DE69209020T2 - Brennkammer mit abgestufter Luftzufuhr - Google Patents

Brennkammer mit abgestufter Luftzufuhr

Info

Publication number
DE69209020T2
DE69209020T2 DE69209020T DE69209020T DE69209020T2 DE 69209020 T2 DE69209020 T2 DE 69209020T2 DE 69209020 T DE69209020 T DE 69209020T DE 69209020 T DE69209020 T DE 69209020T DE 69209020 T2 DE69209020 T2 DE 69209020T2
Authority
DE
Germany
Prior art keywords
combustion chamber
air supply
graduated air
graduated
combustion
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 - Fee Related
Application number
DE69209020T
Other languages
English (en)
Other versions
DE69209020D1 (de
Inventor
Gale V Slocum
Albert Myers
Kenneth Winston Beebe
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE69209020D1 publication Critical patent/DE69209020D1/de
Application granted granted Critical
Publication of DE69209020T2 publication Critical patent/DE69209020T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F23R3/26—Controlling the air flow
    • 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
    • F23R3/06—Arrangement of apertures along the flame tube

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
DE69209020T 1991-12-18 1992-12-03 Brennkammer mit abgestufter Luftzufuhr Expired - Fee Related DE69209020T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US80913991A 1991-12-18 1991-12-18

Publications (2)

Publication Number Publication Date
DE69209020D1 DE69209020D1 (de) 1996-04-18
DE69209020T2 true DE69209020T2 (de) 1996-11-07

Family

ID=25200632

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69209020T Expired - Fee Related DE69209020T2 (de) 1991-12-18 1992-12-03 Brennkammer mit abgestufter Luftzufuhr

Country Status (7)

Country Link
US (1) US5351474A (de)
EP (1) EP0547808B1 (de)
JP (1) JPH05248268A (de)
KR (1) KR930013441A (de)
CN (1) CN1076014A (de)
DE (1) DE69209020T2 (de)
NO (1) NO924936L (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19829398A1 (de) * 1998-07-01 2000-01-05 Asea Brown Boveri Gasturbine
DE102006048842A1 (de) * 2006-10-13 2008-04-24 Man Turbo Ag Bypasssystem einer Brennkammer
DE102012015449A1 (de) * 2012-08-03 2014-02-20 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise

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JP2846268B2 (ja) * 1994-04-07 1999-01-13 三菱重工業株式会社 ガスタービン
DE19520291A1 (de) * 1995-06-02 1996-12-05 Abb Management Ag Brennkammer
US5924276A (en) * 1996-07-17 1999-07-20 Mowill; R. Jan Premixer with dilution air bypass valve assembly
US6070406A (en) * 1996-11-26 2000-06-06 Alliedsignal, Inc. Combustor dilution bypass system
US5906093A (en) * 1997-02-21 1999-05-25 Siemens Westinghouse Power Corporation Gas turbine combustor transition
US6220035B1 (en) * 1997-09-15 2001-04-24 Alliedsignal Inc. Annular combustor tangential injection flame stabilizer
US6082093A (en) * 1998-05-27 2000-07-04 Solar Turbines Inc. Combustion air control system for a gas turbine engine
JP4317651B2 (ja) * 2000-07-21 2009-08-19 三菱重工業株式会社 ガスタービンプラントおよびガスタービンプラントの制御方法
US20020104316A1 (en) * 2000-11-03 2002-08-08 Capstone Turbine Corporation Ultra low emissions gas turbine cycle using variable combustion primary zone airflow control
US6449956B1 (en) * 2001-04-09 2002-09-17 General Electric Company Bypass air injection method and apparatus for gas turbines
JP2002317650A (ja) * 2001-04-24 2002-10-31 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
JP3978086B2 (ja) * 2002-05-31 2007-09-19 三菱重工業株式会社 航空機用ガスタービンシステム，及びガスタービンシステム並びにその動作方法
US6840048B2 (en) * 2002-09-26 2005-01-11 General Electric Company Dynamically uncoupled can combustor
GB2405197B (en) 2003-08-16 2005-09-28 Rolls Royce Plc Fuel injector
GB0319329D0 (en) 2003-08-16 2003-09-17 Rolls Royce Plc Variable geometry combustor
US7284378B2 (en) 2004-06-04 2007-10-23 General Electric Company Methods and apparatus for low emission gas turbine energy generation
JP2005171795A (ja) * 2003-12-09 2005-06-30 Mitsubishi Heavy Ind Ltd ガスタービン燃焼装置
US7047723B2 (en) * 2004-04-30 2006-05-23 Martling Vincent C Apparatus and method for reducing the heat rate of a gas turbine powerplant
US7000396B1 (en) * 2004-09-02 2006-02-21 General Electric Company Concentric fixed dilution and variable bypass air injection for a combustor
US20060130486A1 (en) * 2004-12-17 2006-06-22 Danis Allen M Method and apparatus for assembling gas turbine engine combustors
US7631504B2 (en) * 2006-02-21 2009-12-15 General Electric Company Methods and apparatus for assembling gas turbine engines
GB2455289B (en) * 2007-12-03 2010-04-07 Siemens Ag Improvements in or relating to burners for a gas-turbine engine
US20090235668A1 (en) * 2008-03-18 2009-09-24 General Electric Company Insulator bushing for combustion liner
US20090260340A1 (en) * 2008-04-17 2009-10-22 General Electric Company Combustor of a Turbine, a Method of Retro-Fitting a Combustor of a Turbine and a Method of Building a Combustor of a Turbine
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
RU2506499C2 (ru) * 2009-11-09 2014-02-10 Дженерал Электрик Компани Топливные форсунки газовой турбины с противоположными направлениями завихрения
RU2010101978A (ru) * 2010-01-15 2011-07-20 Дженерал Электрик Компани (US) Соединительный узел для газовой турбины
US8276386B2 (en) 2010-09-24 2012-10-02 General Electric Company Apparatus and method for a combustor
US8448444B2 (en) * 2011-02-18 2013-05-28 General Electric Company Method and apparatus for mounting transition piece in combustor
US8601820B2 (en) * 2011-06-06 2013-12-10 General Electric Company Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
US20120308947A1 (en) * 2011-06-06 2012-12-06 General Electric Company Combustor having a pressure feed
US8407892B2 (en) * 2011-08-05 2013-04-02 General Electric Company Methods relating to integrating late lean injection into combustion turbine engines
US9010120B2 (en) * 2011-08-05 2015-04-21 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US9010082B2 (en) * 2012-01-03 2015-04-21 General Electric Company Turbine engine and method for flowing air in a turbine engine
US20130180253A1 (en) * 2012-01-13 2013-07-18 General Electric Company System and method for supplying a working fluid to a combustor
EP2644997A1 (de) 2012-03-26 2013-10-02 Alstom Technology Ltd Mischanordnung zum Mischen von Kraftstoff mit einem Strom aus sauerstoffhaltigem Gas
US9052115B2 (en) * 2012-04-25 2015-06-09 General Electric Company System and method for supplying a working fluid to a combustor
US8695352B2 (en) * 2012-07-12 2014-04-15 Solar Turbines Inc. Baffle assembly for bleed air system of gas turbine engine
US20140245746A1 (en) * 2013-03-04 2014-09-04 General Electric Company Combustion arrangement and method of reducing pressure fluctuations of a combustion arrangement
US9376961B2 (en) * 2013-03-18 2016-06-28 General Electric Company System for controlling a flow rate of a compressed working fluid to a combustor fuel injector
US20150107255A1 (en) * 2013-10-18 2015-04-23 General Electric Company Turbomachine combustor having an externally fueled late lean injection (lli) system
EP2868898A1 (de) 2013-10-30 2015-05-06 Siemens Aktiengesellschaft Verbesserter Teillastbetrieb einer Gasturbine mit einstellbarem Bypass-Strömungskanal
EP2933559A1 (de) 2014-04-16 2015-10-21 Alstom Technology Ltd Kraftstoffmischanordnung und Brennkammer mit einer solchen Mischanordnung
DE102014209544A1 (de) * 2014-05-20 2015-11-26 Siemens Aktiengesellschaft Turbinenanordnung
EP2957835B1 (de) 2014-06-18 2018-03-21 Ansaldo Energia Switzerland AG Verfahren zur Rückführung von Abgas aus einer Brennkammer eines Brenners einer Gasturbine sowie Gasturbine zur Durchführung des Verfahrens
JP6370728B2 (ja) * 2015-02-27 2018-08-08 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、ガスタービン、及びガスタービンの運転方法
FR3055403B1 (fr) * 2016-08-29 2021-01-22 Ifp Energies Now Chambre de combustion avec un deflecteur d'air comprime chaud, notamment pour une turbine destinee a la production d'energie, notamment d'energie electrique

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US2458066A (en) * 1944-07-20 1949-01-04 American Locomotive Co Combustion chamber
US2621477A (en) * 1948-06-03 1952-12-16 Power Jets Res & Dev Ltd Combustion apparatus having valve controlled passages for preheating the fuel-air mixture
US3577878A (en) * 1967-11-10 1971-05-11 Lucas Industries Ltd Flame tubes for gas turbine engines
US3691761A (en) * 1967-11-10 1972-09-19 Squire Ronald Jackson Apparatus for regulation of airflow to flame tubes for gas turbine engines
US3731484A (en) * 1967-11-10 1973-05-08 Lucas Ltd Joseph Apparatus for regulation of airflow to flame tubes for gas turbine engines
DE2020416A1 (de) * 1970-04-27 1971-11-11 Motoren Turbinen Union Brennkammer fuer Gasturbinentriebwerke
US4063415A (en) * 1972-06-30 1977-12-20 The United States Of America As Represented By The Secretary Of The Army Apparatus for staged combustion in air augmented rockets
US3930369A (en) * 1974-02-04 1976-01-06 General Motors Corporation Lean prechamber outflow combustor with two sets of primary air entrances
US3930368A (en) * 1974-12-12 1976-01-06 General Motors Corporation Combustion liner air valve
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US4259837A (en) * 1979-06-13 1981-04-07 General Electric Company Water and steam injection system for emission control of gas turbines
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US4807433A (en) * 1983-05-05 1989-02-28 General Electric Company Turbine cooling air modulation
US4628687A (en) * 1984-05-15 1986-12-16 A/S Kongsberg Vapenfabrikk Gas turbine combustor with pneumatically controlled flow distribution
US4982570A (en) * 1986-11-25 1991-01-08 General Electric Company Premixed pilot nozzle for dry low Nox combustor
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19829398A1 (de) * 1998-07-01 2000-01-05 Asea Brown Boveri Gasturbine
DE102006048842A1 (de) * 2006-10-13 2008-04-24 Man Turbo Ag Bypasssystem einer Brennkammer
DE102006048842B4 (de) 2006-10-13 2019-10-10 Man Energy Solutions Se Brennkammer für eine Gasturbine
DE102012015449A1 (de) * 2012-08-03 2014-02-20 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise
US9328665B2 (en) 2012-08-03 2016-05-03 Rolls-Royce Deutschland Ltd & Co Kg Gas-turbine combustion chamber with mixing air orifices and chutes in modular design

Also Published As

Publication number Publication date
EP0547808B1 (de) 1996-03-13
CN1076014A (zh) 1993-09-08
JPH05248268A (ja) 1993-09-24
DE69209020D1 (de) 1996-04-18
KR930013441A (ko) 1993-07-21
EP0547808A1 (de) 1993-06-23
NO924936L (no) 1993-06-21
US5351474A (en) 1994-10-04
NO924936D0 (no) 1992-12-18

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee