DE3663847D1 - Combustor for gas turbine engine - Google Patents
Combustor for gas turbine engineInfo
- 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
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)
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) |
Families Citing this family (58)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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)
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 |
-
1986
- 1986-06-04 EP EP86304249A patent/EP0204553B1/de not_active Expired
- 1986-06-04 US US06/870,388 patent/US4763481A/en not_active Expired - Fee Related
- 1986-06-04 DE DE8686304249T patent/DE3663847D1/de not_active Expired
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 |