant at all rates ofsteamn flow.
Pilot valve's manual adjustment allows lowering the water level at
low load and vice versa.
3.78 Industrial Steam Turbines
These turbines in addition to power generation supply some
steam for manufacturing processes that (steam) would otherwise be
wasted. Some such turbines are as follows:
1. Pass Out or Extraction Turbines. In these turbines (Fig.
3.95) the high pressure steam from the boiler enters the High
276 POWER PLANT
H I - -
$ TO
To PR0CES
FEED
WATER TO CONLNSER
Fig. 3.95
Fig. 3.96
main steam enter the turbine where steam expands. Fig. 3.98 shows
such turbine arrangement.
(XI?AUST
STEAM
- l 1
STEAM
ENGINE
70 CONDENSER rOCONdWSER
Fig. 3.97 Fig. 3.98
Fig. 3.98 (a) shows the use of industrial steam turbines to apply
process steam and generate by product power. C1 and C2 are the
condensers and P1 and P2 are the condenser pumps.
Condensing
Non-condensing sin extraction
turbine turbine Condensing double
Steam extroctpon turbine
High
Boiler pressure
-
drive Intermediate
pressure
Process
______ steom
uses
L
Heater pressure
it r
J
- Water
Feed pumD
= 1 - 0.098 = 0.902
W3 = Weight of air supplied per kg of coal fired
W3 = IV I - W2 = 13.14 - 0.902 = 12.238 kg
= Weight of water evaporated per kg of fuel fired
300,000
k
30,000 - 10 g.
(ii) To Calculate Heat Absorbed:
H1 = Heat absorbed by air preheater per kg of
coal fired
= Weight of air x Temperature rise x Specific heat
= w9 x (90 - 45) x 0.24
= 12.238 x 45 x 0.24 = 132 kg cal.
H2 = Heat absorbed by boiler
= Weight of water evaporated per kg of coal
x (Total heat in 1 kg of steam
- Heat in feed water - Heat in air)
= 10 [666 - (120 - 0) - 1321
= 4140 kg cal.
H3 = Heat absorbed by economiser
= Weight of water evaporated
x Temperature rise
= 10 1120 - 501 = 700 kg cal.
H4 = Heat absorbed by superheater
= Weight of water evaporated x [Super heat
temperature - saturated temperature]
x Specific heat
= 10 [300 - 1901 x 0.5
= 10x 110 x 0.5 = 550 kcal.
283
STEAM POWER PLANT
= C X C.V.
(
C() CO
CO
where C is the weight of carbon per kg of fuel, and CO and CO2
represent the per cent of volume of carbon monoxide and carbon
dioxide in flue gases respectively and C.V. is the calorific value of
coal
0.4 ] = 130 kg cal
= 0.64 x 6800[
7194q0
I J_& 4 17 Mv. MRS
Coat
S/T( BA.QD
ROO.,'
*RQANGCM T
Fig. 3.99
BOIL
BUNKER
FURNACE
L) A RA TOP
/ ECONOMISER
CONTROL ROOM
WE
PiI V
/'/RT
PRECIPITATOR
Fig. 3.100
Turbine
Boiler
'ondenser
FEED PUMP
Fig. 3.101
(iv) Thermal efficiency of steam power plant can be improved
by carrying out regenerative heating of the feed water.
Such heating of the water is carried out by using the heat
of steam partl y tapped from the turbine. In this method
(Fig. 3.102) the steam from boiler flows intt am tur-
bine. After partial expansion e of sonic
the ste'nis tapped
from the first stage of the turbine and dire, d to feed
water heater and then to feed tank. The remaini. .g steam
enters the second stage of the turbine where it continues
to expand. At the outlet from the second stage some of the
steam is directed into water heater and then to feed tank.
The other part of steam goes to the third stage of the
turbine and expands there to the final pressure and enters
the condenser. The condensate is delivered by pump to
feed tank.
So E 1 e
Condenser
Fig. 3.102
POWER PLANT
290
(ti) Feed pipe. It means any pipe under pressure through which
'ed water passes directly to the boiler and that this pipe is not
.ntegral part of the boiler.
(v) Steam pipe. It is any pipe through which steam passes from
the boiler to the prime mover and the steam pressure exceed
,
3.5 kg/cm.
2. BoilerRcgistratiofl. The boiler cannot be fixed unless it has
heen registered. The owner of the boiler has to apply for the registra-
ii, a of boiler to the chief inspector of the boiler. The inspector will
then exanune the boiler and submit the report to the chief inspector.
If the boiler is approved for registration acertificate is issued to time
owner for time use of boiler for a period of 12 months at a given
maximum pressure. The boiler registration number is mentioned in
the certificate.
3. Restriction on Use of Boiler. Restriction on the use of boiler
areas follows
(i) No owimerof a boiler shall use unless it has been registered.
(iio lfthe boiler hasbcen transferred from one state to another.
state it should not be used until the transfer has been
reported in the prescribed manner.
(ju) The boiler should not be used at a pressure than the
maximum pressure recorded in the boiler certificate.
Time boiler should be in the charge of a person holding
competenc y certificate.
-1 Renewal of Certificate. A certificate authorising the use of
boiler shall he renewed under the following condition,,;
()It expir y of the period for which it was granted.
(it) When an y accident occurs to tin- boilers.
m jj \Vhieim the boiler has been moved to another state.
STEAM POWER PLANT 291
Type of Furwce K)
Horizontal cyclone furnace -0.15
Furnace with vertical
primary chambers . ).7 --0.4
Two chamber furnaces -
Open furnaces with hydraulic
ash disposal 0.7-0.85
Chamber furnaces with
dry ash disposal 0.94
U) Devices used for ejection of flue gases into the atmosphere.
(vi) Efficiency of dust collecting and gas cleaning plants.
The basic characteristic for calculation of environmental effects
of effluents from power generating power plar tue emission of
a particular pollutant per unit time. The toxic substances present
in the flue gases may have harmful effects on vegetation, animals,
people, buildings and structures. For example vegetables are most
sensitive to the content ofSO2 gas in the atmosphere. The toxic effect
of SO 2 gas is associated with deterioration of the surfaces of leaves.
People living in NO2 contaminated areas suffer from reduced
respiratory function, have a higher incidence of respirator y diseases
and exhibit certain changes in the peripheric blood.
The environmental control of the atmosphere at thermal power
plants is mainly aimed at minimising the discharge of toxic substan-
ces into the atmosphere. This will preserve the purity ofatmop}iere
and water basins.
This can be achieved as follows
(i) By decreasing the discharge of solid ash particles Ash
contents of various fuels is different. Modern ash cIIee-
296 POWER PLANT
Economiser efficiency
113 14x 104
(b) 100= X 10
329x103
= 42.5%. Axis.
(c) H = Total heat utilised
= 112+113 = 1164 x iO + 14 x io
= 1304 x iO' kcal/hr
= Over all efficiency
= x 100
= 1304 x 103
X 100 = 82.3%. Ans.
1584 x
This shows that by installing economiser the efficiency of the
boiler plant is increased.
Example 3.14. Determine the quantity of air required per kg of
coal burnt in a steam power plant furnace fitted with a 62 ni high
stack. The draft jiroduced is 38 mm of water and temperature of flue
gases is 419'C. Boiler house temperature is 29CC.
Solution. h = Draught = 38 mm of water
W = Weight of air required per kg of coal
burnt
Ti = Absolute temperature of air outside the
chimneys
= 29 + 273 = 302K
T = Average absolute teniperature of
chimney (stack) gases.
=410+273=683K
62 m.
H = Height of chimney =
1 (w+i ii
h=353H[_
i (w^1
jj
38=353x62 _ j xj
1302 w
16 kg.
STEAM POWER PLANT 301
IM
Boiler Turbine
-3
Condenoer
Th condenrat
PumP
Fig. 3.103
Power of/)unh/) = 100 11. P.
Rate O/ste(iFfl flow = 8 x 10' kg/hr.
The entlzalpr and velocity fr the fluids at different points ofeycle
are tfl(liCute(l in table 3.2 (A)
Table 3.2 (A)
- I.e,tto,i r:fltha!J). (/.(/kg.%4.joeIi.y (_f7!Ie) I
Steam leaving theh.iI,r(l--IP YQ - 80_
,Ste.tiii t. flterIlIg tho , tilrhii'2 2) - . 776 81)
STEAM POWER PLANT 303
304
a POWER PLANT
(c) Q = Heat loss from turbine to atmosphere
40,000
8 x 10' 0.5 kcal/kg of steam flow.
Applying general energy equation
H vi
Vi
As all the items work at the same level
Z2 =
= 80 rn/sec
1)3 =160 rn/sec
H2 = 776 kcal/kg
H3 = 550 kcallkg
W = work done
= If + qL
= 200.7 + q x 466.7 kcal.
Now t = Temperature of super-heated steam
= 330 C
054
II = Heat of super heated steam
= 11 + Ci,, (t. - t)
= 667.4 + 0.54 (330 - 197.4) k.cal
= 739 k.cal
H1 =H' +H
= 200.7 + q x 466.7 + 739 k.cal.
Since the temperature of steam in the common main is 260'C
and saturation temperature is 197.4C it is obvious that steam is
still in super heated condition.
H2 1=Heat of 2 kg of steam in the main
= (H + C (t - t)1 x 2
= (667.4 + 0.54 (260 - 197.4) x 2
= 1402.4 k.cal.
Now H1 = H2
200.7 + q x 466.7 + 739 = 1402.4
q=0.91.
Example 3.22. Calculate the efficiency of boiler in which coal
consumption is 65 kg per hour and which generates 370 kg of steam
per hour at 0.93 dryness fraction and at a pressure of 8 bar ablso
lute. Coal used has the following composition per kg.
Carbon = 0.71
Hydrogen = 0.05
Oxygen = 0.11
Sulphur = 0.02
Ash =0.71
Feed water temperature = 24°C.
Solution.
P = Pressure of steam
= 8 bar
STEAM POWER PLANT
309
From steam tables
hf = sensible heat
= 721 kJ/kg
hfg Latent heat of steam
= 2046.5 kJ/kg
x = Dryness fraction
H = Heat of 1 kg of steam
= hf+ x. hfg
= 7211-0.93 x-2046.5
= 2624.3 kJ/kg
HL = Heat supplied to steam per kg
=H- heat contained in 1 kg of feed water
=2624.3- 1x4.18x(24_O)
= 2524kJ/kg
W = weight of steam produced per hour = 370 kg
112 = Heat of steam
= WxH 1 =370x2524
= 933880
Cv = Calorific value of coal
= 65 kg
113 = Total heat input
= c x Wi
= 29367.4 x 65
= 1908855 kJ
Yj = Boiler efficiency
= 112 x 100
H3
933880
= 1908855 x 100
= 49%.
Example 3.23. A boiler working at a pressure of 10 bar generates
2100kg of dry and saturated steam per hour. The feed water is heated
by an economiser to a temperature 91105°C. Coal consumed is 208
kg and calorific value of coal is 30200 kJ/ kg. If 12% of coal remains
unburnt determine:
(a) thermal efficiency of boiler
(b) thermal efficiency of boiler and grate combined.
Solution. x = Dryness fraction = 1
m Rate of production of steam
= 2100 kg/h
AT = Feed water temp. rise
= 105°C
P = Pressure
= 10 Bar
h = Heat of steam at 10 bar pressure
= hg
= 2776 kJ/kg
hfj = Heat contained in feed water
=1x4.18xAT
= lx 418 x 105
= 439 kJ/kg
h i = Heat used to produce 1 kg of steam in boiler.
= h - hfTI
= 2776 - 439
STEAM POWER PLANT
311
= 2337 kJ/kg
Unburnt coal = 10%
W = Coal consumed = 208 kg
mi = Mass of coal actually burnt
= 208 x 90
= 187.2 kg
rn2 = mass of steam produced per kg of coal actually burnt.
mi
- 2100
- 187.2
= 11.2 kg
H1 = Total heat of steam
= 1712 X h1
=11.2x2337
= 26174.4 kJ
C = Calorific value of coal
= 30200
TIb = Boiler efficiency
H1
= - x 100
26174A
x 100
=
= 86.6%
ilg = Efficiency of boiler and grate
171
power plant is to convert the availability (to do work) of the fuel into
work (in the form of electrical energy ) in the most efficient manner,
taking into consideration cost, space, safety, and environmental
concerns.
A schematic diagram of a steam power plant is shown in Fig.
3.104. High-pressure superheated steam leaves the boiler, which is
also referred to as a steam generator, and enters the turbine. The
steam expands in the turbine and, in doing so, does work, which
enables the turbine to drive the electric generator. The low-pressure
steam leaves the turbine and enters the condenser, where heat is
transferred from the steam (causing it to condense) to the cooling
water.
Stock
QSS OUt Air in
4irprehectgr
High pressure
super heated Turbine
steam
-- Economrser
I-jot
[w t e r
Hot
aIr- Low.press4ire
steam
.
- Super-heater
Fuel—
-JA
- - Condenser
Cooling
water
Out
__.1_
Steam boiler
Water
Pumps Cooling
water
Cooling water
from river or
take or cooling
tower
Fig. 3.104
PROBLEMS
3.1. (a) What are the different types of coal conveyors? Describe the
construction and operation of belt-conveyor and screw
conveyor.
(b) Describe a grab bucket elevator.
STEAM POWER PLANT 313
3.2. (a) What is meant by 'over feed' and 'under feed' principles of
firing coal?
(b) What are the different methods of firing coal ? Discuss the
advantages of mechanical methods of firing coal.
(c) Make neat sketch and explain the working of:
(i) Chain gratestoker. (ii) Spreader stoker.
(iii) Multi retort stoker.
((I) What is Fluidised Bed Combustion system. Sketch and
describe a Fluidised Bed Combustion (FBC) system. State
the advantages of FBC system.
3.3. Describe the various types of grates used with hand fired fur-
naces.
3.4. Name the various methods of ash handling. Describe the
pneumatic system of ash handling. Why it is essential to quench
the ash before handling?
3.5. (a) Describe the various methods used to fire pulverised coal.
(b) Make a neat sketch of ball and Race mill and explain its
working.
(c) State the advantages of pulverised fuel firing.
3.6. Name the different types of coal-pulverising mills. Describe
Ball-Mill.
3.7. Describe the various types of burners used to burn pulverised
coal.
3.8. Name various draught systems. Describe the operation of a
balanced draught system.
3.. What is the cause of smoke ? State the factors .cessarv for its
prevention.
3.10. Name the different types ofchinineys used. Star ic advantages
of steel chimney. Derive an expression for the height ofchirnney.
3.11.(a) What are the harmful effects caused by using impure water
in boilers? Describe the various methods of purif ying feed water.
(b) What is meant by make up water of boiler and how is this
water fed into a boiler?
3.12. Describe the various methods used to control the degree of
superheat. Name the advantages gained by using super-heat
Steam.
3.13. What is condenser ? Name the different types of condenser.
Describe the operation of(i) Surface condenser (ii) Jet condenser.
3.14. What are the different types of cooling towers used in . a steam
power plant. Discuss their specific advantages.
3.15. What is asteam trap? Where it is located? Describe Ball Float
steam trap.
3.16. What are the requirement ofa well designed pipe line in a steam
power plant. Name and describe the various expansion bends
used in piping steam.
3.17. What are the advantages of using large capacity boilers ?
Describe the operation of:
(i) Velox Boiler (u) Benson Boiler (iii) Loeffler Boiler.
—22
314 POWER PLANT
4.0 Introduction
Diesel engine power plant is suitable for small and medium
outputs. It is used as central power station for smaller power
supplies and as a standby plants to hydro-electric power plants and
steam power plants.
The diesel power plants are commonly used where fuel prices or
reliability of supply favour oil over coal, where water supply is
limited, where loads are relatively small, and where electric line
service is unavailable or is available at too high rates. Diesel power
plants in common use have capacities up to about 5 MW.
Fig. 4.1 (a) shows various parts of an I.C. engine. The cylinder
is the main body of the engine where in direct combustion of fuel
takes place. The cylinder is stationary and the piston reciprocates
inside it. The connecting rod transmits the force given by the piston
to the crank, causing it to turn and'thus convert the reciprocating
notion of the piston into rotary motion of the crankshaft.
The valves may be provided
(i) at the top
or (ii) on the side of the engine cylinder.
Fig. 4.1 (b) shows a typical overhead valve assembly.
The cam lifts the push rod through cam follower and the push
rod actuates the rocker arm lever at one end. The other end of the
rocker arm then gets depressed and that opens the valve. The valve
returns to its seating by the spring after the cam has rotated. The
valve stem moves in a valve guide acts as a bearing.
On a four stroke engine, the inlet and exhaust valves operate
once percycle, i.e., in two revolutions of the crankshaft. Consequent-
ly , the cam shaft is driven by the crankshaft at exactly half its
rotational speed.
DIESEL ENGINE POWER PLANT 317
.tn9
Inlet Exhaust
Inlet v bauM
,alve
I
ribustuon
pace
Stan
I flys
is
P
in der
QQOfl
)ifl
oflflecting
rod
:rank pin
rank
Crank co
rank Shaft
h roq
uide
—Corn
VERTICAL
tN-LI WE
V- TYPE
1IiI10 11 ojIl
,HORIZONTAL TYPE
(C)
(a) (b)
Fig. 4.1
EXPANSIO.V
LU çiJO
Cx t'kl 61,
bc. F111
;) .o
C
CY
Oo
COMPRESS ON
EXHAUST
VOLUME
Fig. 4.3 Fig. 4.4
DIESEL ENGINE POWER PLANT 323
FUEL VALVE
-CYLINDER
1
EXHAUST PORT
TR4A'S PER
PORT
INLET PORT
U ELECTOR
a
(b) (c)
Fig. 4.5
" TDC
UJI
e
b 91
US 0
VOLUME
8DC
Fig. 4.6 shows the indicator diagram for two stroke diesel
engine. In this diagram bc represents the compression of air, cd
represents constant pressure combustion line, de represents expan-
sion and exhaust and scavenging are indicate1 by eab.
Fig. 4.7 shows valve timing diagram for two-stroke diesel en-
gine. TDC and BDC represents top dead centre and bottom dead
centre respectively. 1PO means inlet port opens and IPC means inlet
port closes, EPO represent exhaust port opens and EPS represents
exhaust port closes. FAS means fuel admission starts and FAE
means foci admission ends.
4.4 Application of Internal Combustion Engines
Internal combustion engines are used in stationary plants,
marine power plants, in various vehicles and aircrafts, their use in
mobile units being predominant, because of their low size and
weight and low fuel consumption.
4.5 I.C. Engine Terminology
The important terms used in an I.C. engine are shown in Fig.
4.8. The inside diameter of engine cylinder is known as bore Top
dead centre (TDC)
Valves in vertical engine
cover and inner dead
Cleoron.. - ____________,- Cylinder centre (IDC) in
volume-.....
Extreme position
horizontal engine
of position at top
is the extreme
position of the pis-
Cylinder ton on head side of
strrlq
the engine.
Extreme position Whereas bottom
of piston at bottom dead centre (BDC)
Piston rod i n vertical engine
and outer dead
Fig. 4.8 centre (ODC) in
horizontal engines
indicate the extreme position at the bottom of the cylinder. Stroke
is the distance between the two extreme positions of the piston.
Stroke is the distance between the two extreme positions of piston.
Let D = Bore
L = Stroke
V1 = Swept volume = (it/4) D2 x L.
Clearance volume is defincd as the space above the piston at top
dead centre.
V= Volume of cylinder = Vi + V
where Vc is the clearance volume.
DIESEL ENGINE POWER PLANT
325
4.6 Engine Performance
(i) IMEP. In order to determine the power developed by the
engine, the indicator diagram of engine should be available. From
the area of indicator diagram it is possible to find an average gas
pressure which while acting on piston throughout one stroke would
account for the network done. This pressure is called indicated moan
effective pressure (I.M.E.P.).
(ii) IHP. The indicated horse power (I.H.P.) of the engine can be
calculated as follows:
I.H.P. Pm L.A.N. n
4500xk
where Pm = I.M.E.P. in kg/cm2
L Length of stroke in metres
A = Piston areas in
N = Speed in R. P.M.
n = Number of cylinders
k = 1 for two stroke engine
= 2 for four stroke engine.
(iii) Brake Horse Power (B.H.P.). Brake horse power is
defined as the net power available at the crankshaft. It is found by
measuring the output torque with a dynamometer.
B.H.P. = 2n NT
4500
where T = Torque in kgm.
N = Speed in R. P.M.
(iv) Frictional Horse Power (F.H.P.). The difference of I.H.P.
and B.H.P. is called F.H.P. It is utilised in overcoming frictional
resistance of rotating and sliding parts of the engine.
F.H.P. = IHP - BHP.
(v) Indicated Thermal Efficiency (1j) . It is defined as the
ratio of indicated work to thermal input.
- I.H.P. x 4500
wxC xJ
where W = Weight of fuel supplied in kg per minute.
Cu = Calorific value of fuel oil in kcal/kg.
J = Joules equivalent = 427.
POWER PLANT
326
I feat abscrbei b y I I! P
!(b)Heectedtocoohngwater.
4
(c)tleat carried awa y bv exhaust g ases.
d)I [eat unaccounted for (b y difference)________
Total
A typical heat balance sheet at full load for Diesel cycle (com-
pression ignition) is as follows
3 D3
150= 800
D2 = 150 x 180 =
12,727
3xit
D = 22.7 cm. Ans.
and L=-xD=-x22.7
= = 75 kW
- . = Output
Efhc ency
Iiput
Output = Efficiency x Input
= 0.4 x 13,954 = 5581 kWh.
4.8 Diesel Engine Power Plant Auxiliaries
Auxiliary equipment consists of the following systems
1. Fuel supply s ystem. It consists of fuel tank for the storage of
fuel, fuel filters and pumps to transfer and inject the fuel. The fuel
oil may be supplied at the plant site by trucks, rail, road, tank, cars
etc.
2. Air intake and exhaust system. It consists of pipes for the
supply of air and exhaust of the gases. Filters are provided to remove
dust etc. from the incoming air. In the exhaust system silencer is
provided to reduce the noise.
Filters may be of dry type (made up of cloth, felt, glass, wool etc.)
or oil bath type. In oil bath type of filters the air is swept over or
through a bath of oil in order that the particles of dust get coated.
The duties of the air intake systems are as follows
(i) To clean the air intake supply.
(ii) To silence the intake air.
(i1) To supply air for super charging.
Th .ntake system must cause a minimum pressure loss to avoid
reducing engine capacit y Sod raising the specific fuel consumption.
Filters must be cleaned periodically to prevent Ieure loss from
332 POWER PLANT
AR n i t SURGE TANI(
41A1111
SiIEN111116W
0^ (1 JACKET
Lrç'M
TM
LT'
JA
11 1 1.5 TARTINO
OVER
FLOVj t I.lR TANK
I—i
AIR LO
I
COMPRESSOR LU8PICAThI
L TANK I
FILTER
COOLING
TOWER
FUEL TANK
4. .1. 4.
Useful Cooling Radiation Friction
work (30%) . exhaust Loss
(28%) (32%) (10%)
Fig. 4.9(b)
The following points should be noted to achic.e good cooling of
diesel engine.
(i) Adequate quantity of water sF. Ad cortinuously flow
throughout the operation of the c igine.
(ii) The cooling water should not be :rosive to metals.
(iii) The cooling water used for cylinder jackets should be free
from scale forming impurities.
(iv) The temperature rise of cooling water should not be more
than 1 1C and the temperature of water leaving the engine
should be limited to 60CC.
4.9.1 Cooling methods
There are two methods of cooling the I.C. Engines.
(a) Air cooling
(b) Water cooling.
Air Cooling. It is a direct method of cooling. In air cooled
engines fins are cast on the cylinder head and cylinder barrel to
increase its exposed surface of contact with air. Air passes over fins
and carries away heat with it. Air for cooling the tins may be
obtained from blower or fan driven b y the engine. Air moment
relative to engine may be used to cool the engine as in case of motor
cycle engine. About 13 to 15' of heat is lost b y this method. Fig. 4.10
shows air cooling system. Simplicit y and lightness are the ad-
vantages of air cooling. But this s y stem is not as c[i'ctive as water
334 POWER PLANT
cooling. The rate olcoohng depends upon the velocity, quantity and
temperature of cooling air and size of surface being cooled.
Fig. 4.10 (a) shows position of valves, Fins and head in air
cooling system. This system is used in motor cycles, scooters and
aeroplans.
ton
nicer
Cylinder
Pi ston
Fins
WQ'i( L.{___
in -
\\ I- J jk
Fig. 4.11
Fq, 4.10
DIESEL ENGINE POWER PLANT 335
.i 'FINS
..h /ET
W4EfKrlsm - --
;
PUMP
DRAIN CCCI'
Fig 4.12
Fig 4 13
(NI(/E
i 7i. - P,.
PU....p
Fig 4 14
11 (' Tin water it-oil fir coolin g i ir j iis Almild Im . tree trout
i m put it its Water Ii it miut h. id, pit mm it it niti ' riir it I alit
C0011119 tower
Soft .. ,j
-; Lcc
Wtr L iflicotr
--- Li ( Efl ( I i Pe
Z
rCW .- / LJ
J
lump
co!i h2
L' Raw %vcter
:m<e u rc waTer bud in
Fig. 4 14 ta
DIESEL ENGINE POWER PLANT
337
4.10 Lubrication
Frictional forces causes wear and tear of rubbing parts of the
engine and thereby the life of the engine is reduced. This requires
that some substance should be introduced between the rubbing
surfaces in order to decrease the frictional force between them. Such
s ubstance is called lubricant The lubricant forms a thin film be-
tween the rubbing surfaces and prevents metal to metal contact.
The various parts ofan I.C. engine requiring lubrication are cylinder
walls and pistons, higend bearing and crank pins small end bearing
and gudgeon pins, main bearing cams and bearing valve tappet and
guides and timing gears etc. The functions of a lubricant are as
follows :
1. It reduces wear and tear of various moving parts by
minimising the force of friction and ensures smooth run-
lung of parts.
2. It helps the piston ring to seal the gases in the cylinder.
3. It removes the heat generated due to friction and keeps
the parts cool.
The various lubricants used in engines are of three types
(1) Liquid Lubricants.
(ii) Solid Lubricants
(It:) Semi-solid Lubricants
Liquid oils lubricants are most commonly used. Liquid
lubricants are of two t ypes: (o) Mineral Oils (h) Fatty oils. Graphite,
white lead and mica are the solid lubricants Semi solid lubricants
or greases as they are often called are made from mineral oils and
fatt v-oils.
A good lubricant should possess tile following properties
(t) It should not change its state with change in temperature.
(ii) It should maintain a Continuous films between the rub-
bing surfaces.
(iii) It should have high specific heat so that it can remove
maximum amount of heat.
(iv) It should be free from corrosive acids.
(v) The lubricant should be purified befoi cit enter the engine.
It should be free from dust, moisture, metallic chips, etc.
The lubricating oil consumed is nearl y 1%of Hlconsump-
tion.
The lubricating oil gets heated because of friction of moving
:;arts and should be cooled before recirculation The cooling water
used in (lie engine may be used for cooling the lubricant. Nearly
2 of heat of fuel is dissipated as heat which is removed by the
lubricating oil.
POWER PLANT
338
HEATER
DIESEL
OIL COOLER J—iJ ICONTRIFU6At
I 11 II R
FLURIC11TN&
OIL TA5
Fig. 415
TO ENGINE
Fig. 4.16
The fuel oil used should be free from impurities. Efforts should
be made to prevent contaminator of. [, feel. An important Step is
to reduce the number of times the fuel is handled Greater amount
of impurities settle down in the storage tank and remaining im-
purities are removed by passing ti oil through filters. Storage tank
may be located above the ground or underground. But underground
storage tanks are preferred. Fig. 4.17 shows an underground storage
tank. It is provided with coils, heated by steam or hot water to reduce
the viscosity and to lower the pumping cost. Main hole is provided
for internal access and repair. Vent pipe is provided to allow the
tank to breathe as it is filled or emptied. Level indicator measures
the quantity of oil in the tank, and an overflow line is provided to
control the quantity of oil.
OIL LEVEL
INOICA TOP
VENT PIPE
CONCRETE
ENGINE ROOM FOOP
Putt FROM OVER Ft OW
UNLOMLING
Pu'lp STEAM FOR
110(. HEATING
S TOPMGE
TANK
Fig. 4.17
- 342 POWER PLANT
INJECT/ON
NOZZLES
HIGH PRE.SUPE
FUEL L'NE
CONTROL
RACK
PUMP
CAMSHAFT
PUMP WITH AN INDIVIDUAL
CflINDER FOR EACH NOZZLE
Fig. 4.19
DIESEL ENGINE POWER PLANT 343
(ii) Pump Injection. In this system individual pump is
provided for each nozzle. The pump measures the fuel charge and
controls the iiljection timing (Fig. 4.19).
(iii) Distributor Injection. In this s ystem (Fig. 420) a pump
measures and pressurises the fuel and supplies to it the various
nozzles through a distributor block.
METMIN
OISTRIBUT
AN PR. 15SU,?
&OCK
PUMP
-.
PPIM.4R y ptp
Fig. 420
Silencer
Exhaust
manifold 4ir duct
Filter
Louvres
Diese' engine-
Fig. 4.22
Switch
board
[
Unitno?
1 0
Office
HU
I
L Unit no 1
1 0Air
compressor
Oil storage
Tanks
Front Entrance
Fig, 4.23
—24
_346 POWER PLANT
'S
/
B.H.P. B.H.P
(a.) (b) (C)
Fig. 4.24
348 POWER PLANT
Fig. 4.26 Fig. 4.27
rotating vane element as shown in Fig. 4.27. The air is taken from
intake and discharged at outlet end. It screw type supercharger the
air is trapped between inter meshing helical shaped gears and
forced out axially. In piston and cylinder type super-charger the
piston compresses the air in a cylinder whereas a centrifugal type
super-charger has an impeler running in a housing at a high speed,
centrifugal supercharger is commonly by used in reciprocating
power plants for aircraft.
4.31 Advantages of Supercharging
Due to a number of advantages of supercharging the modern
diesel engines used in diesel plants are generally supercharged. The
various advantages of supercharging are as follows
(i) For given output engine size is reduced.
(ii) Engine output can he increased by about 30 to 5017(.
(iii) The specific fuel consumption of a super charged engine
is less than natural aspirated engine. This is due to the
fact that combustion is supercharged engine is better duo
to better mixing of fuel and air.
DIESEL ENGINE POWER PLANT 351
in numbers.
(lx) Maintenance is easier.
Example 4.6. A diesel engine has a brake thermal el/u ie,u-v of
3O. If the calorific ca/ac of fuel used in 10000 kcal 1kg, ca/cu/cjfe
the brake specific fuel consumption..
ion-.
Solution. = Brake thermal efficiency 0.3
I.H.P. hr = 632.5 kcal
= F P hr equivalent
Tm
x C.N.
it
240 - 0.83.
(e) Indicated specific fuel consumption =
where W = Amount of fuel used per hour.
Indicated specific fuel consumption
PROBLEMS
4.1. How will you classif y I.C. engines? Describe the working of two
stroking of two stroke and four stroke cycle diesel engines.
Discuss their relative merits and demerits.
4.2. What are the different methods of cooling diesel engine? Com-
pare air cooling and water cooling.
4.3. Describe the various methods used for starting diesel engine.
Describe in correct sequence the steps for starting and stopped
procedure.
4.4. Describe the auxiliary-equipment of diesel engine power plant.
4.5. Give the layout of a diesel engine plant.
4.6. What are the various methods of fuel injection? What precau-
tions should be observed to ensure that fuel injection is satisfac-
tory?
4.7. What are the various factors to be considered while selecting the
site for diesel engine power plant? Discuss the advantages and
disadvantages of the diesel power plant.
4.8. Compare I.C. engine with steam engine and state the advantage
of I.C. engine over steam engine.
4.9. What is the importance of heat balance sheet ? What are the
various items considered while drawing the heat balance sheet
ofl,C. engine? Give a typical heat balance at full load for an I.C.
engine.
4.10. Describe the procedure of testing diesel power plant perfor-
mance. How is plant maintenance carried out?
4.11. Write short notes on-the following:
(a) Lubrication of diesel power plant.
(b) Indicated Thermal Efficiency, I.H.P. and B.H.P.
(c) Applications diesel power plant.
(d) Warming up of diesel engine.
4.12. Describe a typical filter and silencer installation for a diesel
engine.
4.13. Define specific fuel consumption. Explain indicated specific fuel
consumption and brake specific fuel consumption.
4.14. A four stroke diesel engine gave the following test results at a
speed of 450 R.l'.M.
Mean effective pressure = 8.50 kg/cm2
Cylinder bore = 22 cm.
Stroke = 26 cm.
Specific fuel consumption = 0.32 kg(BHP/hr
Calorific value of fuel = 11800 kcal per kg.
DIESEL ENGINE POWER PLANT 355
Mechanical Efficiency = 38%
Determine the following:
(a) B.H.P.
(b) l.H.P.
(c) Indicated thermal efficiency.
(d) Brake thermal efficiency.
4.15. Compare a diesel and petrol engine.
4.16. Write short notes on the following:
(a) I.C. engine fuels.
(b) Cost of diesel power plant.
4.17. (a) What is supercharging ? What methods are used for super-
charging diesel engines?
(b) Discuss the advantages of supercharging.
4.18. (a) Under what conditions diesel generating plants are
preferred?
(b) On what factors is the size of the generating plant selected?
(c) Draw a net diagram of a cooling system used for diesel power
plants showing all the essential components. What are the
advantages ofdouble circuit over single circuit system? What
precautions should be taken to ensure that cooling is satisfac-
tory?
4.19. Name the methods used to purify lubricating oil.
• • : . : •
1J i'J., f
T O . t•jA
.)R' 11k. / 4.• IØ ;-i.
01 '
• .•...-. •
Jl • : •• k
• ,• . .. .-. ..... ,.
5
Nuclear Power Plant
,.
POWER PLANT
358
India went nuclear in 1956 when its first research reactor went
critical at Trombay. Six units are now under various phases of
operation construction or design two each at Kota, Kalpakkam and
Narora. They are all of the CANDU (Canadian-Deuterium-
Uranium) type, most suited to Indian conditions. India has limited
deposits of uranium and would not be dependent on foreign enrich-
ment facilities or a foreign supply to enriched fuel, (used in the
Tarapur power plant). CANDU reactors, which use fuel available
within the country, do not require large capital and operating
outlays for fuel enrichment. The nuclear power generation will be
about 2270 MW by 1991-92 in our country.
5.2 Chain Reaction
Uranium exist as isotopes of U 238, U234 and U235 . Out of these
isotopes U235 is most unstable. When a neutron is captured by a
nucleus of an atom of U 5 , it splits up roughly into two equal
fragments and about 2.5 neutrons are released and a large amount
of energy (nearly 200 million electron volts MeV) is produced. This
is called fission process. The neutrons so produced are very fast
moving neutrons and can be made t .o'fission other nuclei of U 235 thus
enabling a chain reaction to take place. When a large number of
fissions occurs, enormous amount of heat is produced.
The neutrons released have a very high velocity of the o
1.5 x 107 metres per second. The energy liberated in the
reaction is according to Einstein law
E = mc2
where E = Energy produced
rn = mass in grams
c = speed of light ih cm/sec equivalent to 3 x 1010 cm,/sec-
Out of 2.5 neutrons released in fission of each nuclei of U 235 , one
neutron is used to sustain the chain reaction, about 0.9 neutron is
captured by U238 which gets converted into fissionable material,
Pu239 and about 0.6 neutrons is partly absorbed by control rod
material, coolant moderator and partly escape from the reactor.
Production of the fissionable material Pit 239 during chain reaction
compensates the burn up of primary fuel U 235 U238 + neutron =
Pu239 . If thorium is used in the reactor core it produces fissionable
material U233.
Th 232 + Neutron .- U33
Pu239 and U233 so produced are fissionable material and can be used
as nuclear fuel and are known as secondary fuel. U 235 is called
primary fuel.
FISSION
FRAGMENT
ESCAPE
*23FA
NEUTRON
'YE
__
NEU -I.1z FAST
______NEUTRON
MOA
Fig. 5.1
5.3 Fertile Material
It is defined as the material which absorbs neutrons and under-
goes spontaneous changes which lead to the formation of fissionable
material. U 235 and Th 22 are fertile materials. They absorb neutrons
and produce fissionable materials Pu 239 and U 233 respectively.
t Ii1fiIIIJ
5.4 Unit of Radioactivity (Curie)
COOLANT
III IJIIUl•
oil
PEFLECTOP
121
MODERATO
PRE55URE
VESSEL
CONCRETE.
SN/EL DG'JG
Fig. 5.2
-COOLANT
360 POWER PLANT
Co
c 'C
-'t:m' Tznl<
y '"n zZ
FueL )d8
P
Fig 53
NUCLEAR POWER PLANT
33
—25
POWER PLANT
'l'al)Ie 5.1
.ictij . •. . J
----------------------------------------------. isrs__
1S.G
2(j -
L . t239 - - 196 - -
I Fu,i Th
(lUCtltttY K. keal/kgC (C)
- coi/,n.hr (4 4
Natural uraniumI 263 0.037 19000 1130
Uranium oxide 18 JO078 I PL_ 2750
1L_1Jr3!iiujn -carbide T---- 20-6 13600 2350J
5.5.2 Moderator
In the chain reaction the neutrons produced are fast moving
neutrons. These fast moving neutrons are far less effective in
causing the fis-ion of U 2 ' and try to escape from the reactor. To
improve the utilization of these neutrons their speed is reduced. It
is done by colliding them with the nuclei of other material which is
lighter, does not capture the neutrons but scatters them. Each such
collision causes loss of energy, and the speed of the fast moving
neutrons is reduced. Such material is called Moderator. The slow
neutrons (Thermal Neutrons) so produced are easily captured by
the nuclear fuel and the chain reaction proceeds smoothly. Graphite,
heavy water and ber y llium arc generally used as moderator.
Reactors using enriched uranium do not require mod''rator. But
enriched uranium is costl y due to processing needed.
A moderator should process the following properties
W It should have high thermal conductivity.
(it) It should be available in large quantities in pure form.
(iii) It should have high melting point in case of solid
moderators and low melting point in case of liquid
moderators. Solid moderators should also possess good
strength and machinability.
(iv) It should provide good resistance to corrosion.
(v) It should be stable under heat and radiation.
nil It should be able to slow down neutrons.
Table 5.2
This shows that heavy water, carbon and, beryllium are the best
moderators.
Table 5.3 indicates density of various moderators.
Table 5.3
P
Moderator Density (gmicm3)
1120 1
1)20 1.1
C 1.65
Be - 1.85
Table 5.4 shows some of the physical constants of heavy water
(D20) and ordinary water (1120).
Table 5.4
constant
0.9982 nVc
Freezing temperature 276.82 273
Boiling temperature I374.5 373}(
Dissociatior Cünstant 0.3x10 -1x10'
Dielectric Constant at293}( 80.5 82
Snecific heat at 293K 1.018 1
takes. up the heat and gets converted into steam in the reactor
which is directly sent to the turbine.
Coolant used should be stable under thermal condition. It
should have a low melting point and high boiling point. It should not
corrode the material with which it conies in contact. The coolant
should have high beat transfercoefficient. The radioactivity induced
in coolant by the neutrons bombardment should be nil. The various
fluids used as coolant,are water (light water or heavy water), gas
(Air, ('02, hydrogen, helium) and liquid metals such as sodium or
mixture of sodium and potassium and inorganic and organic fluids.
Power required to pump the coolant should be minimum. A
coolant of greater density and higher specific heat demands less
pumping power and water satisfies this condition to a great extent.
Water is it good coolant as it is available in large qualities can be
eailv handled, provides some lubrication also and offers no unusual
corrosion problems. But due to its low boiling point (2 12F at
atmospheric pressure) it. is to he kept under high pressure to keep
it in the liquid state to achwve a high that transfer efficiency. Water
when used as cooluit 11101.11d be free from impurities otherwise the
impurities ma y become radioactive and handling of water will be
difficult
5.5.8 Coolant Cycles
coolant while circulating through thc reactor passages take
up heat. produ..., lu..' to chain reaction and trnnskr this heat to the
f?cd water in three w..vs as follows
(a) Direct Cycle. III s y stem [Fig, 5.1 (a )l coolant 'wluch is
water leaves the reactor in the form of steam. Boiling water reactor
ues this system.
(1..) Single Circuit S ystc,n. In this s ystem ll'ig. 5.4 (b)l the coolant
transfers the heat to the feed water in the steam generator. This
system is used in pressurised reactor.
(c) Double Cir cu it S y stem. In this s y stem [Fig. 5.4 (c)] two
coolant are used. Primary coolant after circulating through the
reactor flows through the intermediate heat exchanger (lIIX) and
passes on its heat to the secondary coolant which transfers its heat
in the feed water in the steam generator. This system is used in
sodium graphite reactor and fast breeder reactor.
5.5.9. Reactor Core
Reactor core consists of fuel rods, moderator and space through
which the coolant flows.
NUCLEAR POWER PLANT 307
PEAC7ORREAcToR
I
YGENERAIOR
FEED
EED
WATER Pump WATER
(ti) (1)
pRIMARY
CORE
STEAM I
GENERATO1 c0NOENWI
I
Lll.11ilII
II II
jt WATER
I: I L
...j COOLA!.IT FEED PUMP
PUMP
CONCRETE SHILDING
Fig. 5.5
Fig. 5.6 shows nuclear power plant using B.W.R. In this reactor
enriched uranium (enriched uranium contains more fissionable
isotope U235 then the naturally occurring percentage 0.7%) is used
as nuclear fuel and water is used as coolant. Water enters the
reactor at the bottom. It takes up the heat generated due to the
fission of fuel and gets converted into steam. Stearn leaves the
reactor at the top and flows into the turbine. Water also serves as
moderator. India's first nuclear power plant at Tarapur has two
reactors (each of 200 MW capacity) of boiling water reactor type.
CONTROL
RODS -.
GENERATOR
REACTOR
CORE -
CONDENSER
FEED PUMP
Fig. 5.6
through the reactor core and takes up the heat liberated due to
nuclear fission of the fuel. In order that water may not boil (due to
its low boiling point 212 F at atmospheric con(litions) and remain in
liquid state it is kept under a pressure of about 1200 p.si.g. by the
pressu riser. This enables water to take up more heat from the
reactor. From the pressuriser water flows to the steam generator
where it passes or its heat to the feed water which in turn gets
converted into steam.
CONTROL
RODS
PRESSURISER
TURBINE GENERATOR
S U'
EACTOR
CORE
CONDENSER
COOLANT • FEED
PUMP PUMP
Fig. 5.7
5.12 Sodium Graphite Reactor (SGR)
The reactor shown in Fig. 5.8 uses two liquid metal coolants.
Liquid sodium (Na) serves as theprimary coolant and an alloy of
sodium potassium (NaK) as the secondary coolant.
Sodium melts at 208C and boils at 1625F. This enable to
achieve high outlet coolant temperature in the reactor at moderate
pressure nearly atmospheric which can he utilized in producing
steam of high temperature, thereby increasing the efficiency of the
plant. Sttani at temperature as high as 1000 has been obtained
b y this s ystem. This shows that by using liquid sodium as coolant
more electrical power carl he generated for a given quantity of the
fuel burn up. Secondl y low pressure in the primary and secondary
coolant circuits, permit the use of less expensive pressure vessel and
pipes etc. Further sodium can transfer its heat very easil y . The only
disadvantage in this system is that sodium becomes radioactive
while passing through the core and reacts chemically with water.
So it is not used directly to transfer its heat to the feed water, but a
secondary coolant is used. Primary coolant while passing through
the tubes of intermediate heat exchanges (I. fIX.) translrs its heat
to the secondary coolant. The secondary coolant then flows through
the tubes of steam generator and passes on its heat to the feedwater.
Graphite is used as moderator in this reactor. For heat exchanger
refer Fig. 5.10 (b) Liquid metals used as heat transfer media have
NUCLEAR POWER PLANT 371
certain advantages over other common liquids used for heat transfer
purposes. The various advantages of using liquid metals as heat
t.ranfer media are that theyhave relatively low melting points and
combine high densities with low vapour pressure at high tempera-
tures as well as with large thermal conductivities.
5.13 Fast Breeder Reactor (FBR)
CONTROL
RODS
L! Ic STEAM T URBINE
I STEAM
CORE -IH I I'll I I 1HXI 6ENER^17
UOLAN7 COOLANT FEED
PUMP PUMP PUMP
Fig. 5.8
Fig. 5.9 shows a fast breeder reactor system. In this reactor the
core containing U23*5 is surrounded by a blanket (a la yer of fertile
material placed outside the core) or fertile material In this
reactor no moderator is used. The fast moving neutrons liberated
due to fission of U23 are absorbed by U 235 which gets converted into
fissionable material Pu2,39 which is capable of sustaining chain
reaction. Thus this reactor is important because it breeds fissionable
material from fertile material U 238 available in large quantities.
Like sodium graphite nuclear reactor this reactor also uses two
liquid metal coolant circuits. Liquid sodium is used as primary
coolant when circulated through the tubes of intermediate heat
exchange transfers its heat to secondary coolant sodium potassium
allo y . The secondary coolant while flowing through the tubes of
steam generator transfer its heat to fied water.
Fast breeder reactors
are better than conven-
tional reactor both from E_ NarO
the point of view of safety -"Mx
and thermal efficiency. U238—.
For India which already is BLANKET
fast advancing towards COPE ________
Fig. 5.10
to stUrfl
- carr
_..JL
r ut C _f q d w.-mtcr
R ac (or
Lf
- ---"I,-,',.
..L-JL)
Ftc)i;
Fuel L.jrJ)es
Moderate hot
l4iaVy water exchangei
moderator
Fig. 5 10(a)
NUCLEAR POWER PLANT 375
flt Urn
INLET
Fig 5.11
IwarE
" TEAM
STEAM
TUREINE ALTER.4t3
7
DE MS S P
OL ATEP
Fig. 5.12
5.19 Breeding
It is the process of producing fissionable material (fissionable
material) from a fertile material such as uranium 238 (U 238 ) and
thorium 232 (Th 232 ) by neutron absorption.
(U238) neutron Pu239
Th 232 4 neutron - U233
Pu 239 and U233 are fissionable materials and can be used in chain
reaction.
5.19.1 Electron Volt (eV)
The electron volt is the amount of energy required to raise the
potential of an electron by one volt.
One electron volt (eV) = 1.60203 x 10-12 erg.
= 1.60203 x 10 -19 Joules.
NUCLEAR POWER PLANT
377
5.20 Thermal Neutrons
Such neutrons are in thermal equilibrium with the material in
which they are moving; for example in the moderator. They poss&'ss
a mean energv.of about 0.025 eV, at normal temperature (15C)
5.21 Fast Neutrons
Fast neutrons are those neutrons which have lost relatively
little energy since being produced in the fission process. The lower
limit of their energy is taken as 1.0 MeV (million electron volts.
The general neutrons energies are as follows
(a) Thermal neutrons –0.025 eV
(l) Intermediate neutrons - 1.0 to 0.1 MeV
(c) Fast neutrons- - 0.1 MeV or more,
Thermal neutrons are the most effective in causing fission and,
therefore it is desirable to slow down or moderate the fast neutrons
which normall y have an energy of about 1 MeV.
5.22 Burn Up
It is the amount of fissible material in a reactor that gets
destroyed clue to fission or neutron capture expressed as a percent-
age of the original quantity of fissionable materials.
5.23 Cost of Nuclear Power Plant
Nuclear power plant is economical if used as base load power
plant and run at higher load factors. The cost of nuclear power plant
is more at low load factors. The overall running cost of a nuclear
power plant of large capacity may be about 5 paisa per kWh but it
may be as high 15 paisa per kWh if the plant is of smaller capacity.
The capital cost of a nuclear power plant of larger capacity (say 250
MW) is nearly Rs. 2500 per kW installed. A typical sub-division of
cost is as follows
Item
(a) Capital cost of land, building and
4_ Approximate Cost %
62%
eujnt etc.
ib) Fuel cost 22%
Maintenance cost
(d) Interest on cap cost ___
The capital investment items include the following:
(i) Reactor plant: (a) Reactor vessel (b) Fuel and fuel handling
system, (c) Shielding. (ii) Coolant system. (iii) Steam turbines,
generators and the associated equipment. (iv) Cost of land and
construction costs.
The initial investment and capii.ii cost ofa nuclear power plant
is higher as compared to a thermal power plant. But the cost if
transport and handling of coal for a theri 1 power plant is much
—26
378 POWER PLANT
higher than the cost of nuclear fuel. Keeping into view the depletion
of fuel (coal, oil, gas) reserves and transportation of such fuels over
long distances, nuclear power plants can take an important place in
the development of power potentials.
5.24 Nuclear Power Station in India
The various nuclear power stations in India are as follows
(i) 'rFpUF Nuclear Power Station. It is India's first nuclear
power plant.. It has been built at Tarapur 60 miles north of Bombay
with American collaboration. It has two boiling water reactors each
of 200 MW capacity and uses enriched uranium as its fuel. It
supplies power to Gujarat and Maharashtra
Tarapur power plant is moving towards the stage of using mixed
oxide fuels as an alternative 'to uranium. This process involves
rec y cling of the plutonium contained in the spent fuel. In the last
couple of ears it has become necessary to limit the output of
reactors to save the fuel c y cle in view of the uncertainty ofenriclied
uraniulil supplies from the United States.
(it) Italia I'ratap Sagar (Rajasthan) Nuclear Station. It has
been built itt 12 miles south vest of Kota in Rajasthan with
Canadian collhurution. It has two reactors each of200 MW capacity
and uses natural uranium iii the form of oxide as fuel and heavy
water as moderator.
(iii) Kalpzrkkam Nuclear l'ower Station. It. is (lie third
nuclear pOwet' :iatiun ill and is being built at about 40 miles
from MO4UOS ( ov. It will he wholl y designed and constructid by
aliaii -i''H i.- aid engineers. It has two fast reactors each oI'235
M\V capach v uid will use natural uranium as its fuel.
The first uiu f 235 MW capacity has started generating power
from .1983 aiu Lt- 235 MW unit is conimissionud iii 1985
The pressnrised buo y water reactors will use natural uritniulli
available in plety in India. The two turbines and steam generators
at the Kalpakkain atomic power project. are the largest (opacity
eneratiI1g sets inalled in our countr y . In this l)owci station about
88SF local machi u p rv and equipment liave been used
(it') Narora Nuclear Power Station. It is India's fourth
nuclear jIO et station and IsbelilgiWilt at. Naroiii in hullindshitliir
District of' Uttar Pr'adesh. This plant will initiall y have two units of
235 MV 'ahi and proviiefl hias,beein made to expand its caj)icity
of 500 MWI It IS ex 1 ucted to be corupleteti by 1991.
This plant 'viii have t\yo reactors of the CAN1)U--- 'II \V
(Canadian De ti trium_Ura! in—l'russuristd heav y \Vatt.r
tern and will ue natural uiniiuni as its fuel. 'ibis plait will ho
and cunttui'tt.'(l by the Indian scientists iIi(I (fl'
NUCLEAR POWER PLANT 379
Fu e l
condary
C 1.0 d ding nfainment
Primary at transport
con fain me system
Ile the core fuel for fast breeder reactor. In fact in breeder reactor
heavy water is used as moderator.
A CANDU reactor of 200 MW capacity requires about 220
tonnes of heavy water in the initial stages and about 18 to 24 tonnes
each year subsequently. Therefore, about one thousand tonnes of
heav y water will be required to start the different nuclear power
stations using heav y water. The total capacity of different heavy
water plants wilt he about 300 tonnes per year ifafl the heavy water
plant under construction start production. It is expected that heavy
water from domestic production will be available from Madras and
Narora atomic power plants. The management of the heavy water
system is a highl y complicated affair and requires utmost caution.
Heavy water is present in ordinary water in the ratio I 6000. One
of the methods of obtaining heavy water is electrolysis of ordinary
water.
5.27 Advantages of Nuclear Power Plant
The various advantages ofa nuclear power plant are as follows:
1. Space requirement of a nuclear power plant is less as
compared to other conventional power plants are of equal
size.
2. A nuclear power plant consumes very small quantity of
fuel Thus fuel transportation cost is less and large fuel
storage facilities are not needed. Further the nuclear
power plants will conserve the fossil fuels (coal, oil, gas
etc. , for other energ y need.
3. There is increased reliabilit y of operation.
4. N ueleir power plants are-not effected by adverse weather
conditions.
5 Nuclear power phints are well suited to meet large power
demands. TI cv give better performance at higher load
factors 80 to 90U.
6. Materials expenditure on metal structures, piping.
storage inecliani.ins are much lower for a nuclear power
plant 01,111 ;i coal burning power plant. For example for a
100 N1 \\ n niclear power plant the weight of machines and
inclLtm ins, weight of metal structures, weight of pipes
and fittings and weight of Illasonrv and bricking up re-
ire nearl y 700 tonnes, 901) tonnes. 200 tonnes and
500 tonnes respectivel y whereas for a 100 MW coal burn-
ng power plant the corresponding value are 2700 tonines,
1250 tinne. 300 tonnos and 1500 tonnes respectively.
Further area of construction site required for 101) MW
nuclear power plant is a h e ctares whereas for a 100 MW
(super critical) whereas < I shows that reaction will he dying down
(subcritical).
5.31 Uranium Enrichment
In some cases the reaction does not take place with naturaL
uraniu : t i ning only 0.71% of U23.
0 0 00
0 0 0 0 0 00 0 0
GAS
0-
000 0 00 0 00 0 00 0 0 0 000 0 0
J
INPUT 00%:O%0oO %oO%o0O%%o
00
- _ 0
00
000 0 - -,
DEPLETED
PRODUCT
I
00 0 •
0 0 001
1
• HEA VY MOLECULES
• LIGHT MOLECULES ENRIcI
Fig. 513
PRODUCT I
1. T/i.' gaseous diffusion ,iithvd. This meth based oil
principle that the diffusion or penetration molt ilar ota gas with a
given molecular weight through a porous barri r is quicker than the
molecules of a heavier gas. Fig. 5.13 shows a p:iriting stage for
gaseous diffusion. Non-saturated uranium he:a-t1ouride (UF 6 ) is
used for gaseous diffusion. The diffusing molecules have small
difference in mass. The molecular weight of U215
F6 = 235 + 6 x 19 = :349 and that of U 235 F6 = 352. The initial mixture
is fed into the gap between the porous harrier. That part of the
material which passes through the barrier is enriched product,
enriched in U 23 F6 molecules and the remainder is depleted
product.
2. Thermal difñision method. In this method (Fig. 5. 14) a column
consisting of two concentric pipes is used. Liquid UF 6 is filled in the
space between the two pipes. Temperature ofone of the pipes is kept
high and that of other is kept low. Due to difference in temperature
the circulation of the liquid starts, the liquid rising along the hot
wall and falling along the cold wall. Thermal diffusion takes place
in the column. The light U 235 F6 molecules are concentrated at the
hot wall and high concentration of U 236 F6 is obtained in the upper
part of the column.
POWER PLANT
Enriched
product
Magnetic field
rgion-
72 -71
Liquid
UF6
i IRA
=.. Enriched
- product -.zI
_J
mv
R
eH
This shows that ions moving at equal velocities but different
masses mbve along circumferences of different radii (Fig. 5.15). Fig.
5.16 shows an electromagnetic separation unit for uranium isotopes.
A gaseous uranium compound is fed into the ion source, where
neutral atoms are ionised with the help of ion bombardment. The
U2).
Ion
source II
: 1/ I
Magnetic
field
region
Accelerating
electrodes
H.V. Power
supply
Fig. 5.16
(J,
0 0 0
. el o Light rncule
• 0 0 •I 0 0
i. • • • . .1
a *Heavy molecule
• I.I a.
I. •a 010.0111
0 010 .1
.•. 01.00
L.° 0°OjOO .•
Fig. 5.17
390 POWER PLANT
led chain reaction takes place so that the heat energy released can
be controlled.
Let V = Volume of energy
N = Fuel atoms/m 3
n = Average neutron density, i.e. number per
m3
cx = Fission cross section
= Neutron flux
v = Average speed of neutrons rn/sec.
F ission cross-section represents the probability of fission per
incident neutron. For example ify is the number of incident neutron
then those causing fission = a y Neutron flux is the, number of
neutrons crossing a plane of area one metre square held at right
angle to velocity v.
= fl x v
S = total fuel atoms in reactor = N.V.
It = number of incident neutrons per second
fuel atoms
= S x = nv. N.V.
x = Number of neutrons causing fission per
second
= It 3< (1 = nv. N.V.a.
Now 3.1 x 1010 fission per second produce a power of one watt
(See example 5.3)
P = Power of nuclear reactor
X n.v.fv.V.a.
= -- = watts. -
:3.1 x 1010 3.1 x 1010
Let the fuel used in the reaction be U2
Mass per atom of U235
At. weight of U235 235
------ k
Avogadro Number 6.02 x 1021
Mass of NV atoms = N.V. x Mass per atom
= x - ---- . = M kg (say)
- 2(
6 . 02x10 -
NUCLEAR POWER PLANT 391
6.02 x 1026 x ,,
NV = ------ -----
23
n.p,N.V.a.
J) = -------------
Now -- watts
- 3.1 x 1010
1()26 M x 582 x 10
ç x 6.02 x
- 3.1x10'0x235
12
= 4.8 x 10 Mo watts.
• with the reactor design. Its values for different reactors are inch
cated in Table 5.5.
Table 5.5
Type of r'actor Conter,um ratio -
BWRI'WRandSGR I .-. L - ..
Aqueous thorium breeder - -. 1.2
Fast breeder reictor
Exa pIe 5.5. Determine the energy released by the fission of 1.5
gm of (J in kWh assuming that energy released per fission is 200
MeV.
396 POWER PLANT
PROBLEMS
5.1. What is a chain reaction? How it is controlled?
5.2. What is a nuclear reactor ? Describe the various parts of a
nuclear reactor.
5.3. What are different types of reactors commonly used in nuclear
power stations? Describe the fast breeder reactor? What are its
advantages over sodium graphite reactor?
5.4. How waste is disposed off in a nuclear power station ? What are
main difficulties in handling radioactive waste?
5.5. Discuss the various factors to be considered while selecting the
site for nuclear power station. Discuss its advantages and disad-
vantages.
5.6. Write short notes on the following:
(a) Boiling water reactor (B.W.R.)
(b) Pressurised water reactor (P.W.R.)
(c) Multiplication factor.
(d) Fertile and fissionable material.
NUCLEAR POWER PLANT 397
-: .- Z1j' •
. ...
.i:tl • ts .. I
J f1J) m0 - •1 - 't ,
-t1q
p. 7.
p.
......
. .
.1• .
.............. ii....
'.
Hydro-Electric Power PIan.
CA 7CHMEN1
AREA
NE
Fig. 6.1
HEAD
RACE
Fig. 6.4
( ii) Earth Dams. Earth dams are used for smaller power plants.
They can be built safety and economically on all types of foundations
of earth and rock. They can be further sub-classified as follows
(a) Earth Dam (b) Rock Fill Dam.
Earthed dams are used when effective height ofdam is not large,
river banks are not steep and the site is unable to take the weight
of gravity dam. Fig. 6.5 shows earth dam.
REINFORCED CONCRETE
CORE WALL
STONE
IMPERVIOUS
X-1
.:'
LL
MATERIAL
WXL.
NEARRV
Rock
Fig. 6.5
404 POWER PLANT
- -
Natural
M embrcire_. slope
ry rubble
Fig. 6.5 (a)
canal
5pifl wQy
Fig. 6.6
River
River River
(
I
(a) (b)
9Z r
HYDRO-ELECTRIC POWER PLANT 407
2.f t
where t = Penstock thickness
d = Diameter of penstock
1= Permissible stress
P = Pressure due to water including water
hammer
= wH
w being the specific weight of water and H head of water.
il = Joint efficiency.
The joint efficiency is about 80% for riveted joints and 90% for
welded joints.
6.5.1 Number of penstocks
A hydro power plant uses a number of water turbines which are
to be supplied water through penstocks. Following alternative
choices may be considered
(i) To use a single penstock for the whole of plant. Such a
penstock will have a manifold at its end with as many
branches as the number of turbines.
(ii) To use one penstock for each turbine separately. In this
case each turbine draws water independently directly
from the reservoir.
(iii) To provide multiple penstocks but each penstock supply-
irg water to atleast two turbines.
408 POWER PLANT
Penstock
Penstock
IMP
Anchor
Block
(c) E.
Fig. 6.6
2./ii
2x105x25
= 1
2X11X106 x08 3-.2 metre
100=2.8 cm. Ans.
6. The Power House and Eq
uipment. Power house consists
of the main building of hydro electric development where the con-
version of energy of water to electrical energy takes place. Some
important
follows items of equipment provided in the power house are as
(i) Turbines (ii) Generators
(iii) Governors
(iv) Relief valve for penstock fittings
(u) Gate valves
(ii) Flow measurement equipment
(vii) Air duct (viii) Water circulating pumps
(ix)Transformers
(x) Switch board equipment and instruments
(xi)Reactors
(xii) Low tension and high tension bus bar
(xiii) Oil circuit breakers
(xi) Outgoing Connections (xiv)Storage batteries
(xvii) Shops and offices. (xvi) Cranes
Pover house should be Structurally stable. The layout of the
ower house should be such that sufficient space is provided around
he equipment like turbines generators, governors, valves, pumps
tc. in order to facilitate the dismantling and repairing.
A power house has three distinct sub divisions in most cases.
(i) The sub-structure (ii) Intermediate structure
(iii) The super structure
POWER PLANT
410
ROOF
GANTRY CRANE
VA1V7
L
InE
w,
ELIEF VALVE
TURBINE
U BE
uNWAT(RIP.Q PIPE A
Fig. 6.7
AM
PENSTOCK P^Ep ML
POWER HOUE
DAM
Fig. 6.9
•; • -
;. I.
-
I-
-U
HYDRO-ELECTRIC POWER PLANT
413
u pp er basin
Steam power plant
Pressure U
pipe tI Motor or
Z— generator
Va(ve
Vove
Purnp(4JfJ Turbine
LI
CANAl.
DAM PENSTQCIçS
Fig. 6.10
(b) Medium Head Plant. When the operating head of water is
from 15 to 50 metres the power plant is called medium head power
plant. This type of plant uses Francis turbines. The forebay provided
at the beginning of penstock serves as water reservoir. The forebay
draws water from main reservoir through a canal or tunnel. Forebay
also stores the rejected water when the load on the turbine decreases
(Fig. 6.11).
(c) High Head Power Plant.
When the hed of water exceeds 50
metres the plant is known as high head power plant. A surge tank
is attached to the penstock to reduce the water hammer effect on
the penstock. Pelton turbines are used in such power plants. Fig.
6.12 shows a high head-power plant.
POWER PLANT
414
- -1
1
Fig. 6:11
TOCK
cwEgE
Fig. 6.12
Wonal Head
);9w fiad
(7a t a i/o io t
Filter Gate
Trash Packs
'ter
Fig. 6.13
HY DRO-ELECTRIC POWER PLANT
415
Fig. 6-1:3 shows a typical high pressure intake head works
Trash racks remove floating or submerged debris dire
ctly at the
intake entrance. Filter gate balances water pressure fbr opening the
gate whereas air vent prevents penstock vacuum
3. Classification according to topography
(i Low land (ii) Hill y area
(iii) Mountatieous region.
4. Cl assification according to load supplied.
) Base load plant
(b) Peak load plant.
5. Cla ssification according to capacit y of plant
(i Micro hydel plants - upto 5 MW
(j) Medium capacity plants —5 to 100 MW
(iii) I ligh capacity plants - 101 to 1000 MW
(iv) S tiper plants - above 1000 MW.
6. Classification according to turbine characteristic i.e.
specific speed.
(i) High specific speed
(ii) Medium specific speed.
6.8 Advantages of H ydro-electric Power Plant
The major tactorwhich goin fav ourofhvclroclectrjc power plant
are as follows
1. Water is the cheapest an: fellable source ofgeneration of
electric power heca it exists as a free gift of nature
2. There are no ash . . poslI problems. Also the atmosphere
is not polluted because no smoke is produced in this plant
3. No fuel transport fion problem.
1. It can take up the loads quickl y and it is capable of meeting
the variable loads without any loss in efliciericy.
5. Its maintenance cost is low.
6. It requires less supervising staff
7. Auxiliaries needed in the plant are less as compared to
steam plant of equal size.
8. Running cost of the plant is low.
9. In addition to the power generation such plants are used
for irrigation and flood control purposes also.
10. Hvdro electric power plants have become economics coin-
petitors with steam power plants and will acquire more
economic advantage with the rise in price of coal and oil.
11. The life of the plant, is more and the effect of age is
COmparativel- siiiall oil overall efficiency of the plant.
Disadvantages. The various disadvantages are as follows
1. The power produced by tilepla nt
depends upon quantity
of water which in turn is dependent upon the rainfall, so
416 POWER PLANT
if the rainfall is in time and proper and the required
amount of water can be collected, the plant will function
satisfactorily otherwise not.
2. Hydro-electric plants are generally situated away from
the load centres. They require long transmission lines to
deliver power. Therefore, the cost of transmission lines
and losses in them will be more.
3. Initial cost of the plant is high.
4. It takes fairly long time for the erection of such plants.
6.9 Mini and Micro Hydro Power Plants
Micro hydro power plants (up to 100 kW capacity), mini hydro
power plants (up to 1 MW) and small plants (up to 10 to 15 MW) can
be successfully used for electrification of isolated pockets of villages
where the transmission system cannot easily reach. This includes
exploitation of mountain streams rivulets and canal drops. The
power from mini-hydro power plants and micro-hydro power plants
will be attractive as the energy generated can be consumed near the
source itself without a big network of sub transmission systems.
Micro/mini hydro development is an extremely valuable,
economic, renewable energy source in its endeavour to meet
decentralised rural need of the country.
The potential in small hydro-electric projects in various
countries ranges from 5 to 15% of the total hydro-potential of that
country. In India the estimated hydro energy potential ofmicro/mini
hydro power plants leads to an installed capacity of 10000 MW
spread over 5000 to 6000 schemes. Small hydro power plants (SHP)
which generate electricity in small scale are now being developed.
These power plants are an attractive renewable source of energy in
remote and hilly regions isolated from main grids.
Various advantages of small i. '-o-power plants (SHP) are as
follows
(i) Readily accessible source of renewable energy.
(ii) Can be installed making use of water head as low as 2 m
and above.
(iii) Does not involve setting up of large dams.
(iv) Least polluting.
(v) Limited initial investments and short gestation pèridds.
(vi) Reduced transmission losses.
The Indian Renewable Energy Development Agency (IREDA) is
encouraging both public and private organisations to set up
smalVininiJmicro hydel power plants.
In our country nearly 120 micro/mini small hydel schemes (up
to 3 MW capacity) with a total capacity of about 86 MW are in
operation. Nearly 117 small power plants of total 125 MW capacity
HYDROELECTRIC POWER PLANT 417
are under con .truction. Eighth five year plan proposals envisage a
capacity addition through such schemes of about 600 MW.
The potential of small hydro power plants (up to 5 MW capacity)
is estimated to be around 5000 MW. This remains largely untapped.
6.10 Draft Tube
It is an integral part of reaction turbine. Draft tube connects the
runner exit to tail race. The area of the top of the draft tube is same
as that of the runner to avoid shock and is of circular cross-section.
The water after doing work on the turbine runner passes through
the draft tube to the tail-race. Draft tube is a metallic pipe or
cQncrete tunnel having gradually increasing cross-sectional area
towards outlet to ensure that as little energy possibly is left in water
as it discharges into the tail-race. Draft tube provides a negative
section head at the runner outlet by which it becomes possible to
install the turbine above the tail-race level without an y loss of head.
Secondly the velocity of water leaving the runner is quite high. Thus
the kinetic energy of water due to this velocity will he lost if the
water is allowed to be discharged freely. So by passing water
through the draft tube, the outlet velocity of water is reduced
considerably and gain in useful pressure head is achieved, that is
the net working head on the turbine inr aes and thus output of
the turbine also increases
6.10.1 Types of Draft Tubes
1. Straight Divergent Tube. it is used by the low specific speed
vertical shaft Francis turbine. This draft tube improves the speed
regulation (luring falling load [Fig. 6.14 (a]. Its maximum cone
angle is S
SECTION AT
(I) (2)
(1
(a) J "^
' '
(2)
0?pw 0
(C) (d)
Fig. 614
418
POWER PLANT
2. Moody Sprathng Draft iii/'.
This draft tube [Fig. 6.14 (ô )j
has all that its conical portion at the Centre reduces the
whirl action of water moving with high velocity centre reduces.
3. Simple Elbow draft tube [Fig. 6.14 ((.)] and draft tube with
circular inlet and rectangular outlet lFig, 6,14 (d[ require lesser
excavation for their instaIIatiin arid thus cost of excavation is less
for such draft tubes.
Efficiency of draft tube is given Lw the following formula
- .
n Efficiency
where H = Actual CO UVCI - S j OI1 of kinetic head into
pressure head
2g 2g
Ill
2g
where V1 = Velocity ofwatr at inlet, of draft tube
V2 = Velocity of water at outlet of draft tube
The various types of surge tanks are shown in Fig. 6.15. The
surge tank shown in Fig. 6.15 (a) has a cylindrical storage reservoir
connected by a vertical branch of pipe to the penstock. The sur-
getank in Fig..6.15 (b) has a conical reservoir whereas surge tank
in Fig. 6.15 (r) has a bell mouth spillway to discharge the excess
water. Fig. 6.15 (d) shows a differcntial surge tank. It has a central
riser with a small hole at its lower end. The water enters the surge
tank through this hole and the function of the surge tank depends
upon the area of hole. The surge tank shown in Fig. 6.15 (e) consists
of separate galleries ; the upper one is o,ed to store water when the
load on the turbine dec., ses and the lower one to suppl y water
when the load on the turhin increases.
0VEP FLOW
RISER j'71
(d) (e)
Fig. 6.15
RUNNER
BUCKET
(V.
........
Fig. 6.16
(a) Buckets (b) Nozzle and needle valve
(c) Shaft (d) Penstock
(e) Tail race channel.
Buckets are the hemispherical cups bolted to a shaft. They are
the main component parts which absorb and transmit the energy of
water. Nozzle imparts a very high velocity to water. Needle valve is
used to control the water discharge to the turbine. Penstóck carries
water from the reservoir to the turbine.
Water coming out of the turbine .is discharged into the tail race.
Fig. 6.16 (a) shows multijet Pelton wheel arrangement.
Fig. 6.16(b) shows super structure of pelton wheel power house.
A power house is provided with a travelling crane which can span
the width of power house and also travel itsentire length. Crane
should be able to lift generator rotor, shaft and runner. The roof and
upper part of the super structure may be either steel truss or rigid
frame.
422 POWER PLANT
Nflr
Flow
Ru
Fig. 6.16(a)
Crone
Water
ol Machine
roan, halt
YOIVCJ F. IL
H
chamber 1L -
Fig. 6.16(b)
TPL
Fig. 6.17
WICKET GATE
5HAF T
•
1_44 WATER LEVEL
.':
DRAFT TUBE
Draft tube
Tail race
Fig. 6.18
Wheel
Guide
blade
de
a l-% h'
Guide - Threaded
blade ring Spindle
Fig. 6.19
Water
Water
inlet
Outlet
'uide
(odes
WA TER
1i 171j ii-\ CASING
TUBE
RUNNER
BLADE TO TAIL
RACE
Fig. 6.19(b)
Fig. 6.19 (b) shows sectional view of turbine. The blades are
attached to the hub ofrunner. The runner is horizontal and it rotates
about a vertical shaft. Water enters the turbine in a radial (inward)
direction through an arrangement of movable wicket gates that
control the water supply and act as stationary nozzles. The water is
discharged in downward axial direction.
6.13.2 Direction of flow of water
According to the direction of flow of water the turbines may be
classified as follows
(i) Tangential flow turbine.
(ii) Radial flow turbine
(a) Radial Outward (b) Radial Inward
(iii) Axial Flow Turbine
(iv) Mixed Flow Turbine (Radial and Axial)
In tangential flow turbines as in case of Pelton turbines the
water strikes the runner in a direction which is tangential to the
path of rotation.
In a radial flow turbine the water moves in a plane perpen-
dicular to the axis of the rotation. In inward flow turbine the water
enters at the outer periphery and discharges at the inner periphery.
In axial flow turbine the path of water during its flow is parallel to
the axis of turbine shaft whereas in case of mixed flow turbine the
water enters radially inward and discharge axially.
—29
_P
where N = Speed in R.P.M.
f= Frequency of generation
HYDRO-ELECTRIC POWER PLANT 427
Penstock
To fl race
Fig. 6.19 (c)
H = GrossEiead
= /1 + Hf
where h = Net head
H1 = Frictional head
H415
HYDROELECTRIC POWER PLANT
429
SLEEVE
ç RIGID FULCRUM H
FROM TURBINE 01.3 TRIBUTIN&
MAIN SHAFT - - VALVE
GEAR PUMP
CIL SUMP
-r- =--qftl
I r=
,LJONPID
SERVOMOTOR OP To TURBINE GUIDE
RELAY CYLINDER t4ECHAM$UM
Fig. 6.20
430 POWER DLANT
I.
FROM RELAY
CYLINDER f1T_,1 r-
J' NEEDLE
1 I NOZZLE
SUPPLY PIPE t
Fig. 6.21
• We know
75
whore P Power produced by a turbine
Q = Discharge in cumecs
H = Net Head is metres
co = Unit weight of water.
Now Q=AxV=k1.D2.V
where D = diameter of the runner
V= Velocity
Voc 'i=k2J
wkb2N ii1=k3D2H
60
where N = speed of turbine in R.P.M.
Now V -ff
POWER PLANT
V=k 3 'i.ii
iEDN
N=k2ff
(Pu =
ThereforQ, D
HYDRO-ELECTRIC POWER PLANT
433
Substituting in equation (i),
PoH312
\ H
N N5
-
Table 6.3 shows the specific speeds for different turbines.
Table 6.3
Turbine
Fra
_L_ Reaction— L =iI
Example 6.2. A turbine develops 18,000 H.P. working under a
head of 520 in when running at 400 R.P.M. Ca/cu/cite the specific
speed of the, turbine. Specify the type of turbine to be used.
Solution. H = Head = 520 R.P.M.
N = R.P.M. = 400 R.P.M.
P = Horse Power = 18,000.
400\'18,000
N 21. 4
5205'4-
For this specific speed Pelton turbine is used.
Example 6.3. Calculate the specific speed of (I turbine and
suggest the type of turbine required for a river having a discharge of
250 litre/sec with an available head of 5 0 ,,zctre. Assume effieiencv
of turbine as 80 and speed 450 R.P.M
Solution. 0 = 420 litre/sec-
11
= 50 inetr
434 POWER PLANT
= efficiency = 80%
Tj
N= 450 R. P.M.
P = Horse power developed
- no)' 0.8 x 1 x 250 x 50 133.3
- 75 75
(Taking w = 1 kg/litre)
Now, N3 = specific speed
N .TP - 450
H514 505'
For this specific speed Pelton turbine is suitable.
Example 6.4. It is desired to build a hydro-electric power station
across a river having a discharge of 30,000 litre/second at a head of
10 rn. Assuming turbine efficiency 80% and speed ratio (Ks) as 0.83,
determine the following:
(a) Is it possible to use two turbines with a speed not less than
120 R.P.M. and specific speed not more than 350 R.P.M.?
(b) Specify the type of runner that can be used. Also calculate
the diameter of runner.
- ru4H
Solution. - 75
where p = Total power available
= Specific weight of water
= Discharge
H = Head (metre)
0.8 x 1 x 30,000 x 10 =3200
P= .
Using two turbine each of capacity 1600 H.P. the specific speed
(N8) of the turbine iscalculated as follows:
N#120 I1600
N8=--=
= 267 R.P.M.
For this speed Francis turbine is suitable
U = Tangential velocity of the runner
nDN
=K. 4WH—
HYDRO-ELECTRIC POWER PLANT 435
where K. speed ratio and D = diameter of runner
60xK I1 60x0.83 Vjj
D—
itxN - itxl2O
= 1.85 metres.
6.18 Efficiency
Different types of efficiencies used in connection with hydraulic
turbine are as follows
(i) Volumetric efficiency (ii) Hydraulic efficiency
(iii) Mechanical efiT cv.
6.18.1 Volumetric efit cy
Some of the water flowing in the turbine may leak through the
joints or some water may not be effective in imparting its energy to
the turbine. The leakage of water reduces the efficiency of the
turbine.
- -
"cc
- . Fig. 6.22
(i) Direct Coupling (ii) Gear Drive.
Direct coupling system is used for low speed turbines. In this
system both the turbine and generator shaft are directly coupled
and run at same speed. Any fluctuation in turbine shaft speed is
directly reflected in generator. In gear drive system spur gears or
bevel gears are used to connect turbine shaft with generator shaft.
This arrangement is quite commonly used.
,t9 [Genercr
Hood race
POWER PLANT
438
- H
where H = Total effective head
Hb = Barometric head.
H5 = Suction head or height of pump about tail water level.
For cavitation free iunning a has to be greater than critical
value acm.
< 11b - us
(Ocrit)
H
H5 5 Fib - acn: H
is a function of specific speed.
When H is large H5 comes out to be negative and therei
becomes essential to provide the pump with negative suction h
i.e. the power house location has to be so fixed that pump operak-
under submerged conditions.
PI
(a) (b)
HYDRO-ELECTRIC POWER PLANT
439
1?
I h.o
'a
Fig. 6.24
Fig. 6.25
Francis turbines are suitable for operation of the plant from 75%
load to full load. Propellor turbines with fixed blade construction are
used at fairly constant load between 759 and 100% of their capacity.
POWER PLANT
440
Budding
Rem
_____-
I Cost (crores
50 50
0 ±J 0i r = 60x0.05
(l+r)-1 (1+O.5)°_J
60 x 0.05
=----j = 0.287 crore
where n = Life in years = 50
Cost of dam and building
50+1060crOres
C2 = Depreciation cost for generaL...
4x0.05 3x0.05
- (1 +0.05)20 - 1 0.65-1
-
=O.2Crore
= Depreciation cost for transmission line and
penstock
11x0.05 11x0.05
(1 + 0.25)2_ 1 - 3.39-1
= 0.23 crore
C - Total annual depreciation cost
= 23 X 104 x -j = 138 x iø
= 1.38 crores.
R = Total income = R 1 + R2
= 5.31 + 1.38 =7.69 crores.
Net profit = R -• = 7.69 - 6.337 = 1.353 crores.
6.26 Hydro-steam Inter-connected System
A hydro power plant maybe used as a base load plant or as peak
load plant but the trend is towards use of hydro power plant with
steam power plant in an inter-connected system. Power from hydro
electric plants usually costs loss and, therefore, when flow of water
is adequate hydro power plant should be used as base load plant and
steam power plant should be used as peak load plant whereas during
low water in reservoir the functions of two plants should be reversed.
By interconnecting hydro power plant with steam power plant
a great deal of saving in cost is achieved and standby requirements
are reduced in an interconnected system. The interconnected svs-
tern should have a suitable load allocation plant set prehand for each
day. Hydro turbines can be started from cold in a few minutes while
steam units need about 5 to 8 hours.
HYDRO-ELECTRIC POWER PLANT
445
TIE
T/1&QE
PLUME
Th'I8RE.
TRE5TLE
€27 Tunnels
The tunnels are generally of circular section (Fig. 6.26) or horse
shoe section (Fig. 6.27). The hand excavated tunnels are usually at
least 6 feet in diameter whereas the minimum economic diameter
for machihe excavated tunnels is nearly 8 feet. Tunnels act as open
channels when flowing partially full and act as pressure conduits
when flowing fully.
6.28 Flumes
Where it becomes difficult or expensive to construct canals, the
water is conve yed through flumes. The flume channel is so designed
that it is able to carry its own weight and that of water as beam
between supports. Flumes may be made up of wood, steel or rein-
forced concrete. Wooden flumes are generally, of rectangular cross-
section width being nearly twice the water depth. Fig. 6.28 shows
the cross-section of a wooden flume. Fig. 6.29 shows the cross-sec-
tion of a semicircular steel flume. Fig. 6.30 shows the ôross-section
of a concrete flume on concrete piers. Reinforced concrete flumes
have longer life and their maintenance cost is low whereas wooden
flume are of shorter life and depreciate more rapidly.
6.29 Spillway and Gates in Dams
CURVAT RE
ROUNOV LIP 47
ENrRANCE
VERT/AL
STi'RI5Ei)
CONCRETE
/NEO W4%L
3ROLLtR
GATE
•j1 9RCLLEO
STEEL GUIDE
q ,86Eg E41FR
dM -
SEAT
CONCRETE I'/DGf
,r pg
SETI'E&W
C4&E n
PIE,?
GA IF
\\
CONCR6TE.
TOWER
INCLINO
P40<
11 \\O P4
I'c&..J SEAL
:
:G.
Fig. 6.40
Fig. 6.40 shows tube valve. This valve is open or closed by
mechanical means. To open or close the valve cylinder (tube) is
moved towards or away from the valve seat with the help of screw
stem activated by a bevel gear. As compared to needle valve this
valve is lighter in weight and is shorter in length.
Frame Operation rod
Closed
Disc
Disc
Fig. 6.40 (a)
HYDRO-ELECTRIC POWER PLANT 451
Butterfly valve. This valve is used not only as intake gate for
penstock but also is used before the turbine to facilitate the inspec-
tion without dewatering the whole of the penstock line. Fig. 6.40 (a)
shows a butterfly valve. It consists of a lens shaped disc which can
be moved in the frame of the valve.
6.32 Average Life of Various Cómpönents
The approximate average life of various components of a
hydropower plant is indicated in Table 6.3.
Table 6.3
JAN
HiI
LLL,:/
!ll / .
NW RAIN SJñA)f
COURSE GAUGE GAUGE
Sd.VEY STATION 5T.4 rKJN
Fig. 6.42
HYDRO-ELECTRIC POWER PLANT 453
where P = Precipitation
R = Run off
E Evaporation.
Precipitation. It includes all the water that falls from atmos-
phere to the earth surface. Mainly precipitation is of two types.
(i) Liquid precipitation (Rainfall)
(ii) Solid precipitation (Snow, Hail storm).
Run-off. Run-off is that portion of precipitation which makes
its way towards streams, lakes or oceans. Run off occurs only if the
rate of precipitation exceeds the rate at which water infiltrates into
the soil and after depressions small and large on the soil surface get
filled with water. Rainfall duration, its intensity and a real distribu-
tion influence the rate and volume of run-off.
Evaporation. Transfer of water from liquid to vapour state is
called evaporation.
Transpiration. It is a process by which water is.released to the
atmosphere by the plants.
6.37 Hydrograph
It is.a graphical representation between discharge (cubic metres
per second) through a river and time.
A hydrograph may be
plotted for several weeks or
even months. Hydrograph mdi-
SURFACE PECK cates the power available from
"'SIN
RUNOFF cessos the stream at different times of
OrSCHARGE UMB the day, week or year. Extreme
4 LIMB conditions of flow can also be
TANGEN studied from a hydrograph.
BASE F I.Ow Hydrograph of stream of river
- TIME - will depend on the charac-
teristics of the catchment and
Fig. 6.43 precipitation over the catch-
ment. Hydrograph will assess
the flood flow of rivers hence it is essential that anticipated
hydrograph could be drawn for river for a given storm. A typical
hydrograph is shown in Fig. 6.43. A hydrograph has a rising limb,
peak and receding limb or recession curve.
6.37.1 Flow Duration Curve
It is a method to represent the run off graphically. This curve is
plotted between flow available during a period versus the fraction
of time. The total power available at the site may be known by this
curve which can be drawn with the help of hydrograph from the
POWER PLANT
available run off data. Fig. 6.43 (a) shows a typical flow duration
curve.
This curve is nearly useful in the analysis of the development of
water power.
C
U
a
% of Time
Fig. 6.43 (a).
6.38 Mass Curve
A reservoir is used tQ conserve water which can be used during
the period of deficiency. A mass curve is a convenient device to
determine storage requirement that is needed to produce a certain
dependable flow from fluctuating discharge of river by a reservoir.
Mass curve is a plot of cumulative
volume of water that can be stored
from stream flow versus time in days,
weeks or months. The slope of the mass
curve at any point represents the F U-
hange of volume per change of time in ________
)ther words the rate of Row at the Time
moment. Hence the mass curve issteep
t4as Curve
when the river flow is large and flat
when the river flow is small. Fig. 6.44 Fig. 6 4 4
shows a mass curve.
6.38.1 Unit Hydrograph
This type of hydrograph represents a volume of one inch of run
off resulting from a rainfall of some unit duration and specified a
real distribution.
Unit h,idrographs of very large floods differ some what from
those of small rainfalls. A unit hydrograph can be contructe frnjH
a hydrograph of the actual run off when there is uniform r.
intensity and uniform a real distribution. The nu!b4r unit
hydrograohs for a given basin is theoreticall y infinin' as t.l.u, i1IV
e one unit hydrograph for every possible duration nt raitttiH aul
'iery possible distribution pattern of rainfall iii the basin . l
HYDRO-ELECTRIC POWER PLANT
.jI5
tice only a limited member of unit hydrographs are used for a given
basin.
A unit hydrograph is constructed as follows
Ci) Measure the total volume of run off from actual
- hydrograph.
(ii) Determine the ordinates of unit hydrograph by dividing
the ordinates of actual ran off by the total volume of run
off in cms. over the drainage area.. This gives unit
hvdrograph for the basin.
(iii) Determine effective duration of run off producing rain for
which the unit hydrograph (WI) is applicable by a study
of the rainfall records.
Unit hydrograph is a very useful tool in estimating the run off
from a basin for a storm of given duration. It helps to predict the
expected flood flow from a catchment if rainfall intensity in the,
catchment area is known.
Fig. 6.44.1 shows a typical unit hydrograph obtained from actual
hydrograph of run off.
Run off
hydrogroh
Unit -
ydrograph
Time (hours)
Fig 6.44.1
6.38.2 Factors affecting run off
Run-off from an area depends upon the following factors
Ci) Precipitation cha racteristics. They include type of storm, its
intensity, extent and duration.
(ii) .\ I'frokçn( characteristics. They include temperature
humidit y , wind, prc'.sure variation etc. Greater temperature and
'ind velocity help evaporation.
(iii) Catchment characteristics. Geographical features of catch-
ment such as size, shape and location of catchment produce sig-
nificant effects on the run-oft
4 5fi POWER PLANT
Main Stream
Tributaries
Iater'Shed Boundary
(t )
HP ±Ln 75
(Taking 1 metric H.P. = 75 kg m/sec)
kW power = 0.746 x H.P.
6.39 Controls in Hydro-electric Plants
The various controls provided in a hydraulic power pLnt are as
follows
(i) Hydraulic controls
(ii) Machine starting and stopping controls
(iii) Machine loading and frequency controls
(iv) Generator and system voltage control
(v) Machine protection.
Hydraulic controls. All water levels are indicated on the
control panels. Water passing through the turbine is recorded in the
control room through water flow indicator and recorder for in-
dividual units. The various hydraulic controls are as follows
(a) Primary and secondary storage level indicators.
(b) Flood control. . (c) Intake gate control.
(d) River flow control.
Machine starting and stopping controls. The water flowing
to the turbine is controlled by means of gates and valves provided
in the supplying conduit and at the turbine inlet. The water supply
to the turbine is regulated in accordance with generator load
through a governor system. During starting of turbines filling of
casing should be done gradually and by pass valves are provided to
limit the rate of water flow.
Machine loading and stopping controls. The load on the
machine is controlled by adjusting the governor speeder control or
by controlling the system frequency.
Generator and system voltage control. The electric power
should be supplied at proper voltage. The voltage control is exercised
through voltage regulators.
HYDRO-ELECTRIC POWER PLANT 459
HYDRO-ELECTRIC POWER PLANT 461
POWER PLANT
462
HYDRO-ELECTRIC POWER PLANT 463
H.P. developed -
75
where 0= water available/sec.
- 120x(1000)2x0.5
- 8760x60x60
w = specific weight of water = 1000 kg/rn3
H = head = 250 metre
= efficiency = 0.7
k = yield factor = 0.5
• H. P. developed = 0.7 x 0.5
8760 x 60 x 60 x 75
35 x 106
876 x 9 4328
•. Average Power = 4328 x 0.746 = 3228 kW
Avepower
Load factor
Maximum demand
Maximum demand
- Average power - 3228
= 8070 kW.
- Load factor - 0.4
The capacity of the power plant can be taken equal to maximum
demand
Capacity = 8070 kW.
Example 6.8. Ca/cu/cite the power that can be deteloped from ci
hydro-electric pou'er station hating the following data
Catchment area = 100 sq. km .
Ateragi' rain fall = 120 cm
Run-off =
Available head = 300 rn
Overall eftcu'ncv o/the power station = 75'.
464 POWER PLANT
(1)qHxfl = 1000x3.4x300
H.P. developed - x 0.75
75 75
1000 x 3.4 x 300 x 0.75 x 0.746
Power in kW =
75
1000 x 3.4 x 300 x 0.75 x 0.746
Power in MW = 75 x 1000
- 3.4 x 300 x 0.75 x 0.746
- 75•
= 7.48 MW. Ans.
Example 6.9. Determine the H.P. that can be developed from a
hydroelectric power plant with following data
Catchment area of reservoir = 3 1618 sq. metre
Mean head =40m
Annual average rainfall = 110cm
Efficiency of turbine 80%
Efficiency of generator = 85%
Load factor . = 45%
Assume that 25% of the rainfall is lost due to evaporation and
4% head lost in penstock.
Solution. Quantity of water available per annum
Q = 3 x 103 x 1.10 x 0.75 = 2.475 x 10 8 cu-m.
Quantity of water available per second
2.475 x 108
Q -------- = 7.85 cu-m/sec.
365 x 24 x 60 x 60
Head H=40m
Overall efficiency () = Turbine efficiency x Generator efficiency
x Penstock efficiency
= 0.8 x 0.85 x 0.96 = 0.65
HYDROELECTRIC POWER PLANT 465
- wQHr1
H.P. developed
- 75 x load factor
1000 x 40 x 7.85 x 0.65
= = 6032. Ans.
75 x 0.45
Example 6.10. (a) In a hydropower plant the reservoir is 200 in
above the turbine house. The annual replenishment of reservoir is
40 x 1010 kg. Calculate the energy available at the generating station
bus bars if the loss of head in the hydraulic system is 20 in the
overall efficiency of the station is 80%.
(b) Also determine the diameter of two steel penstocks if maxi-
mum demand of 50 MW is to be supplied.
Solution. (a) n = Efficiency = 0.8
h' = Loss in head = 20 rn
h = Actual head available
=200-h 1 =200-20= 180
E = Energy available at the turbine house
= mgh = 40 x 1010 x 9.81 x 180
= 70.63 x 1013 J
- 70.63 x iø' -
16.84 x 107 kWh.
- 36x105 -
(As 1 kWh = 36 x io J)
Energy output E X 1 = 16.84 x 107 x 0.8
= 13.48 x 107 kWh. Ans.
(b) Kinetic energy of water
= mV = Loss of potential energy of water
,mV2=mgh
V='K='I2x9.81x180=59.4 rn/sec.
= Energy available from a mass in kg of water when it flows
with the velocity 59.4 rn/sec.
= mV = I in x 5942 J/s or Watts.
=A
-- = 0.38 = 0.19 m 2
= 0.19
D=O.242rn. Ans.
6.43(a) Hydro Power Plants in India
Some of the hydro power plants installed in our country are
mentioned in Table 6.4
6.43.1 Hydro Power in India
Hydro power represents a renewable source of energy which
enjoys man y intrinsic advantages. Our country has large
hydropotential.
It is essential to produce cheap power for airound development
of the country. Our fossil fuel reserve is limited and we are still at
infancy indeveloping nuclear power and hence as far as possible the
long term planning for power development should be hydropower
,oriented. As no fuel is required to produce power therefore, power
produced will be cheaper than other conventional means in the long
run. In India the scope of Miter power development is tremendous.
Only a part of the easily available water power potential has been
developed so far Hydro power plants do not pollute the atmosphere.
Hence in order to keep the atmosphere free from harmful pollution,
water power is the ideal source of power. Being endowed by nature
with a variety of sources its tropical geographical position, its rivers
and wind power mark out for India much hydro power potential.
Hydro power being a renewable source of energy must undoubtedly
receive a high priority in our energy development programme. Total
hydro potential in our country is estimated to be equivalent to about
75,400 MW at 60% load factor of which only 11 to 12% has been
exploited so far. The assumption that hydel generation despite its
high capital costs and long gestation period, is cheap and clean has
rarely been questioned.
HYDRO-ELECTRIC POWER PLANT 467
Table 6.4
S.No. Name of the project River and the State Type of dam Power
develo
1. Srisai!arn Hyd! Project Andhra Pradesh IMasonry and 770
gravity
2. Upper Sileru H y dro Andhra Pradesh Masonry Division 120
Electric Project Weir
3. Umiarn Hyde! Power Urnaim River, Assam Concrete Earthen 39
Project
4. Subarnarokha Hyde!- Subarnarekha, Bihar Masonry Earthen 120
cum-Water Supply
Project
5. Ukar Project Tapi, Gujarat Masonry Earthen 160
6. Chonani Hyde! Project Tawi, Jammu and Masonry Division 37
Kashmir We,ir
7. Sala! Hyde! Project Chenab Kashmir Concrete Gravity 960
8. Iddiki 1-lyde! Project Iddiki, Kerala Concrete Arch
Concrete Gravity 800
Masonry Gravity
9. P Pamba and Kakhi Concrete Gravity
I river. Kerala
Masonry 300
Masonry
10. 1 Chainbal Valley Project Chamba!, river
(i) Gandhi Sagar Madhya Pradesh Concrete Gravity 115
(Li) Jawahar Sagar, Chamba! (M.P.) " 99
Kotah Darn
(iii) Rana Pratap Sagar 128
Dam
11. Kodayar Hydro-Electric Kodayar, Tamil Nadu - 100,
Project
12 Kundah Basin Develop- On different rivers, - 425
merit Project. Kundah Basin, Tamil
Nadu
13. Mettur Ilydro-Electric Mettur Tamil Nadu Concrete Gravity 200
Project
14. jPeriyar Hydro-Electric Periyar, Tamil Nadu Forebay Dam 140
Project
15. Koyria Hydro-Electric Koyna, Maharashtra Rubble Concrete 900
Project
16. Sharavathi Hydro-
Electric Project
(ii Linga Makki Dam Sharavathi, Ka r- Masonry Earthen 891
nataka
(ii) Talakala!a Dam
17. Tungabhadra Project Turigabhadra, Kar- MasonrY ('irav ,_[126
468 POWER PLANT
HYDROELECTRIC POWER PLANT 473
=
75
where = Specific we ,.' ht of water = 1000 kg/M3
Q = Discharge
ii = Efficiency = 0.7
2.447 x io =.1000 x Q x 14 x 0.7
75
Q = 187.3 m3/sec.
As the head is low and discharge is high so a propeller type of
turbine should be used.
(b) N = Specific speed
1150
= (Approx.) 1150 1150
14 1/4 =
=596
N = Speed of rotation
N. . H.'-44 596x14'4
- 'IP- '12.447 xiO
= 103 R.P.M.
For generator N =
p
where f= Frequency in cycles per second.
= 50 cycles/sec
• p = Number of poles
103_120x50
60
p = 58.3 = 60 (say) ...
As the number of poles is necessarily an even number.
• Again N==.°<5° = 100 R. P.M.
p 60
Example 6.12. A steel penstock carries 12 m 3/sec of water under
a head of 240 rn The penstock diameter is 2.8 Tn and the allowable
stress in penstock material is 1400 kg/M 2 . Determine the following:
(a) Water hammer pressure assuming velocity of pressure
wave 1425 rn/sec.
(b) Thickness ofpenstock.
(c) Describe water hammer.
—32
POWER PLANT
474
Solution.
(a) Q = Discharge = 12 m3/sec.
d Diameter of penstock = 2.8 m
H= Head =240m
V1 = Velocity of pressure wave = 1425 mlsec.
V2 = Velocity of water
Q = V2 x d2
12 = V2 x x (2.8)2
V2 = 1.95 rn/sec.
= Water hammer pressure
- Vi . V2 - = 283 m.
g 9.81
POWER PLANT
476
11100
(j
V.
600
200
2
- Weeks
Fig. 6.46
more) 11 91.7
200 (and more)
10 83.3
300 (and
8 - 66.7
400 (and more)
7 58.3
600 (and more)
5 41.7
700 (and more)
3 25
900 tand more)
1000 (and more) 2 ____ 16.7 T
Fig. 6.47 shows a flow duration curve. When selecting a suitable
site for a hydro power plant the flow data for a number of.years are
collected and hydrograPhs and flow duration curveEr the various
periods are determined.
HYDRO-ELECTRIC POWER PLANT
477
2 9U1
10.00
800
lop 600
'.- 00
C
U
U,
200
Fig. 6.47
HYDRO-ELECTRIC POWER PLANT 479
= 61,159 __=
0.212 or 21.2%.
24 x 12,000
Example 6.17. (a) What is pondage factor c
(b) Determine the firm capacity of a rix . f. rioer hydro power
plant to be used as 9 hours peaking plant assuming daily flow in a
river to be constant at 16 m31sec.
Also calculate pondage factor and pondage if the head of the
plant is 12 m and overall efficiency is SO%.
Solution.
(a) Pondage factor is the ratio of total in flow hours in a given
period to the total number of hours plant running during
the same period.
(b) P = Firm capacity without pondage
w.Q.H.r1
- 75
where w = Specific weight of water
= 1000 kg/m3 i6. Iz
Q = Discharge = 16 m3/s
H = Head = 12 m
Overall efficiency = 0.8
P = = 2048 H.P.
480 POWER PLANT
Q 1 =9 hours flow = 16 x 24
9
= 42.67 m3/s
P1 = Firm power with pondage
=2048x2.67
= 5468 H.P.
S Magnitude of pondage
= (24 - 9) = 15 hours flow
=15x60x60x.16
= 864 x 103 m3.
Example 6.18. The following data is supplied for a hydropower
plant.
Catchment area = 2200 sq km
Annual average rain fall = 150 cm
Available head = 130 m
Turbine efficiency = 0.86
Generator efficiency = 0.91
Percolation and evaporation losses = 18%
Determine
(a) Power development in kW taking load factor as Unity.
(b) Suggest type of turbine to be used if the speed of runner is
to be maintained below 260 R. P.M.
Solution.
A = Area = 2200 sq km
= 2200 x 106 m2
h = Annual average rainfall = 150 cm
150
= 1.5 m
HYDRO-ELECTRIC POWER PLANT 481
482 POWER PLANT
p
f= frequency
50 cycles/sec.
p Number of poles 26
120 x 50
N = = 230 R.P.M.
Since the generator is directly coupled to the turbine the speed
of turbine used must be equal to the synchronous speed of the
generator.
w.Q.H
P= Power = XY
280 =
P 1 = 6400
Number of Francis turbines required
= P= 107x103 = 17. Ans.
(b) Let P2 = Power capacity of each Kaplan turbine
-- N.'P2
230
_fP
00 -
2812"
P2 196 x 102
Number of Kaplan turbines required
HYDRO-ELECTRIC POWER PLANT 483
_f_107x103.6 Ans.
- P2 - 196 x 102
Example 6.20. A pump storage power plant has a gross head of
300 ni. The hedd race tunnel is 3.8 in and 650 in The
in sec. and friction factor is 0.017. if the overall
flow velocity is 7
efficiency, of pumping and generation are 84% and 89% respectively
determine the plant efficiency. The power plant discharges directly
in the lower reservoir.
Solution. f = Friction factor = 0.17
qp = Pumping efficiency = 0.84
= Generation efficiency = 0.89
L = Tunnel length = 650 in
H = head = 300 in
V = Flow velocity = 7 m/s
D = Diameter of head race tunnel
= 3.8 in
him= Frictional head loss
f.L.V 0.017x650x72
- 2gD - 2x9.81
= 7.26 in
Now h1=kH
7.26=kx300
k=0.024
Plant efficiency ('1) is given by
i-k X Tip X Tl
15
484 POWER PLANT
8-12 28
12-16 32
16-20 42
20-24 50
TIME (HCURS)-.--
Fig. 6.48
Q = 189 m3/seçond.
Example6.22. A penstock supplies water at a head equivalent
to 18 kg/cm2. There is a possibility of 15% increase in pressure due
to transient conditions. The design stress and efficiency ofjoint may
be taken as 1000 kgkm 2 and 88% respectively, if internal diameter
of penstock is 1.3 m find wall thickness of penstock.
Solution. p = Total pressure
=18+0.15x18 -
= 20.7 kg/cm2
- .,-
D = Internal diameter
=1.3m
R = Internal radius
=0.65m.
=65cm
1= Design stress
il = Efficiency
= 0.88
t = Wail thickness of penstock
It is given by the following formula . .......-
= pR
+ 0.15 cm
f.t-0.6p
- 20.7 x 65 +0.15
- 1000x0.88-0.6x20.7
= 1.7 cm.
6.45 Power House Planning
The basic requirement for power house planning is functional
efficiency coupled with aesthetic beauty. Two types of power plants
may be used.
(i) Surface power plants. The building of such power plants
is located above the ground.
(ii) Underground power plants. The building of these power
plants is situated in caverns excavated below the ground. Surface
power plants are quite commonly used.
486 POWER PLANT
After the choice of the type of power plant is made, the following
decisions may then be taken.
(i) The size of power plant and the arrangement of various
units.
(ii) The equipment to be located indoors and outdoors. For
example transformers and inlet valves can be located
either inside or outside the power plant.
6.46 Surface Power Plants
They have less space restrictions than the underground power
plants. The following parts of the power plant should be properly
designed.
1. Power house structure. Power house structure can have
following three divisions:
(i) Sub structure (ii) Intermediate structure
(iii) Super structure.
The sub-structure is that part of power house structure which
is situated below the turbine level. The sub-structural transmits the
load of the structure to the foundation. Sub-structure is usually
below the ground level and houses the following
(i) Draft tube (ii) Tail water channel
(iii) Drainage pipes of waste water
(iv) Drainage galleries (u) Grout galleries
The intermediate structure extends from the top of the draft
tube to the top of the generator foundation. It houses the following:
(i) Turbine including its casing
(ii) Galleries for the auxiliary machines
(iii) Governor servo-motor system.
The turbine flour is below the generator floor and is accessible
through stairs from the generator floor.
The super structure is the portion extending from the generator
floor called th main floor up to the rooftop.
It houses the following
(i) Generators (ii) Governors
(iii) Control room (iv) Exciters
U') Auxiliary equipment. Such as needed for
(a) ventilation (b) cooling
(vi) Main travelling gantry crane at the roof level.
(vii) Control room (viii) Offices and stores.
2. Power house dimensions. The super structure of the power
plant has the following three bays.
(i) Machine hail or unit bay (ii) Erection or loading bay
(iii) Control bay.
Machine hail size depends on the number of units, the distance
between the units and size of machines. The machine hall must have
HYDRO-ELECTRIC POWER PLANT 487
a height which will enable the cranes to lift the rotor of the generator
or runner of the turbine clear off the floor.
The loading bay is used to load and unload the vehicles and
where dismantled parts of the machines can be placed and where
small assembling of the equipment can be done.
The control bay houses the main control consisting of control
switches, panels etc. The control bay should be quite spacious.
3. Cables and Bus Bars. High voltage and low voltage cables
should be carried separately cables and bus bars are placed in cable
ducts provided in the floor of the generator or placed in the bus bar
galleries.
4. Operation room. The operat m room may be located inside
the turbine room. The instructions are sent to the operation room
from the control room. The operation room is the centre from where
the machines are controlled and switch gear operated.
5. Miscellaneous equipment. Proper planning for the follow-
ing should be carried out
(i) Transformers (ii) Service cranes
(iii) Lighting (iv) Ventilation.
5.47 Under ground power plants
They are safe against earth tremors, rock slides and snow
avalanches. The various factors which affect the choice are as
Ibilows
(i) Rock quality (ii) Tunneling ease
(iii) Over all economy.
An aesthetically significant advantage offered by an under-
ground power plant is the preservation of the natural land scape
features. The surface power plants would necessitate the deforesta-
tion, interference with natural landscape on account of the material
transportation and constructional activities.
6.48 Components of underground power plant
The various components of an underground power plant are as
follows
(i) Machine hail It houses the turbines and generators
(ii)Transformer hail
(iii)Control room
(iv) Erection bay : It is used for the assembly of rotor stator. It
is also used to serve as repair bay.
(v)Cable gallery
(vi) Valve c/iarnbt'r: It is used to house control valves
488 POWER PLANT
—33
490 POWER PLANT
A Cu = 0.986
Solution.
H = Head = 340 m
P = Power = 9.5 x 10 kW
C, = Coeff. of velocity = 0.986
- V1 = Velocity of jet
= Cu 'J
= 0.986 Ix
9.81x 340 = 80.53 mIs
V2 = Velocity of wheel
= Speed ratio x
= 0.48 x 12-x - -8- 9.
1 x3 4 0 3
= 9. 2 mIs
N= RPM 740
D = Wheel diameter
itDN
V2
60
- it xD x 740
D = 1.01 m
d = Jet diameter
= x D = x 1.01
=0.168m
n = Number of jets required
q = Discharge throughout jet
= x d2 x V1 = x (0.168)2 x 80.53
= 1.78 m3/sec
TI = Overall efficiency = 0.87
P
Ti
Water
- 9500
W.Q.H
where w = Specific weight of water
08 P
9.81x0.23x43
P = 77.6 kW
MS = specific speed
N.'48Ox'fi
- - 435/4 -38.4
P1 =4512kW -
Number of Francis turbines required
P 77224
P 1 4512'
= 17,,1 = 18 (say)
(b) For Kaplan turbine
VP
N3-N
H514
710 - 250VP
- 30
P2 = 32618 kW
Number of Kaplan turbines required
77224
32618 = 2.36 = 3 (say).
Q = Q x 3.43
= 16 x 3.43 = 55 m3/s
P 1 = Firm power with pondage
= P x Pondage factor
= 1506.8 x 343 = 5168.3 kW
Pondage = (24 - 7) 17 hours flow
= 17 x 60 x 60 x Q
17 x 60 )< 60 x 16
= 9.8 x io m3.
Example 6.27. (a) A run of river plant is used as a peak loud
plant with weekly load factor of 26% all the capacity being firm
capacity. Determine the nzini,nuni flow in river so that power plant
may act as base load plant when rated installed capacity is 12 MW
and operating head is 17 in with plant ef ficiency 85%.
494 POWER PLANT
(b) Also determine the laity load factor when stream flow is
16 m3/sec.
Solution.
(a) C = Capacity of plant = 12 MW
H = Head = 17 m
r = Plant efficiency = 85%
Load factor = Average load
Maximum demand
0.26 = Average load
12 x 1000
Average load = 3120 kW
E = Electrical energy generated in one week
= Average load x 24 x 7
=3120x24x7=52x 104 kWh
P
Now ii =
where P = Power developed
P
0.85
P = 141.75 Q kW
E 1 = Tot! energy generated in one week
=Px24x7
= 141.75 x 24 x 7 x Q
= 23814 x Q kWh
Now E=E1
52 x iO = 23814 x Q
Q = 21.8 m3/s
(b) When Q = Flow rate
= 16 m3/s
P 1 = Power developed = 141.75 x 16
= 2268 kW
= Energy generated per day
= P1 x 24
= 2268 x 24
HYDRO-ELECTRIC POWER PLANT 495
= 54432 kWh
Average load
Daity load factor -
- Maximum load
- 54432
= 0.19 = 19%.
- 24 x 12 x 1000
PROBLEMS
7.0 Introduction
Gas turbine power plant has relatively low cost and can be
quickly put into commission. It requires less space. This plant is of
smaller capacity and is mainly used for peak load service.
Gas turbine power plants are very promising for regions where
liquid or gaseous fuel is available in large quantities. Gas turbine
installations require only a fraction f water used by their steam
turbine counterparts Gas turbine has made rapid progress during
the past decade due mainly to the large amount of research. The size
of gas turbine plants used in a large System varies normall y from
10 to 25 MW and the largest size used is about 50 MW. The thermal
efficiency of gas turbine plant is about 22% to 2511.
In our country it may be expected that by 1995 installation of
medium and large size combined cycle plants (CCP) will pick up and
gas turbines will record a faster growth rate. In C.C.P. plants
atmospheric pollution by fly ash will be corresponding lower, cooling
water requirement will be reduced combined cycle gas based power
plants are more economical than coal based power plants as coal
transportation was exorbitantly expensive. Moreover the gas based
power plant has the shortest gestation period as it could be put on
stream in barely two years. In any other system it takes at least five
years to commission a project. More gas power plants would ensure
utilisation of natural gas.
7.0 (A) : Classification of Gas Turbine Plants
Gas turbine plants-may be classified according to the following
criteria
1. Type of load:
(a) Peak load plants (b) Standby plants
(c) Base load plants.
500 POWER PLANT
2. Application:
(a) Aircraft (b) Locomotive
(c) Marine (d) Transport.
3. Cycle.
(a) Open cycle plants (b) Closed cycle plants.
4. Number of shafts:
(a) Single shaft (b) Multi-shaft.
5. Fuel:
(a) Liquid (b) Solid
(c) Gas.
OIL
M1P..JI
Fig. 7.1
GAS TURBINE POWER PLANT
501
Turbine. Turbine drives the compressor and the load. Both
impulse and reaction turbines can be used in gas turbine plants. As
compared to steam turbines gas turbines have few stages because
they operate on smaller pressure drops.
Axial flow type turbines are commonly used. The various re-
quirements of turbines are as follows:
(i) Light Weight
(ii) High Efficiency
(iii) Reliability in operation
(iv) Long working life.
Combustion Chamber. In the combustion chamber, combus-
tion of fuel takes place. The combustion process taking place inside
the combustion chamber is quite important because it is in this
process that energy, which is later converted into work by the
turbine, is supplied. Therefore, the combustion chamber should
provide thorough mixing of fuel and air as well as combustion
products and air so that complete cbmbustion and uniform tempera-
ture distribution in the combustion gases may be achieved. Combus-
tion should take place at high efficiency, because losses incurred in
the combustion process have a direct effect on the thermal efficiency
.of the gas turbine cycle. Further the pressure losses in the combus-
tion chamber should be low and the combustion chamber should
provide sufficient volume and length for complete combustion of the
fuel.
Initially the temperature developed in combustion chamber is
too high. The difficulty is avoided by adding a satisfactory amount
of air to maintain stable combustion conditions and then the
products of combustion are cooled to a temperature suitable for use
in gas turbine by introducing secondary air. The sum of primary and
secondary air supplied is total air needed for combustion. Fig. 7.2
shows the combustion chamber. In combustion chamber used for
aircraft engines a large quantity of air is used to keep the tempera-
ture of combustion chamber to about 650°C. The air fuel ratio may
be of the order of6O: 1 in this case.
74-
SECONDARY AIR
AIR
M8USTIOW
/ CHAMBER
FVEL Oil.
Fig. 7.2
52 POWER PLANT
iii) Air ratio. It is defined as the amount of air (in pounds or kg)
entering the compressor inlet per unit of network output of the
turbine.
The size of gas turbine plant is dependent on rate of flow of air
in relation to the useful horse power output. Lower the air rate
smaller will be the size of plant. Inter cooling and re-heating reduces
the air rate. An increase in the compressor and turbine efficiencies
will decrease the air rate. An increase in compressor inlet tempera-
ture will decrease the net output of the turbine and hence will
increase the air rate.
(iv) Pressure ratio. It is defined as the ratio of absolute pressure
at the compressor outlet to the absolute atmospheric pressure at
compressor inlet.
(u) Compression efficiency or machine efficiency. This term is
related to the compressor, and is defined as the work required for
ideal compression to the actually required by the compressor for a
given pressure ratio.
Actual work required by the compressor is always more than
the ideal work.
Air rate or Air ratio is a criterion of the size of the plant, i.e. the
lower the air rate the smaller the plant. From the mechanical and
metallurgical point of view the lowering of the air rate results in
turbines of smaller physical dimensions with a more a nearly
uniform temperature distribution. The work ratio acts as a guide in
the determination of the size of gas turbine. If the work ratio is high
the variations in the compressor and turbine efficiencies will have
less effect on the thermal efficiency of the cycle than ifthe work ratio
is low. A plant with a high work ratio will have higher part load
performance efficiency than a plant with a low work ratio.
7.3 Engine Efficiency or Turbine Efficiency
It is defined as the ratio of net output of the turbine to the power
that should be ideally produced by the turbine. Network output of
the turbine is always less than ideal output.
Ideal conditions mean : (1) that compression and expansion
processes are isentropic ; (2) that no losses occur in combustion
chambers, heat exchangers, inter-coolers, and pipes connecting the
different components (3) that heat transfer in heat exchangers is
complete, that working fluid behave as perfect gas with constants
specific heats ; and (4) rise in temperature on cold side is equal to
drop in temperature on hot side.
U
04 POWER PLANT
6i4SOUT . GAS /N
Fig. 7.4
AIR
INTER I REGENERATOR
COOLER
Fig. 7.5 (a)
B AF FLES •
"AM COOLANT
OUT
1Ia•u_ _I.t
"TUBE PLATE
1'T(J8E5 COOLANT
END COVER
IN
Fig. 7.5 (b)
Fig. 7.6
LOAD
WATER
COOLER
AREEERATOR
COMBUSTION
CHAMBER
Fig. 7.7
Some of the gases used in closed cycle gas turbine plant are as
follows
(i) Helium (He) (ii) Krypton (Kr)
(iii) Hydrogen (112) (iv) Oxygen (02)
(v) Nitrogen (N2) (vi) Carbon-dioxide (CO2)
(vii) Ammonia (NH3) (viii) Methane (CH4)
(ix) Ethylene (C2114)
7.9 Some Other Possible Arrangements
Some other arrangements of open cycle system areas follows:
(i) Simple Open Cycle—Twin Shaft. In this arrangement air
enters the compressor (C) and after being compressed it flows to
combustion chamber. The gases then expand in the turbines (T).
The exhaust of burnt gases takes place in the atmosphere (See Fig.
7.8).
4
GAS TURBINE POWER PLANT 509
Fig. 7.8
(ii) Inter Single Shaft Open Cycle. The air from low pressure
compressor (L.P.C.) flows to inter-cooler and then to high pressure
compressor (H.P.C.). The high pressure compressor delivers the air
to combustion chamber (C.C.). The gases then expand in theturbine
(Fig. 7.10).
WATER
Fig. 7.9
Fig. 7.10
Fig. 7.11
CHAMBER
Fig. 7.12
poller rotates the air enters axially and leaves radially. When the
impeller rotates the pressure in the region R falls and, therefore,
the air enter through the eye. The air then flows radially outward
through the impeller blades. After that the air flows through the
converged passages of diffuser blades and finally the air flows to
compressor outlet (Fig. 7.13).
DAPFM
8.A DES
4fPEW
PLAT1
IMPELLI
BLADE.-
Fig. 7.13
Fig. 7.14
N Cw-esso'i
I AIR
INTAKE
I
CYUNDER
RECEVtR
TURBINE
EXW.WS1
Fig. 7.15
GAS TURBINE POWER PLANT 513
ward moment of pistons. Each piston acts as a single stage air
compressor on its inner face and as an air bounce cushion on its
outer face. During outward movement of pistons some energy is
stored in bounce cylinder. The energy is utilised for causing inward
movement of pistons which compress the air in air cylinder and
diesel cylinder. Air at a pressure of about 75 to 100 p.s.i., flows from
compressor cylinder into central air space and then it enters the
diesel cylinder through intake ports. The mixture of air and com-
bustion gases at about a temperature of 1000°F leave through
exhaust ports to the turbine where these gases are expanded to
atmospheric pressure.
The advantages of the system are:
(i) As there are no unbalanced forces and no side forces on
cylinder wall, the engine is vibration free.
(ii) The system is smaller and lighter than a diesel engine of
the same output. Thermal efficiency higher than that of
diesel engine and nearly 40% is obtained in this system.
(iii) As compared to open cycle gas turbine system the size of
this system is about one third the size of open cycle plant.
(iv) Air rate is lower in this system.
The main disadvantages of the system are being its difficult
starting and control.
7.14 Advantages of Closed Cycle Gas Turbines
The various advantages of closed cycle gas turbines are as
follows:
1. As the working fluid does not mix with the products of
combustion, therefore, it is possible to use a gas of higher
density and higher specific heat than air such as krypton,
argon, xenon etc. This will reduce the size of various
components. Helium has been successfully used as work-
ing medium in closed cycle gas turbines. The specific heat
of helium at constant pressure being nearly five times that
of the air so heat drop and hence energy dealt per kg of
mass flow is about five times in turbines using helium as
working medium, as compared to gas turbine using air.
Heat exchanger used in gas turbines using lum as
working medium has a surface area of about I that of heat
exchanger used in gas turbines using air as working
medium. Therefore, the size of helium unit is comparative-
ly smaller.
2. As the working medium does not mix with the product of
combustion so there is no accumulation of carbon deposits
on blades and nozzles of the turbine. The compressor
remains free of dust as the working medium may be
514 POWER PLANT
Disadvantages
1. Part load performance is low. This can be improved by
using inter-cooler and reheater.
2. Reduction in component efficiencies lowers the thermal
efficiency of the cycle.
3. The gas turbine in open cycle requires a large quantity of
air.
7.16 Relative Thermal Efficiency at Part Load
The relative thermal efficiency at part loads for various cycles
assuming full load ther. 1 o fficiency of each cycle is 100% as shown
in Fig. 7.16.
ac
tOADY. -
Fig. 7.16
2.
pressure in the diffuser. The air is then compressed in the compres-
sor to a pressure of about 3.5 kg/cm The compressor used is
generally radial or axial type. The air is then supplied to the
combustion chamber. The liquid fuel is injected into the combustion
chamber where its combustion takes place. The hot gases expand in
the turbine. The turbine extracts enough energy to drive the com-
pressor and the necessary auxiliary equipment. The hot gases are
then expanded through exit nozzle and they leave the nozzle at high
velocity and cause a momentum due to which the engine exerts a
forward thrust (Fig. 7.17.).
COMPRESSOR WMtJ I
CHAMBER
AIR
00000000
fti11 iiI i_0 0 0 00 000
- -
_- EXHAUST
0 0 0 0 000 GASES
000000
FUEL NOZZLE
DIFFUSER
Fig. 717
the heat exchanger and the hot air flows to the combustion chamber.
Products of combustion are expanded in the high pressure turbine
and then in low pressure turbine.
7.22 Advantages of Gas Turbine Over Steam Turbine
The various advantages of a gas turbine over a steam turbine
are as follows
L.P. TUP.SI,VE
AIR FILTER r
INTER
COOLER
-
'TARTIAn
MOTOR ALTERNATOR H.P
If-
- H.P I COMBU.snOlv
COMPRESSOR URBINE I CHAMBER
-. Fig. 7.18
(i) Its operation is simple and it can be quickly started
(ii) Its initial and maintenance costs are low.
(iii) It requires few parts and their design is simple.
(iv) It has low weight-power ratio.
(u) Its lubrication cost is low.
(vi) Maximum operating pressure is about 6 kg/cm 2 , therefore
the material is not subjected to heavy stresses. However
due to high temperature of gases (nearly 900C) the
material used should be able to withstand it.
(vii) In gas turbine the inlet temperature is about 806C
whereas it is about 500 C C in case of steam turbine. There-
fore, thermal efficiency of gas turbine is more than steam
turbine other things being equal in both cases.
7.23 Gas Turbine Cycle Efficiency
Gas turbines may operate either on a closed or on an open cycle.
The majority of gas turbines currently in use operate on the open
cycle in which the working fluid, after completing the cycle is
exhausted to the atmosphere. The air fuel ratio used in these gas
turbines is approximately 60: 1.
The ideal cycle for gas turbine is Brayton Cycle or Joule Cycle.
This cycle is of the closed type using a perfect gas with constant
Constant
Adiabatic I
pressure
I-I
LA
I'.,
Vol urn e Entropy
Fig. 7.19 Fig. 7.20
.m
our
a
GHAIA1D
COMPRESS"
Fig. 7.22
'T I
PRESSURE
LIMCS
HeAT
Fig. 7.23
POWER PLANT
522
1 - K(Ti-Ts)
For isentropic compression and isentropic expansion thermal
efficiency is given by
r I: K(Tl-T5)
t T4 = (F4
T 3 T3Pa
y = 1.4 for air
Fig. 7.24 14 - 11/i4
74
= T3[]= 29O[
= 5OOK
(y-1y
T2 P2
Ti Pi
L2 - 1)/i [ 1.4 - I)/1.4
, T2 T, [ 973
T i 6
= 554'K
Compressor work = K (T4 - Ts) = 0.24 (500 - 290)
= 50.4 kcal
(Assuming K = 0.24)
Work done by turbine = K (T i - T2)
= 0.24 (973 - 554) = 100.56 kcal
Net work done = 100.56 - 50.4 = 50.16 kcal
GAS TURBINE POWER PLANT
$23
Heat supplied = K (Ti - 7'4) = 0.24 (973 - 500)
= 0.24 x 473 = 1135 kcal.
Cycle efficiency ('1) = Net work done -
Heat supplied - 113.5
= 0.44 = 44%
Work ratio = Net work done
----- = 50.16 0.49
Work done by turbine 100.56
Specific work output = 50.16 kcal
= 50.16 x 426.94 = 21,415 kgfm/kg.
as (1 kcal = 426.94 kgfm)
7.26 Combined Working of Gas Turbine Plant and
Steam Power Plant
When a load is to be supplied by both steam power plant and
gas turbine power plant then the base load is supplied by steam
power plant and peak load is supplied by gas turbine power plant.
The size of gas turbine plants used in a large system varies normally
from 10 to 25 MW and largest size used is about. 50 MW. A gas
turbine plant can be started quickly and has a short starting time
as compared to steam power plant. Gas turbine plants are par-
ticularly useful and economical where cost of gis is not excessive.
The capital cost of gas turbine power plants is less as compared to
steam power plant of equal size. The fixed charges of gas turbine
power plants are also lower than those of steam power plant of same
size.
7.27 Gas Turbine Power Plants in India
Gas turbine power plants are quite helpful in meeting the
growing power demand of the country with the minimum capital
cost-
Some of the gas turbine power plants in our country are as
follows
(a) Gas turbine power plant in Namrup. This power plant
is located at Namrup in Assam. it is of 70 MW capacity.
(b) Uran gas turbine power plant. This power plant is of 240
MW (60 x 4) capacity and is located at Uran in Maharashtra.
(c) Auraiya Gas power plant. This is India's largest combined
cycle module having 652 MW capacit y . It supplies power to the
northern gid. It is situated in Uttar Pradesh. It has been con-
structed by NT.P.C. India's largest public sector power utility in the
field of power generation and transmission. Th Mitshubishi Heavy
POWER PLANT
524
;Industry of Japan had collaborated with N.T.P.C. in the construc-
tion of this prestigious project.
PROBLEMS
7.1. What are the essential components of a simple open cycle gas of
turbine plants ? How intercooling and regeneration help in
improving thermal efficiency of the plant?
7.2. Describe a closed cycle gas turbine plant. What are the ad-
vantages of closed cycle?
7.3. What are the advantages and disadvantages of gas turbine
power plant? Discuss the applications of such plant.
7.4. What are the various(actors to be considered while selecting the
site for gas turbine power plant?
7.5. Give the layout plan of gas turbine power plant.
7.6. What methods are used to improve the efficiency of gas turbine?
7.7. What are the various compressors used in gas turbine ? State
their relative advantages and disadvantages?
7.8. Explain free piston gas generator turbine system?
7.9. What are the requirements (Qualities) of fuel used in gas tur-
bines'? Compare kerosene and gasoline as fuels.
7.10. State the principle ofjet propulsion. Describe a turbojet engine.
7.11. Write short notes on the following:
(a) Pressure ratio
(b) Semi-closed cycle
(c) Specific thrust of turbo-jet engine.
(d) Relative thermal efficieicy at part loads of various ga tur-
bine cycles.
7.12'(a) Define work ratio.
(b) Which is better, a high or low work ratio? Why?
7.13. Compare a gas turbine with a steam turbine?
7.14. Define air rate. Does a low air rate increase or decrease the size
of an engine?
7.15. List the five operating variables that strongly effect the thermal
efficiency of an open cycle g isturbine.
Solution. The thermal efficiency of an open cycle gas turbine is
heavily dependent upon the following operating variables:
(i) Pressure ratio
(ii) Turbine efficiency
(iii) Turbine inlet temperature
(iv) Compressor efficiency
(u) Atmospheric or compçessor inlet air temperature.
-.1
•
• I ••tst.'
- -.
% •1' -
a
LIJ
Instrumentation
8.0 Introduction
In every power station different t ypes c,f instruments are used.
They measure pressure, temierature and flow etc. in the plant. The
various functions of such instruments can be summarised as follows:
(i) They provide guidance to operate the power plant effi-
ciently and economically.
(ii) They can be used to checkthe internal conditions of the
equipment and thus provide maintenance guidance.
(iii) The y enable economical supervision.
(iv) The y -hell) in plant performance calculations.
(v) They help in costs accounting and cost allocations.
8.1 Classification of Instruments
The various type of instruments can be divided in t o two
categories as follows:
(i) Electrical Instruments.
(ii) Mechanical Instruments.
Elec'trical Instruments. Electrical instruments include am-
meters, voltmeters, wattmeters power factor meters, ground detec-
tor and reactive voltampere meters.
Mechanical Instruments. Mechanical instruments used for
various purposes are of the following types.
8.2 Measurement of Pressure
Instruments known as gauges are used to measure pressures
The various gauges used are as follows:
(i) Barometers
(ii) Manometer gauges
(iii) Vacuum gauges
(iv) Pressure gauges.
A barometer is a device for measuring atmospheric pressure.
Manometers are used to measure pressure below or above atmos-
pheric pressure. ti-tube manometers used for measuring pressure
INSTRUMENTATION 527
Pat
Fi
0
528 POWER PLANT
zo;'^
box
—0— _^ ^-^ I Indicator
I I Flexible
_ jocouie
II auxiliary
couple
Hot
junction
Furnace
Ground
Pipe
L Cold junction
Fig. 8.4
INSTRUMENTATION
52S
(iii) Glass tube mercury thermometers. They are used to measure
temperature of feedwater, condensate, circulating water and bear-
ing oil etc.
8.4 Flow Measurement
The various flow meters used measured flow rate areas follows:
(i) Steam flow meters. They are used to measure steam output
of boilers and turbine supply etc.
(ii) Water flow meters. These are used to measure feed water
condensate and pump discharge.
(iii)Airflow meters. Rate of flow of water is generally measured
by a venturi meter. Fig. 8.5 shows a venturi meter, a simple device
operating on the Bernoulli's principle. It consists of two tapering
lengths of pipe A and B interconected by a cylindrical part C. The
diameter of the wide ends is equal to that of the pipe in which the
rate of discharge is being measured. On the cylindrical parts
piezometric tubes Ti and T2 are fixed. As the water flow from end 1
to end 2 a difference between water level (h) in the PiezometerS is
obtained.
1i Y21
I
hf
1 I .p - _
I
rç11
A iC 8
Compression
cylinder
U,
0
E
To drain
Fig. 8.6
INSTRUMENTATiON
531
ELECTRICAL
CONTROL
TURBINES
AND
cONTROl. _f L / I 1
AUXiLIARIES._1-[IIJ LI: [IIJ4OPERATORS
AUXIUARI
-
534 POWER PLANT
Fig. 8.7
This apparatus as shown in Fig 8.7 consists of levelling bottle
A, measuring burrette B and three absorbing pipettes, C, D and E.
The pipettes C, D and E contain respectively solutions of potassium
hydroxide for absorption of CO2 , pyrogallic acid for absorption of
02 and curous chloride for absorption of CO. These pipettes
provided with stop cocks, K1 , K2 and K3 respectively. The
connects the apparatus to the flue gas.
100 cc. of flue gas sample is filled in the measuring burrette
lowering the levelling bottle A. The stop cock Ki is opened and by
• adjusting the bottle A the flue gas sample is transferred to pipette
C wherç CO2 is absorbed. The remaining gas is brought back to
measuring burette B and Volume measured. The difference between
original volume (100 c.c.) and this volume is the volume of CO2.
Again flue gas is transferred to pipette D where 02 is absorbed. The
remaining gas is brought back to B and volume measured. Dif-
ference of two volumes is the volume ofO 2 . Finally gas is transferred
to pipette E where CO is absorbed. The gas is brought back to
measuring burette B and volume measured. Difference in volumes
is the volume of CO. when percentage of CO2, 02 and CO are known,
the remainder of the gas is assumed to the nitrogen.
During a test of boiler performance flue gas samples are
analysed periodically to find the contents of CO2, 02, CO and N2.
8.15 Oxygen Meter
The presence of dissolved oxygen in feed water for boiler is
responsible for the corrosion of boiler tubes and impairs the perfor-
mance of condenser. The deaerating system is included in the plant
INSTRUMENTATION 535
-- Meter
Cool In
water
g1 Cat0nt
head dtvice To
T d.c.
mains
H
ritice_'L.,,
Drain
Fig. 8.8
Fig. 8.8 shows a dissolved oxygen meter. In this meter the
difference in thermal conductivity of pure hydrogen gas is compared
with that of a mixture of hydrogen and oxygen. Hydrogen enters
from the right chamber and displaces some of the ox ygen in the
sampled water. Consequently the required conditions for instru-
ment based on the principle mentioned above are fulfilled.
8.16 Impurity Measuring Instruments
The feed water used in a boiler to generate steam may consist
of the following impurities
(i) Calcium sulphate (CaSO4) and other sulphates
(ii) Sodium chloride and other chlorides
(iii) CO 2 from evaporators
(iv) Metallic pieces picked up by steam while passing through
pipes
(v) Silica from dust etc.
(vi) Oxygen from air in condensers etc.
These impurities should be kept to the minimum.
Fig. 8.9 shows dionic water purity meter. The principle used in
the meter is that the electrical conductivity of an electrolyte dis-
solved in water depends on the amount of salt in solution i.e. the
extent of impurity. The resistance between the opposite faces of a
cube of standard water in the instrument is compared with the
resistance when the water contains more impurities.
536 POWER PLANT
Temp. c
bimetal
Insulating
tube
CAM m ow
Collar
(-v.a)
flow at water
sample
Fig. 8.9
I Gas I I! UL6 To
- IL__..JI Rccord
—rr----- cr
A C.Mairis
Fig. 8.10
Photoc11
Duct qr
Power PcordQr
f:)jy TT ArnptItQr
Lamp tor
U
Fig. 8.11
PROBLEMS
-36
538 POWER PLANT
(a) Pressure
(5) Temperature
(c) Steam flow.
8.3. Write short notes on the following:
(a) Hay's CO2 recorder
(b) Selection of instruments.
8.4. Explain area system and centralised system for the arrange-
ments of instruments and controls in a steam power plant.
8.5. Describe any three controls used in steam power plant.
8.6. Explain how a venturi.meter is used to measure rate of water
discharge in a pipe.
8.7. Describe Orsat apparatus used for flue gas analysis.
8.8. Describe oxygen meter.
8.9. Sketch and describe the feed water impurity measuring instru-
ment.
8.10. Sketch and describe the photo-cell type smoke meter.
8.11. Sketch and describe the reflected light dust recorder.
Miscellaneous Problems
power station but this would be offset by factors like higher efficien-
cy and improved cycle of operation.
Working. The various components of MHD generator are
shown in Fig. 9.1. The hot ionized
T SONISED
gas passes between the poles of an
6A electro-magnet and induces a
1 potential difference between a
pair of electrodes which are at
j right angles of magnetic field and
a current starts flowing in the
MAG LOAD resistive load connected between
(uels and air. Although the conventional (or nuclear) steam power
plant is still used in large-scale power-generating systems, and
conventional piston engines and gas turbines are still used in most
transportation power systems, the fuel cell may eventually become
a serious competitor. The fuel cell is already being used to produce
power for space and other special applications.
Advantages -
1. It is simple.
2. It has high power to weight ratio.
3. Theoretical efficiency as high as 90 (7 can be expected but
it is possible only at light loads.
Disadvantages
1. Its cost is high.
2. It has relatively short life particularly at high tempera-
tures.
3. It is very essential to select proper materials for com-
ponents so that the reaction cannot attack them.
The hydrogen and oxygen for operating the cell are stored in
liquid form to minimise the volume occupied. The Hydrox (H 2, 02)
cells are of two types.
(i) Low temperature cell. In this cell the temperature of
-1 rtrolyte is 90 ' C. The electrolyte may be pressurised up to four
atmospheres.
(ii) hg" pressure cell. In this cell the temperature of
electrolyte is anout 300'C and it is pressurised up to 45 atmospheres.
Depending upon the type of fuel used the fuelcells are classified
as follows : (a) Hydrogen (H 2) fuel cell ; (b) Hvdrozine (N2 H4) fuel
cell (c) Hydrocarbon fuel cell ; (d) Alcohol (Methanol) fuel cell.
Fuel cells are particularly suited for low voltage and high
current applications.
9.3 The Indian Electricity Act 1910
Some extracts of the Indian Electricity Act are as follows:
Definitions
(i) Area of supply. It means the area within which alone a
licensee is for the time being taken authorised by this licence to
supply energy.
(ii) Consumer. Consumers means any person who is supplied
with energy by a licensee or the government or by any other person
engaged in the business of supplying energy to the public under this
Act or any other law for the time being in force and includes any
person whose premises are for the time being connected for the
MISCELLANEOUS PROBLEMS •543
qt
TURBINE
PUMP .. 7E",
Fig. 9.3
MISCELLANEOUS PROBLEMS 549
P RATION
—lc_ f
7,
I \EPAN5I01V
4-
V —a-
S —'-
Fig. 9.4 Fig. 9.5
9.5.3 Reheat Cycle
In this cycle steam is extracted from a suitable point in the
turbine and reheated generally to the original temperature by flue
gases. Reheating is generally used when the pressure is high say
above 100 kg/cm'. The various advantages of reheating are as
follows
Fig. 9.6
(i) It increases dryness fraction of steam at exhaust so that
blade erosion due to impact of water particles is reduced.
(ii) It increases thermal efficiency.
(iii) It increases the work done per kg of steam and this results
in reduced size of boiler.
The disadvantages of reheating are as follows:
(i) Cost of plant is increased due to the reheater and its long
connections.
(ii) It increases condenser capacity due to increased dryness
fraction.
Fig. 9.6 shows flow diagram of reheat cycle. First turbine is high
pressure turbine and second turbine is low pressure(L.P.)- turbine.
This cycle is shown on T.S (Temperature entropy) diagram (Fig.
9.7).
550 POWER PLANT
-,- S
Fig. 9.7
(Hi -H2)+(H3-H4)
Efficiency
- H 1 + (H3 - H2) - HL4
where = Total heat of steam at 1
Hi
H2 = Total heat of steam at 2
H3 = Total heat of steam at 3
H4 = Total heat of steam at 4
= Total heat of water at 4.
HOT
WELL.
Fig. 9.8
RCLcv
TLIR5INE
S TEAM
TURBINE
MERCUR',
SOiL ER
TER
I EXCHANGER
Fig. 9.9
552 POWER PLANT
Heaters
Fig. 9.10
iO
127-41.1
=0.870.16 kg.
ui T y pe of fuel available
( it) Type of load to be supplied
(iii) Reliability of operation
(iv> Cost of land
v) Cost of fuel transportation
(j) Availability of cooling water
(vii) Cost of power transmission.
2. Location of Power Plant. It should be installed near the
load centre so that the cost for transmitted power is reduced. It
should be nearer to source of fuel and sufficient amount of water
should he available near the power station. The soil should be such
that special and costly foundation is not required. The plant site
should he accessible by road or railway line so that the transporta-
tion of equipment is easy.
3. Building for a Power Plant. The power plant building
should be simple, rugged and should have pleasing appearance. The
size, arrangement and shape of power plant depends upon the type
of power plant. The roofs are made usually flat. The roof deck can
be carried on reinforced concrete s1a)s and beams. The floors may
be made up of concrete or tiles. Concrete floors as preferred. The
structure should be fire proof. While laying out the various equip-
ment allowari.ces should he made for sufficient clearance and
walkway s. Some space should be left for future expansion. The
rooms of the building should be spacious, uncrowded, well lighted
and clean.
4. Selection of Prime Mover. Depending on the load and type
of power stations, the selection ofsteaun turbine, hydraulic turbines,
.boilers, diesel engines, gas turbiies should be made. The units
installej should have capacity more than the peak load and some
provisions should be made Tor future expected load. For example the
peak load of one city is 36 MW. Then two units each of 20 MW or
four units each of 10 MW could be used keeping in view the future
load.
Heat transfer is the primary function of the boiler. It should be
capable of utilising the heat of the combustion of fuel to a great
extent. In central power stations water tube boilers are preferred.
Coal fired boilers have higher efficiency, than boilers using oil or gas
as fuel because hydrogen loss is more in gaseous fuels. Pulverised
fuel is preferred in case of low ranking fuels such as lignite etc. The
cost of boiler depends upon operating pressure, operating tempera-
ture, type of firing and efficiency desired. Higher pressure requires
forced circulation. For higher temperature superheaters are needed
and, therefore, cost becomes high. The system used for coal tiring in
the boiler also influences the cost of boiler. Stoker firing is cheaper
than pulverised fuel firing. The efficiency of boiler is increased by
MISCELLANEOUS PROBLEMS
557
9.7 Blo-Gas
The most important sources of organic waste for the production
of bio gas in India is cow-dung and agricultural wastes. The cow-
clung and agricultural waste are used extensively as direct sources
of e tiergv in rural meas. The development of the technology for
hio . gas production from organic wastes to preserved their manurial
value and at the same timQ to provide the rural area with a
substitute source of energy has been recognised. Indian has about
237 million cattle population and if the entire dung field from the
cattle population is utilized for the hio gas production in an opt nuin
manner, the annual gas availability would be about 66,000 million
in s . Agricultuial wastes have the capcity to produce a lot more gas
than cow-dung A kilogram of paddy straw can produce about six
cubic feet of a ga as against a kilogram of cow-dung which call
t)rodli('e about 1.3 cubic teed of gas. in a 1)10-gas plant apart from the
gas that is produced, enriched mnamuire is also obtained.
A number of institutionS have played a significant role in thd'
development (it technology of hio-gas production. The Khadi and
village Industries Commission has played It ke y role in popularmang
the installation of Gobar Gas plants . i n the country.
The program inc of hio-gas as being i in plemented now in I ud i a
is oriented towards establishing mairill, small size plants to serve
the needs of individual families. To achieve maximum econoniv as
also for accelerating the development of bio-gas potential it is
considered 1imt large size ofbio-gas plants should be established for
serving the whole village community in a village. Some of the
institutionS carr ying out research on bio-gas technology are as
follow -
(I (obar Gas Research centre of Khadi and Village In-
dustries Commission.
I ridian Agricultural Research Institute, New Delhi.
National Environmental Engg. Institute, Nagpur.
One of the main advantages ot'street lighting or home lighting
with bio-n is that the entire process will he simple with absolutely
no recurri ig expenditure Also in case of bio-gas system failure the
villagers themselves will be able to rectify the fault. Further the
same gas th. is used for cooking can after a simple pro cess of
MISCELLANEOUS PROBLEMS 559
C3 1
CL
cj IZ
Io
I-
a.
Q
U,
C
.-
0
0
x 0)
-I U-
a
a.
POWER PLANT
562
House Lighting
Better -- Cooking
[SanitationJ
BioBiogas Water -- pumping
Plant jEnergy
Water heating
be used as base load plant and steam power plant should be used as
peak load power plant. If the amount of water available is less at
hydro plant then the steam power plant should supply the base load
and hydro-plant should act as peak load again. Diesel power plants
are generally used as as peak load plants.
When pumped storage plant is used in combination with steam
power plant then pumped storage plant is used to supply sudden
peak loads of short duration. The advantages of pump storage plant
in an inter connected system are as follows
(a) It stores the energy using off peak energy of thermal plant
and the same is supplied during demand.
(b) It minimises wastage of off-peak energy of steam power
plant.
(c) Use of pumped storage plant helps in loading economically
the steam power plant. During coordination of hvdro
power plant and gas turbine power plant the gas turbine
power plant is used peak load plant. The high working cost.
of gas turbine plant is compensated b y lower fixed cost and
lower operating and maintenance cost.
Inter connected power system can provide large savings both in
capacit y and fuel cost at the same time ensuring reliability and
contmuit y ot'jmwcr supply. The main purpose oiiter-connection IS
to distribute the load among the interconnected power plants system
ill to achieve the overall economy.
The various advantages of combined working of different types
ot power plants are as follows
(a) There is a reliability of power supply to consumers be-
cause in the event of power failure at one of the power
plants the system can be fed from other powers plant to
avoid complete shut down.
(b) The spinning reserve required in a power system in
reduced.
Combined working of different types of power plants
reduces the amount of generating capacity required to be
installed as compared to that which would he required
without inter-connection.
The inter-connection of various power plants helps in
reducing the amount of generating capacity to he in-
stalled.
' In an inter-connected system the overall cost of energY is
less
54 POWER PLANT
4
3:
4
K
Fig. 9.11
Power plant
-
A
-__
- - Nr
Ru n off river plant
power plant
H ydro,werp!tnt with sut1icient stor ag-
.. -
Uj
Fig. 9.12
IOC
Fig. 9.13
566; POWER PLANT
PROBLEMS
10.1 Introduction
A power station is equipped with electrical equipment for power
generation and supply of ekctrca1 power. The major electrical
equipment in a power plant consists of the following
(i) Generators (ii) Excitors
(iii) Transformers (it') Reactors
'v) Circuit breakers (w) Switch board
(tti) Control board equipment.
10.2 Generator
It is an important part of a power plant. All modern type of
alternating current generators (alternators) essentiall y consist of
fixed stator and revolving rotor.
Stator mainly consists of following three parts
(i Stator frame
(ii Stator core
(iii ) Stator windings.
The stator frame is of circular in shape and is made of welded
steel plates. The core is made of stampings of high permeability, low
hysteresis and eddy current losses. The rotors are generall y built in
cylinderical form and diameter of rotor is limited to 100 to 110 cm.
Large number of deep slots are machined in the rotor to accoin-
modate the field windings which will carr y field currents. There
should be a in plc passage in the rotor through which cooling fluid
can he circulated freely.
Generators coupled directly to the steam turbines are called
turbo-generators and those (lircctiv coupled to water turbines are
called \vat er wheel generators.
The fiw.nv at which generator operates is given by
568 POWER PLANT
f -- p_fl
/ 120
where f= frequenc y in cycles per second
ii = speed in R.P.M.
p = number of poles of the generator.
The frequency is the standard one used in the particular
country. In India it is 50 cycles per second. The number of poles is
necessarily an even number.
The generators used with diesel engines are of salient pole type
having large diameters and short lengths. The number of poles
varies between 4 to 28 as the speed range of diesel engines driving 4
the generator varies between 1500 to 214 R.P.M. A common range
of capacities is from 25 to 5000 WA, the power factor rating being
0.8 lagging. A 3 phase 50 cycles per second suppl y is to be obtained
from generators and a common voltage rating is . 1 . 1() V. Generator
efficiency varies between 92 to 95.
A common voltage rating for turbo-alternators is 11 kV, The
turbo-alternators are generall y rated at 0.8 power factor lagging
most of turbo-alternators are 2 pole generators with a speed of H)()
R.P.M. Their efficiency may be taken between 98 1Y, and 99g..
The water wheel generators are built with salient (projecting)
poles as they require large number of poles and run at comparatively
low speeds. Therefore water wheel generator rotors are much
greater in diameter than turbo-generator rotors. The water wheel
generators usually run at 62.5 to 125 R.P.M.
In a power plant several generators are run in parallel with each
other. The parallel opetation of generators has the following ad-
vantages
1 There exists a high reliability of power supply to the
consumers.
(ii) It becomes possible to achieve more stable frequenc y and
voltage under conditions of varying load.
(iii) Better economy in running of power stations and their
equipment is obtained.
10.3 Exciter
The generator needs an exciter to build up the necessary voltage
on no load arid then to keep it constant on load, when greater
excitation will be required. The exciter is a D.C. generator shunt or
compound. The capacit y of the exciter depends on the speed, on the
voltage rating of ac. generator and on the voltage required to
compensate for the drop due to load on generator.
MAJOR ELECTRICAL EQUIPMENT IN POWER PLANTS 569
transformer for one generator. In such case the kVA capacity of the
3-phase transformer must then be the same as that of generator to
which it is connected.
While selecting the type of transformer, the significant operat-
ing characteristic of the transformers as well as their initial cost
should be considered. The losses in the transformer are also an
important criterion for their selection. A 3-phase transformer is
preferable compared with a bank of three single phase transformer
as the core loss is about 20% less in 3-phase transformer.
Following factors should be considered in deciding the
suitability of particular type of transformer for a particular applica-
tion:
(a) Load factor (6) Losses
(c) Initial cost (d) Cost of losses
(e) Continuity of service (J) Methods of cooling
(g) Percentage impedance voltage
(h) Floor area (i) Weight
(j) Regulation of voltage.
Different methods of cooling the transformers are ü'sed. Two
commonly used methods used are a s' self-oil cooled transformers or
forced oil cooled transformer. Self-oil cooled transformers do not
need any external equipment and are self-contained whereas forced
oil cooled transformers require pumps etc.
Fig. 10.1 (a) shows a power transformer. The various parts are
as follows
1. Tank 2. Magnetic circuit (core)
3. Radiators 4. Windings
5. Transformer oil 6. Oil gauge
7. Relay 8. Vent pipe
9. Oil conservator 10. Terminal bush
11. Terminal bush
12. Temperature indicating thermometer
13. Tank supporting frame.
The tank of transformer is made of steel. The core and windings
comprise an assembly which is placed with in the tank. The core
serves as the magnetic circuit for the flux set up by the windings.
The windings are made of copper wire. The transformer oil which is
a special grade of mineral oil serves two functions as follows:
(i) it serves as medium for transfer of heat generated in the
windings and core to the air surrounding the transformer.
(iij to insulate the current carrying parts from each other and
from the earthed tank.
REACTORS
FEEDERS
REACTOR
a
FEEDERS
Fig. 10.2
faulty feeder only through the reactors which thus limit the fault
current.
(d) Bus bar reactors in Tie-bar system. Fig. 10.4 shows this
system. This system helps in reducing fault currents in the same
way as the ring bus bar reactor system but in addition it has the
advantage of limiting the currents.
4Reactors
FEEDERS
Fig. 10.3
10.9 Circuit-breakers
Their function is to break a circuit when various abnormal
conditions arise and create a danger for the electrical equipment in
an installation. There are two types of circuit breakers.
574 POWER PLANT
BUS BAR
REACTORS
FEEDERS
Fig. 10.4
AIR
Fig. 10.7
XG RN
Fig. 10.8
XGXN
Fig. 10.9
MAJOR ELECTRICAL EQUIPMENT IN POWER PLANTS 577
CB 0 CB 0 C8 CG C8 CB
4
I
Ic,
s4S4
CSCBCO CB3 C8 CB
-
s4 s,L s4
CB C8 CB1 CB C8 CS
TO TRANSMISSION LINES
LVB = low voltage bus bar
HVS = High voltage bus bar
T = Step up transformer. III
Fig. lOiG -
TO CTATIAKI
AU XII. IA RI.
CE
LVB
live BC
10 1RANSMSSION LINES
Fig. IOu
578 POWER PLANT
1
T
LINE
Fig. 10.12
R ELECTRO
GNET
PRIMARY
WINDING
CLOSED
SECONDARY
WINDING
LOWER
ELECTROMAGNET
TAPPED PRIMARY
WIN DINS
Fig. 10.13
580 POWER PLANT
1A
H91!B
10 TRIP
CIRCUIT
OF LINE A
Fig. 10.14
(i) Supports
(a) Poles (b) Towers
(ii) Conductors (iii) Insulators
(iv) Transformers (v) Protective devices
(vi) Control devices.
Poles or towers support the structures which support the con-
ductors above the ground. Both poles and towers should ful fill the
following requirements
(i) High mechanical strength
(ii) High durability
(iii) Light weight
(iv) Low maintenance cost
(v) Low initial cost.
Poles may be made of materials like wood, steel, cement concrete
etc. Usually RCC poles are used.
Fig. 10.15 shows RCC pole for single circuit and Fig. 10.15 (a)
shows RC. C pole for doub}e circuit.
Towers made of steel are mechanically sturdy and durable and
are commonly used. Fig. 10.16 and Fig. 10.17 show steel towers. The
steel towers are generally four legged, each leg anchored properly.
Pole
Fig. 10.15(a)
MAJOR ELECTRICAL EQUIPMENT IN POWER PLANTS 583
Conductors are generally made of copper, aluminium, copper
clad steel and steel cored aluminium conductors are used to carry
electrical power from one end to the other for transmission and
distribution. Conductors should ful-fill the following requirements.
tor
II
Sheds
Fig. 10.19.2 shows a strain insulator. They are used for high
voltage transmission step up transformers are used at the generat-
ing end and step down transformers are used at the receiving end.
DUCT ER
CLA
ULATOR
3 r
xlOO
V
,.
1
where V = Sending end voltage
Vr = Receiving end voltage
Regulation
Efficiency. Efficiency of transmission line is given by
Pr
S
ii
= Efficiency
Power loss. Power loss in a 3-phase transmission line is given
by
Power loss =3JR
where I = current in line
R = Resistance of each phase.
The spacing of the transmission line between conductors is
chosen considering the voltage between phases and the reactance
and capacitance constants.
Capacitance (c). Capacitance of transmission line is defined
as the ratio of charge to voltage
C= V
where Q = charge j
V = voltage
I UI I ;3 F.
Capacitive reactance (Xc). It is given by
- 1
c_ 21c -
where f= frequency
Charging current (!). It is defined as the ratio of voltage to
capacitive reactance
S
5
--S
Xr S..
t5
AC System )J lYD)A
(a) Single phase AC system
U) Single phase two wire ).
(ii) Single phase two wire with mid-point earthed
(iii) Single phase three wire.
(a) Two phase AC system
(i) Two phase three wire
(ii) Two phase four wire
(c) Three phase AC system
(i) Three phase four wire.
However, three phase alternating currents system Is mostly
used. When transmission is being-carried on over-head lines great
care is taken to insulate the conductors from the cross arms and
support towers.
The single phase system has its own limitations and therefore
has been replaced by poly-phase system.
Poly-means many (two or more than two) and phase means
windings or circuits each of them having a single alternating voltage
of the same magnitude and frequency. Hence a polyphase system is
essentially a combination or two or more than two voltages. These
voltages have same magnitude and frequency but are displaced from
one another by equal electrical angle called phase difference.
- 360 electrical degrees
- - N
Aq
where 0 = Phase difference 11
N = Number of phases
In two phase s y stem there are two equal voltages of same
magnitude and frequency having a phase difference of 90 degrees
electrical
In three phase system there are three voltages of same mag-
nitude and frequency and having a phase difference of 120 degrees
electrical.
588 POWER PLANT
Bulk
consumer
11 kV
Primary distributor
33kV 1
3W.r
P VVjtI
Tr
Substation L1
Factory Distribution
Sub-station
Fig. 10.19 (a)
11 k V/400 V
Transformer
11 kV I 1 400v12301, 34', 4 Wire
.Ph ¶
Distributior
Substation
Hou5e I I I I House
-
ory Mouse
Fig. 10.19(b)
Fig. 10.20
. .
POWER 1l; 11 II V
PLANTt
'1/400 OR 200
OR 137 K STEP UP
\TRANSFoRMER
10 SUB STATION
(220KV)
PRIMARY 720166 0R335V
STEP DOWN
TRANSMISSION 'r•" TRANSFORMER
I
TO SUB STATION
(66kv)
SECONDARY I
TRANSMI59014JI l6/11 NV
. STEP DOWN
TRANSFORMER
T
10 SUB STATION
(11KV) I
PRIMARY
DISTRIBUTION 11NV140V
STEP DOWN
TRANSFORMER
TO LOW VOLTAGE
DISTRIBUTOR
Fig. 1 fl 21 -
PROBLEMS
Non-Conventional Sources of
Energy
11.0 Introduction
In our country power is needed in plenty to sustain our in-
dustrial growth and agricultural production. Existing sources of
energy such as coal, oil, water and uranium may not be sufficient to
meet the increasing energy demands This requires that scientists
and engineers should undertake research work which would help in
exploring the possibilities of harnessing energy from several non-
conventional sources of energy. The various non-conventional sour-
ces of energy ae as follows
(i) Solar energy (ii) Wind energy
(iii) Bio-gas and bio-mass (iv) MHD generat9r
(v) Geo thermal (vi) Tidal power
(vii) Fuel cells (viii) Thermo-electric generation
(ix) Thermionic converter.
It is recognised that an early, smooth and successful transition
from fossil fuel (coal, oil, water) to new and renewable sources of
energy depends on a strong, integrated and purposeful R and D
programme. In our country the Commission for Additional Sources
of energy is responsible for the development of new and renewable
sources of energy. The technology to obtain power from renewable
sourccs should be so developed that power generated is cheaper. The
power plants working on renewable sources of energy should have
low capital cost, there should be no pollution of atmosphere and
running cost should be less.
The Energy Ministry proposes to give a bigger thrust to the
exploitation of new and renewable (non-conventional) sources of
energy to meet a variety of energy needs in urban and far flung rural
areas in a decentralised manner.
The main advantages of non-conventional sources ofenergy are
as f0llows
NON-CONVENTIONAL SOURCES OF ENERGY
597
the sky. The total solar radiation received at any point on the earth's
surface is the sum of direct and diffuse radiation.
Fig. 11.1 (a) shows solar energy storage.
0)
0) o
CJ)
00
LU
ÜILU
'U
0 0
a)
0 0
0 00
0D 0 a. -=
0) E Eu
1 211 F-P.
0
0) n
= 0
w E
a) a)
0
Cn
CL
ID 0
>. t, IIUl
0)
;flirIl9
j1a,c
uJ jJjQJ
Fmfl,) :)Jg
U) oh
rim
C
0
I L9
F; 60-
can convert sun light into electricity. These photo-voltaic cells are
being used in rural areas and isolated locations for a variety of
applications such as () water pumping for irrigation and drinking
water supply.
(ii) Community and street lighting.
(iii) Power supply for micro wave repeater station.
(iv) Communication equipment, radio and television
receivers.
(v) Solar water heaters.
(vi) Solar refrigeration.
11.2 Solar Radiation Measurement
Following two type of instruments are used for solar radiation
measurement
W P vrheliotneter. It collimates the radiation to determine the
-
beam intensity as a function of incident angle.
(ii) Pyronorneti'r. It measures the total hemi-spherical solar
radiation. The pyranometer is quite popular.
11.3 Solar Constant -
It is the rate at which solar energy arrives at the top of atmos-
phere. This is the amount of energy received in unit time on a unit
area perpendicular to the sun's direction at the mean distance of the
earth from the sun. The rate of arrival of solar radiations vary
throughout the year. According to National Aeronautics and Space
Administration (NASA) the solar constant is expressed in following
three ways.
(i) 1.353 kilowatts per square metre or 1353 watts per square
metre.
(ii) 429.2 Btu per square foot per hour.
(iii) 1164 kcal per sq. m. per hour.
nocv;f f
ui
11.4 Solar Energy Collectors
Solar energy can be exploited in various ways as follows
(i) By direct conversion to a fuel by photosynthesis. 4
Solar.
radiation
\\% Absorbin
Surf oc
TrQnsporcr
cover DItS
Hot water
Cold water
Fig. 11.1
Stay
rois
C)'
Mr r or
strips \
\ t'"_
0 -Absorber
rettec tir tube
II 2 1' 3
--40
602 POWER PLANT
Absorb
er
dish I
Fig 11.4.
Hot water
np Cooling
lower
Solar
çGenerotcr Pump pon d
Organic Hot
workmg brine
fluid
Turbine
Fig. 11.5
Water circuit
Solar
Array of
collectors Hot
water
Butane
r
Bu tan: ro p
boiler ectors
PumpT
1
I 1urbne
Water for •
[1
irrigation purposeWell
:^
L Condenser
Fig ll.
Railer Incident
solar rays
To 9r
z $tots
Fig 11.7
fliT )T
- Boner
Fig. 1 1 .8
tion has been space craft for which silicon solar cell is the most
highly developed type.
Various advantages of solar cells are as follows
(i) They need little maintenance
(it) They have longer life
(iii) They do not create pollution problem
(iv) Their energy source is unlimited
(u) These are easy to fabricate
(vi) They call made from raw materials which are easily
available in larger quantities.
The disadvantages of solar cells are as follows
(i) Compared with other sources of energy solar cells produce
electric power at very high cost.
(ii) Solar cell output is'lot constant and it varies with the time
of day and weather.
(iii) They can be used to generate small amount of electric
power.
Solar cells have also been usea to operate irrigation pumps,
vigational signals, highway emergency cell systems, rail road
cro- rw signals_etc.
The mosr common configuration of a typical solar cell to form a
p . n junction semi-conductor is shown in Fig. 11.9.
Solar
rays
Load
Current
collection grid
(metal
P - fleion
Base material Difttjsed
layer
Metal
conductor
Fig. 119
orrog"
rganic
fluid
T^ 7
un
Condenser
Circulating Feed
pump pump
Fig. 11.10
• 1 1 110 rate 1 .2 trillion kWh ofeleiric;rl c I w Ijgy per y ear. Wind mills
have been usi of for several cent urie in cmintrie like Denmark,
Netherland China. Europe. Persia etc fit Itigli wind speeds
are obtainable in coastal aias of Sot ir.ishtra Western Rajasthan
and snow parts of (errl India Iii these areas there could be a
poilnlity (f uing nirditini and lal 6 iicd wind mills for genera-
tioi of elCt rRit \
4ome of the haractere-tics ol wind (rIrIg\ ale as I'ollows
\'irul power s y stems are ii n olhit inn
(it) It is it renewable source of energy
iii The eni rgy generated by wind-power sv'tvms is cheaper
when produced on small scale. On largesraic it is confliCt!-
tive v lth conventronal pOWCF gvnerw ing systems.
Wind energy svtrriis avoid fuel prove-ion and transport.
however tilowing prribRiiis are a,ociated with wind energy
I I \\i;id cfl(rgv is fliictiiiting in nature
= MV'2
= pA.V.V2 = pAV3
= p.A.V3
Sb
Wnd
turbine
Fig. 1.11
-.--Wind
Wind mill
head
'RotOr
Supportirg
Structure
Fig. 11.12
Gent
Fig. 11.13
CONTROL COUPLING
POWER
PITCH
CONTROL GENERATOR
J
SPCEO
& TS
OtJTPUl
TEMPERATURE
POWER
ROLLER
Fig. 11.13(a)
POWER PLANT
4
M
I +
Sn,
I He
____12h.25rnir. H
Fig 11 4
OykQ
Power
Basin
523
slut's
Fig. 11.15
Fig. 11.15 shows a single basin one way tidal power plant. In
this plant a basin is allowed to get filled during the flood tide and
during the ebb tide, the water flowing from the basin to te sea
thruugh the turbine and generates power. The power is iilahle for
a short duration during ebb tide.
In single basin two way tidal power plant the power is generated
hoh duing flood tide as well as ebb tide. The direction of flow
through the turbines during the ebb and flocd tides alternates but
machine acts as a turbine for either direction of flow.
Dyhe
Low basin
High
basin
Sluice\,<
Sea
Fig. 11.16
Fig. 11.16 shows a double basin one way tidal power plant. In
this plant one basin is intermittently filled by flood tide and ocher
is intermittently drained by ebb tide. For some more details of tidal
power see Chapter 1.
11.22 Advantages and Disadvantages of Tidal Power
Advantages
Various advantages are as follows:
(i It is free from pollution.
(it) It is ir.exhaustible and does not depend on rain.
(iii) Tidal power plants do not require large area of valuable
land because they are located on sea shore.
—41
618 POWER PLANT
Scum layer
lays,
sludg :Sludge
Outlet
Fig. 11.17
Fixed dome digester. Fig. 11.17 (a) shows circular fixed dome
digester plant. The fixed dome is made of masonry structure. The
digestion takes place in the masonry well. The gas generated is
taken out from the top. Are movable man hole cover sealed with clay
is provided.
GAS PIPE
N HOLE JLOOSE COVER
INLET
PIPE
DISPLACEMENT
UL
O
, UTLET
SLURRY
Fig. 11.17(a)
LEVELLE
SURFACE
SLURRY
Fig. 11.17(b)
11.24.2 Thejmionic Generation
This method of power generation utilises the thermionic emis-
sion effect which means emission of electrons from heated metal
surface. The energy required to extract an electron from the metal
is called work function of the metal and depends on the nature of
metal and its surface condition.
11.24.3 Thermionjc Converter
The thermionic converter utilises thermionjc emission effect. It
consists of two metal (or electrodes) with different work functions
sealed into an evacuated vessel on heating one electrode, the
electrons are emitted which travel to opposite colder electrode called
collector or anode.
The hot electrode (emitter or cathode) emits electrons and
acquires a positive charge whereas colder electrode collects
electrons and becomes negatively changed. A voltage (or clectro
motive force) thus develops between the electrodes and a direct
current starts flowing in the load connected as shown in Fig. 11.17
(c).
The electrode with the large work function is maintained at
higher temperature than one with the smaller work function.
NON-CONVENTIONAL SOURCES OF ENERGY 621
C.VTAT ED
1101 SF-L.
ELE.CTROI
COLD
ELECTRObE
RON ,
Uok..up Hd
Fig. 11.18
11.25.2 Closed cycle systems
-J
There are two types of closed cycle MHD generator systems
(i) seeded invert gas system
(ii) liquid metal system.
Fig. 11.19 shows a liquid metal system. In this system a liquid
metal is used as working fluid. The liquid potassium coming out of
breaker reactor at high temperature is possessed through a nozzle
to increase its velocity before passing to MHD generator. The liquid
potassium coming out of MHD generator is passed through a heat
exchanger (boiler) to ue it q remaining heat to system to run a
turbine and then pumped back to the reactor. There are lot of
operational and constructional difficulties in this system. MUD-
NON-CONVENTIONAL SOURCES OF ENERGY 623
GEN indicates MHD Generator, Inv. means invertor and S.T. indi-
cates steam turbine.
Condenser
Magnin F..6
wIhr
140
Gen
Nozzle Seperolor
eoCiOI
Gen.roor
Steam
Pump Liquid
Fig. 11.19
The '- triotis hurdles in the progress of MHD power plant are as
follows
(i) Development of super conductor magnet.
(ii) Materials to withstand high temperatures.
(iii) Efficient conversion of 1)C to AC crosioiik,ss electrodes.
(ic) Heavy losses in the power electrodes.
11 26 Fuel Cell
l"til rell details are discussed in Chapter 9.
11.27 Thermo-Electric Power
This method of producing electrical energ y uses see-beck effect
according to whici an is produced when in a loop of two
dissimilar mçtals the juncttons arc kept at different temperatures
The efficienv of thermo-electri 'r( , nerator depends upon the
temperatures ul hot and cold ju'.ctions.
Material-i
iot coi
Junctjøt, Junction
14 Matericil-2
cm
Fig. 11.20
- a. x
NON-CONVENTIONAL SOURCES OF ENERGY
625
where = Seebeck coefficient
AT = Temperature difference
=T2-
where T2 = temperature of cold junction
= Temperature of hot junction.
+Ve
cts 0
—v e
Ternperoture(°K)
Fig. 11.21
Hot
A
Cold
Fig. 11.22
P:E
B
D.C. Load
Fig. 11.23
=o500 m3IS
to = specific weight of water = 1025 kg/rn3
P = Power
=X
75 T1
= 4.3 x 104H.P.
E = Energy per cycle
= P x 0.736 x T
= 4.3 x 10 x 0.736 x 3 = 9.3 x 10 kWh.
N = Number of tidal cycle per year 705
Total out put per year
= E x N = 9.3 x 10'x 705
= 6.4 x 107 kWh.
628 POWER PLANT
F 1.8x103
(620+280)j = 1.32
2
Tcl I M
[TL^
l Mi-
--
Tc
[620-2801 1 1.32-1
- 620 i 132+
280
0.12 = 12
NON-CONVENTIONAL SOURCES OF ENERGY
629
= 52%.
PROBLEMS
11.9. State the factors to be considered while selecting the site for wind
mill.
11.10. Write short notes on the following:
(a) Bto mass
(b) Bib gas
(c) Fuel cell
(d) Power coefficient of wind mill.
11.11. (a) Describe MI-ID generator principle.
(b) Describe an open cycle and a closed cycle MHD power gener-
ator.
11.12. What is tidal power? What is tidal range? State advantages
and disadvantages of tidal power.
11.13. (a) Name the main components of tidal power plant.
(b) State the points to be considered while selecting a site for
tidal power plant.
11.14. I-io.v do you classify tidal power plants. Describe
(a) single basin one way
(b) double basin one way tidal power plant.
11.15. How do you classify bio-gas plants? Describe a continuous type
bio gas plant and fixed dome type plant.
11.16. Describe various parts of a wind electric generating plant.
11.17. State the advantages of MHD p ower generation system.
11.18. Write short note on the following:
(i) Thermo-electric power
(ii) Thermo-electric power generator
(iii) Materials for thermal electric power generator
(iv) Figure of merit.
Cv) Basic components ofa wind energy conversion system.
11.19. Write short notes on the following:
(i) Performance of wind machines
(ii) Overall efficiency of aero-generat.or
(zn) Efficiency of aero-turbine
(iv) Methods of regulation of tidal power.
11.20. Write short notes on the following
(i) Methods for maintaining bio-gas production
(ii) Geothermal energy resources.
. :
12
12.1 Introduction
The electric power demand is continuouLy increasing. The
electric utilities and faced with simultaneous demand for increased
power as well as problem of harmful imp.rities which are ejected
into the environment surrounding the utilities. The power engineer-
ing specialists should develop and implement the effective means in
the field of environmental protection from harmful effluents of
power plants. The effects of power plant pollutants on the environ-
ment are raifily on the air and water and to a lesser extent on the
land.
Most of the pollution in the cities can be avoided if power plants
are located outside the city boundary. The pollution from the nuclear
power plants is radio-active waste in the form of gases, liquids and
solids whose radio-active property may retain number of years. The
dumping and leakage of these wastes are major problems in ouclear
power plants.
dombustion generated pollution is by far the largest man-made
contributor to atmospheric pollution. The principal pollutants
emitted by fossil fuel tired boilers in large power plants are products
of incomplete combustion such as combustible particulate matter
CO, NOx, SOx and fly ash and particulates formed due to the use of
fuel additives.
The methods of control of pollutants include:
(1) low excess air combustion (excess air 2%).
(ii) staged combustion with heat removal between stages.
(iii) flue gas re-circulation.
(it') gasification of coal and residual fuel oil.
(v) fluidised bed combustion.
ENVIRONMENT POLLUTION AND ITS CONTROL 633
j) 1
Q = A . lt)i) lt)0 1'
where A. = Fraction (if ' solini particles carried off from furnace with
flue gase-..
W = Ash content ofworkiiig Itlass of fuel in c
1'= Content of conil,astili . le in fl y ash in
The ash is also a problem as it also emits heat to the atmosphere
as well as small parto:l'. of ash are carried Lv the air. Large
quantity of heat d,sc}iiig'd to the at iiosphrn- also is a cause of
pollution. 'Toxic substance, contained in flue oases discharged from
stacks iii' ther.nial po'.'. or pLiiits (an produce harmful effects on the
Whole complex of living nature or the bio-sphere The bin-sphere
comprises the atmosphere la y er near the earth's surface and upper
la y ers of soil and water basins.
Depending on the t y pe of fuel and capacit y of boiler the ash
collection from (hernial power plamits can be effected b y the following
devices
Ash'collecter (it) Fl y ash scrubbers
(iii) Electro static pr.'cipit.at.ors.
Fly ash, cinders, various gases and smoke discharged from the'
stack become atmospheric contaminants. Gases diffuse in all direc-
tions. The path followed b y the flue gases depends upon the thermal
and dynamic properties of gases and wind flow past the stack
The various variables affecting the area over which flue gases
ronstitme:its will settle out are as follows
(i) Stack height
(ii) Stack exit gas velocity
(iii) Wind velocity
(im.') Gas temperature
(m.) Particle size
(m.'i ) Surrounding topography.
ENVIRONMENT POLLUTION AND ITS CONTROL 635
E x h us
cc3s
ler
Rac tic
tank
0
waste
Fig . 12 1
In the scrubber following reactions take place.
Ca (011)2 SO2 -. CaSO3 I 110
CaCO 3 - SO 2 CaS0 3 CO2
The c'iticiuin sulphite (CaSO3) SO produced gets partially
oidiscd to calcium sulphate. Iii most of the cases products of
neutr:iltsatw i.are not utilistd hut go to waste. Lime stone SCrul)herS
are capat)li. removing up t )O'; Of' So, from the entering
the ciuhher wiuch may have 0.2 to 0.3 502.
\'irtous ilvantages of wet scrubber are as follows
'i ) I ugh efficiency
Ui) 1 .usv flue gas energ y requirement
(iii Good reliability.
The disadvantages are as follows
(i) 11 igh capital and operating cost
ii) ('ostiv disposal problem for the waste material which is
water logged sludge.
12.5.2 Catalytic oxidation
It used to produce sulphuric acid. from dilute 502 in the flue
gas. The sulphuric acid is separated from tlue gases.
12.5.3 Magnesium oxide scrubbing
In this process magnesium sulphate and sulphite salts are
regenerated. producing a concentrated stream of 50 1 and mag-
nesium oxide ( \Ig( )) for reuse in the scrubbing loop.
Mg() S0 2 MgSO.i
640 POWER PLANT
Thi . iu:i riuiiu iphitiS( f, )1 11 d react.- further . () and
at&r hi jerIII lZiiesiLllfl hi -ilpht
I -( )_• I I_( I lg l Is( .c
HR
I +
the boiler.
Recover of waste heat escaping through the boiler chimne y by
use of superheater, economiser and combustion air preheater
reduces ill" conuiflpti)n in boiler. Heat lost in boiler chimney
flue gases at various teln } )erilture for various excess air levels have
h(-(-n shown in Fig 12 12.
I. Preheating of Solid Stocks for 11CIt lk'(oVerV
This technique is also used for recovery of heat f'i'on flue gases
going out of the s y stem examples are Multi-chambered Ring Fur-
naces used in brick, refractory/ceramic industries, carbon electrode
industr y , Rotary kilns in cello nt industr y In all these appliance the
charges are, prhcatc-d b y the counter current contact of the flue
gases which-are consequently exiled (luring this process before it is
Il
tA
to
LB
to
to
0
fl
6
()
P
u 20 40 60 80 100
1. Eocess or--
Fig 12 3 Rci . cnship of ". oxygen in waste gases and '. excess air.
eqwnunitut. .• exces5 air:. The general relationship between
the uxv,:i c ' :i:t. and 'xc&ss air Idr both low ('V, fill
lulat furnace g;u and rich fuel coke oven gas. heav y fuel oil
ett. I> 'va in Fig l d. 'ftc• It:uu that the fcirim uong
Ii niitI bed e.inuHitiuu •,! rid hi more (flleii:leV as compared to
f:irniccs using puiveried coal. Iii the figure curve A is for blast
lui, uetiu gu. thuc cur ve P m i c:nvcrt'r gas mid curve C is for
fuel oil and coke oven gas
648 POWER PLANT
PROBLEMS
t in I Wet Scrubber
Electrostatic Pieci pttitor.
12.7 l)escribt the various t y pes of waste waters from a si in power
plant and the methods for removing impurities frorn waste
vafors.
12 S. l)eciil i the ill utants of atomic power plants uiid their control
1 ,-,g Write short ti,tcs on the following:
Noise control at power plants
.u .i Standardiations for environment pollution.
(III I Iliernial pollution,
12.10. Discuss the cleaning of ventilation au at atomic power plants.
12,11. Discuss Iliet econom y in furnaces of boilers
13
13.1 Introduction
The direct energy conversion systems convert naturally avail-
able energy into electricity there being no intermediate conversion
into mechanical energy.
The various direct energy conversion systems are is follows.
1. Thermo electric conversion system
2. Therrnionic conversion system
3. Electrostatic mechanical gnerators
4. Photo voltaic power system
5. Electro gas dynamic generator (EGD)
6. MHD system
7. Nuclear batteries
8. Fuel cells
13.2 Thermo-electric Conversion System
The direct conversion of heat energy into electric energy (i.e.
without a conventional electric generator) is based on seebeck
Thermo electric effect Fig. 13.1 shows two dissimilar materials
joined together in the form of a loop so that there are two junctions.
If a temperature difference is maintained between hot and cold
junctions an electric current will flow round the loop. The magnitude
of the current will depend upon
(i) temperature difference
and (ii) materials used
Material-1,Cold
Hot
Junction
unction
McI
Fig. 13.1
—43
POWER PLANT
650
Cold Cold
Load
Fig. 13.2
Temp ero1ure,K----
Fig. 13.3
Lii
Co r. Cold
Load
Fig. 13.4
Heat Reservoir
f4-A A-.
I I
1-
ii:.i L
L 1 (-B
I.
L - sink
Load
Fig. 13.5
POWER PLANT
652
RL
=L
where aAB = seebeck coefficient
R = Resistance of thermo couple
Evocuc
vessel 0-c.
Load
Heat input
Fig. 13.6
= A V e - ilKT amp/cm2
Where A is constant and has the value equal to
120 x 10 4 Amp/m 2 as described in the previous section.
k2
A- 1z3
h = Planck's constant
e = Charge
Q = work function in o
T = Temperature (K)
K = Boltzmann constant J1
m = mass of an electron (kg)
Now, J = Current leaving cathode
POWER PLANT
654
• e V6)/KT
Jc =A T e-
=A 1?
Ja = electron current leaving the anode
J. =AV VJKT.,
J = net current density flow
J= Jc - Ja
= A 7 e'M - A7e -
V Voltage output
= 01 -0. -OP
where 0, = Cathode work function
= Anode work function
op = Plasna potential drop.
P = Power produced = J.V
(work output)
H = Heat Supplied to the cathosk (cathode heat flux)
QC
- Ac
"
=J(Ø+--)+ M, - 77 )
= Efficiency of generator =
where I' = JV
Qc
Collector
electrode
Load
Attract(
etectro
a
rode
Fig. 13.7
fonised go Plates
Fig. 13.8
u = Gas velocity
E' = Total electric field
= E2 + B . u
=-7+Bu
= (B.u.d. - u)
EIclrodes R Lood
Fig. 13.9
- =I.Rg.I
=I2Rg
E,,
Rg -
Ell
asRi.=R
4Rg
- B2u2d2
as Eo = Bud.
4Rg
d
Putting the value of Rg as Rg
- oA
B2ti 2d2
we get, niax = ---- GA
=•
Combustion
chamber
Nozzle
- EIctrodes
Load
(,s flow
Generator
channI
POWER PLANT
658
O IdLJ1 Load
pressOr
rom Cooler
1
Fig. 13.11 shows over all power cycle for MHD generator.
11 16\tOC3
01
0.
El
01
4 14et rejection
- Entropy, $
Fig. 13.12 shows Temp. entropy diagram for the cycle.
In the overall power cycle, the MHD converter takes the place
of a turbine in a conventional vapour or gas turbine cycle. Still, a
compressor must be used to elevate the pressure, heat is added at
high pressure and the flow is accelerated before entering the con-
verter.
Pig. shows Temp. entropy (T-S) diagram for the cycle.
flth = Thermal efficiency
It is limited by carnot efficiency
Now P1 =P2
Pressure, P3= P4
- work output - ( h 20 - h30 ) - (h 10 - h40)
11th - heat input - ( h20 - h10)
Where the indicated enthalpies are stagnation values which
take inço account the K.E. of the flow. The stagnation enthalpy is
(lCfiflCd as
ho =h + V2
= = 0.19 ohm
10 x 0.26
f__W^
voc
Fig. 13.13
Rl,0kO, V
oc
Fig. 13.14
+. 1. I I 1
au uc [(I.II
ectrodes Cell-'
Fig. 13.15
•1
HA H
IIIFig. 13.16
ii
664 POWER PLANT
The batter y voltage is now the same as that of a single cell, but the
current is the sun of the currents supplied by the individual cells.
Fig. 13.16 shows such arrangement.
13.17 Power of Battery
The power 01 a battery (i.e. the rate at which stored energy is
withdrawn) in it is equal to the product of the ernf in volts and
the current in amperes thus,
Power (w t) EMF (volts) . current (amp(' . .•)
Specific power is the maximum rated power output per kg of
battery can s.ipply. Rating '.arious batteries by specific power per-
mits rapid performance comparison of different kinds of batteries.
13.17.1 Energy efficiency () of battery.
It is given by:
- Useful_enegy out put ('vatt hours)
1 - Re charge energy (watt hours)
13.17.2 Cycle life of battery
The cycle life of battery is Lhe number of times the battery can
be charged and discharged under specified conditions.
13.18 Principal and analysis of H2, 02 (Hydrogen-oxygen)
fuel cell
This cell is quite commonly used. Fuel cells are particularly
suitabh' for low voltage and high current applications. Fuel cells are
chemical devices in which the chemical energy of fuel is converted
directly into electrical energy chemical energy is the free enegy of
the reactants used.
Fig. 13.17 shows a hydrogen oxygen fuel cell.
Load
H 2 in o.
Fig. 13.1 r A Hydi3x (H2, 02 cell).
DIRECT ENERGY CONVERSION SYSTEMS
665
The main components of a full cell are as follows.
(i) Fuel electrode (anode)
(ii) an oxidant or air electrode (cathode)
and (iiL an electrolyte. The electrolyte is typically 40% KOH be-
cause of its high electrical conductivity and it is less
corrosive than acids.
In most fuel cells, hydrogen (pure or impure) is the active
material at the negative electrode and oxygen (from the oxygen or
air) is active at the positive electrode. Since hydrogen and oxygen
are gases, a fuel cell requires a solid electrical conductor to serve as
a current collector and to provide a terminal at each electrode. The
solid electrode material is generally porous.
Porous nickel electrodes and porous carbon, electrodes are
generally used in fuel cells. Platinum and other precious metals are
being used in certain fuel cells. The porous electrode has a larger
number o f sites, where the gas electrolyte and electrode are in
contact the electro chemical reactions occur at these sites. The
reactions are formall y very slow, and catalyst is included in the
electrode to expedite them. The best electrochemical catalysts are
finely divided platinum or platinum-like metal deposited on or
incorporated with the porous electrode material.
The reactions which take place are as follows
4KOH -* 4K t 4 (OH)
Anode: 2112 - 4(OH) - 41120 + 4e
Cathode: 02 + 2H20 + 4e - 4(OH)
Cell reaction: 21-1 2 + 02 - 21-120
The electrons liberated at the anode find their way to the
cathode through the external circuit. This transfer is equivalent to
the flow of a current from the cathode to the anode. The movement
of electrons constitutes a current passing through an external load.
Thus useful work is obtained directly from the chemical process.
The gases in the hydrogen oxygen cell must be free from carbon-
dioxide, because this gas can combine with the potassium dydroxide
electrolyte to form potassium carbonate. If this occurs, the electrical
resistance of the cell is increased and its Output voltage is decreased.
Consequently, when air is used to supply the required oxygen,
carbon dioxide must first be removed by scrubbing with an alkaline
medium (i.e. lime).
Depending or. the fuel used the main types of fuel cells are as
follows
(i) Hydrogen (1-1 2 ) fuel cell,
(ii) Hydrazine (N 21-14 ) fuel cell
—44
POWER PLANT
666
) M+
10
T11
M = [1+ z(Ti, + TO
= (4x 106) (Q =
0.139= 13.9% Ans.
7.026x
Carnot efficiency this device
Tr - Ts 2000-1000 0 0
T' - 2000
= 50% Ans.
670 POWER PLANT
PROBLEM
If
OBJECTIVE TYPE QUESTIONS
673
(a) There is no direct contact between steam and cooling
water in surface condensers.
(b) Secondary air is not supplied in cyclone burner used to
burn pulverised coal.
15. A venturimeter is generally used to measure rate of flow
of
(a) air (b) steam
(c) water.
16. Pipes carrying steam are generally made up of
(a) cast iron (b) steel
(c) copper.
17. Running cost of hydra-electric power plant is
(a) more than running cost of a steam power plant
(b) less than running cost of steam power plant
(c) equal to running cost of a steam power plant.
18. The initial cost of erecting a nuclear power plant is
(a) equal to the initial cost of steam power plant olsame
size.
(b) less than the initial cost ofa steam power plant olsanie
size.
(c) more than the initial cost of a steam power plant of
same size.
19. State whether the following statements are true or false
(a) In fire tube boilers the gases pass through tubes and
water surrounds these tubes.
(b) More heating surfaces is available in bent tube boilers.
20. The modern steam turbines are
(a) reaction turbines (b) impulse turbine
(c) impulse-reaction turbines.
21. The nuclear power plant at Tarapur has
(ci) pressurised water reactors
(b) boiling water reactors
(c) sodium graphite reactors.
22. The boiling water reactor uses
(a) enriched uranium as fuel th plutonium
(c) thorium.
23 Fill in the blanks
Narora atomic power station is located in ... .... (ALP
V.P., Gujarat)
4 of Full Load—..
Fig. 14.1
—45
POWER PLANT
682
(c) In water tube boilers water flows through tubes and hot
gases flow outside the tubes.
86. Name two fire tube boilers.
87. State three factors which affect the efficiency of a steam
turbine.
88. State the pressure and temperature ranges commonly
used for boilers.
89. (a) Define speed factors for a diesel engine.
(b) State speed factors for low speed, medium speed, and
high speed diesel engines.
90. The approximate efficiency of a water tube boiler used for
power purposes without heat recovery equipment using
coal is
(0)45% (b) 7517,
(c) 95%.
91. The ratio of piston stroke t'o bore of c y linder for internal
combustion engines varies between
(a) 0.9and-1.9
(b) 0.5 and 0.8
(c) 0.3 and 0.6.
92. State basic characteristics of a boiler unit.
93. Compare a hydro power plant and steam power Plant..
94. State the methods of feeding various types of fuels into
furnace.
95. The velocity of water in the penstock for high head pOWCI
plant is abçut
(a) 12 m!sec (b) 7 in/see
(c) 3 im/sec.
96. The steam consumption in large turbines is aI)OUt
(a) 5 kg per kWh (b) 10 kg per kWh
(r) 15 kg per kWh (d) None of the aove.
97. The most economical average vacuum in a condenser for
steam turbine is about
(cu) 42 cm of mercury (b) 22 cm of mercury
(c) 72 cm of mercury (d) None of the above.
9S. Statements (True or false)
OBJECTIVE TYPE QUESTIONS 683
121. The low head hydropower plants are those which usually
have water head
(a) less than 5 m (b) less than 15 m
(c) less than 30 m (d) None of the above.
122. Air fuel ratio required for the combustion in diesel engine
is about
(a)15:1 (b) 5:1
(c) 10: 1 (d) none of the above.
123. The air-fuel ratio by weight required in gas turbine is
(a)30:1 (h) 60:1
(c) 90: I (d) none of the nhovc
124. Name three gases used in closed cycle gas turbine plant.
125. Turbo alternators are generally rated at
(a) 0.8 power factor lagging
(b) 0.6 power factor lagging
(c) 0.5 power factor lagging
(d) None of the above
126. Define superstructure and sub-structure of a hydropower
plant.
127. Tick mark the correct answers
(A) The function of superheater is
(a) to increase steam temperature sufficiently above
saturation temperature
(b) to preheat the air entering the furnace
(c) to heat the feed water entering the boiler.
(B) The capital cost of gas turbine power plant is about
(a) Rs. 500 to 700 per kW
(b) Rs. 1500 to 1700 per kW
(c) Rs. 2500 to 2700 per kW.
POWER PLANT
686
128. State five outstanding features of a gas turbine power
plant.
129. State the functions of a super heater in a steam power
plant.
130. State whether the following statements are true or false.
(a) Francis turbine and propeller turbine are reaction
turbines.
(h) Impulse turbine utilises the kinetic energy of a high
velocity jet of water to transform the water energy into
mechanical energy.
(c) Reaction turbine develops power from the combined
action of pressure energy and kinetic energy of water.
(ci) The operating cost of diesel power plant is less as
compared to steam power plant of equal capacity.
(e) Diesel power plants have good over load capacity.
(f) A hydro-plant can he easily started from cold conditions.
(g) Major drawback of a diesel power plant is limited unit
generation capacity.
(h) A diesel power plant has higher thermal efficiency
than a steam power plant of comparable size.
131. State two factors to be considered while selecting generat-
ing nits.
132. Name four effects of impurities present in feed water for
boiler.
133. State the factor considered in selecting the coal handling
s y stem in a steam power plant
134. The heating value of natural gas at ST.I'. is
(a) 7000 kcallm 3 (b) 9000 kcal/in1
(cj) 11000 kcal/in3.
135. The national research centre for research and develop-
ment work in nuclear energy in our country is
(ci) Bhahha atomic research centre (BARC)
(h ) Tata institute of fundamental research
(C) Saha institute of nuclear physics.
136. State four limitations in the use of nucl.ar power pIant.
137. State two limitations in the use or solar energy.
138 Name two materials used for making solar cells.
139. Statements
OBJECTIVE TYPE QUESTIONS 687
OBJECTIVE TYPE QUESTIONS 691
ANSWERS
1. (a) 2. (ix) 3. (b) 4. (a)
5. (c) 6. (a) 7. (a)
8. (a) True (b) True (c) True (d) False (e) False (/) True (g) True.
9. (a) 10. (a) False (b) True (c) True.
11. (a) 12. (a) 13. (a) 14. (i) True (ii) False
15. (c) 16. (b) 17. 'b) 18. (C)
19. (a) True (&) True 20. (c) 21. (b) 22. (a)
23. (i)U.P. (ii) Tamil Nadu (iii) Tamil Nadu (iv) Delhi
24(c) 25. (b) 26. (c) 27. (b)
28.(a) 29(a) 30. (a)' 31. (b)
32. (z) Natural gas (ii) Blast furnace gas
3. (a) Laminated asbestos (b) Mineral wool (c) Glass wool.
34. (c)
35. (a) 100 in and above (b) 30 to 50 in (c) 25 to 60 m
36. (a) 10 to 35 (b) 60 to 300 (c) 300 to 1000. 37. (a)
38. (a) 39. (b) 40. (b)
41. (a) True (b) True (c) False (d) True (e) False (/) False.
42. (a) 43. (a) Francis turbine (6) Pelton turbine.
44. (a) True (b) True (c) True (d) True (e) False (J) True (g) True.
45. (b) 46. (b) 47. (c)
48. (a) Gravity (6) upstream, down steam.
49.(c) 50.(c) 51(c) 53(c)
54. (a) True (6) True 55. (cx)
56. (a) True (b) True (c) True
57. (c) 58. (b) 59. (b) 60. (b)
61. (c) 62. (cx) True (b) True (c)True
OBJECTIVE TYPE QUESTIONS
693
63. (i) Pressure compounded steam turbine is the most efficient
turbine because the ratio of blade velocity to steam velocity
remains constant whereas velocity compounded turbine has low
efficiency because the ratio of blade velocity to steam velocity is
not optimum.
(ii) Pressure compounded steam turbine has large number of stages
and, therefore, it is most expensive whereas a velocity com-
pounded steam turbine has relatively fewer number of stages
and hence its initial cost is less.
64. (a) 65. (b) 66. (a) 67. (c)
68. (c) 69 (/,) 'in
71. (i) It should have high thermal efficiency.
(ii) Its initial cost should be low.
It should occupy small space.
(iv) It should be easily accessible and serviceable.
W) Its maintenance cost should be low.
72. W True (ii) False (iii) True (iv) True.
73. (c) 74. (b)
r y ___I__ - . .
75. I__suz, Hydro electric power plants involve nvolve large capital expendi-
tures. The capital cost of a diesel power plant is lowest.
(b) Operating cost of steam power plant is more than..a hydro
power plant.
(c) Reliability of hydro plant, steam power plant and nuclear
power is almost equal whereas reliability of diesel power
plant is more than other plants.
(d) Planning, design and construction of a nuclear power plant
is very difficult and takes long time whereas planning design
and construction of steam power plant is easier than hydro-
power plant. Planning design and construction of a diesel
power plant is the easiest.
76(a) 77(b) 78.(a)
79(c) 800)
81. (a) False (b) True (c) True (d) False (e) True (1) True
(g) True (h) True.
82. The ad'antages ofsuper charging in diesel engine areas follows:
(i) It increases the output of the engine.
(ii) It overcomes the effect of high altitudes.
(iii) It reduces the weight of the engine per horse power
developed.
83. (i) Feed pumps (ii) Feed water heater
(iii) Air preheater (it') Draught equipment.
84. (a) Stop valve (b) Safety valve (c) Fusible plug (d) Pressure
gauge.
85. (a) False (b) True (c) True.
86. (i) Locomotive boiler (ii) Cornish boiler
87. (t) Steam pressure and temperature at the throttle valve of
turbine.
(ii) Exhaust steam pressure and temperature.
(iii) Number of bleedings.
POWER PLANT
694
88. The pressure and temperature ranges for steam generators are
as follows
(1)70 to 140 kg/cm 2 steam temperature range of 450 to 560 C.
(u) 56 to 70 kg/cm 2 steam pressure with temperature range of
440C to 480°C.
(in) 28 to 56 kg/cm 2 steam with temperature range of 400 to
440 C.
(iv) 17.5 to kg/cm 2 saturated at 400'C.
(') 9 to 17.5 kg/C,112 saturated steam superheated to 65 C super
heat.
89. (a) The speed factor (S.F.) of diesel eng,ne is given by
S.F. =-----
3048 x iü
where N = Rotational speed in R.P.M.
V = Piston speed in centimetres per second.
Speed factor is also given by
1524 x
where 1, stroke of piston in centimetres.
)h) The speed factor for low speed engine is less than 1.2 whereas
for medium speed engine it varies between 1.2 and 3.5. For h h
speed engines the speed factor is between 3.5 and 11.
90. (b) 91(a)
92. Boiler units consists of a steam boiler, a furnace a nw
auxiliary device for heating water and air, and draught e,
meritetc. 'l'lie basic characteristics ofa boiler unit are its capacit
and steam parameters. The capacity of boiler unit is the amount
of steam in kilograms produced per second. The parameters
characterising steam are pressure and temperature of super-
heated steam and pressuie and dryness fraction for saturated
steam.
91 Comparison of hydro and steam power plants.
These plants are compared as follows
(i) Capital Cost. The capital cost of hydro power plant is high as compared
to steam power plant of equal size.
(ii) Operating Cost. The operating cost of both the plants is about same.
(iii)Maintenance Cost. Maintenance cost ofstcani power plant is high as
compared to hydro power plant.
(it) Location near load centre. Steam power plant can be easily located
near load centre. Whereas hydropower plant cannot be located near load
ce.ltre.
,t') Sterling period. Hydro power plant can be quickly started from cold
Cofldtti')flS whereas it takes about 5 to 10 hours to put steam power plant
uperition.
OBJECTIVE TYPE QUESTIONS 695
it) Load Sharing. When both steam power plant and hvd ro power plants
are used to suppl y the given toad it is preferable to use hydropower plant
as base load plant if sufficient amount of water is available at power plant
Site and steam power plant is used as peak toad plants However if the
amount of water available at hydro power plant Site is small then it is
desirable to use steam power pla ifl as base load plant and hydro power plant
as peak load plant
94. Solids fuels like coal, cock etc. are burnt on grate in the furnace
stokers are used to feed the fuel automaticall y . Air enters from
bottom of grate and burns the fuel
l'ulverised fuels enter the furnace through burners. The flame in the
furnace ignites the fuel and it burns ii) SUSp'flSiOfl.
Oil fuel is supplied to furnace t rough b.irners which atomise the oil
into in in ute droplets and mix it with air. The mixture ignites and burns
Gas fuel is also supplied through burners. However gas needs no
at o in is a tio ri
95. (b) 96. (a) 97. (c)
98. (I) True (ii) True (iii) False (it) False.
99. t(1) High ash contents (h) Excessive moisture content (c) Low
calorilic value.
100. (a True (II)True (c ) Irue (il) True (0) True.
101, The moderators commonl y used are as follows
(i) Light water (1120)
(ii) Det.urium or heavy water (1)20)
tie) Carbon
(ic') Beryllium.
102 The function ofa steam condensers are as follows
0 1 Exhaust pressure or back pressure of steam is redtice t.herby
the capabilit y of prime mover to work is increased.
(ii) Exhaust steam from prime mover is condensed into water v.,hich
IS re-used as hot feed to boiler. B y doing so saving in watti- cost
in av he substa n tial in large steam power plant.
103. The function of it carburettor is to discharge into air steam the
desired quantity of liquid fuel, to atomise it and to produce a
homogeneous air fuel mixture.
104 1 1;) True ( h ) False )c) True (ii) False.
105 0 106. (a) 107. (h)
lOS. nt
109. There are usuall y two types ofstearn pressure gauges
I (ou rd on pressure gauge
Ut Diaphragm pressure gauge
lit). (z) Ill. ((1) 112. ((iTrup(b)True)elTrueftflTriie
113. The basic factors considered during the design of a nuclear power
reactor are as fell ''vs
(i) Reactor type
i:) Power rating ufrenctom in megawatts
(it,) (...nla ot SyStem
(it ) Control svste in
(I) Rates of neut run production and tit> ion
696 POWER PLANT
•1
POWER PLANT
698
142. (i) Axial flow (ii) Centrifugal type (iii) Positive displacement.
143. (a) Less than 20 m (b) Less than 150 in (c) Less than 500 in.
144. (i) Stone masonry (ii) Concrete and R.C.0 (iii) Earth (iv) Rock
pieces and fragments.
145. (i) When good rock y foundation strata are not available
(it) When height of darn is more than approximately 250 in.
146. (t) Liver flow dams
(u) Non over flow dams.
147. Arch dams can be described under the following three types.
(i) Constant radius arch dam
(ii) Constant angle arch dam
(iii) Variable radius an6 variable angle arch darn.
148. (i) Gravity darn (ii) Arch dam (iii) Buttress darn (iv) Earthen
dam.
149. (i) Kaplan or Francis turbine
(ii) Francis or Pelton turbine
(iii) Pelton turbine.
150. (i) Radial (ii) Axial.
151. (i) Runner is that portion of a reaction turbine which revolves
and converts the water head into mechanical energy.
(ii) Spillways are the structures provided with darn to allow a
-,I
178. (b)
179. (i) The best sites for WECS are found offshore and the sea Coast.
(ii) The second best site are in mountains.
180. Advantages:
(i) It is a renewable source of energy
(ii) It is non-polluting
(iii) Low cost.
Disadvantages:
(i) It is dilute and fluctuating in nature.
(ii) It is noisy in operation.
(iii) Large areas are needed.
181. (a) -. 182 Air, fuel and water
183. (b)
184. (i) Pulverised fuel firing method can handle successfully high as)
coals which can not be fired easily by conventional burninl
methods.
(ii) High temperature is the furnace can be achieved.
185. (a) 186. (b) 187. (c)
188. (b)
189. (i) Dolomite (ii) Fused alumina (iii) Zirconia
190. (i) True (ii) True (iii) True.
191. (i) (e) (ii) (0) (iii) (d) (iv) (b) (v) (/) (vi) (c)
192. (a) 5(b) 1.3 (c) Peak toad plant d) 800-900C
194. (a)True(b)True
195. (i) Pressure, filters (ii) Gravity filters
196(a).
Appendix A
CONVERSION TABLES
(i) Length
- 1 inch = 2.54 cm
1 foot = 30.48 cm
1 yard = 0.9143 metre
1 metre 3.28 feet = 39.37 inches
1 t(micron) = 3.281 x 10- 6 ft
=O.00lmm
(u)Area
1 M2= 10.7639 ft2
1 inch 2 = 6.4516 cm2
(iii) Weight
1 ton = 1.016 tonnes
1 kg = 2.204 lb
llb=453.6gm.
I Imperial gallon of water weights 10 lb
(iv) Volume
1 Cu. ft. = 0.0283 cu. m.
1 Cu. in. = 16.39 cu. cm.
I Imperial gallon = 4.543 litres.
(v) Density
1 kg/rn 3 = 0.062 lb/ft3
1 lb/ft2 = 16.02 kg/M2
(vi) Energy
1 ft. lb = 0.13825 kg.m
1 kcal (kilocalories) = 3.961 B.T.U.
1 H.P. (F.P.S. units) = 746 watts
1 metric H.P. = 735.5 watts = 0.7355 kW
1 H.P. = 2544 B.T.U. per hour
1 kcal/kg = 1.8 B.T.UJIb
1 metric H.P. = 4500 kg-m/minnte
= 10.54 kcal per minute
1 British H.P. = 550 ft. lb per second
1 kWh (kilowatt-hour) = 3413 B.T.U.
702 POWER PLANT
= 860 kcal.
1 erg = 2.78 x iO kWh
1 joule = 107ergs
1 kg-rn = 2.34 x 10 kcal
1 kW = 1 kJ/sec.
1 eV = 1.6 x 1012 erg = 1.6 x 10-10 joules.
(vii) Pressure
1 standard atmosphere = 14.696 p.s.i
= 1.033 kg/cm2
29.92 inches of mercury
= 760 mm of mercury
= 10.332 tn HO
= 33.8985 feet H20
1 cm of Hg = 0.01359 kg/cm3
1 p.s.i. = 0.0703 kg/cm!
1 kg/cm3 = I ata = 754.6 mmHg.
1 mm of'iater = 1 kg/rn2
(viii) Temperature
K=273+C
°R= 460 + 'F
where °K = Degree Kelvin
= Degree Rankiiie
'C = Degre Centigrade.
j4;' •
Appendix B
Properties of Dry Saturated Steam
Entropy
Pressure Snfuru Sensible Latent Total I Specific Liquid Vapour
p kg/sq lion heat hw heat L hct ii ilunie Ol
cm tempera- k(-al/kg kcal/kg kcalikg Vsin'/kg kcal/kg kcal/kg
lure
K
T (C)
0.02 17.1
L.Lj
I 17.1 5.8 6022 6827
H(7)
2.0803
0.0428.6 286 580.3J_ 6809 3546 0.0936 2.0219
0.06 35.8 3 5.8 6114 24.19 0.1232 1.9880
0.08 41.1 41.1 572.9 614.0 18.45 0.1407 1.9642
0.10 45.4 6570.5 6159 1 14.96 0.1539 1.9458
0j2 49M 686 6176 L' 26 ° 0J652 1.9308
0.13 59.6 660 619.6 I 10.22 0A892 1.9126
0.20 59.7 63.6 622.3 7.797 0.2976 1.8892
025 6459k q 6245146.325 2I24 1.8712
0.30 68.7 57.9 -.626.3
- 5.331 0.2242 J8562
0.35 72.3 72.3555.5 627.8 4.614 1 0.2348 1.8444
0.40 75.4 75.4 553.8 62 .2 02439
1.6334
0.50
0.60
80.9
85.5
809
855 f547.0
L550.6 631.5 3.304 LO 2593
1.8156
633.4 L2.785 L0.21.8019
0.70 89.3 89.3 545.8 635.1 2.411 0.2832 1.7889
0.80 93.0 93.0 ..J 543.5 6362 2.128 0.2931
0.90 96.2 .--962
962J 541.4 637.8 1.7693
1.806 L03018
1.0 _3.9.1 i 536.8 639.0 1.727 0.3056 1.7600
104.1 104.1 536.9 641.0 1.457 0.3235 1.7467
1.4 118.7 108.9 533.9 6428 1 261 0.3354 1.7344
2 7 112.9531.4 644.3 1.113 0.3460 1.7283
1.86.3 116.5 529.1 645.7 0.996 0.3554 1.7148
96 1199 527.0 646.9 0 903 0.3639 i
2 6.8 127.2 522.0 649.5 0.7341 0.3823 1.6888
M2.51 2.2 133.4 5182 651.6 0.6180 1 0.3977 1.6748
3.5 1382 138.4'1 514.5 653.4 0.5352 0.4 110 1 6625
4.0 142.9 1417 1 511.2 654.9 0.4418 0.4227 1.6515
4.5 - 147.2 148.1 L £P-±4 33 1 6425
5.0 rMJ15245L .2.42.3825iQ!.6311
55 154.7 155.9 5025 658.4 0.3489
--- -.----
0.4515 16295
1
6.0 158.1 I 159.4 L 499.94 6593 03222 1 0.4596 1.6165
O29O4671l 165
7.0 164.2 165.7 495.2 I 6609 1 -
0 2785
-- -0.1742 1.6075 1
L1 5 168.7 L4930 6617
02609 0.4808 ----I
L60 . [_ 0 .J7j4 - 430.9T6623 1 02111
i3 (5) I
L8.5 !_i- 1 u -662.9 T 2217
19 50I3
9.0 -14.5 I7'• 4..' 663.4 0.2195 . 04985 15562
10 --1179.0 181.3 4, 1 i 664.40i985 05090 1.5775
11832 147920181:1 i 08615698
12
L_ 187.1 189.9 470.1 665.9 9.1668 0.5335 1.5628
13 190.7 193.9 473.0 666.6 0.1415 0.5358 1 5556
--
L 14 4 4.S' 4i
l 3I 469.4 L 7.o I oi4s8o5336 i5493
15 1974 ,j, 200.7 I 466.7 667.4 0.1346 1 0 5508 1 5432
16 200.4 204.0 163.4 667.8 0,1164 0.5577 1.5375
17 203.4 207.1 461.1 6682 0.1192 j.5643 15321
18 206.2 210.1 1 458.2 1 6683 0128 0.5705 1.5270i
19 L 2088 . 455.5 668.5 0.1070 05764 1.5220
20 211.4 215.8 452.9 668.7 0.1027 9.5821 1,5173
22 216.2 221.0 4479 668 9
-_ L 220.8 6.04 JiI.0 401)350L06026 '15504
268 40.0785 I 1.4 92 1
26 829.0 2250 433.8 668.8 0.0725 0.6205 L4850 -1
30 i 232.6 23111 --429.5
- 668.6 0.06802 0.6287
"t'r - 1.4780
32 2364 243.1 425.2 .4 0.06372 06364 -- 1.4813
344_239MJ 421.1 6685 0.05991 37±L450
L 230.1 417.1 L. 0.0565 1 .
[_38 24.2 -. 254.1 413.0 667 1 005365 9,6573 1.4530 I
F40 i 2492 257.4 409:2 6666 0.05169 0.6637 114474
E 42 252.1 267: 405.666.5 0.04817 0,6698 1 1.4478
44 254.5 26394 401,6 6665 01)4588 1.4365
L 46 257.6 266.9 397.9 6648 0.04378 0.6813 J 1.4314
48 260.2 269.8 394.2J 664.1 0.04185 L_1215
50 2627 272.7 390.7 0.04007 0.6921 I 14215J
55 268.7 279.6 819661.5 0. O3616t' 7046 1.4098
60 - 274.3 286.1 . 373 4 1 6595 003289 0.7162
65 279.6 292.2 . 365.3 0.03009 0.7270 .1. 2211
70 284.5 299.0 359.3 1 6573 0.02469 0.7371 j 1.378J
Ej80 1 293.6 308.8 341.8 650.6 L 0.02374 0.7557 1.3591
90 . 301.1 319._j 326.6 I 6456 L 0.02064 0.7731 _1413
100 1 309.5 3287 318.8 640.5 1 001815 , 07893 13245
150 340.5 374.1 338.8 612.9 001044 1 3.8622 1.2514
200 4272 H728 oTo 9404 1.1715
LP_ 1 _374.0 1 501.1j 501.1L0 00310Q
APPENDIX
705
Properties of Superheated Steam
0.10 617 619 642 664.5 687.5 710.1 734 758 782.0 807 832.5 1
834.3
0.51J 6:31.5 641 664 687 710 734 737.5 782 807
1.00 639.3 - 632 663 686.3 710 733.5 757.5 782 806.5 S32 858
th
- 669 718.5 746 772.5 7995 826 853
3001 (108.6 - - -
- 683.5 715J435 771 797.5 824.5 85
(1007 5966
000829
I FZ 108.2
157.3
595.3
5:150
4_js 5
399.0
I 0.1095:3 I
147.2
137.8 8
7
( 2)
(1 01020
0.01090
_iii.1IiiIJFiII.
129.1
121.0
59:1.2
592,))
600.2
600.7
8
9 0.01170 113.4 592.1 600.1
10 0,01251 106.4 591.6 61)1.6
0.01338 -1 . 602
12 0.01429 93.90 590.5 602.5
13 (1.01556 88.19 589 9 602.9
14 0.0163 82.91 589.4 603.4
15 0.0174 77.90 588.8 603.0
16 0.0185 73.40 588.3 601.3
17 0.0197 69.10 587.7 604.6
18 0.0210 65.10 587.1 6(15 1
19 0.0224 69.35 586.6 605,0
20 0.0238 57.81 586.0 606.6
21 0.0254 54.56 585.5 606.5
22 0.0274 5 1.49 544 9 "06 0
23 0.0286 48.63 584.3 607.3
24 0.0304 45.L4 583.8 6(17.8
25 0,0323 43.41 583.3 608.2
26 0.0342 41.04 582.6 608.6
27 - 0.0263 38.82 582.1 609.5
28 0.0386 36.78 581.5 6(19.5
29 0.0408 34.77 581.0 . (100
30 0.114:32 32.93 581) 4 6(0.4
31 0.0458 :31.30 579.8 610.8
32 0.0485 29.60 579.3 611 .3
33 0.0513 28.05 578.3 611 '7
34 ()0542_, 26.61 578 1_,1___
612
36 0.0606 7 22 57 57711 613.))
613.4
37 0.064)) 22.77 56.4
38 0.0676 21.66 575.9 613 9
39 0,0713 28.56 5751 614.6
40 0.0752 19,55 574 7 614.3
41 0 ((793 18.60 574,1 615,2
42 00836 17.70 573.6 61.5,1;
43 0E01i81 16.85 5730 616.1)
44 0,11928 16.04 572.4 616.1
45 00977 15,28 571.8 611; 8
- 46 0.10S 14.56 571 2 17 2
47 - ().103 1:3.48 570.7
JOTh 13,23 - 570.1
49 120 _,j;1__-, 618.5
APPENDIX
ii ---IIIII1I
J
50 ,__
(2)
0.126 12.03
(4)
569.0 61 'JJJ
707