NO911712L - Fordampningskjoelt halsseksjon for brennkammer med lavt nox utslipp samt fremgangsmaate for drift av samme. - Google Patents

Fordampningskjoelt halsseksjon for brennkammer med lavt nox utslipp samt fremgangsmaate for drift av samme.

Info

Publication number
NO911712L
NO911712L NO91911712A NO911712A NO911712L NO 911712 L NO911712 L NO 911712L NO 91911712 A NO91911712 A NO 91911712A NO 911712 A NO911712 A NO 911712A NO 911712 L NO911712 L NO 911712L
Authority
NO
Norway
Prior art keywords
fireplaces
procedure
operating
same
nox emissions
Prior art date
Application number
NO91911712A
Other languages
English (en)
Norwegian (no)
Other versions
NO911712D0 (no
Inventor
Kenneth Winston Beebe
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of NO911712D0 publication Critical patent/NO911712D0/no
Publication of NO911712L publication Critical patent/NO911712L/no

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
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants

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)
NO91911712A 1990-05-03 1991-04-30 Fordampningskjoelt halsseksjon for brennkammer med lavt nox utslipp samt fremgangsmaate for drift av samme. NO911712L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/520,267 US5127221A (en) 1990-05-03 1990-05-03 Transpiration cooled throat section for low nox combustor and related process

Publications (2)

Publication Number Publication Date
NO911712D0 NO911712D0 (no) 1991-04-30
NO911712L true NO911712L (no) 1991-11-04

Family

ID=24071863

Family Applications (1)

Application Number Title Priority Date Filing Date
NO91911712A NO911712L (no) 1990-05-03 1991-04-30 Fordampningskjoelt halsseksjon for brennkammer med lavt nox utslipp samt fremgangsmaate for drift av samme.

Country Status (7)

Country Link
US (1) US5127221A (zh)
EP (1) EP0455487A1 (zh)
JP (1) JPH04227414A (zh)
KR (1) KR940001924B1 (zh)
CN (1) CN1056563A (zh)
CA (1) CA2040780A1 (zh)
NO (1) NO911712L (zh)

Families Citing this family (60)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0564181B1 (en) * 1992-03-30 1996-11-20 General Electric Company Combustor dome construction
FR2691209B1 (fr) * 1992-05-18 1995-09-01 Europ Propulsion Enceinte contenant des gaz chauds refroidie par transpiration, notamment chambre propulsive de moteur-fusee, et procede de fabrication.
US5501011A (en) * 1992-05-18 1996-03-26 Societe Europeenne De Propulsion Method of manufacture of an enclosure containing hot gases cooled by transportation, in particular the thrust chamber of a rocket engine
US5410884A (en) * 1992-10-19 1995-05-02 Mitsubishi Jukogyo Kabushiki Kaisha Combustor for gas turbines with diverging pilot nozzle cone
US5309710A (en) * 1992-11-20 1994-05-10 General Electric Company Gas turbine combustor having poppet valves for air distribution control
US5487275A (en) * 1992-12-11 1996-01-30 General Electric Co. Tertiary fuel injection system for use in a dry low NOx combustion system
US5359847B1 (en) * 1993-06-01 1996-04-09 Westinghouse Electric Corp Dual fuel ultra-flow nox combustor
US5406798A (en) * 1993-10-22 1995-04-18 United Technologies Corporation Pilot fuel cooled flow divider valve for a staged combustor
US5402634A (en) * 1993-10-22 1995-04-04 United Technologies Corporation Fuel supply system for a staged combustor
GB2297151B (en) * 1995-01-13 1998-04-22 Europ Gas Turbines Ltd Fuel injector arrangement for gas-or liquid-fuelled turbine
DE19520291A1 (de) * 1995-06-02 1996-12-05 Abb Management Ag Brennkammer
EP0747635B1 (en) * 1995-06-05 2003-01-15 Rolls-Royce Corporation Dry low oxides of nitrogen lean premix module for industrial gas turbine engines
US5813232A (en) * 1995-06-05 1998-09-29 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
US5647215A (en) * 1995-11-07 1997-07-15 Westinghouse Electric Corporation Gas turbine combustor with turbulence enhanced mixing fuel injectors
DE19615910B4 (de) * 1996-04-22 2006-09-14 Alstom Brenneranordnung
US5850732A (en) * 1997-05-13 1998-12-22 Capstone Turbine Corporation Low emissions combustion system for a gas turbine engine
JP3448190B2 (ja) * 1997-08-29 2003-09-16 三菱重工業株式会社 ガスタービンの燃焼器
US6089025A (en) * 1998-08-24 2000-07-18 General Electric Company Combustor baffle
US6453658B1 (en) 2000-02-24 2002-09-24 Capstone Turbine Corporation Multi-stage multi-plane combustion system for a gas turbine engine
JP4851674B2 (ja) 2000-05-01 2012-01-11 キャプストーン タービン コーポレーション エネルギーシステムと併用する環状燃焼器
WO2003093664A1 (en) * 2000-06-28 2003-11-13 Power Systems Mfg. Llc Combustion chamber/venturi cooling for a low nox emission combustor
KR100831772B1 (ko) 2001-11-30 2008-05-27 파워 시스템즈 엠에프지., 엘엘씨 질소산화물 저 배출 연소기용 연소 챔버/벤츄리 냉각장치및 방법
US6915636B2 (en) * 2002-07-15 2005-07-12 Power Systems Mfg., Llc Dual fuel fin mixer secondary fuel nozzle
US6923642B2 (en) * 2003-10-08 2005-08-02 General Motors Corporation Premixed prevaporized combustor
US7066042B2 (en) 2004-01-07 2006-06-27 Sanford L.P. Advancing/retracting mechanism
US7146816B2 (en) * 2004-08-16 2006-12-12 Honeywell International, Inc. Effusion momentum control
US7389643B2 (en) * 2005-01-31 2008-06-24 General Electric Company Inboard radial dump venturi for combustion chamber of a gas turbine
US7387489B2 (en) * 2005-10-17 2008-06-17 Honeywell International Inc. Bleed valve outlet flow deflector
US7797945B2 (en) * 2006-09-06 2010-09-21 Honeywell International Inc. Bleed valve outlet flow deflector
US8096133B2 (en) * 2008-05-13 2012-01-17 General Electric Company Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface
US7712314B1 (en) * 2009-01-21 2010-05-11 Gas Turbine Efficiency Sweden Ab Venturi cooling system
US20100192580A1 (en) * 2009-02-03 2010-08-05 Derrick Walter Simons Combustion System Burner Tube
US20100192582A1 (en) 2009-02-04 2010-08-05 Robert Bland Combustor nozzle
US20110041507A1 (en) * 2009-08-18 2011-02-24 William Kirk Hessler Integral Liner and Venturi for Eliminating Air Leakage
US9341118B2 (en) * 2009-12-29 2016-05-17 Rolls-Royce Corporation Various layered gas turbine engine component constructions
US20110167828A1 (en) * 2010-01-08 2011-07-14 Arjun Singh Combustor assembly for a turbine engine that mixes combustion products with purge air
US8381526B2 (en) * 2010-02-15 2013-02-26 General Electric Company Systems and methods of providing high pressure air to a head end of a combustor
RU2519014C2 (ru) 2010-03-02 2014-06-10 Дженерал Электрик Компани Диффузор для камеры сгорания турбины (варианты) и камера сгорания турбины
US20110225974A1 (en) * 2010-03-22 2011-09-22 General Electric Company Multiple Zone Pilot For Low Emission Combustion System
CN102175041B (zh) * 2010-12-23 2012-06-27 中国航天科技集团公司第六研究院第十一研究所 间壁式再生冷却气氧酒精火炬式点火器
US9016039B2 (en) * 2012-04-05 2015-04-28 General Electric Company Combustor and method for supplying fuel to a combustor
RU2493495C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
RU2493492C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд и форсуночный модуль
RU2493494C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
RU2493493C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
RU2511977C2 (ru) * 2012-06-27 2014-04-10 Николай Борисович Болотин Форсуночный блок камеры сгорания гтд
RU2515909C2 (ru) * 2012-07-04 2014-05-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Кольцевая малоэмиссионная камера сгорания газотурбинного двигателя
AU2013219140B2 (en) * 2012-08-24 2015-10-08 Ansaldo Energia Switzerland AG Method for mixing a dilution air in a sequential combustion system of a gas turbine
JP6012407B2 (ja) * 2012-10-31 2016-10-25 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及びガスタービン
US10215412B2 (en) * 2012-11-02 2019-02-26 General Electric Company System and method for load control with diffusion combustion in a stoichiometric exhaust gas recirculation gas turbine system
US9518739B2 (en) 2013-03-08 2016-12-13 Pratt & Whitney Canada Corp. Combustor heat shield with carbon avoidance feature
US9638057B2 (en) 2013-03-14 2017-05-02 Rolls-Royce North American Technologies, Inc. Augmented cooling system
US9803555B2 (en) * 2014-04-23 2017-10-31 General Electric Company Fuel delivery system with moveably attached fuel tube
RU2687475C1 (ru) * 2018-07-16 2019-05-13 федеральное государственное автономное образовательное учреждение высшего образования "Южно-Уральский государственный университет (национальный исследовательский университет)" Малоэмиссионная кольцевая камера сгорания для газовых турбин
JP7307441B2 (ja) * 2021-03-23 2023-07-12 トヨタ自動車株式会社 燃焼器
CN116265810A (zh) 2021-12-16 2023-06-20 通用电气公司 利用成形冷却栅栏的旋流器反稀释
CN116592392A (zh) 2022-02-07 2023-08-15 通用电气公司 操作具有可变燃烧室的燃烧器的方法
US11835236B1 (en) 2022-07-05 2023-12-05 General Electric Company Combustor with reverse dilution air introduction
US11788724B1 (en) * 2022-09-02 2023-10-17 General Electric Company Acoustic damper for combustor
US11747019B1 (en) * 2022-09-02 2023-09-05 General Electric Company Aerodynamic combustor liner design for emissions reductions

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1108090A (fr) * 1954-07-01 1956-01-09 Snecma Perfectionnement aux fusées
US3584972A (en) * 1966-02-09 1971-06-15 Gen Motors Corp Laminated porous metal
US3728039A (en) * 1966-11-02 1973-04-17 Gen Electric Fluid cooled porous stator structure
US3585800A (en) * 1967-07-27 1971-06-22 Aerojet General Co Transpiration-cooled devices
DE1626032A1 (de) * 1967-08-31 1971-01-14 Daimler Benz Ag Thermischer Belastung ausgesetzter und mit einem Gas zu kuehlender Teil eines Gasturbinentriebwerkes
US3623711A (en) * 1970-07-13 1971-11-30 Avco Corp Combustor liner cooling arrangement
US3777484A (en) * 1971-12-08 1973-12-11 Gen Electric Shrouded combustion liner
US4004056A (en) * 1975-07-24 1977-01-18 General Motors Corporation Porous laminated sheet
US4158949A (en) * 1977-11-25 1979-06-26 General Motors Corporation Segmented annular combustor
US4195475A (en) * 1977-12-21 1980-04-01 General Motors Corporation Ring connection for porous combustor wall panels
US4180972A (en) * 1978-06-08 1980-01-01 General Motors Corporation Combustor support structure
US4420929A (en) * 1979-01-12 1983-12-20 General Electric Company Dual stage-dual mode low emission gas turbine combustion system
US4232527A (en) * 1979-04-13 1980-11-11 General Motors Corporation Combustor liner joints
US4269032A (en) * 1979-06-13 1981-05-26 General Motors Corporation Waffle pattern porous material
US4302940A (en) * 1979-06-13 1981-12-01 General Motors Corporation Patterned porous laminated material
US4292801A (en) * 1979-07-11 1981-10-06 General Electric Company Dual stage-dual mode low nox combustor
US4312186A (en) * 1979-10-17 1982-01-26 General Motors Corporation Shingled laminated porous material
US4698963A (en) * 1981-04-22 1987-10-13 The United States Of America As Represented By The Department Of Energy Low NOx combustor
US4422300A (en) * 1981-12-14 1983-12-27 United Technologies Corporation Prestressed combustor liner for gas turbine engine

Also Published As

Publication number Publication date
KR910020305A (ko) 1991-12-19
NO911712D0 (no) 1991-04-30
JPH04227414A (ja) 1992-08-17
KR940001924B1 (ko) 1994-03-11
CN1056563A (zh) 1991-11-27
CA2040780A1 (en) 1991-11-04
US5127221A (en) 1992-07-07
EP0455487A1 (en) 1991-11-06

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