DE69715256T2 - Brennkammer - Google Patents
BrennkammerInfo
- Publication number
- DE69715256T2 DE69715256T2 DE69715256T DE69715256T DE69715256T2 DE 69715256 T2 DE69715256 T2 DE 69715256T2 DE 69715256 T DE69715256 T DE 69715256T DE 69715256 T DE69715256 T DE 69715256T DE 69715256 T2 DE69715256 T2 DE 69715256T2
- Authority
- DE
- Germany
- Prior art keywords
- combustion chamber
- combustion
- chamber
- 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 - Lifetime
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
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- 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
-
- 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
- F23R3/34—Feeding into different combustion zones
-
- 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
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9623307A GB2319078B (en) | 1996-11-08 | 1996-11-08 | Combustor arrangement |
PCT/GB1997/003085 WO1998021527A1 (en) | 1996-11-08 | 1997-11-10 | Combustor arrangement |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69715256D1 DE69715256D1 (de) | 2002-10-10 |
DE69715256T2 true DE69715256T2 (de) | 2003-04-30 |
Family
ID=10802664
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69715256T Expired - Lifetime DE69715256T2 (de) | 1996-11-08 | 1997-11-10 | Brennkammer |
Country Status (6)
Country | Link |
---|---|
US (1) | US6360525B1 (de) |
EP (1) | EP0961907B1 (de) |
CN (1) | CN1110650C (de) |
DE (1) | DE69715256T2 (de) |
GB (1) | GB2319078B (de) |
WO (1) | WO1998021527A1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE112014005025B4 (de) | 2014-02-12 | 2021-08-26 | Publichnoe Aktsionernoe Obschestvo "Gazprom" | Ringförmige Verbrennungskammer in einem Gasturbinen-Triebwerk und Verfahren zu dessen Betrieb |
Families Citing this family (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE59901946D1 (de) * | 1998-04-23 | 2002-08-08 | Siemens Ag | Brennkammeranordnung |
WO2000049337A1 (de) * | 1999-02-16 | 2000-08-24 | Siemens Aktiengesellschaft | Brenneranordnung und verfahren zum betrieb einer brenneranordnung |
US6474071B1 (en) * | 2000-09-29 | 2002-11-05 | General Electric Company | Multiple injector combustor |
US6962055B2 (en) * | 2002-09-27 | 2005-11-08 | United Technologies Corporation | Multi-point staging strategy for low emission and stable combustion |
US7284378B2 (en) * | 2004-06-04 | 2007-10-23 | General Electric Company | Methods and apparatus for low emission gas turbine energy generation |
DE10348604A1 (de) * | 2003-10-20 | 2005-07-28 | Rolls-Royce Deutschland Ltd & Co Kg | Kraftstoffeinspritzdüse mit filmartiger Kraftstoffplatzierung |
EP1531305A1 (de) * | 2003-11-12 | 2005-05-18 | United Technologies Corporation | Multipoint-Kraftstoffinjektor |
US7506511B2 (en) * | 2003-12-23 | 2009-03-24 | Honeywell International Inc. | Reduced exhaust emissions gas turbine engine combustor |
US7546740B2 (en) * | 2004-05-11 | 2009-06-16 | United Technologies Corporation | Nozzle |
EP1847778A1 (de) * | 2006-04-21 | 2007-10-24 | Siemens Aktiengesellschaft | Vormischverbrennungsanlage für Gasturbine und Verfahren zum Betrieb |
US7810333B2 (en) * | 2006-10-02 | 2010-10-12 | General Electric Company | Method and apparatus for operating a turbine engine |
US8015814B2 (en) * | 2006-10-24 | 2011-09-13 | Caterpillar Inc. | Turbine engine having folded annular jet combustor |
EP1970629A1 (de) * | 2007-03-15 | 2008-09-17 | Siemens Aktiengesellschaft | Gestufte Brennstoffversorgung |
DE102007043626A1 (de) | 2007-09-13 | 2009-03-19 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität |
GB2454247A (en) * | 2007-11-02 | 2009-05-06 | Siemens Ag | A Combustor for a Gas-Turbine Engine Has a Burner Head with Fuel Delivered at a Compound Angle |
GB2455289B (en) * | 2007-12-03 | 2010-04-07 | Siemens Ag | Improvements in or relating to burners for a gas-turbine engine |
US8122700B2 (en) * | 2008-04-28 | 2012-02-28 | United Technologies Corp. | Premix nozzles and gas turbine engine systems involving such nozzles |
US8347630B2 (en) * | 2008-09-03 | 2013-01-08 | United Technologies Corp | Air-blast fuel-injector with shield-cone upstream of fuel orifices |
US10018115B2 (en) | 2009-02-26 | 2018-07-10 | 8 Rivers Capital, Llc | System and method for high efficiency power generation using a carbon dioxide circulating working fluid |
EA024852B1 (ru) * | 2009-02-26 | 2016-10-31 | Палмер Лэбз, Ллк | Способ и устройство для сжигания топлива при высокой температуре и высоком давлении и соответствующие система и средства |
RU2506499C2 (ru) * | 2009-11-09 | 2014-02-10 | Дженерал Электрик Компани | Топливные форсунки газовой турбины с противоположными направлениями завихрения |
US8850819B2 (en) * | 2010-06-25 | 2014-10-07 | United Technologies Corporation | Swirler, fuel and air assembly and combustor |
US9003804B2 (en) | 2010-11-24 | 2015-04-14 | Delavan Inc | Multipoint injectors with auxiliary stage |
US8899048B2 (en) | 2010-11-24 | 2014-12-02 | Delavan Inc. | Low calorific value fuel combustion systems for gas turbine engines |
FR2982010B1 (fr) * | 2011-10-26 | 2013-11-08 | Snecma | Chambre de combustion annulaire dans une turbomachine |
US9188063B2 (en) | 2011-11-03 | 2015-11-17 | Delavan Inc. | Injectors for multipoint injection |
US9644844B2 (en) | 2011-11-03 | 2017-05-09 | Delavan Inc. | Multipoint fuel injection arrangements |
DE102012001777A1 (de) | 2012-01-31 | 2013-08-01 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenringbrennkammer |
US9745936B2 (en) | 2012-02-16 | 2017-08-29 | Delavan Inc | Variable angle multi-point injection |
RU2561956C2 (ru) * | 2012-07-09 | 2015-09-10 | Альстом Текнолоджи Лтд | Газотурбинная система сгорания |
US9333518B2 (en) | 2013-02-27 | 2016-05-10 | Delavan Inc | Multipoint injectors |
US20140260302A1 (en) * | 2013-03-14 | 2014-09-18 | General Electric Company | DIFFUSION COMBUSTOR FUEL NOZZLE FOR LIMITING NOx EMISSIONS |
EP2796789B1 (de) | 2013-04-26 | 2017-03-01 | General Electric Technology GmbH | Rohrbrennkammer für eine Rohr-Ring Anordnung in einer Gasturbine |
JP6210810B2 (ja) * | 2013-09-20 | 2017-10-11 | 三菱日立パワーシステムズ株式会社 | デュアル燃料焚きガスタービン燃焼器 |
US9709279B2 (en) | 2014-02-27 | 2017-07-18 | General Electric Company | System and method for control of combustion dynamics in combustion system |
US9845956B2 (en) * | 2014-04-09 | 2017-12-19 | General Electric Company | System and method for control of combustion dynamics in combustion system |
US9897321B2 (en) | 2015-03-31 | 2018-02-20 | Delavan Inc. | Fuel nozzles |
US10385809B2 (en) | 2015-03-31 | 2019-08-20 | Delavan Inc. | Fuel nozzles |
JP6822868B2 (ja) * | 2017-02-21 | 2021-01-27 | 三菱重工業株式会社 | 燃焼器及びガスタービン |
US11181274B2 (en) | 2017-08-21 | 2021-11-23 | General Electric Company | Combustion system and method for attenuation of combustion dynamics in a gas turbine engine |
RU2765592C1 (ru) * | 2018-10-30 | 2022-02-01 | Аэроджет Рокетдайн, Инк. | Форсунка с форсуночными элементами, расположенными в окружных рядах, которые чередуются между закручиванием против часовой стрелки и закручиванием по часовой стрелке |
US11073114B2 (en) | 2018-12-12 | 2021-07-27 | General Electric Company | Fuel injector assembly for a heat engine |
US11286884B2 (en) | 2018-12-12 | 2022-03-29 | General Electric Company | Combustion section and fuel injector assembly for a heat engine |
FR3099546B1 (fr) * | 2019-07-29 | 2021-08-06 | Safran Aircraft Engines | Chambre de combustion comportant des systèmes d'injection secondaires injectant de l'air et du carburant directement dans des zones de recirculation de coin, turbomachine la comprenant, et procédé d'alimentation en carburant de celle-ci |
US20230220802A1 (en) * | 2022-01-13 | 2023-07-13 | General Electric Company | Combustor with lean openings |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3118489A (en) * | 1960-12-01 | 1964-01-21 | Union Carbide Corp | Reverse flow jet burner with gas vortex flame holders |
DE1932881C3 (de) * | 1969-06-28 | 1978-06-29 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Brennkammer für Gasturbinentriebwerke |
CH577627A5 (de) * | 1974-04-03 | 1976-07-15 | Bbc Sulzer Turbomaschinen | |
JPS5825932B2 (ja) * | 1977-04-15 | 1983-05-31 | トヨタ自動車株式会社 | ガスタ−ビンエンジンの燃焼室構造 |
DE3238684A1 (de) * | 1982-10-19 | 1984-04-19 | Kraftwerk Union AG, 4330 Mülheim | Gasturbinenbrennkammer |
CH672366A5 (de) * | 1986-12-09 | 1989-11-15 | Bbc Brown Boveri & Cie | |
US4903492A (en) * | 1988-09-07 | 1990-02-27 | The United States Of America As Represented By The Secretary Of The Air Force | Dilution air dispensing apparatus |
US4991398A (en) * | 1989-01-12 | 1991-02-12 | United Technologies Corporation | Combustor fuel nozzle arrangement |
CH684963A5 (de) * | 1991-11-13 | 1995-02-15 | Asea Brown Boveri | Ringbrennkammer. |
US5303542A (en) * | 1992-11-16 | 1994-04-19 | General Electric Company | Fuel supply control method for a gas turbine engine |
FR2698157B1 (fr) * | 1992-11-18 | 1994-12-16 | Snecma | Système d'injection aérodynamique de chambre de combustion. |
US5491970A (en) | 1994-06-10 | 1996-02-20 | General Electric Co. | Method for staging fuel in a turbine between diffusion and premixed operations |
US5596873A (en) * | 1994-09-14 | 1997-01-28 | General Electric Company | Gas turbine combustor with a plurality of circumferentially spaced pre-mixers |
WO1996027766A1 (de) * | 1995-03-08 | 1996-09-12 | Bmw Rolls-Royce Gmbh | Axial gestufte doppelring-brennkammer einer gasturbine |
FR2770283B1 (fr) * | 1997-10-29 | 1999-11-19 | Snecma | Chambre de combustion pour turbomachine |
-
1996
- 1996-11-08 GB GB9623307A patent/GB2319078B/en not_active Expired - Fee Related
-
1997
- 1997-11-10 DE DE69715256T patent/DE69715256T2/de not_active Expired - Lifetime
- 1997-11-10 WO PCT/GB1997/003085 patent/WO1998021527A1/en active IP Right Grant
- 1997-11-10 US US09/297,857 patent/US6360525B1/en not_active Expired - Lifetime
- 1997-11-10 EP EP97911374A patent/EP0961907B1/de not_active Expired - Lifetime
- 1997-11-10 CN CN97181225A patent/CN1110650C/zh not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE112014005025B4 (de) | 2014-02-12 | 2021-08-26 | Publichnoe Aktsionernoe Obschestvo "Gazprom" | Ringförmige Verbrennungskammer in einem Gasturbinen-Triebwerk und Verfahren zu dessen Betrieb |
Also Published As
Publication number | Publication date |
---|---|
DE69715256D1 (de) | 2002-10-10 |
EP0961907A1 (de) | 1999-12-08 |
GB2319078A (en) | 1998-05-13 |
US6360525B1 (en) | 2002-03-26 |
GB2319078B (en) | 1999-11-03 |
EP0961907B1 (de) | 2002-09-04 |
WO1998021527A1 (en) | 1998-05-22 |
CN1110650C (zh) | 2003-06-04 |
GB9623307D0 (en) | 1997-01-08 |
CN1242830A (zh) | 2000-01-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8328 | Change in the person/name/address of the agent |
Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN |