JP2003194338A - 可変出口形状を有するガスタービンエンジン用燃料/空気プレミキサ及び出口速度の制御方法 - Google Patents

可変出口形状を有するガスタービンエンジン用燃料/空気プレミキサ及び出口速度の制御方法

Info

Publication number
JP2003194338A
JP2003194338A JP2002361309A JP2002361309A JP2003194338A JP 2003194338 A JP2003194338 A JP 2003194338A JP 2002361309 A JP2002361309 A JP 2002361309A JP 2002361309 A JP2002361309 A JP 2002361309A JP 2003194338 A JP2003194338 A JP 2003194338A
Authority
JP
Japan
Prior art keywords
fuel
air
premixer
outlet
valve
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.)
Pending
Application number
JP2002361309A
Other languages
English (en)
Japanese (ja)
Inventor
R Jan Mowill
モウィル アール.ジャン
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.)
Individual
Original Assignee
Individual
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
Priority claimed from US10/014,415 external-priority patent/US6925809B2/en
Application filed by Individual filed Critical Individual
Publication of JP2003194338A publication Critical patent/JP2003194338A/ja
Pending 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50Combustion chambers comprising an annular flame tube within an annular casing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/101Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
    • F23D11/102Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber
    • F23D11/103Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber with means creating a swirl inside the mixing chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/62Mixing devices; Mixing tubes
    • F23D14/64Mixing devices; Mixing tubes with injectors
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
JP2002361309A 2001-12-14 2002-12-12 可変出口形状を有するガスタービンエンジン用燃料/空気プレミキサ及び出口速度の制御方法 Pending JP2003194338A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/014415 2001-12-14
US10/014,415 US6925809B2 (en) 1999-02-26 2001-12-14 Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities

Publications (1)

Publication Number Publication Date
JP2003194338A true JP2003194338A (ja) 2003-07-09

Family

ID=21765345

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002361309A Pending JP2003194338A (ja) 2001-12-14 2002-12-12 可変出口形状を有するガスタービンエンジン用燃料/空気プレミキサ及び出口速度の制御方法

Country Status (2)

Country Link
EP (1) EP1319896A3 (de)
JP (1) JP2003194338A (de)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006090327A (ja) * 2004-09-23 2006-04-06 Snecma ターボ機械燃焼室に空気/燃料混合物を噴射する発泡性空気力式システム
JP2009052558A (ja) * 2007-08-28 2009-03-12 General Electric Co <Ge> 統合制御弁を有するガスタービンエンジン燃焼器アセンブリ
JP2009052560A (ja) * 2007-08-28 2009-03-12 General Electric Co <Ge> ガスタービン内における燃料及び空気の混合のためのシステム及び方法
KR20190104900A (ko) * 2018-03-01 2019-09-11 제네럴 일렉트릭 컴퍼니 가스 터빈 엔진용 연료 분사기 조립체

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DE10210034B4 (de) * 2002-03-07 2009-10-01 Webasto Ag Mobiles Heizgerät mit einer Brennstoffversorgung
GB2405197B (en) * 2003-08-16 2005-09-28 Rolls Royce Plc Fuel injector
DE502005001634D1 (de) * 2004-05-05 2007-11-15 Alstom Technology Ltd Brennkammer für gasturbine
WO2006059986A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
WO2006060004A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Combustor for turbine engine
US7854112B2 (en) 2004-12-01 2010-12-21 United Technologies Corporation Vectoring transition duct for turbine engine
WO2006060000A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
DE602004019710D1 (de) 2004-12-01 2009-04-09 United Technologies Corp Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
DE602004028297D1 (de) 2004-12-01 2010-09-02 United Technologies Corp Umfangsbrennkammer für spitzenturbinenmotor
EP1825117B1 (de) 2004-12-01 2012-06-13 United Technologies Corporation Turbinentriebwerk mit von einem differentialgetriebe angetriebenem fan und verdichter
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
WO2006059968A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
US7921636B2 (en) 2004-12-01 2011-04-12 United Technologies Corporation Tip turbine engine and corresponding operating method
EP1825116A2 (de) 2004-12-01 2007-08-29 United Technologies Corporation Ejektor-kühlung des aussengehäuses eines tip-turbinen-triebwerks
US11015808B2 (en) 2011-12-13 2021-05-25 General Electric Company Aerodynamically enhanced premixer with purge slots for reduced emissions
CN105485722B (zh) * 2015-12-30 2017-11-10 中国科学院工程热物理研究所 一种可引射流体的扩张段燃烧器
GB2606206A (en) * 2021-04-29 2022-11-02 Bosch Thermotechnology Ltd Uk A two-stage air-gas mixing unit for an air-gas mixture burning appliance
US11821389B2 (en) 2021-08-20 2023-11-21 Caterpillar Inc. Method and system for supplying fuel gas
CN114321978B (zh) * 2021-11-29 2022-10-21 南京航空航天大学 一种扩压器出口流量分配智能调节系统及调节方法

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US4255927A (en) 1978-06-29 1981-03-17 General Electric Company Combustion control system
JPS5545739A (en) 1978-09-29 1980-03-31 Japan Crown Cork Co Ltd Bonding of polyolefin liner to metallic crown cap
US4297842A (en) 1980-01-21 1981-11-03 General Electric Company NOx suppressant stationary gas turbine combustor
JPS5741524A (en) 1980-08-25 1982-03-08 Hitachi Ltd Combustion method of gas turbine and combustor for gas turbine
DE3306892A1 (de) * 1983-02-26 1984-08-30 Jörg 8775 Partenstein Köster Gasbrenner zur beheizung von industrieoefen
EP0169431B1 (de) 1984-07-10 1990-04-11 Hitachi, Ltd. Brennkammer für eine Gasturbine
JPH0663646B2 (ja) 1985-10-11 1994-08-22 株式会社日立製作所 ガスタ−ビン用燃焼器
US4994149A (en) 1986-03-06 1991-02-19 Delta Projects Inc. Diluent substitution apparatus
JP2644745B2 (ja) 1987-03-06 1997-08-25 株式会社日立製作所 ガスタービン用燃焼器
DE3770823D1 (de) 1987-10-19 1991-07-18 Hitachi Ltd Einrichtung zur regulierung des verbrennungsluftdurchsatzes in gasturbinenbrennkammern.
US5638674A (en) 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US5572862A (en) 1993-07-07 1996-11-12 Mowill Rolf Jan Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
US5613357A (en) 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
US5377483A (en) 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
JP3706443B2 (ja) * 1996-09-24 2005-10-12 三菱重工業株式会社 アニュラ型ガスタービン燃焼器
EP1036988A3 (de) * 1999-02-26 2001-05-16 R. Jan Mowill Kraftstoff/Luft-Vormischeinrichtung mit veränderlicher Geometrie und Methode, die Ausströmgeschwindigkeit zu regeln
WO2001040713A1 (en) * 1999-12-03 2001-06-07 Mowill Rolf Jan Cooled premixer exit nozzle for gas turbine combustor and method of operation therefor

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006090327A (ja) * 2004-09-23 2006-04-06 Snecma ターボ機械燃焼室に空気/燃料混合物を噴射する発泡性空気力式システム
JP4695952B2 (ja) * 2004-09-23 2011-06-08 スネクマ ターボ機械燃焼室に空気/燃料混合物を噴射する発泡性空気力式システム
JP2009052558A (ja) * 2007-08-28 2009-03-12 General Electric Co <Ge> 統合制御弁を有するガスタービンエンジン燃焼器アセンブリ
JP2009052560A (ja) * 2007-08-28 2009-03-12 General Electric Co <Ge> ガスタービン内における燃料及び空気の混合のためのシステム及び方法
KR20190104900A (ko) * 2018-03-01 2019-09-11 제네럴 일렉트릭 컴퍼니 가스 터빈 엔진용 연료 분사기 조립체
KR102201125B1 (ko) 2018-03-01 2021-01-11 제네럴 일렉트릭 컴퍼니 가스 터빈 엔진용 연료 분사기 조립체

Also Published As

Publication number Publication date
EP1319896A3 (de) 2004-05-12
EP1319896A2 (de) 2003-06-18

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