JPS54158729A - Liner cooling method and device of combustion device - Google Patents

Liner cooling method and device of combustion device

Info

Publication number
JPS54158729A
JPS54158729A JP3713979A JP3713979A JPS54158729A JP S54158729 A JPS54158729 A JP S54158729A JP 3713979 A JP3713979 A JP 3713979A JP 3713979 A JP3713979 A JP 3713979A JP S54158729 A JPS54158729 A JP S54158729A
Authority
JP
Japan
Prior art keywords
cooling method
liner cooling
combustion
combustion device
liner
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.)
Pending
Application number
JP3713979A
Other languages
Japanese (ja)
Inventor
Jieemusu Kenuootei Miruton
Riyuuisu Fuorutsu Hawaado
Kaaru Kingu Robaato
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JPS54158729A publication Critical patent/JPS54158729A/en
Pending 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/045—Air inlet arrangements using pipes
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Spray-Type Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Separation Using Semi-Permeable Membranes (AREA)
JP3713979A 1978-04-04 1979-03-30 Liner cooling method and device of combustion device Pending JPS54158729A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US89322178A 1978-04-04 1978-04-04

Publications (1)

Publication Number Publication Date
JPS54158729A true JPS54158729A (en) 1979-12-14

Family

ID=25401226

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3713979A Pending JPS54158729A (en) 1978-04-04 1979-03-30 Liner cooling method and device of combustion device

Country Status (5)

Country Link
JP (1) JPS54158729A (en)
DE (1) DE2913223A1 (en)
FR (1) FR2422035A1 (en)
GB (1) GB2017827B (en)
IT (1) IT1163665B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5932862U (en) * 1982-08-27 1984-02-29 三菱重工業株式会社 gas turbine combustor
JPS6287733A (en) * 1985-10-04 1987-04-22 エム・テ−・ウ−・モト−レン−・ウント・ツルビ−ネン−ウニオ−ン・ミユンヘン・ゲゼルシヤフト・ミツト・ベシユレンクテル・ハフツング Combustion chamber for gas turbine drive

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4132066A (en) * 1977-09-23 1979-01-02 United Technologies Corporation Combustor liner for gas turbine engine
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
US4622821A (en) * 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
FR2599821B1 (en) * 1986-06-04 1988-09-02 Snecma COMBUSTION CHAMBER FOR TURBOMACHINES WITH MIXING HOLES PROVIDING THE POSITIONING OF THE HOT WALL ON THE COLD WALL
WO1989012788A1 (en) * 1988-06-22 1989-12-28 The Secretary Of State For Defence In Her Britanni Gas turbine engine combustors
FR2714152B1 (en) * 1993-12-22 1996-01-19 Snecma Device for fixing a thermal protection tile in a combustion chamber.
DE19508110A1 (en) * 1995-03-08 1996-09-12 Bmw Rolls Royce Gmbh Combustion chamber of gas turbine
DE19547703C2 (en) * 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Combustion chamber, in particular ring combustion chamber, for gas turbine engines
GB9919981D0 (en) * 1999-08-24 1999-10-27 Rolls Royce Plc Combustion apparatus
FR2826102B1 (en) * 2001-06-19 2004-01-02 Snecma Moteurs IMPROVEMENTS TO GAS TURBINE COMBUSTION CHAMBERS
US8387396B2 (en) * 2007-01-09 2013-03-05 General Electric Company Airfoil, sleeve, and method for assembling a combustor assembly
US20130074471A1 (en) * 2011-09-22 2013-03-28 General Electric Company Turbine combustor and method for temperature control and damping a portion of a combustor
GB201116608D0 (en) * 2011-09-27 2011-11-09 Rolls Royce Plc A method of operating a combustion chamber
US20130283806A1 (en) * 2012-04-26 2013-10-31 General Electric Company Combustor and a method for repairing the combustor
WO2015116269A2 (en) * 2013-11-04 2015-08-06 United Technologies Corporation Quench aperture body for a turbine engine combustor
US10968829B2 (en) 2013-12-06 2021-04-06 Raytheon Technologies Corporation Cooling an igniter body of a combustor wall
EP3077640B1 (en) * 2013-12-06 2021-06-02 Raytheon Technologies Corporation Combustor quench aperture cooling
US10443848B2 (en) * 2014-04-02 2019-10-15 United Technologies Corporation Grommet assembly and method of design
CN105091030A (en) * 2014-05-23 2015-11-25 中航商用航空发动机有限责任公司 Sleeve for flame tube and flame tube
US9976743B2 (en) 2014-07-03 2018-05-22 United Technologies Corporation Dilution hole assembly
US20160178199A1 (en) * 2014-12-17 2016-06-23 United Technologies Corporation Combustor dilution hole active heat transfer control apparatus and system
EP3037725B1 (en) 2014-12-22 2018-10-31 Ansaldo Energia Switzerland AG Mixer for admixing a dilution air to the hot gas flow
US20160209035A1 (en) * 2015-01-16 2016-07-21 Solar Turbines Incorporated Combustion hole insert with integrated film restarter
US10094564B2 (en) * 2015-04-17 2018-10-09 Pratt & Whitney Canada Corp. Combustor dilution hole cooling system
FR3055950B1 (en) * 2016-09-14 2019-09-27 Safran Helicopter Engines COMBUSTION CHAMBER FOR TURBOMACHINE COMPRISING MEANS FOR IMPROVING THE COOLING OF AN ANNULAR WALL IN THE WAKE OF AN OBSTACLE
US11015529B2 (en) 2016-12-23 2021-05-25 General Electric Company Feature based cooling using in wall contoured cooling passage
FR3081211B1 (en) 2018-05-16 2021-02-26 Safran Aircraft Engines TURBOMACHINE COMBUSTION CHAMBER SET
US11022308B2 (en) * 2018-05-31 2021-06-01 Honeywell International Inc. Double wall combustors with strain isolated inserts
US11255543B2 (en) * 2018-08-07 2022-02-22 General Electric Company Dilution structure for gas turbine engine combustor
US11371701B1 (en) * 2021-02-03 2022-06-28 General Electric Company Combustor for a gas turbine engine
US20220390112A1 (en) * 2021-06-07 2022-12-08 General Electric Company Combustor for a gas turbine engine
US11774098B2 (en) * 2021-06-07 2023-10-03 General Electric Company Combustor for a gas turbine engine
CN114135901A (en) * 2021-11-08 2022-03-04 中国航发四川燃气涡轮研究院 Ablation-proof flame tube large-hole jet sleeve

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB665155A (en) * 1949-03-30 1952-01-16 Lucas Ltd Joseph Improvements relating to combustion chambers for prime movers
NL127178C (en) * 1959-11-20
FR1273296A (en) * 1960-11-10 1961-10-06 Rolls Royce Combustion equipment for gas turbo-engines
FR1277573A (en) * 1961-01-10 1961-12-01 Lucas Industries Ltd Combustion chamber for internal combustion engine
GB1240009A (en) * 1968-07-27 1971-07-21 Leyland Gas Turbines Ltd Flame tube
DE1957147A1 (en) * 1968-11-15 1970-06-04 Rolls Royce Flame tube for combustion systems of gas turbine engines
FR2055720A1 (en) * 1969-08-01 1971-04-30 Snecma
US3899882A (en) * 1974-03-27 1975-08-19 Westinghouse Electric Corp Gas turbine combustor basket cooling
DE2606704A1 (en) * 1976-02-19 1977-09-01 Motoren Turbinen Union COMBUSTION CHAMBER FOR GAS TURBINE ENGINES

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5932862U (en) * 1982-08-27 1984-02-29 三菱重工業株式会社 gas turbine combustor
JPS6287733A (en) * 1985-10-04 1987-04-22 エム・テ−・ウ−・モト−レン−・ウント・ツルビ−ネン−ウニオ−ン・ミユンヘン・ゲゼルシヤフト・ミツト・ベシユレンクテル・ハフツング Combustion chamber for gas turbine drive
JPH0459531B2 (en) * 1985-10-04 1992-09-22 Emu Tee Yuu Motooren Unto Tsurubiinen Union Myunhen Gmbh

Also Published As

Publication number Publication date
GB2017827A (en) 1979-10-10
GB2017827B (en) 1983-02-02
FR2422035A1 (en) 1979-11-02
DE2913223A1 (en) 1979-10-11
IT1163665B (en) 1987-04-08
IT7921515A0 (en) 1979-04-03

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