EP0801268A3 - Chambre de combustion pour turbine à gaz - Google Patents

Chambre de combustion pour turbine à gaz Download PDF

Info

Publication number
EP0801268A3
EP0801268A3 EP97810159A EP97810159A EP0801268A3 EP 0801268 A3 EP0801268 A3 EP 0801268A3 EP 97810159 A EP97810159 A EP 97810159A EP 97810159 A EP97810159 A EP 97810159A EP 0801268 A3 EP0801268 A3 EP 0801268A3
Authority
EP
European Patent Office
Prior art keywords
combustion chamber
recirculation zones
outer recirculation
mixing section
fuel
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
Application number
EP97810159A
Other languages
German (de)
English (en)
Other versions
EP0801268A2 (fr
EP0801268B1 (fr
Inventor
Klaus Dr. Döbbeling
Timothy Griffin
Hans Peter Knöpfel
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.)
GE Vernova GmbH
Original Assignee
ABB Research Ltd Switzerland
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
Application filed by ABB Research Ltd Switzerland filed Critical ABB Research Ltd Switzerland
Publication of EP0801268A2 publication Critical patent/EP0801268A2/fr
Publication of EP0801268A3 publication Critical patent/EP0801268A3/fr
Application granted granted Critical
Publication of EP0801268B1 publication Critical patent/EP0801268B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F23R3/34—Feeding into different combustion zones
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00015—Pilot burners specially adapted for low load or transient conditions, e.g. for increasing stability

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Combustion Of Fluid Fuel (AREA)
EP97810159A 1996-04-09 1997-03-18 Méthode d'exploitation d'une chambre de combustion pour turbine à gaz Expired - Lifetime EP0801268B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19614001A DE19614001A1 (de) 1996-04-09 1996-04-09 Brennkammer
DE19614001 1996-04-09

Publications (3)

Publication Number Publication Date
EP0801268A2 EP0801268A2 (fr) 1997-10-15
EP0801268A3 true EP0801268A3 (fr) 1999-07-14
EP0801268B1 EP0801268B1 (fr) 2003-12-10

Family

ID=7790796

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97810159A Expired - Lifetime EP0801268B1 (fr) 1996-04-09 1997-03-18 Méthode d'exploitation d'une chambre de combustion pour turbine à gaz

Country Status (5)

Country Link
US (1) US5885068A (fr)
EP (1) EP0801268B1 (fr)
JP (1) JP3907779B2 (fr)
CN (1) CN1165937A (fr)
DE (2) DE19614001A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0985882B1 (fr) 1998-09-10 2003-12-03 ALSTOM (Switzerland) Ltd Amortissement des vibrations dans des combusteurs
EP0994300B1 (fr) * 1998-10-14 2003-11-26 ALSTOM (Switzerland) Ltd Brûleur pour la conduite d'un générateur de chaleur
DE19855034A1 (de) * 1998-11-28 2000-05-31 Abb Patent Gmbh Verfahren zum Beschicken eines Brenners für Gasturbinen mit Pilotgas
US6286298B1 (en) * 1998-12-18 2001-09-11 General Electric Company Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavity
US6295801B1 (en) * 1998-12-18 2001-10-02 General Electric Company Fuel injector bar for gas turbine engine combustor having trapped vortex cavity
GB2399600B (en) * 2001-10-26 2005-12-14 Alstom Technology Ltd Gas turbine adapted to operate with a high exhaust gas recirculation rate and a method for operation thereof
WO2004020901A1 (fr) * 2002-08-30 2004-03-11 Alstom Technology Ltd Bruleur hybride et procede d'utilisation correspondant
ITMI20032621A1 (it) * 2003-12-30 2005-06-30 Nuovo Pignone Spa Sistema di combustione a basse emissioni inquinanti
US20060107667A1 (en) * 2004-11-22 2006-05-25 Haynes Joel M Trapped vortex combustor cavity manifold for gas turbine engine
CN101243287B (zh) * 2004-12-23 2013-03-27 阿尔斯托姆科技有限公司 具有混合段的预混燃烧器
US20070204624A1 (en) * 2006-03-01 2007-09-06 Smith Kenneth O Fuel injector for a turbine engine
DE102006041955A1 (de) * 2006-08-30 2008-03-20 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Steuerung der Verbrennung in einer Brennkammer und Brennkammervorrichtung
EP1950494A1 (fr) * 2007-01-29 2008-07-30 Siemens Aktiengesellschaft Chambre de combustion pour turbine à gaz
EP2107312A1 (fr) 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Chambre de combustion pilote dans un brûleur
FR2940865B1 (fr) 2009-01-08 2011-04-01 Augier Procede et systeme de transmission de l'energie electrique
CN101776283B (zh) * 2009-01-13 2012-06-20 北京航空航天大学 带射流注入的火焰稳定装置
CN102877984B (zh) * 2012-10-24 2014-12-03 北京航空航天大学 一种带前缘气缝结构的超燃冲压发动机火焰稳定装置
EP2889542B1 (fr) * 2013-12-24 2019-11-13 Ansaldo Energia Switzerland AG Procédé pour le fonctionnement d'une chambre de combustion pour turbine à gaz et chambre de combustion
CN104566460A (zh) * 2014-12-26 2015-04-29 北京华清燃气轮机与煤气化联合循环工程技术有限公司 一种具有突扩通道的燃料空气混合器
CN108006695B (zh) * 2016-11-01 2019-12-06 北京华清燃气轮机与煤气化联合循环工程技术有限公司 优化用于燃气轮机的预混合燃料喷嘴的方法
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
CN112128975B (zh) * 2020-09-25 2021-11-09 郑州釜鼎热能技术有限公司 一种空煤气上喷卷吸高温烟气蓄热体中燃烧与传热的热风炉
CN112984500B (zh) * 2021-01-27 2022-12-06 杭州聚能环保科技股份有限公司 一种卧式单炉胆煤粉锅炉
CN113279857B (zh) * 2021-05-27 2022-03-15 中国科学院工程热物理研究所 一种适用于无人飞行器的高推重比燃气涡轮发生器

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3879939A (en) * 1973-04-18 1975-04-29 United Aircraft Corp Combustion inlet diffuser employing boundary layer flow straightening vanes
US4062182A (en) * 1974-12-21 1977-12-13 Mtu Motoren-Und Turbinen-Union Gmbh Combustion chamber for gas turbine engines
US4488869A (en) * 1982-07-06 1984-12-18 Coen Company, Inc. High efficiency, low NOX emitting, staged combustion burner
US5359847A (en) * 1993-06-01 1994-11-01 Westinghouse Electric Corporation Dual fuel ultra-low NOX combustor
DE4426351A1 (de) * 1994-07-25 1996-02-01 Abb Research Ltd Brennkammer
US5638682A (en) * 1994-09-23 1997-06-17 General Electric Company Air fuel mixer for gas turbine combustor having slots at downstream end of mixing duct

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4395223A (en) * 1978-06-09 1983-07-26 Hitachi Shipbuilding & Engineering Co., Ltd. Multi-stage combustion method for inhibiting formation of nitrogen oxides
JPS6057131A (ja) * 1983-09-08 1985-04-02 Hitachi Ltd ガスタ−ビン燃焼器の燃料供給方法
CH674561A5 (fr) * 1987-12-21 1990-06-15 Bbc Brown Boveri & Cie
DE4408136A1 (de) * 1994-03-10 1995-09-14 Bmw Rolls Royce Gmbh Verfahren und Vorrichtung zur Kraftstoff-Aufbereitung für eine Gasturbinen-Brennkammer

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3879939A (en) * 1973-04-18 1975-04-29 United Aircraft Corp Combustion inlet diffuser employing boundary layer flow straightening vanes
US4062182A (en) * 1974-12-21 1977-12-13 Mtu Motoren-Und Turbinen-Union Gmbh Combustion chamber for gas turbine engines
US4488869A (en) * 1982-07-06 1984-12-18 Coen Company, Inc. High efficiency, low NOX emitting, staged combustion burner
US5359847A (en) * 1993-06-01 1994-11-01 Westinghouse Electric Corporation Dual fuel ultra-low NOX combustor
US5359847B1 (en) * 1993-06-01 1996-04-09 Westinghouse Electric Corp Dual fuel ultra-flow nox combustor
DE4426351A1 (de) * 1994-07-25 1996-02-01 Abb Research Ltd Brennkammer
US5638682A (en) * 1994-09-23 1997-06-17 General Electric Company Air fuel mixer for gas turbine combustor having slots at downstream end of mixing duct

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles

Also Published As

Publication number Publication date
DE59711087D1 (de) 2004-01-22
JP3907779B2 (ja) 2007-04-18
EP0801268A2 (fr) 1997-10-15
DE19614001A1 (de) 1997-10-16
JPH1038275A (ja) 1998-02-13
CN1165937A (zh) 1997-11-26
US5885068A (en) 1999-03-23
EP0801268B1 (fr) 2003-12-10

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