DE502008000175D1 - Magervormischbrenner für ein Gasturbinentriebwerk - Google Patents
Magervormischbrenner für ein GasturbinentriebwerkInfo
- Publication number
- DE502008000175D1 DE502008000175D1 DE200850000175 DE502008000175T DE502008000175D1 DE 502008000175 D1 DE502008000175 D1 DE 502008000175D1 DE 200850000175 DE200850000175 DE 200850000175 DE 502008000175 T DE502008000175 T DE 502008000175T DE 502008000175 D1 DE502008000175 D1 DE 502008000175D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- turbine engine
- premix burner
- lean premix
- lean
- 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.)
- Active
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
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
- F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
-
- 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
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
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 (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200710050276 DE102007050276A1 (de) | 2007-10-18 | 2007-10-18 | Magervormischbrenner für ein Gasturbinentriebwerk |
Publications (1)
Publication Number | Publication Date |
---|---|
DE502008000175D1 true DE502008000175D1 (de) | 2009-12-17 |
Family
ID=40328904
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE200710050276 Withdrawn DE102007050276A1 (de) | 2007-10-18 | 2007-10-18 | Magervormischbrenner für ein Gasturbinentriebwerk |
DE200850000175 Active DE502008000175D1 (de) | 2007-10-18 | 2008-09-29 | Magervormischbrenner für ein Gasturbinentriebwerk |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE200710050276 Withdrawn DE102007050276A1 (de) | 2007-10-18 | 2007-10-18 | Magervormischbrenner für ein Gasturbinentriebwerk |
Country Status (3)
Country | Link |
---|---|
US (1) | US8910483B2 (de) |
EP (1) | EP2051010B1 (de) |
DE (2) | DE102007050276A1 (de) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8266911B2 (en) * | 2005-11-14 | 2012-09-18 | General Electric Company | Premixing device for low emission combustion process |
DE102005062079A1 (de) * | 2005-12-22 | 2007-07-12 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormischbrenner mit einer Zerstäuberlippe |
US10655844B2 (en) * | 2009-02-10 | 2020-05-19 | Bsh Home Appliances Corporation | Pedestal for a burner of a household appliance |
US10690351B2 (en) | 2009-02-10 | 2020-06-23 | Bsh Home Appliances Corporation | Home cooking appliance having a pedestal burner |
US8375548B2 (en) * | 2009-10-07 | 2013-02-19 | Pratt & Whitney Canada Corp. | Fuel nozzle and method of repair |
IT1399989B1 (it) * | 2010-05-05 | 2013-05-09 | Avio Spa | Gruppo di iniezione per un combustore di una turbina a gas |
DE102010019773A1 (de) | 2010-05-07 | 2011-11-10 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormischbrenner eines Gasturbinentriebwerks mit Strömungsleitelement |
CN101871393A (zh) * | 2010-05-31 | 2010-10-27 | 哈尔滨工程大学 | 基于叶片式金属-水反应推进装置的发动机 |
EP2400222A1 (de) * | 2010-06-28 | 2011-12-28 | Siemens Aktiengesellschaft | Verbrennungsvorrichtung |
US20130206107A1 (en) * | 2010-07-02 | 2013-08-15 | American Performance Technologies, Llc | Carburetor and methods therefor |
US8365534B2 (en) * | 2011-03-15 | 2013-02-05 | General Electric Company | Gas turbine combustor having a fuel nozzle for flame anchoring |
CN103062798B (zh) * | 2011-10-18 | 2016-02-17 | 中航商用航空发动机有限责任公司 | 一种燃烧室燃油喷射和混合装置 |
DE102011116317A1 (de) | 2011-10-18 | 2013-04-18 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormischbrenner eines Fluggasturbinentriebwerks |
US9423137B2 (en) * | 2011-12-29 | 2016-08-23 | Rolls-Royce Corporation | Fuel injector with first and second converging fuel-air passages |
JP5924618B2 (ja) * | 2012-06-07 | 2016-05-25 | 川崎重工業株式会社 | 燃料噴射装置 |
CN103791518B (zh) * | 2012-10-31 | 2016-03-09 | 中航商用航空发动机有限责任公司 | 一种燃烧室燃油喷射与混合装置及航空发动机 |
CN103807878B (zh) * | 2012-11-13 | 2016-04-20 | 中航商用航空发动机有限责任公司 | 一种燃烧室燃油喷射与混合装置及包括该装置的燃烧室 |
US9441543B2 (en) * | 2012-11-20 | 2016-09-13 | Niigata Power Systems Co., Ltd. | Gas turbine combustor including a premixing chamber having an inner diameter enlarging portion |
CN103851647B (zh) * | 2012-12-04 | 2016-01-20 | 中航商用航空发动机有限责任公司 | 燃烧室燃油喷射与混合系统及其燃烧室 |
EP2951505A4 (de) * | 2013-02-01 | 2016-01-06 | Hamilton Sundstrand Corp | Kraftstoffinjektor für höhenbedingten start und betrieb eines gasturbinenmotors |
US20150285502A1 (en) * | 2014-04-08 | 2015-10-08 | General Electric Company | Fuel nozzle shroud and method of manufacturing the shroud |
CN107110503B (zh) | 2014-10-17 | 2020-11-27 | 诺沃皮尼奥内股份有限公司 | 用于减少在燃气涡轮机中的NOx排放的方法、空气燃料混合器、燃气涡轮机和旋流器 |
CN104456628B (zh) * | 2014-11-10 | 2016-08-31 | 中国科学院工程热物理研究所 | 一种主燃级贫预混的分层部分预混低污染燃烧室 |
US10830445B2 (en) * | 2015-12-30 | 2020-11-10 | General Electric Company | Liquid fuel nozzles for dual fuel combustors |
US10352570B2 (en) | 2016-03-31 | 2019-07-16 | General Electric Company | Turbine engine fuel injection system and methods of assembling the same |
KR102498300B1 (ko) * | 2016-11-14 | 2023-02-09 | 한화에어로스페이스 주식회사 | 가스터빈용 연료 분사 장치 |
US10954859B2 (en) | 2017-07-25 | 2021-03-23 | Raytheon Technologies Corporation | Low emissions combustor assembly for gas turbine engine |
US11480338B2 (en) | 2017-08-23 | 2022-10-25 | General Electric Company | Combustor system for high fuel/air ratio and reduced combustion dynamics |
US11561008B2 (en) | 2017-08-23 | 2023-01-24 | General Electric Company | Fuel nozzle assembly for high fuel/air ratio and reduced combustion dynamics |
GB201716585D0 (en) * | 2017-09-08 | 2017-11-22 | Rolls Royce Plc | Spray nozzle |
DE102017217328A1 (de) * | 2017-09-28 | 2019-03-28 | Rolls-Royce Deutschland Ltd & Co Kg | Düse mit axialer Verlängerung für eine Brennkammer eines Triebwerks |
DE102017218529A1 (de) * | 2017-10-17 | 2019-04-18 | Rolls-Royce Deutschland Ltd & Co Kg | Düse für eine Brennkammer eines Triebwerks |
DE102018106051A1 (de) * | 2018-03-15 | 2019-09-19 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammerbaugruppe mit Brennerdichtung und Düse sowie einer Leitströmungserzeugungseinrichtung |
JP6546334B1 (ja) | 2018-12-03 | 2019-07-17 | 三菱日立パワーシステムズ株式会社 | ガスタービンの燃焼器及びこれを備えたガスタービン |
GB201820206D0 (en) | 2018-12-12 | 2019-01-23 | Rolls Royce Plc | A fuel spray nozzle |
EP4050261A4 (de) * | 2019-10-23 | 2023-11-22 | IHI Corporation | Flüssigbrennstoffinjektor |
US11701726B2 (en) | 2021-10-05 | 2023-07-18 | Collins Engine Nozzles, Inc. | Material deposition for fluid injectors |
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US3474970A (en) * | 1967-03-15 | 1969-10-28 | Parker Hannifin Corp | Air assist nozzle |
US3530667A (en) * | 1967-11-02 | 1970-09-29 | Rolls Royce | Fuel injector for gas turbine engines |
US3684186A (en) * | 1970-06-26 | 1972-08-15 | Ex Cell O Corp | Aerating fuel nozzle |
US3703259A (en) * | 1971-05-03 | 1972-11-21 | Gen Electric | Air blast fuel atomizer |
US3980233A (en) * | 1974-10-07 | 1976-09-14 | Parker-Hannifin Corporation | Air-atomizing fuel nozzle |
US4170108A (en) * | 1975-04-25 | 1979-10-09 | Rolls-Royce Limited | Fuel injectors for gas turbine engines |
US4327547A (en) * | 1978-11-23 | 1982-05-04 | Rolls-Royce Limited | Fuel injectors |
US4260367A (en) * | 1978-12-11 | 1981-04-07 | United Technologies Corporation | Fuel nozzle for burner construction |
US4470262A (en) * | 1980-03-07 | 1984-09-11 | Solar Turbines, Incorporated | Combustors |
US5042445A (en) * | 1988-09-23 | 1991-08-27 | Cummins Engine Company, Inc. | Electronic controlled fuel supply system for high pressure injector |
GB9112324D0 (en) * | 1991-06-07 | 1991-07-24 | Rolls Royce Plc | Gas turbine engine combustor |
GB2272756B (en) * | 1992-11-24 | 1995-05-31 | Rolls Royce Plc | Fuel injection apparatus |
DE19527453B4 (de) * | 1995-07-27 | 2009-05-07 | Alstom | Vormischbrenner |
FR2753779B1 (fr) * | 1996-09-26 | 1998-10-16 | Systeme d'injection aerodynamique d'un melange air carburant | |
DE19729246C2 (de) * | 1997-07-09 | 2001-06-28 | Deutsch Zentr Luft & Raumfahrt | Zerstäuberdüse für die Kraftstoffzerstäubung in Brennern |
US6161387A (en) * | 1998-10-30 | 2000-12-19 | United Technologies Corporation | Multishear fuel injector |
US6389815B1 (en) * | 2000-09-08 | 2002-05-21 | General Electric Company | Fuel nozzle assembly for reduced exhaust emissions |
US6453660B1 (en) * | 2001-01-18 | 2002-09-24 | General Electric Company | Combustor mixer having plasma generating nozzle |
US6530227B1 (en) * | 2001-04-27 | 2003-03-11 | General Electric Co. | Methods and apparatus for cooling gas turbine engine combustors |
US6484489B1 (en) * | 2001-05-31 | 2002-11-26 | General Electric Company | Method and apparatus for mixing fuel to decrease combustor emissions |
JP3584289B2 (ja) * | 2002-01-21 | 2004-11-04 | 独立行政法人 宇宙航空研究開発機構 | 液体微粒化ノズル |
US6865889B2 (en) * | 2002-02-01 | 2005-03-15 | General Electric Company | Method and apparatus to decrease combustor emissions |
DE10219354A1 (de) * | 2002-04-30 | 2003-11-13 | Rolls Royce Deutschland | Gasturbinenbrennkammer mit gezielter Kraftstoffeinbringung zur Verbesserung der Homogenität des Kraftstoff-Luft-Gemisches |
US6718770B2 (en) * | 2002-06-04 | 2004-04-13 | General Electric Company | Fuel injector laminated fuel strip |
GB0219461D0 (en) * | 2002-08-21 | 2002-09-25 | Rolls Royce Plc | Fuel injection arrangement |
US6986255B2 (en) * | 2002-10-24 | 2006-01-17 | Rolls-Royce Plc | Piloted airblast lean direct fuel injector with modified air splitter |
US6898938B2 (en) * | 2003-04-24 | 2005-05-31 | General Electric Company | Differential pressure induced purging fuel injector with asymmetric cyclone |
JP4065947B2 (ja) * | 2003-08-05 | 2008-03-26 | 独立行政法人 宇宙航空研究開発機構 | ガスタービン燃焼器用燃料・空気プレミキサー |
GB2404729B (en) * | 2003-08-08 | 2008-01-23 | Rolls Royce Plc | Fuel injection |
JP3944609B2 (ja) * | 2003-12-16 | 2007-07-11 | 川崎重工業株式会社 | 燃料ノズル |
US7036302B2 (en) * | 2004-03-15 | 2006-05-02 | General Electric Company | Controlled pressure fuel nozzle system |
US7779636B2 (en) * | 2005-05-04 | 2010-08-24 | Delavan Inc | Lean direct injection atomizer for gas turbine engines |
DE102005022772A1 (de) * | 2005-05-12 | 2007-01-11 | Universität Karlsruhe | Brenner mit Teilvormischung und -vorverdampfung des flüssigen Brennstoffs |
US7673460B2 (en) * | 2005-06-07 | 2010-03-09 | Snecma | System of attaching an injection system to a turbojet combustion chamber base |
JP2007162998A (ja) * | 2005-12-13 | 2007-06-28 | Kawasaki Heavy Ind Ltd | ガスタービンエンジンの燃料噴霧装置 |
US7878000B2 (en) * | 2005-12-20 | 2011-02-01 | General Electric Company | Pilot fuel injector for mixer assembly of a high pressure gas turbine engine |
DE102005062079A1 (de) * | 2005-12-22 | 2007-07-12 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormischbrenner mit einer Zerstäuberlippe |
US7762073B2 (en) * | 2006-03-01 | 2010-07-27 | General Electric Company | Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection ports |
GB2439097B (en) * | 2006-06-15 | 2008-10-29 | Rolls Royce Plc | Fuel injector |
JP4421620B2 (ja) * | 2007-02-15 | 2010-02-24 | 川崎重工業株式会社 | ガスタービンエンジンの燃焼器 |
US7926744B2 (en) * | 2008-02-21 | 2011-04-19 | Delavan Inc | Radially outward flowing air-blast fuel injector for gas turbine engine |
DE102008014744A1 (de) * | 2008-03-18 | 2009-09-24 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrenner für eine Gasturbine mit Spülmechanismus für eine Brennstoffdüse |
US8061142B2 (en) * | 2008-04-11 | 2011-11-22 | General Electric Company | Mixer for a combustor |
GB0812905D0 (en) * | 2008-07-16 | 2008-08-20 | Rolls Royce Plc | Fuel injection system |
US8555645B2 (en) * | 2008-07-21 | 2013-10-15 | General Electric Company | Fuel nozzle centerbody and method of assembling the same |
JP5472863B2 (ja) * | 2009-06-03 | 2014-04-16 | 独立行政法人 宇宙航空研究開発機構 | ステージング型燃料ノズル |
US8387391B2 (en) * | 2010-12-17 | 2013-03-05 | General Electric Company | Aerodynamically enhanced fuel nozzle |
-
2007
- 2007-10-18 DE DE200710050276 patent/DE102007050276A1/de not_active Withdrawn
-
2008
- 2008-09-29 EP EP20080165427 patent/EP2051010B1/de not_active Expired - Fee Related
- 2008-09-29 DE DE200850000175 patent/DE502008000175D1/de active Active
- 2008-10-20 US US12/289,051 patent/US8910483B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP2051010A1 (de) | 2009-04-22 |
US20090100837A1 (en) | 2009-04-23 |
DE102007050276A1 (de) | 2009-04-23 |
EP2051010B1 (de) | 2009-11-04 |
US8910483B2 (en) | 2014-12-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |