DE60237262D1 - Methode und Anlage zur Reduzierung der Schadstoffausstosses der Brennkammer - Google Patents

Methode und Anlage zur Reduzierung der Schadstoffausstosses der Brennkammer

Info

Publication number
DE60237262D1
DE60237262D1 DE60237262T DE60237262T DE60237262D1 DE 60237262 D1 DE60237262 D1 DE 60237262D1 DE 60237262 T DE60237262 T DE 60237262T DE 60237262 T DE60237262 T DE 60237262T DE 60237262 D1 DE60237262 D1 DE 60237262D1
Authority
DE
Germany
Prior art keywords
combustion chamber
pollutant emissions
reducing pollutant
reducing
emissions
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
Application number
DE60237262T
Other languages
English (en)
Inventor
Michael Jerome Foust
Hukam Chand Mongia
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
Application granted granted Critical
Publication of DE60237262D1 publication Critical patent/DE60237262D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • F23R3/343Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE60237262T 2001-05-31 2002-05-20 Methode und Anlage zur Reduzierung der Schadstoffausstosses der Brennkammer Expired - Lifetime DE60237262D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/871,343 US6484489B1 (en) 2001-05-31 2001-05-31 Method and apparatus for mixing fuel to decrease combustor emissions

Publications (1)

Publication Number Publication Date
DE60237262D1 true DE60237262D1 (de) 2010-09-23

Family

ID=25357242

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60237262T Expired - Lifetime DE60237262D1 (de) 2001-05-31 2002-05-20 Methode und Anlage zur Reduzierung der Schadstoffausstosses der Brennkammer

Country Status (6)

Country Link
US (1) US6484489B1 (de)
EP (1) EP1262718B1 (de)
JP (1) JP4162429B2 (de)
BR (1) BR0201961B1 (de)
DE (1) DE60237262D1 (de)
NO (1) NO332838B1 (de)

Families Citing this family (55)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020162333A1 (en) * 2001-05-02 2002-11-07 Honeywell International, Inc., Law Dept. Ab2 Partial premix dual circuit fuel injector
US6865889B2 (en) 2002-02-01 2005-03-15 General Electric Company Method and apparatus to decrease combustor emissions
US6898938B2 (en) * 2003-04-24 2005-05-31 General Electric Company Differential pressure induced purging fuel injector with asymmetric cyclone
US7062920B2 (en) * 2003-08-11 2006-06-20 General Electric Company Combustor dome assembly of a gas turbine engine having a free floating swirler
US7121095B2 (en) * 2003-08-11 2006-10-17 General Electric Company Combustor dome assembly of a gas turbine engine having improved deflector plates
US6976363B2 (en) * 2003-08-11 2005-12-20 General Electric Company Combustor dome assembly of a gas turbine engine having a contoured swirler
US7104464B2 (en) * 2003-12-25 2006-09-12 Kawasaki Jukogyo Kabushiki Kaisha Fuel supply method and fuel supply system
US8348180B2 (en) * 2004-06-09 2013-01-08 Delavan Inc Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same
US7415826B2 (en) * 2005-07-25 2008-08-26 General Electric Company Free floating mixer assembly for combustor of a gas turbine engine
US7581396B2 (en) * 2005-07-25 2009-09-01 General Electric Company Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers
US20070028618A1 (en) * 2005-07-25 2007-02-08 General Electric Company Mixer assembly for combustor of a gas turbine engine having a main mixer with improved fuel penetration
US20070028595A1 (en) * 2005-07-25 2007-02-08 Mongia Hukam C High pressure gas turbine engine having reduced emissions
US7464553B2 (en) * 2005-07-25 2008-12-16 General Electric Company Air-assisted fuel injector for mixer assembly of a gas turbine engine combustor
US7565803B2 (en) * 2005-07-25 2009-07-28 General Electric Company Swirler arrangement for mixer assembly of a gas turbine engine combustor having shaped passages
US7878000B2 (en) * 2005-12-20 2011-02-01 General Electric Company Pilot fuel injector for mixer assembly of a high pressure gas turbine engine
US7762073B2 (en) * 2006-03-01 2010-07-27 General Electric Company Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection ports
US8001761B2 (en) * 2006-05-23 2011-08-23 General Electric Company Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor
US20100251719A1 (en) 2006-12-29 2010-10-07 Alfred Albert Mancini Centerbody for mixer assembly of a gas turbine engine combustor
DE102007034737A1 (de) 2007-07-23 2009-01-29 General Electric Co. Verfahren und Vorrichtung zur aktiven Steuerung des Brennstoffzustroms zu einer Mischeinheit einer Gasturbinenbrennkammer
DE102007038220A1 (de) 2007-08-13 2009-02-19 General Electric Co. Pilotmischer für eine Mischeinrichtung einer Gasturbinentriebwerksbrennkammer mit einer primären Brennstoffeinspritzeinrichtung und mehreren sekundären Brennstoffeinspritzanschlüssen
DE102007050276A1 (de) * 2007-10-18 2009-04-23 Rolls-Royce Deutschland Ltd & Co Kg Magervormischbrenner für ein Gasturbinentriebwerk
US7926744B2 (en) * 2008-02-21 2011-04-19 Delavan Inc Radially outward flowing air-blast fuel injector for gas turbine engine
US8061142B2 (en) 2008-04-11 2011-11-22 General Electric Company Mixer for a combustor
US8225610B2 (en) * 2008-12-08 2012-07-24 General Electric Company Fuel delivery system and method of assembling the same
US20100263382A1 (en) 2009-04-16 2010-10-21 Alfred Albert Mancini Dual orifice pilot fuel injector
US9354618B2 (en) 2009-05-08 2016-05-31 Gas Turbine Efficiency Sweden Ab Automated tuning of multiple fuel gas turbine combustion systems
US8437941B2 (en) 2009-05-08 2013-05-07 Gas Turbine Efficiency Sweden Ab Automated tuning of gas turbine combustion systems
US9671797B2 (en) 2009-05-08 2017-06-06 Gas Turbine Efficiency Sweden Ab Optimization of gas turbine combustion systems low load performance on simple cycle and heat recovery steam generator applications
US9267443B2 (en) 2009-05-08 2016-02-23 Gas Turbine Efficiency Sweden Ab Automated tuning of gas turbine combustion systems
US8365532B2 (en) * 2009-09-30 2013-02-05 General Electric Company Apparatus and method for a gas turbine nozzle
US9027350B2 (en) * 2009-12-30 2015-05-12 Rolls-Royce Corporation Gas turbine engine having dome panel assembly with bifurcated swirler flow
US20110162375A1 (en) * 2010-01-05 2011-07-07 General Electric Company Secondary Combustion Fuel Supply Systems
US8726668B2 (en) 2010-12-17 2014-05-20 General Electric Company Fuel atomization dual orifice fuel nozzle
US20120151928A1 (en) 2010-12-17 2012-06-21 Nayan Vinodbhai Patel Cooling flowpath dirt deflector in fuel nozzle
US9920932B2 (en) 2011-01-26 2018-03-20 United Technologies Corporation Mixer assembly for a gas turbine engine
US8312724B2 (en) 2011-01-26 2012-11-20 United Technologies Corporation Mixer assembly for a gas turbine engine having a pilot mixer with a corner flame stabilizing recirculation zone
US8973368B2 (en) 2011-01-26 2015-03-10 United Technologies Corporation Mixer assembly for a gas turbine engine
US8893500B2 (en) 2011-05-18 2014-11-25 Solar Turbines Inc. Lean direct fuel injector
US8919132B2 (en) 2011-05-18 2014-12-30 Solar Turbines Inc. Method of operating a gas turbine engine
JP5044034B2 (ja) * 2011-07-26 2012-10-10 川崎重工業株式会社 ガスタービンエンジンの燃料噴霧装置
US11015808B2 (en) 2011-12-13 2021-05-25 General Electric Company Aerodynamically enhanced premixer with purge slots for reduced emissions
US9182124B2 (en) 2011-12-15 2015-11-10 Solar Turbines Incorporated Gas turbine and fuel injector for the same
US20130232978A1 (en) * 2012-03-12 2013-09-12 Zhongtao Dai Fuel air premixer for gas turbine engine
JP5924618B2 (ja) * 2012-06-07 2016-05-25 川崎重工業株式会社 燃料噴射装置
CN103423768B (zh) * 2013-08-09 2015-07-29 中国航空工业集团公司沈阳发动机设计研究所 一种双燃料燃烧室喷嘴自身引气清吹系统
BR112016011777A2 (pt) 2013-11-27 2017-08-08 Gen Electric Aparelhos de bocal de combustível
US10451282B2 (en) 2013-12-23 2019-10-22 General Electric Company Fuel nozzle structure for air assist injection
JP6695801B2 (ja) 2013-12-23 2020-05-20 ゼネラル・エレクトリック・カンパニイ 可撓性支持構造体を備えた燃料ノズル
JP6567537B2 (ja) 2014-02-13 2019-08-28 ゼネラル・エレクトリック・カンパニイ コーキング防止塗膜、その処理、及びそれを備えた炭化水素流体通路
US20150285502A1 (en) * 2014-04-08 2015-10-08 General Electric Company Fuel nozzle shroud and method of manufacturing the shroud
US10502425B2 (en) * 2016-06-03 2019-12-10 General Electric Company Contoured shroud swirling pre-mix fuel injector assembly
US10738704B2 (en) 2016-10-03 2020-08-11 Raytheon Technologies Corporation Pilot/main fuel shifting in an axial staged combustor for a gas turbine engine
US11480338B2 (en) 2017-08-23 2022-10-25 General Electric Company Combustor system for high fuel/air ratio and reduced combustion dynamics
US11561008B2 (en) 2017-08-23 2023-01-24 General Electric Company Fuel nozzle assembly for high fuel/air ratio and reduced combustion dynamics
US10557630B1 (en) 2019-01-15 2020-02-11 Delavan Inc. Stackable air swirlers

Family Cites Families (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2551276A (en) 1949-01-22 1951-05-01 Gen Electric Dual vortex liquid spray nozzle
US2968925A (en) 1959-11-25 1961-01-24 William E Blevans Fuel nozzle head for anti-coking
US3302399A (en) 1964-11-13 1967-02-07 Westinghouse Electric Corp Hollow conical fuel spray nozzle for pressurized combustion apparatus
US3474970A (en) 1967-03-15 1969-10-28 Parker Hannifin Corp Air assist nozzle
US3630024A (en) 1970-02-02 1971-12-28 Gen Electric Air swirler for gas turbine combustor
US3638865A (en) 1970-08-31 1972-02-01 Gen Electric Fuel spray nozzle
US3899884A (en) 1970-12-02 1975-08-19 Gen Electric Combustor systems
US3853273A (en) 1973-10-01 1974-12-10 Gen Electric Axial swirler central injection carburetor
US3980233A (en) 1974-10-07 1976-09-14 Parker-Hannifin Corporation Air-atomizing fuel nozzle
US4198815A (en) 1975-12-24 1980-04-22 General Electric Company Central injection fuel carburetor
US4105163A (en) 1976-10-27 1978-08-08 General Electric Company Fuel nozzle for gas turbines
US4216652A (en) * 1978-06-08 1980-08-12 General Motors Corporation Integrated, replaceable combustor swirler and fuel injector
US4567857A (en) 1980-02-26 1986-02-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Combustion engine system
US4418543A (en) 1980-12-02 1983-12-06 United Technologies Corporation Fuel nozzle for gas turbine engine
US4845940A (en) 1981-02-27 1989-07-11 Westinghouse Electric Corp. Low NOx rich-lean combustor especially useful in gas turbines
US4584834A (en) 1982-07-06 1986-04-29 General Electric Company Gas turbine engine carburetor
US5020329A (en) 1984-12-20 1991-06-04 General Electric Company Fuel delivery system
GB2175993B (en) 1985-06-07 1988-12-21 Rolls Royce Improvements in or relating to dual fuel injectors
CA1306873C (en) 1987-04-27 1992-09-01 Jack R. Taylor Low coke fuel injector for a gas turbine engine
JP2518986Y2 (ja) * 1989-01-20 1996-12-04 川崎重工業株式会社 ガスタービンの燃焼器
US5097666A (en) 1989-12-11 1992-03-24 Sundstrand Corporation Combustor fuel injection system
US5323604A (en) 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
US5435884A (en) 1993-09-30 1995-07-25 Parker-Hannifin Corporation Spray nozzle and method of manufacturing same
GB9326367D0 (en) 1993-12-23 1994-02-23 Rolls Royce Plc Fuel injection apparatus
US5444982A (en) 1994-01-12 1995-08-29 General Electric Company Cyclonic prechamber with a centerbody
DE69506308T2 (de) 1994-04-20 1999-08-26 Rolls Royce Plc Brennstoffeinspritzdüse für Gasturbinentriebwerke
US5584178A (en) 1994-06-14 1996-12-17 Southwest Research Institute Exhaust gas combustor
US5613363A (en) 1994-09-26 1997-03-25 General Electric Company Air fuel mixer for gas turbine combustor
US5590529A (en) 1994-09-26 1997-01-07 General Electric Company Air fuel mixer for gas turbine combustor
JPH08261464A (ja) * 1995-03-20 1996-10-11 Ishikawajima Harima Heavy Ind Co Ltd 乱流混合燃料噴射弁
US5822992A (en) 1995-10-19 1998-10-20 General Electric Company Low emissions combustor premixer
US6047550A (en) 1996-05-02 2000-04-11 General Electric Co. Premixing dry low NOx emissions combustor with lean direct injection of gas fuel
AU7357298A (en) 1997-03-26 1998-10-20 San Diego State University Foundation Fuel/air mixing device for jet engines
DE59801583D1 (de) * 1997-07-17 2001-10-31 Siemens Ag Brenneranordnung für eine feuerungsanlage, insbesondere eine gasturbinenbrennkammer
US6141967A (en) 1998-01-09 2000-11-07 General Electric Company Air fuel mixer for gas turbine combustor
US6195607B1 (en) 1999-07-06 2001-02-27 General Electric Company Method and apparatus for optimizing NOx emissions in a gas turbine
US6381964B1 (en) * 2000-09-29 2002-05-07 General Electric Company Multiple annular combustion chamber swirler having atomizing pilot
US6363726B1 (en) * 2000-09-29 2002-04-02 General Electric Company Mixer having multiple swirlers

Also Published As

Publication number Publication date
JP4162429B2 (ja) 2008-10-08
EP1262718B1 (de) 2010-08-11
BR0201961A (pt) 2003-04-22
NO20022563L (no) 2002-12-02
NO20022563D0 (no) 2002-05-30
BR0201961B1 (pt) 2011-11-16
JP2003004231A (ja) 2003-01-08
US6484489B1 (en) 2002-11-26
US20020178732A1 (en) 2002-12-05
EP1262718A3 (de) 2005-09-07
EP1262718A2 (de) 2002-12-04
NO332838B1 (no) 2013-01-21

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