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GB705611A - Improved gas turbine power plant - Google Patents

Improved gas turbine power plant

Info

Publication number
GB705611A
GB705611A GB19976/51A GB1997651A GB705611A GB 705611 A GB705611 A GB 705611A GB 19976/51 A GB19976/51 A GB 19976/51A GB 1997651 A GB1997651 A GB 1997651A GB 705611 A GB705611 A GB 705611A
Authority
GB
United Kingdom
Prior art keywords
turbine
combustion chamber
gas turbine
air
plant
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB19976/51A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ROBERT HENRI FISCHER
Original Assignee
ROBERT HENRI FISCHER
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by ROBERT HENRI FISCHER filed Critical ROBERT HENRI FISCHER
Priority to GB19976/51A priority Critical patent/GB705611A/en
Publication of GB705611A publication Critical patent/GB705611A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

705,611. Gas turbine plant; jet propulsion plant. FISCHER, R. H. Nov. 27, 1951 [Aug. 24, 1951], No. 19976/51. Class 110 (3). [Also in Group XII] In a gas turbine plant comprising a combustion chamber and a compressor c disposed on opposite sides of the turbine rotor d, substantially the whole of the compressed air is fed through passages b in the turbine rotor to the combustion chamber in which the direction of the flow of said air is reversed whilst a part of the compressed air short circuits the combustion chamber and is used to cool the external surfaces of the turbine blades. The compressor which is of the axial flow or centrifugal type is formed integral with the turbine as shown. The turbine is of the impulse or reaction type and may either drive a power shaft h or feed a jet propulsion nozzle. The combustion chamber comprises an annular air-jacketed flame tube f having air inlet slits j, k as shown together with fuel injectors g and sparking plugs for starting purposes, starting being effected by an electric motor.
GB19976/51A 1951-08-24 1951-08-24 Improved gas turbine power plant Expired GB705611A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB19976/51A GB705611A (en) 1951-08-24 1951-08-24 Improved gas turbine power plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB19976/51A GB705611A (en) 1951-08-24 1951-08-24 Improved gas turbine power plant

Publications (1)

Publication Number Publication Date
GB705611A true GB705611A (en) 1954-03-17

Family

ID=10138249

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19976/51A Expired GB705611A (en) 1951-08-24 1951-08-24 Improved gas turbine power plant

Country Status (1)

Country Link
GB (1) GB705611A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE954465C (en) * 1954-11-05 1956-12-20 Daimler Benz Ag Combustion chamber, especially for smaller gas turbines
DE1079895B (en) * 1956-10-02 1960-04-14 Avco Mfg Corp Fuel evaporator for gas turbine combustion chambers
DE1091815B (en) * 1959-12-01 1960-10-27 Rudolf Haag Gas turbine with partial admission of fuel gas and compressed air to the turbine wheel
EP0173774A1 (en) * 1980-01-20 1986-03-12 Jacov Shapiro Gas turbine engine
US5111688A (en) * 1988-01-22 1992-05-12 Measurex Corporation Device and method for calibrating a non-destructive sheet strength measuring system
WO1997023715A2 (en) * 1995-12-21 1997-07-03 Siemens Aktiengesellschaft Process for operating a gas turbine and gas turbine operating in this way

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE954465C (en) * 1954-11-05 1956-12-20 Daimler Benz Ag Combustion chamber, especially for smaller gas turbines
DE1079895B (en) * 1956-10-02 1960-04-14 Avco Mfg Corp Fuel evaporator for gas turbine combustion chambers
DE1091815B (en) * 1959-12-01 1960-10-27 Rudolf Haag Gas turbine with partial admission of fuel gas and compressed air to the turbine wheel
EP0173774A1 (en) * 1980-01-20 1986-03-12 Jacov Shapiro Gas turbine engine
US5111688A (en) * 1988-01-22 1992-05-12 Measurex Corporation Device and method for calibrating a non-destructive sheet strength measuring system
WO1997023715A2 (en) * 1995-12-21 1997-07-03 Siemens Aktiengesellschaft Process for operating a gas turbine and gas turbine operating in this way
WO1997023715A3 (en) * 1995-12-21 1997-09-04 Siemens Ag Process for operating a gas turbine and gas turbine operating in this way

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