CA917933A - Combustion chamber for gas turbine - Google Patents

Combustion chamber for gas turbine

Info

Publication number
CA917933A
CA917933A CA062640A CA62640A CA917933A CA 917933 A CA917933 A CA 917933A CA 062640 A CA062640 A CA 062640A CA 62640 A CA62640 A CA 62640A CA 917933 A CA917933 A CA 917933A
Authority
CA
Canada
Prior art keywords
combustion chamber
gas turbine
turbine
gas
combustion
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
CA062640A
Inventor
Guillot Jack
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.)
Bennes Marrel SA
Original Assignee
Bennes Marrel SA
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 Bennes Marrel SA filed Critical Bennes Marrel SA
Application granted granted Critical
Publication of CA917933A publication Critical patent/CA917933A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
    • 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
    • F02C7/22—Fuel supply systems
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • 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

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)
  • Spray-Type Burners (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
CA062640A 1968-10-18 1969-09-22 Combustion chamber for gas turbine Expired CA917933A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR69050513 1968-10-18

Publications (1)

Publication Number Publication Date
CA917933A true CA917933A (en) 1973-01-02

Family

ID=9695675

Family Applications (1)

Application Number Title Priority Date Filing Date
CA062640A Expired CA917933A (en) 1968-10-18 1969-09-22 Combustion chamber for gas turbine

Country Status (11)

Country Link
US (1) US3650106A (en)
AT (2) AT279483B (en)
BR (1) BR6913235D0 (en)
CA (1) CA917933A (en)
CH (1) CH531643A (en)
DE (3) DE1966660A1 (en)
ES (1) ES372250A1 (en)
FR (1) FR1592591A (en)
GB (1) GB1251749A (en)
NL (1) NL6915497A (en)
SE (1) SE356332B (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5089708A (en) * 1973-12-14 1975-07-18
CH586375A5 (en) * 1975-06-25 1977-03-31 Bbc Brown Boveri & Cie
JPS5242907U (en) * 1975-09-22 1977-03-26
US4129985A (en) * 1975-11-17 1978-12-19 Kawasaki Jukogyo Kabushiki Kaisha Combustor device of gas turbine engine
US4900246A (en) * 1977-05-25 1990-02-13 Phillips Petroleum Company Apparatus for burning nitrogen-containing fuels
GB2040031B (en) * 1979-01-12 1983-02-09 Gen Electric Dual stage-dual mode low emission gas turbine combustion system
US4393651A (en) * 1980-09-02 1983-07-19 Chandler Evans Inc. Fuel control method and apparatus
GB9108235D0 (en) * 1991-04-17 1991-06-05 Rolls Royce Plc A combustion chamber assembly
US5361577A (en) * 1991-07-15 1994-11-08 General Electric Company Spring loaded cross-fire tube
EP2157286A1 (en) * 2008-08-21 2010-02-24 Siemens Aktiengesellschaft Gas turbine comprising angled duct and method for guiding the flow onto the turbine
US20110091829A1 (en) * 2009-10-20 2011-04-21 Vinayak Barve Multi-fuel combustion system
US9388738B2 (en) * 2011-10-04 2016-07-12 Siemens Energy, Inc. Casing for a gas turbine engine
US9328925B2 (en) * 2012-11-15 2016-05-03 General Electric Company Cross-fire tube purging arrangement and method of purging a cross-fire tube
US20140137536A1 (en) * 2012-11-21 2014-05-22 General Electric Company Super telescoping cross-fire tube and method of assembling a combustor structure
US9353952B2 (en) * 2012-11-29 2016-05-31 General Electric Company Crossfire tube assembly with tube bias between adjacent combustors
JP2015135212A (en) * 2014-01-17 2015-07-27 ヤンマー株式会社 gas turbine engine
US10161635B2 (en) * 2014-06-13 2018-12-25 Rolls-Royce Corporation Combustor with spring-loaded crossover tubes
JP6325930B2 (en) * 2014-07-24 2018-05-16 三菱日立パワーシステムズ株式会社 Gas turbine combustor
US10473117B2 (en) * 2015-07-22 2019-11-12 United Technologies Corporation Diffuser case for a gas powered turbine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2638745A (en) * 1943-04-01 1953-05-19 Power Jets Res & Dev Ltd Gas turbine combustor having tangential air inlets for primary and secondary air
US3172257A (en) * 1962-08-30 1965-03-09 Ingersoll Rand Co Hot gas power plant arrangement
GB998371A (en) * 1964-05-04 1965-07-14 Rolls Royce Ignition means for a continuous flow engine
CH434875A (en) * 1966-06-21 1967-04-30 Huber Robert Fuel injection valve with electromagnetic actuation

Also Published As

Publication number Publication date
AT279483B (en) 1970-03-10
DE1946905A1 (en) 1970-05-06
BR6913235D0 (en) 1973-01-02
SE356332B (en) 1973-05-21
GB1251749A (en) 1971-10-27
US3650106A (en) 1972-03-21
FR1592591A (en) 1970-05-19
DE1966660A1 (en) 1973-07-12
NL6915497A (en) 1970-04-21
ES372250A1 (en) 1971-10-16
DE1966661A1 (en) 1973-07-12
DE1946905B2 (en) 1973-09-13
AT301271B (en) 1972-07-15
CH531643A (en) 1972-12-15

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