EP0781967A3 - Gasturbinenringbrennkammer - Google Patents
Gasturbinenringbrennkammer Download PDFInfo
- Publication number
- EP0781967A3 EP0781967A3 EP96810777A EP96810777A EP0781967A3 EP 0781967 A3 EP0781967 A3 EP 0781967A3 EP 96810777 A EP96810777 A EP 96810777A EP 96810777 A EP96810777 A EP 96810777A EP 0781967 A3 EP0781967 A3 EP 0781967A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- combustion chamber
- downstream
- gas turbine
- compressor
- fuel injection
- 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.)
- Granted
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
- F23R3/10—Air inlet arrangements for primary air
-
- 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
- F23R3/28—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
- F23R3/42—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
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19549143 | 1995-12-29 | ||
DE19549143A DE19549143A1 (de) | 1995-12-29 | 1995-12-29 | Gasturbinenringbrennkammer |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0781967A2 EP0781967A2 (de) | 1997-07-02 |
EP0781967A3 true EP0781967A3 (de) | 1999-04-07 |
EP0781967B1 EP0781967B1 (de) | 2003-04-02 |
Family
ID=7781645
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96810777A Expired - Lifetime EP0781967B1 (de) | 1995-12-29 | 1996-11-12 | Gasturbinenringbrennkammer |
Country Status (5)
Country | Link |
---|---|
US (1) | US5839283A (de) |
EP (1) | EP0781967B1 (de) |
JP (1) | JPH09196379A (de) |
CN (1) | CN1088151C (de) |
DE (2) | DE19549143A1 (de) |
Families Citing this family (137)
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DE19914666B4 (de) * | 1999-03-31 | 2009-08-20 | Alstom | Brenner für einen Wärmeerzeuger |
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US7603841B2 (en) * | 2001-07-23 | 2009-10-20 | Ramgen Power Systems, Llc | Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel |
US6694743B2 (en) | 2001-07-23 | 2004-02-24 | Ramgen Power Systems, Inc. | Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall |
US7003961B2 (en) * | 2001-07-23 | 2006-02-28 | Ramgen Power Systems, Inc. | Trapped vortex combustor |
JP2003065537A (ja) * | 2001-08-24 | 2003-03-05 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器 |
JP2003074854A (ja) * | 2001-08-28 | 2003-03-12 | Honda Motor Co Ltd | ガスタービン・エンジンの燃焼器 |
JP2003074853A (ja) * | 2001-08-28 | 2003-03-12 | Honda Motor Co Ltd | ガスタービン・エンジンの燃焼器 |
EP1507120A1 (de) * | 2003-08-13 | 2005-02-16 | Siemens Aktiengesellschaft | Gasturbine |
IL165233A (en) * | 2004-11-16 | 2013-06-27 | Israel Hirshberg | Energy conversion facility |
US20060156734A1 (en) * | 2005-01-15 | 2006-07-20 | Siemens Westinghouse Power Corporation | Gas turbine combustor |
DE102006004840A1 (de) * | 2006-02-02 | 2007-08-23 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer mit Kraftstoffeinspritzung über den gesamten Brennkammerring |
WO2007102807A1 (en) * | 2006-03-06 | 2007-09-13 | United Technologies Corporation | Angled flow annular combustor for turbine engine |
FR2917487B1 (fr) * | 2007-06-14 | 2009-10-02 | Snecma Sa | Chambre de combustion de turbomachine a circulation helicoidale de l'air |
WO2011059567A1 (en) | 2009-11-12 | 2011-05-19 | Exxonmobil Upstream Research Company | Low emission power generation and hydrocarbon recovery systems and methods |
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CA2934541C (en) | 2008-03-28 | 2018-11-06 | Exxonmobil Upstream Research Company | Low emission power generation and hydrocarbon recovery systems and methods |
US20090241547A1 (en) * | 2008-03-31 | 2009-10-01 | Andrew Luts | Gas turbine fuel injector for lower heating capacity fuels |
JP5580320B2 (ja) | 2008-10-14 | 2014-08-27 | エクソンモービル アップストリーム リサーチ カンパニー | 燃焼生成物を制御するための方法およびシステム |
US8221073B2 (en) * | 2008-12-22 | 2012-07-17 | Pratt & Whitney Canada Corp. | Exhaust gas discharge system and plenum |
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US8474266B2 (en) * | 2009-07-24 | 2013-07-02 | General Electric Company | System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle |
DE102009046066A1 (de) | 2009-10-28 | 2011-05-12 | Man Diesel & Turbo Se | Brenner für eine Turbine und damit ausgerüstete Gasturbine |
US8381532B2 (en) * | 2010-01-27 | 2013-02-26 | General Electric Company | Bled diffuser fed secondary combustion system for gas turbines |
DE102010023816A1 (de) | 2010-06-15 | 2011-12-15 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammeranordnung |
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WO2012003078A1 (en) | 2010-07-02 | 2012-01-05 | Exxonmobil Upstream Research Company | Stoichiometric combustion with exhaust gas recirculation and direct contact cooler |
CN107575308A (zh) | 2010-07-02 | 2018-01-12 | 埃克森美孚上游研究公司 | 低排放三循环动力产生***和方法 |
EA029336B1 (ru) | 2010-07-02 | 2018-03-30 | Эксонмобил Апстрим Рисерч Компани | Системы и способ производства энергии путем стехиометрического сгорания с обогащенным воздухом и рециркуляцией отработавшего газа |
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GB1048968A (en) * | 1964-05-08 | 1966-11-23 | Rolls Royce | Combustion chamber for a gas turbine engine |
US3879939A (en) * | 1973-04-18 | 1975-04-29 | United Aircraft Corp | Combustion inlet diffuser employing boundary layer flow straightening vanes |
DE3836446A1 (de) * | 1988-10-26 | 1990-05-03 | Proizv Ob Nevskij Z Im V I | Verfahren fuer die luftzufuhr zur brennzone einer brennkammer und brennkammer zur durchfuehrung dieses verfahrens |
US4991398A (en) * | 1989-01-12 | 1991-02-12 | United Technologies Corporation | Combustor fuel nozzle arrangement |
US5207064A (en) * | 1990-11-21 | 1993-05-04 | General Electric Company | Staged, mixed combustor assembly having low emissions |
CH684963A5 (de) * | 1991-11-13 | 1995-02-15 | Asea Brown Boveri | Ringbrennkammer. |
DE4419338A1 (de) * | 1994-06-03 | 1995-12-07 | Abb Research Ltd | Gasturbine und Verfahren zu ihrem Betrieb |
DE4435266A1 (de) * | 1994-10-01 | 1996-04-04 | Abb Management Ag | Brenner |
US5619855A (en) * | 1995-06-07 | 1997-04-15 | General Electric Company | High inlet mach combustor for gas turbine engine |
-
1995
- 1995-12-29 DE DE19549143A patent/DE19549143A1/de not_active Withdrawn
-
1996
- 1996-11-12 EP EP96810777A patent/EP0781967B1/de not_active Expired - Lifetime
- 1996-11-12 DE DE59610298T patent/DE59610298D1/de not_active Expired - Fee Related
- 1996-11-18 US US08/751,721 patent/US5839283A/en not_active Expired - Fee Related
- 1996-12-25 JP JP8345880A patent/JPH09196379A/ja not_active Abandoned
- 1996-12-27 CN CN96123618A patent/CN1088151C/zh not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2627721A (en) * | 1947-01-30 | 1953-02-10 | Packard Motor Car Co | Combustion means for jet propulsion units |
US4177637A (en) * | 1976-12-23 | 1979-12-11 | Rolls-Royce Limited | Inlet for annular gas turbine combustor |
US4455840A (en) * | 1981-03-04 | 1984-06-26 | Bbc Brown, Boveri & Company, Limited | Ring combustion chamber with ring burner for gas turbines |
EP0651207A1 (de) * | 1993-10-27 | 1995-05-03 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Unterscheidliche Luftzuführumkreiskanäle eines Diffusors |
GB2288010A (en) * | 1994-04-02 | 1995-10-04 | Abb Management Ag | Premixing burner |
Also Published As
Publication number | Publication date |
---|---|
CN1158383A (zh) | 1997-09-03 |
EP0781967A2 (de) | 1997-07-02 |
DE19549143A1 (de) | 1997-07-03 |
US5839283A (en) | 1998-11-24 |
EP0781967B1 (de) | 2003-04-02 |
DE59610298D1 (de) | 2003-05-08 |
JPH09196379A (ja) | 1997-07-29 |
CN1088151C (zh) | 2002-07-24 |
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