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Prestressed Concrete Girder Bridge AT KM 105 + 545 On Topi Darband Road

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1

PRESTRESSED CONCRETE GIRDER BRIDGE


AT KM 105 + 545
ON TOPI DARBAND ROAD
INTRODUCTION
This document is prepared for the Prestressed Pre Cast Girders and R.C.C. deck slab bridge situated on SWABI
TOPI DARBAND road at KM 105 + 545. This document is submitted as part of the Contract Agreement between the
Consultants M/S KHYBER CONSULTING ENGINEERS (KCE) and the Client NATIONAL HIGHWAY AUTHORITY
(NHA) for design of the SWABITOPIDARBAND road. AASHTO LRFD 1994, (BRIDGE DESIGN SPECIFICATIONS),
is the governing code.

1. GENERAL INFORMATION
1.1 DESIGN SPECIFICATION
1.1.1

AASHTO LRFD code 1994 (BRIDGE DESIGN SPECIFICATIONS)

1.1.2

AASHTO Standard specifications 1996.

1.1.3

Pakistan Code of Practice for Highway Bridges (PCPHB) 1967.

1.2 DESIGN PHILOSOPHY

(Limit states, of AASHTO LRFD 1994)

1.2.1

Service limit state (Flexural design of PC Girders and stability check of the abutments).

1.2.2

Strength limit state (Design of all the structural components except PC girders).

1.2.3

Fatigue limit state (Design of PC girders).


Note: The bridge is a single span simply supported so it does not need to be investigated
for the Extreme Event Limit States (Sec. 4.7.4.2).

1.3 LIVE LOADS


1.3.1

Single Lane of Military Class 70 Loading

(PCPHB, 1967.).

1.3.2

Class A Loading (PCPHB).

1.3.3

HS20-44 Truck (AASHTO standard 1996).

1.3.4

Design Lane Load plus Design Truck (HL 93, AASHTO LRFD 1994).

1.3.5

Design Lane Load plus Design Tandem (HL 93, AASHTO LRFD 1994).

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1.4 HYDROLOGICAL INFORMATION (Ref: AASHTO LRFD)


1.4.1

Catchment area

= 2.02 Km2.

1.4.2

Discharge (100 years)

= 29.33 m3/sec.

1.4.3

Time of concentration

= 1.31 hrs.

1.4.4

Scour Depth with respect to H.F.L.

= 1.35 meters.

1.4.5

Coefficient of run off

= 0.6

1.4.6

Lacey s silt factor

= 1.25

Note: The finished road elevations determine height of the Bridge; H.F.L. shown on the drawings is
the flood that can pass easily under the Bridge.
1.5

GEOTECHNICAL INFORMATION
soil

1.5.1

Unit weight of the soil under the abutment foundation

1.5.2

Angle of internal friction of the granular backfill

1.5.3

Presumptive allowable bearing capacity (Ref: AASHTO LRFD code)

1.5.4

Recommended value to be used for the general geology anticipated


at the bridge site (Foliated metamorphic rock: Slate, Schist)

= 17300 N/m3.

= 35
2.9 to 3.8 MPa.
= 3.4 MPa.

Note: Presumptive allowable bearing capacity is by no mean a substitute for proper soil investigation.
Detailed geotechnical investigation must be carried out, to finalize the bearing capacity, at the time of
construction (Based on the agreed proposition) and the Sub Structure will be updated accordingly.

Rational formula for discharges (Hydrology in Practice by Elezabeth M. Shaw pp/297).


Hydrology in Practice by Elizabeth M. Shaw pp/298).

Ref: Lacey s scour depth equation for regime channels.

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2. SUPER STRUCTURE DESIGN


2.1

GENERAL IFORMATIONS ABOUT BRIDGE GEOMETRY (Ref: AASHTO LRFD)

2.1.1

No. of Spans

=1

2.1.2

Each Span Length

= 30 meters.

2.1.3

Total Span Length

= 30 meters.

2.1.4

Effective Span Length

2.1.5

Skew Angle

2.1.6

Type of Superstructure

Pre Cast Prestressed Concrete


Girders and RCC Deck Slab.

2.1.7

No. of Girders per Span

= 4

2.1.8

Clear Width of the Bridge

= 8500 mm.

2.1.9

Total Width of the Bridge

= 10100 mm.

2.1.10

No. of Diaphragms per Span

2.1.11

Type of guardrail

= 29.3 meters.
= 0

=5
R.C.C. Guard Rail Post and Pre-cast
Guard Rails.

Note: Detailed dimensions of the PC girders, diaphragms, deck slab, footpaths (safety curbs) and
railings are shown in the drawings whereas a General Cross Section of the Bridge is shown below:

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2.2

GENERAL IFORMATIONS ABOUT DESIGN PARAMETERS (Ref: AASHTO LRFD)

2.2.1 Resistance factors, , are:


2.2.1.1

Flexure and tension of reinforced concrete

= 0.90

2.2.1.2

Shear and torsion in normal density concrete

= 0.90

2.2.1.3

Axial compression with spirals and ties

2.2.1.4

Bearing on concrete

= 0.70

2.2.2 Load modifiers are :


2.2.2.1

Ductility, nD

2.2.2.2

Redundancy, nR

2.2.2.3

Operational importance, nI

= 0.75

Strength
1.0
1.0

Service
1.0
1.0

Fatigue
1.0
1.0

1.0

N/A

N/A

2.2.3 Load combinations and Load factors: Following limit states are investigated.
2.2.3.1

Service I limit state

2.2.3.2

Strength I Limit State

2.2.3.3

Fatigue Limit State

2.2.4 Live load distribution factors (per lane) are:


2.2.4.1

For bending moment in interior girders

= 0.744

2.2.4.2

For bending moment in exterior girders

2.2.4.3

Factor for shear in interior girders

= 0.846

2.2.4.4

Factor for shear in exterior girders

= 0.846

= 0.744

Note: Load factors relative to moment and shear AASHTO LRFD code 1994 are used.
2.2.5 Dynamic load allowance (not applied to the design lane load) are:
2.2.5.1

For Fatigue Limit State

IMFati-

= 15 %

2.2.5.2

For all HL 93 loading (AASHTO LRFD code 1994)

IM

= 33 %

2.2.5.3

For Class A loading of the PCPHB

IM

= 13 %

2.2.5.4

For Military Class 70 Ton loading of the PCPHB

IM

= 10 %

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2.3

STRUCTURAL BEHAVIOR

2.3.1

Type of the Structure

Simply supported

2.3.2

Interaction between the Girder and Deck Slab

Acting as I-Beam for self


weight of the girder, weight
of the deck slab &weight of
the diaphragms and acting as a
composite section for the Live Load &
superimposed dead loads of the
wearing coarse, curbs and guard
railings.

2.3.3

Interaction between Diaphragm, Girder and


Deck Slab

The diaphragms are primarily acting


as bracing element.

2.3.4

Structural model for bridge design

2.4

Beam line method: The use of


Distribution Factors recommended by
AASHTO LRFD takes into account
structural interaction among various
girders and deck slab. The D.Fs. are
either based on 2 D Grillage model
or 3 - D Finite Element analysis of
eccentrically stiffened shell assembly.

MATERIAL PROPERTIES

2.4.1

Concrete used in the PC girders

Class D concrete of 28 days cylinder


compressive strength of 350 kg/cm2
(35 MPa.).

2.4.2

Strength of concrete at transfer

Minimum 280 kg/cm2 (28 Mpa.).

2.4.3

Concrete used in the deck slab, diaphragms,


Curbs, railings, back walls, wing walls,
transom/girder seat, rollovers and footings.

Class A concrete of 28 days


cylinder compressive strength of
210 kg/cm2 (21 MPa.).

2.4.4

High strength steel used in the PC girders

Stress relived low relaxation


Grade 270 (1860 MPa.) 7 wire
strands, conforming to ASTM A-416

2.4.5

Stress in the high strength steel at mid section


immediately after transfer (excluding F. Losses)

69 % of the ultimate strength


(i.e. 0.69 * fpu)

2.4.6

Normal reinforcement steel

Grade 60 (414 MPa) deformed round


bars confirming to ASTM A-615.

2.4.7

Modulus of elasticity of prestressing steel strands

Ep

= 197,000 MPa.

2.4.8

Modulus of elasticity of reinforcing steel

Es

= 200,000 MPa.

2.4.9

Modulus of elasticity of concrete

Ec

= 4800*

f c MPa.

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2.5

GEOMETRICAL PROPERTIES OF THE PC GIRDERS

2.5.1

Height of the Girder

= 1850 mm.

2.5.2

Top flange width

= 500 mm.

2.5.3

Bottom flange width

= 600 mm.

2.5.4

Web thickness

= 170 mm.

2.5.5

Effective flange width

Beff

= 2525 mm.

2.5.6

Cross sectional area of the I Beam

Ag

= 580525 mm2.

2.5.7

Distance of Neutral Axis of I-Section from Bot- fibers

Yb-I

= 788.136 mm.

2.5.8

Distance of Neutral Axis of I-Section from Top fibers

Yt-I

= 1061.864 mm.

2.5.9

Distance of N.A of Comp- section from Bot-fibers

Yb-c

= 1255.86 mm.

2.5.10

Distance of N.A of Comp- section from Top-fibers

Yt-c

= 794.14 mm.

2.5.11

Moment of inertia of the I-Section

II-Sec

= 2.235 E+11 mm4.

2.5.12

Moment of inertia of the Composite section

Ic-Sec

= 5.403 E+11 mm4.

Note: X Section at the mid section, End Block and Tendon arrangement at the end are shown in the
figures on the next page.

Tendon arrangement at End Block, End Block Details and X Section at mid section

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2.6

APPLIED MOMENTS ON THE PC GIRDERS

2.6.1

Service dead load moment due to self-weight of the girder

Mgirder

= 1.495 x 106 N m.

2.6.2

Service dead load moment due to weight of the deck slab

Mslab

= 1.301 x 106 N m.

2.6.3

Service dead load moment due to weight of the diaphragms

Mdiaph

= 0.248 x 106 N m.

2.6.4

Service dead load moment due to weight of the wearing coarse,


safety curbs and railings.

Ms.i.d.

= 0.438 x 106 N m.

2.6.5

Service live load moment

ML.L.

= 2.706 x 106 N m

Note: HL 93, AASHTO LRFD 1994 code provisions for max- live load moment governs.
2.7

PRESTRESSED CONCRETE GIRDER DESIGN INFORMATION.


2.7.1

Type of prestressing steel used

7 wire strands of Grade 270


(1860 MPa.)

2.7.2

Diameter of the strand

2.7.3

Area of the prestressing steel (3 tendons/36 strands)

2.7.4

No. of tendons per girder

=3

2.7.5

No. of strands per tendon

= 12

2.7.6

Diameter of the grooved rigid metallic sheath pipe

= 69 mm

= 12.7 mm (0.5)
Ap

= 3554 mm2.

Note: Stressing/Jacking shall be performed form both ends with STRONGHOLD or equivalent
system. Net stresses (at mid section) in all the tendons immediately after transfer of prestress force
to girders is 0.69*fpu. Also, net jacking force in each tendon is:
Fo = 1.522 x 106 N.
2.8

NET JACKING FORCE IN THE TENDONS BEFORE RELEASE AND CORRESPONDING ELONGATION OF
THE TENDONS.
Tendon No.
1
2
3

Force in the Tendons


N
Kg
1.652 x 106
168460
1.664 x 106
169702
1.676 x 106
170940

Elongation of steel in each


tendon (mm)
215
216
218

Note: The loads and elongation given are the total quantities. Half of the elongation shall be achieved
at each end.

Weigh in motion records at various bridge sites of Pakistan indicates a truck configuration of 3-Axle 45 Ton (Abbreviated as PK3A45 by Khyber
Consulting Engineers) will cause 2.561 x 106 N m including an Impact of 13 %.

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2.9

PRESTRESS LOSSES IN THE TENDONS


2.9.1

Loss due to elastic shortening of concrete

= 2.58 %.

2.9.2

Loss due shrinkage of concrete

= 3.931 %.

2.9.3

Loss due to creep of concrete

= 7.579 %

2.9.4

Loss due to relaxation of steel

= 1.380 %.

2.9.5

Loss due to anchorage set/take up/Anchorage PULL IN

2.9.6

Frictional losses

= 3.062 %.
Frictional losses are different for each
Tendon due to difference in length
and angular change of the tendons.
k = 4.92X10-6 per mm (0.0015 per ft)
= 0.25

Wobble coefficient
Curvature coefficient
Frictional losses in the tendons are given below:
Frictional loss in Tendon No. 1

8.568 %

Frictional loss in Tendon No. 2

9.370 %

Frictional loss in Tendon No. 3

10.167 %

Note: Losses, jacking force and elongation given here are valid only for 7-wire strands.
2.10 STRESSES IN THE PC GIRDERS AT DIFFERENT STAGES OF LOADING.
2.10.1

Stresses in the Girder Immediately after Transfer (at mid section).


Type of Stresses

Extreme fiber stresses in tension


Extreme fiber stresses in compression
2.10.2

Applied Stresses
MPa
- 0.259
-13.507

Code Limiting Stress Values


MPa.
+1.313
-15.169

Stresses in the Girder at Working Load Condition/Service Load Condition


(at mid section).
Type of Stresses

Extreme fiber stresses in tension


Extreme fiber stresses in compression

Applied Stresses
MPa
+ 2.702
- 13.344

Code Limiting Stress Values


MPa
+ 2.936
-15.514

Note: All the stresses are checked at the mid-section (span) of the girder

Sec. 9.16.1, AASHTO standard 1996.


Note: Value of the Wobble coefficient given in Sec. 5.9.5.2.2b of AASHTO LRFD 1994 code is 7.45 times less than the value given by AASHTO
standard 1996 code. We have adopted the Conservative (AASHTO standard) value.

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2.11 SHEAR DESIGN OF THE PC GIRDERS (Ref: AASHTO LRFD)
2.11.1

Ultimate applied shear force

Vu

= 1.295 x 106 N.

2.11.2

Ultimate moment corresponding to the ultimate shear

Mu

= 0.879 x 106 N m.

2.11.3

Effective depth for shear

dv

= 1566 mm.

2.11.4

Effective width of the web

bv

= 135.5 mm.

2.11.5

Angle of the tendon force with the C.L. of the girder (average)

= 6

2.11.6

Area of concrete at the end block

Ag

= 580525 mm2.

2.11.7

Depth of neutral axis at the end block

Yb-I

= 788.136 mm.

2.11.8

Moment of inertia of the girder at the end

Ig

= 2.35 x 1011 mm4.

2.11.9

Angle of inclination of diagonal compressive stresses

= 23.5

Factor indicating ability of diagonally cracked concrete to


transmit tension

= 2.935

2.11.11

Shear capacity of the concrete

Vc

= 305810 N.

2.11.12

Shear capacity of the girder due to Prestress force in the girder

Vp

= 470380 N.

2.11.13

Transverse reinforcement

2.11.14

Shear carried by the transverse reinforcement

2.11.15

Nominal shear capacity of the girder

Vn = Vc+Vs+ Vp = 1481950 N.

2.11.16

Effective shear resisting capacity of the girder

Vr = * Vn

2.11.17

Ratio of the shear resisting capacity to ultimate applied shear

= 1.03

2.11.18

Horizontal shear flow at the interface of Girder and Deck slab

= 374736 N/m.

2.11.19

Area of concrete engaged in shear transfer

Acv

= 500000 mm2.

2.11.20

Permanent net compressive force normal to the shear plane

Pc

= 14223 N/m.

2.11.21

Area of shear reinforcement crossing the shear plane

Avf

= 1065 mm2/m.

2.11.22

Cohesion factor

= 0.52 MPa.

2.11.23

Friction Factor

= 0.6

2.11.24

Nominal horizontal shear resistance of the interface plane

Vn

= 444898 N/m.

2.11.25

Effective horizontal shear resistance of the interface plane

Vr

= 400408 N/m.

2.11.26

Ratio of the horizontal shear resistance to the applied shear flow

= 1.074

2.11.10

10 stirrups @ 200 mm c/c.


Vs

= 705560 N.

= 1333755 N.

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2.12 DESIGN OF POST TENSIONED ANCHORAGE ZONE (Ref: AASHTO LRFD)
2.12.1

Design of General Zone

2.12.1.1

Load factor for the jacking force

P/S

2.12.1.2

Distance from the end at which stress is to be measured

= 175 mm.

2.12.1.3

Distance of the center of the bursting force parallel to the vertical


face of the girder

dburst1

= 925 mm.

2.12.1.4

Distance of the center of the bursting force parallel to the lateral


face of the girder

dburst2

= 250 mm.

2.12.1.5

Net stresses in the top fibers at distance of 175 mm

ft

= -4.724 N/mm2.

2.12.1.6

Net stresses in the bottom fibers at distance of 175 mm

2.12.1.7

Ultimate jacking force per tendon/bearing plate

Pu

= 1.826 x 106 N.

2.12.1.8

Thickness of the member

= 500 mm.

2.12.1.9

Center to center spacing of anchorage plates

= 500 mm.

2.12.1.10

Number of tendons in a row

=3

2.12.1.11

Limiting stress from the approximate analysis

fca

= -15.445 N/mm2.

2.12.1.12

Ratio of the limiting stress to applied stresses in top fibers

= 3.27

2.12.1.13

Ratio of the limiting stress to applied stresses in bottom fibers

= 2.58

2.12.1.14

Bursting force corresponding to dburst1

Tburst1

= 1.475 x 106 N.

2.12.1.15

Bursting force corresponding to dburst2

Tburst2

= 1.004 x 106 N.

2.12.1.16

Bursting reinforcement for Tburst1

16 12 bars @ 110 mm (both faces)

2.12.1.17

Bursting reinforcement for Tburst2

12 12 bars @ 110 mm (B.F.)


two layers of 6 bars each)

2.12.2

Design of Local Zone

2.12.2.1

Maximum area of the supporting surface

= 250,000 mm2.

2.12.2.2

Gross area of the bearing plate

Ag

= 90,000 mm2.

2.12.2.3

Effective net area of the bearing plate

Ab

= 82,146 mm2.

2.12.2.4

Factored bearing resistance of the anchorage

Pr

= 1.85 x 106 N.

2.12.2.5

Ratio of the bearing resistance Pr to ultimate jacking force Pu

fb

= 1.2

= -5.990 N/mm2.

= 1.013

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2.13 DEFLECTION IN THE PC GIRDERS
2.13.1

Deflection due to live load and its dynamic effect

= + 14.53 mm.

2.13.2

Deflection due to initial pretress force

= - 42.14 mm.

2.13.3

Deflection due to weight of the girder and deck slab

= + 37.57 mm.

2.13.4

Deflection due to weight of the diaphragms

= + 5.07 mm.

2.13.5

Deflection due to weight of the curbs, railings and wearing coarse

2.13.6

Net deflection at working load condition

= + 19.35 mm.

2.13.7

Allowable deflection due to total loads for simply supported structures

= + 61.04 mm.

2.13.8

Allowable deflection due to live load and its dynamic effect

= 36.63 mm.

2.13.9

Ratio of allowable net deflection to applied net deflection

= 3.15

2.13.10

= + 3.21 mm.

Ratio of allowable live load deflection to applied live load deflection

= 2.52

Note: Net deflection is within the allowable limits.


2.14

DESIGN OF DECK SLAB (Ref: AASHTO LRFD)

2.14.1

Minimum depth of the deck slab (Sec. 9.7.1.1, AASHTO LRFD 1994)

= 175 mm.

2.14.2

Thickness of the deck slab

= 200 mm.

2.14.3

Width of strip for positive moment (+M)

= 2049 mm.

2.14.4

Width of strip for negative moment (-M)

= 1851 mm.

2.14.5

Primary Reinforcement steel used

Grade 60 steel (ASTM A 615)

2.14.6

Secondary Reinforcement steel used


(Distribution and shrinkage steel)

Grade 40 steel (ASTM A 615)

2.14.7

Total service load positive moment

= 30769 N m.

2.14.8

Total service load negative moment

= 38721 N m.

2.14.9

Ultimate positive moment

= 52544 N m.

2.14.10

Ultimate negative moment

= 64392 N m.

2.14.11

Main positive reinforcement

16 @ 140 mm c/c.

2.14.12

Main negative reinforcement

16 @ 140 mm c/c.

2.14.13

Ultimate positive moment capacity of the deck slab

Md(+ve)

= 72480 N m.

Sec.8.9.3.1, AASHTO standard 1996 & Sec. 2.5.2.6.2, AASHTO LRFD 1994.

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2.14.14

Ultimate negative moment capacity of the deck slab

Md (-ve)

= 79186 N m.

2.14.15

Ratio of positive moment capacity to ultimate applied positive moment

= 1.38

2.14.16

Ratio of negative moment capacity to ultimate applied negative moment

= 1.23

Note: Strip method is used for design of the deck slab (Sec. 4.6.2.1 AASHTO LRFD 1994). Moments
are given for a unit width of a meter.
2.15

DIAPHRAGMS

2.15.1

Height of the diaphragm

= 1850 mm.

2.15.2

Width of the diaphragm

= 200 mm.

2.15.3

Structural action :

Primarily used as bracing element for stability and nominal


Longitudinal and transverse reinforcement is provided.

3. SUB STRUCTURE DESIGN


3.1

GENERAL INFORMATION

3.1.1

Type of abutment

Coarse Rubble Masonry.

3.1.2

Width of the abutment at the top

= 975 mm.

3.1.3

Width of the CRM wall at the bottom

= 4575 mm.

3.1.4

Length of the CRM wall

= 10100 mm.

3.1.5

Height of the CRM wall

= 8700 mm.

3.1.6

Total Height of abutment (to the deck Level)

= 12420 mm.

3.1.7

Type of footing

3.1.8

Width of footing

= 6575 mm.

3.1.9

Length of footing

= 10700 mm.

3.1.10

Depth of footing

= 1000 mm.

3.1.11

Type of pads

R.C.C. Open/Spread footing.

Elastomeric Bearing Pads

Note: Detailed dimensions of the abutment, abutment footing, wing walls, back wall, transom, and
rollover are shown on the drawings whereas a Cross Section of the Abutment is shown below.

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Cross Section of the Abutment Wall


3.2

STABILITY ANALYSIS OF THE ABUTMENTS.

3.2.1

Weight of the structure (including weight of the footing and backfill)


on the footing

= 12.13 x 106 N.

3.2.2

Total stabilizing force (weight of footing is not included)

= 5.46 x 106 N.

3.2.3

Total stabilizing moment about toe of the CRM wall

= 38.54 x 106 N m.

3.2.4

Total sliding force

= 3.53 x 106 N.

3.2.5

Total overturning moment about toe of the CRM wall

= 16.61 x 106 N m.

3.2.6

Coefficient of friction between the CRM wall and footing

3.2.7

Factor of safety against sliding

(F.O.S.)Sliding

= 1.55

3.2.8

Factor of safety against overturning

(F.O.S.)O.T.

= 2.32

= 0.45

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14
3.2.1

PRESSURE DISTRIBUTION AT BASE OF THE FOOTING.

3.2.1.1

Stresses at toe of the footing (minus sign shows compression)

qmax

= - 0.31 MPa.

3.2.1.2

Stresses at heel of the footing

qmin

= - 0.06 MPa.

3.2.1.3

Presumptive allowable bearing capacity (Ref: AASHTO LRFD)

2.9 to 3.8 MPa.

3.2.1.4

Recommended value of use

= 3.4 MPa.

3.2.1.5

Ratio of presumptive allowable bearing capacity to max stress at toe of footing

= 10.97

Pressure Distribution Diagram for the Abutment Footing

Distance from the toe


6.58

0.00

0.00

-0.05

-0.06
Pressure ( Mpa )

-0.10

-0.15

-0.20

-0.25

-0.30

-0.31

-0.35

PRESSURE DISTRIBUTION DIAGRAM FOR THE ABUTMENT FOOTING

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3.3

STRUCTURAL DESIGN OF SUB STRUCTURE ELEMENTS

3.3.1

DESIGN OF BEARING PADS (Ref: AASHTO LRFD)

3.3.1.1

Total service load on the bearing pad

PTotal

= 0.987 x 106 N.

3.3.1.2

Service live load on the bearing pad

PL.L.

= 0.491 x 106 N.

3.3.1.3

Thermal coefficient for normal density concrete

= 10.8 x 10-6 /C.

3.3.1.4

Shrinkage coefficient/Strain

3.3.1.5

Width of bearing pad

= 400 mm.

3.3.1.6

Length of bearing pad

= 300 mm.

3.3.1.7

Thickness of interior layers of Elastomer

hri

= 15 mm.

3.3.1.8

Number of interior layers of the Elastomer

=2

3.3.1.9

Total thickness of the Elastomer

hrt

= 45 mm.

3.3.1.10

Shape factor of each layer

Si

= 5.71

3.3.1.11

Shear modulus of the Elastomer

= 1.2 MPa.

3.3.1.12

Applied compressive stress due to total load

= 8.2 MPa.

3.3.1.13

Applied compressive stress due to live load

= 4.09 MPa.

3.3.1.14

Limiting compressive stress for the total load

= 11.0 MPa.

3.3.1.15

Limiting compressive stress for the live load

= 4.52 MPa.

3.3.1.16

Factor of safety against failure due to total load compressive stress

= 1.34

3.3.1.17

Factor of safety against failure due to live load compressive stress

= 1.11

3.3.1.18

Compressive strain

= 5.2 %

3.3.1.19

Compressive deflection

= 2.25 mm.

3.3.1.20

Total shear deformation

= 14.89 mm.

3.3.1.21

Net rotation due to dead and live loads

= 4.51 x 10-3 RAD.

3.3.1.22

Required thickness of the steel plate based on Service Limit State

hS

= 1.3 mm.

3.3.1.23

Required thickness of the steel plate based on Fatigue Limit State

hFat-

= 0.7 mm.

3.3.1.24

Thickness of the steel plate provided in the Bearing Pad

3.3.2

= 3.00 x 10-4.

= 1.5 mm.

DESIGN OF GIRDER SEAT/TRANSOM

3.3.2.1

Width of the transom

= 975 mm.

3.3.2.2

Depth of the transom

= 600 mm.

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3.3.2.3

Effective depth of the transom

= 544 mm.

3.3.2.4

Minimum area of steel

= 1705 mm2.

3.3.2.5

Moment of inertia of the transom

= 1.755 x 1010 mm4.

3.3.2.6

Modulus of elasticity of the transom concrete

= 21831 MPa.

3.3.2.7

Flexural rigidity of the transom

EI

=3.83 x 1014 N-mm2

3.3.2.8

Reinforcement steel

16 12 bars uniformly distributed.

Note: The transom is provided as a rigid element to distribute the load of super structure at top of the
abutment wall (CRM wall). Its flexural rigidity is more than sufficient to distribute the load uniformly
over the abutment and to take care for any localized differential settlement in CRM wall.
3.3.3

DESIGN OF WING WALLS

3.3.3.1

Thickness of the wing wall

= 300 mm.

3.3.3.2

Effective depth of wing wall

= 244 mm.

3.3.3.3

Ultimate moment on the interface of wing wall and backwall

3.3.3.4

Area of steel provided

= 1922 mm2.

3.3.3.5

Moment capacity of the wing wall with As-mini

= 113744 N m.

3.3.3.6

Ratio of ultimate moment capacity to ultimate applied moment

= 1.25

3.3.3.7

Shrinkage and temperature steel

= 1100 mm2.

3.3.3.8

Main flexural reinforcement

12 @ 150 mm c/c (B.F.)

3.3.3.9

Shrinkage and temperature reinforcement

10 @ 140 mm c/c (B.F.)

= 91150 N m.

3.3.3.10

Ultimate shear at the interface of wing wall and backwall

3.3.3.11

Ultimate shear capacity of the wing wall

= 447640 N.

3.3.3.12

Ratio of the shear capacity and ultimate applied shear

= 4.91

3.3.4

= 91150 N.

DESIGN OF BACKWALL

3.3.4.1

Thickness of the Backwall

= 300 mm.

3.3.4.2

Effective depth of the backwall

= 244 mm.

3.3.4.3

Ultimate moment at base of the Backwall

3.3.4.4

Minimum area of steel

Mu

= 28971 N m/m
= 665 mm2/m

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3.3.4.5

Moment capacity of the section

3.3.4.6

Ratio of ultimate moment capacity and ultimate applied moment

3.3.4.7

Main reinforcement steel

12 @ 170 mm c/c. (B.F.)

3.3.4.8

Shrinkage steel

10 @ 150 mm c/c. (B.F.)

3.3.4.9

Ultimate shear at base of the Backwall

= 30830 N.

3.3.4.10

Ultimate shear capacity of the backwall

= 165794 N.

3.3.4.11

Ratio of the ultimate shear capacity to ultimate applied shear

= 5.4

3.3.5

= 39420 N m/m.
= 1.36

DESIGN OF THE ABUTMENT FOOTING

3.3.5.1

Width of the footing

= 6575 mm.

3.3.5.2

Length of the footing

= 12100 mm.

3.3.5.3

Depth of the footing

= 1000 mm.

3.3.5.4

Clear cover for the flexural steel

= 75 mm.

3.3.5.5

Effective depth of the footing

= 917 mm.

3.3.5.6

Applied punching shear on the footing

= 12.21 x 106 N.

3.3.5.7

Punching shear capacity of the footing

= 38.31 x 106 N.

3.3.5.8

Ratio of the punching shear capacity to applied punching shear

3.3.5.9

Applied beam shear

= 0.464 x 106 N.

3.3.5.10

Beam shear capacity of the footing

= 7.54 x 106 N.

3.3.5.11

Ratio of the beam shear capacity to the applied beam shear

= 16.24

3.3.5.12

Ultimate moment, in shorter direction, at face of the support

3.3.5.13

Reinforcement steel provided in shorter direction (A s-mini) 16 @ 180 mm c/c.

3.3.5.14

Ultimate moment capacity in shorter direction

3.3.5.15

Ratio of the ultimate moment capacity to ultimate


applied moment In shorter direction

3.3.5.16

Ultimate moment, in longer direction, at face of the support

3.3.5.17

Reinforcement steel provided longer direction (As-mini)

3.3.5.18

Ultimate moment capacity in longer direction

3.3.5.19

Ratio of the ultimate moment capacity to ultimate

= 3.14

Mu1

Mr1

= 0.231 x 106 N-m/m.

= 0.252 x 106 Nm/m.


= 1.09

Mu2

= 0.231 x 106 N-m/m.

16 @ 180 mm c/c.
Mr2

= 0.316 x 106 Nm/m.

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applied moment in longer direction

= 1.37

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