DE3663847D1 - Combustor for gas turbine engine - Google Patents

Combustor for gas turbine engine

Info

Publication number
DE3663847D1
DE3663847D1 DE8686304249T DE3663847T DE3663847D1 DE 3663847 D1 DE3663847 D1 DE 3663847D1 DE 8686304249 T DE8686304249 T DE 8686304249T DE 3663847 T DE3663847 T DE 3663847T DE 3663847 D1 DE3663847 D1 DE 3663847D1
Authority
DE
Germany
Prior art keywords
combustor
gas turbine
turbine engine
engine
gas
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
DE8686304249T
Other languages
English (en)
Inventor
Michael Francis Cannon
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.)
Alstom Power UK Holdings Ltd
Original Assignee
Alstom Power UK Holdings Ltd
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
Priority claimed from GB08515658A external-priority patent/GB2176274B/en
Application filed by Alstom Power UK Holdings Ltd filed Critical Alstom Power UK Holdings Ltd
Application granted granted Critical
Publication of DE3663847D1 publication Critical patent/DE3663847D1/de
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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36—Supply of different fuels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/12—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour characterised by the shape or arrangement of the outlets from the nozzle
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03041—Effusion cooled combustion chamber walls or domes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
DE8686304249T 1985-06-07 1986-06-04 Combustor for gas turbine engine Expired DE3663847D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8514388 1985-06-07
GB08515658A GB2176274B (en) 1985-06-07 1985-06-20 Combustor for gas turbine engine

Publications (1)

Publication Number Publication Date
DE3663847D1 true DE3663847D1 (en) 1989-07-13

Family

ID=26289341

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8686304249T Expired DE3663847D1 (en) 1985-06-07 1986-06-04 Combustor for gas turbine engine

Country Status (3)

Country Link
US (1) US4763481A (de)
EP (1) EP0204553B1 (de)
DE (1) DE3663847D1 (de)

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US4845952A (en) * 1987-10-23 1989-07-11 General Electric Company Multiple venturi tube gas fuel injector for catalytic combustor
JPH02503106A (ja) * 1987-12-28 1990-09-27 サンドストランド・コーポレーション 強制渦燃料噴射を持ったガスタービン
US5197278A (en) * 1990-12-17 1993-03-30 General Electric Company Double dome combustor and method of operation
US5261226A (en) * 1991-08-23 1993-11-16 Westinghouse Electric Corp. Topping combustor for an indirect fired gas turbine
US5259184A (en) * 1992-03-30 1993-11-09 General Electric Company Dry low NOx single stage dual mode combustor construction for a gas turbine
US5261223A (en) * 1992-10-07 1993-11-16 General Electric Company Multi-hole film cooled combustor liner with rectangular film restarting holes
DE4306956A1 (de) * 1993-03-05 1994-09-08 Abb Management Ag Brennstoffzuführung für eine Gasturbine
US5437158A (en) * 1993-06-24 1995-08-01 General Electric Company Low-emission combustor having perforated plate for lean direct injection
DE4328294A1 (de) * 1993-08-23 1995-03-02 Abb Management Ag Verfahren zur Kühlung eines Bauteils sowie Vorrichtung zur Durchführung des Verfahrens
US6082113A (en) * 1998-05-22 2000-07-04 Pratt & Whitney Canada Corp. Gas turbine fuel injector
US6289676B1 (en) 1998-06-26 2001-09-18 Pratt & Whitney Canada Corp. Simplex and duplex injector having primary and secondary annular lud channels and primary and secondary lud nozzles
US6314716B1 (en) 1998-12-18 2001-11-13 Solar Turbines Incorporated Serial cooling of a combustor for a gas turbine engine
US6256995B1 (en) 1999-11-29 2001-07-10 Pratt & Whitney Canada Corp. Simple low cost fuel nozzle support
US6334310B1 (en) * 2000-06-02 2002-01-01 General Electric Company Fracture resistant support structure for a hula seal in a turbine combustor and related method
US6536216B2 (en) * 2000-12-08 2003-03-25 General Electric Company Apparatus for injecting fuel into gas turbine engines
JP3962554B2 (ja) 2001-04-19 2007-08-22 三菱重工業株式会社 ガスタービン燃焼器及びガスタービン
US6871488B2 (en) * 2002-12-17 2005-03-29 Pratt & Whitney Canada Corp. Natural gas fuel nozzle for gas turbine engine
US20070193272A1 (en) * 2006-02-21 2007-08-23 Woodward Fst, Inc. Gas turbine engine fuel injector
DE102006042124B4 (de) * 2006-09-07 2010-04-22 Man Turbo Ag Gasturbinenbrennkammer
JP4764392B2 (ja) * 2007-08-29 2011-08-31 三菱重工業株式会社 ガスタービン燃焼器
US9291139B2 (en) * 2008-08-27 2016-03-22 Woodward, Inc. Dual action fuel injection nozzle
US8230687B2 (en) * 2008-09-02 2012-07-31 General Electric Company Multi-tube arrangement for combustor and method of making the multi-tube arrangement
US20100089020A1 (en) * 2008-10-14 2010-04-15 General Electric Company Metering of diluent flow in combustor
KR100969857B1 (ko) * 2008-11-21 2010-07-13 한국생산기술연구원 연료 연소장치
US9140454B2 (en) 2009-01-23 2015-09-22 General Electric Company Bundled multi-tube nozzle for a turbomachine
EP2211110B1 (de) * 2009-01-23 2019-05-01 Ansaldo Energia Switzerland AG Brenner für eine gasturbine
DE102009024269A1 (de) * 2009-06-05 2010-12-09 Honeywell Technologies S.A.R.L. Mischvorrichtung für einen Gasbrenner
US8205598B2 (en) * 2010-02-08 2012-06-26 International Engine Intellectual Property Company, Llc Fuel injector nozzle
EP2405200A1 (de) * 2010-07-05 2012-01-11 Siemens Aktiengesellschaft Verbrennungsvorrichtung und Gasturbinenmotor
US9625153B2 (en) 2010-11-09 2017-04-18 Opra Technologies B.V. Low calorific fuel combustor for gas turbine
US8844260B2 (en) * 2010-11-09 2014-09-30 Opra Technologies B.V. Low calorific fuel combustor for gas turbine
US9134023B2 (en) * 2012-01-06 2015-09-15 General Electric Company Combustor and method for distributing fuel in the combustor
US20130318976A1 (en) * 2012-05-29 2013-12-05 General Electric Company Turbomachine combustor nozzle and method of forming the same
US9267690B2 (en) 2012-05-29 2016-02-23 General Electric Company Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same
JP5911387B2 (ja) * 2012-07-06 2016-04-27 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器およびガスタービン燃焼器の運用方法
US9958160B2 (en) 2013-02-06 2018-05-01 United Technologies Corporation Gas turbine engine component with upstream-directed cooling film holes
EP2954261B1 (de) 2013-02-08 2020-03-04 United Technologies Corporation Gasturbinenbrennkammer
US9534787B2 (en) * 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
US9671112B2 (en) 2013-03-12 2017-06-06 General Electric Company Air diffuser for a head end of a combustor
US9650959B2 (en) 2013-03-12 2017-05-16 General Electric Company Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
US9347668B2 (en) 2013-03-12 2016-05-24 General Electric Company End cover configuration and assembly
US9366439B2 (en) 2013-03-12 2016-06-14 General Electric Company Combustor end cover with fuel plenums
US9759425B2 (en) 2013-03-12 2017-09-12 General Electric Company System and method having multi-tube fuel nozzle with multiple fuel injectors
US9765973B2 (en) 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
US9651259B2 (en) 2013-03-12 2017-05-16 General Electric Company Multi-injector micromixing system
US9528444B2 (en) 2013-03-12 2016-12-27 General Electric Company System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US10914470B2 (en) 2013-03-14 2021-02-09 Raytheon Technologies Corporation Combustor panel with increased durability
JP6033457B2 (ja) * 2013-10-18 2016-11-30 三菱重工業株式会社 燃料噴射器
CN106796034A (zh) 2014-09-05 2017-05-31 西门子公司 联焰导管
US9840992B2 (en) * 2015-03-06 2017-12-12 Elwha Llc Fuel injector system and method for making air-filled diesel droplets
EP3073198B1 (de) * 2015-03-27 2019-12-25 Ansaldo Energia Switzerland AG Integriertes zweikraftstofffördersystem
JP6621658B2 (ja) 2015-12-22 2019-12-18 川崎重工業株式会社 燃料噴射装置
WO2018011827A1 (en) 2016-07-15 2018-01-18 Indian Institute Of Technology (Iit Madras) A swirl mesh lean direct injection concept for distributed flame holding for low pollutant emissions and mitigation of combustion instability
US10890329B2 (en) 2018-03-01 2021-01-12 General Electric Company Fuel injector assembly for gas turbine engine
US10935245B2 (en) 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports
US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
US11073114B2 (en) 2018-12-12 2021-07-27 General Electric Company Fuel injector assembly for a heat engine
US11156360B2 (en) 2019-02-18 2021-10-26 General Electric Company Fuel nozzle assembly

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH284190A (de) * 1950-09-04 1952-07-15 Bbc Brown Boveri & Cie Metallene Brennkammer zur Erzeugung heisser Gase, insbesondere Treibgase für Gasturbinenanlagen.
US3720058A (en) * 1970-01-02 1973-03-13 Gen Electric Combustor and fuel injector
US3777484A (en) * 1971-12-08 1973-12-11 Gen Electric Shrouded combustion liner
US4004056A (en) * 1975-07-24 1977-01-18 General Motors Corporation Porous laminated sheet
GB1559779A (en) * 1975-11-07 1980-01-23 Lucas Industries Ltd Combustion assembly
US4422300A (en) * 1981-12-14 1983-12-27 United Technologies Corporation Prestressed combustor liner for gas turbine engine
EP0095788B1 (de) * 1982-05-28 1985-12-18 BBC Aktiengesellschaft Brown, Boveri & Cie. Brennkammer einer Gasturbine und Verfahren zu deren Betrieb
GB2135440B (en) * 1983-02-19 1986-06-25 Rolls Royce Mounting combustion chambers

Also Published As

Publication number Publication date
EP0204553B1 (de) 1989-06-07
EP0204553A1 (de) 1986-12-10
US4763481A (en) 1988-08-16

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Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee