WO2009028474A1 - ガスタービン燃焼器 - Google Patents

ガスタービン燃焼器 Download PDF

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Publication number
WO2009028474A1
WO2009028474A1 PCT/JP2008/065136 JP2008065136W WO2009028474A1 WO 2009028474 A1 WO2009028474 A1 WO 2009028474A1 JP 2008065136 W JP2008065136 W JP 2008065136W WO 2009028474 A1 WO2009028474 A1 WO 2009028474A1
Authority
WO
WIPO (PCT)
Prior art keywords
oil fuel
lengths
nozzle pipe
pipe base
gas turbine
Prior art date
Application number
PCT/JP2008/065136
Other languages
English (en)
French (fr)
Inventor
Yoshitaka Terada
Tetsu Konishi
Katsuyoshi Omae
Original Assignee
Mitsubishi Heavy Industries, Ltd.
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 Mitsubishi Heavy Industries, Ltd. filed Critical Mitsubishi Heavy Industries, Ltd.
Priority to EP08828209.0A priority Critical patent/EP2182195B1/en
Priority to CN200880103222A priority patent/CN101784776A/zh
Priority to US12/670,039 priority patent/US8544276B2/en
Publication of WO2009028474A1 publication Critical patent/WO2009028474A1/ja

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
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36—Supply of different fuels
    • 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
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)

Abstract

　低コストとなるガスタービン燃焼器を提供する。そのため、油燃料を供給する油燃料通路とガス燃料を供給するガス燃料通路とを備えた複数のメインノズルがノズル管台１１に環状に支持されたガスタービン燃焼器において、複数の油燃料通路を、ノズル管台１１を貫通して設けると共に、複数の油燃料通路と各々接続され、ノズル管台１１に立設された複数の立設配管２１を設け、ノズル管台１１の外部において立設配管２１同士を多角形状に最短距離で接続する複数の接続配管２２とを設け、該接続配管２２の１つに油燃料の供給部１４を接続して、各々の油燃料通路に油燃料を分配するようにした。
PCT/JP2008/065136 2007-08-29 2008-08-26 ガスタービン燃焼器 WO2009028474A1 (ja)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP08828209.0A EP2182195B1 (en) 2007-08-29 2008-08-26 Gas turbine combustor
CN200880103222A CN101784776A (zh) 2007-08-29 2008-08-26 燃气涡轮机燃烧器
US12/670,039 US8544276B2 (en) 2007-08-29 2008-08-26 Gas turbine combustor having a dual fuel supply system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2007-222037 2007-08-29
JP2007222037A JP4764392B2 (ja) 2007-08-29 2007-08-29 ガスタービン燃焼器

Publications (1)

Publication Number Publication Date
WO2009028474A1 true WO2009028474A1 (ja) 2009-03-05

Family

ID=40387194

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2008/065136 WO2009028474A1 (ja) 2007-08-29 2008-08-26 ガスタービン燃焼器

Country Status (6)

Country Link
US (1) US8544276B2 (ja)
EP (1) EP2182195B1 (ja)
JP (1) JP4764392B2 (ja)
KR (1) KR101121373B1 (ja)
CN (1) CN101784776A (ja)
WO (1) WO2009028474A1 (ja)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011137452A (ja) * 2009-12-31 2011-07-14 General Electric Co <Ge> 振動数調整可能なブラケットレス流体マニホルド
CN102741614A (zh) * 2010-03-30 2012-10-17 三菱重工业株式会社 燃烧器及燃气轮机
CN112780416A (zh) * 2021-01-29 2021-05-11 安徽应流航空科技有限公司 一种主燃油分配结构

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8745987B2 (en) * 2010-10-28 2014-06-10 General Electric Company Late lean injection manifold
US9163841B2 (en) * 2011-09-23 2015-10-20 Siemens Aktiengesellschaft Cast manifold for dry low NOx gas turbine engine
JP5931636B2 (ja) 2012-07-30 2016-06-08 三菱日立パワーシステムズ株式会社 燃焼器ノズル組体、これを備えている燃焼器及びガスタービン
EP3060851B1 (en) * 2013-10-24 2019-11-27 United Technologies Corporation Circumferentially and axially staged can combustor for gas turbine engine
CN104154565B (zh) * 2014-07-22 2016-04-20 中国航空动力机械研究所 用于发动机燃烧室的燃油总管及制造方法和航空发动机
KR101709004B1 (ko) * 2015-07-03 2017-02-21 두산중공업 주식회사 가스터빈의 연소장치 및 이의 제어방법
CN105841192B (zh) * 2016-05-29 2018-02-13 无锡商业职业技术学院 一种用于燃气轮机的燃烧喷嘴
US11002193B2 (en) 2017-12-15 2021-05-11 Delavan Inc. Fuel injector systems and support structures

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55500647A (ja) * 1978-09-15 1980-09-11
JPS57186026A (en) * 1981-04-17 1982-11-16 Gen Electric Gas turbine fuel device
JPH04314933A (ja) * 1991-01-18 1992-11-06 General Electric Co <Ge> ガスタービンエンジン燃料マニホルド
JPH085075A (ja) * 1994-06-13 1996-01-12 Westinghouse Electric Corp <We> ガスタービン

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2690648A (en) * 1951-07-03 1954-10-05 Dowty Equipment Ltd Means for conducting the flow of liquid fuel for feeding burners of gas turbine engines
US4201046A (en) * 1977-12-27 1980-05-06 United Technologies Corporation Burner nozzle assembly for gas turbine engine
US4763481A (en) * 1985-06-07 1988-08-16 Ruston Gas Turbines Limited Combustor for gas turbine engine
US5231833A (en) * 1991-01-18 1993-08-03 General Electric Company Gas turbine engine fuel manifold
US5657632A (en) * 1994-11-10 1997-08-19 Westinghouse Electric Corporation Dual fuel gas turbine combustor
US5833141A (en) * 1997-05-30 1998-11-10 General Electric Company Anti-coking dual-fuel nozzle for a gas turbine combustor
US6038861A (en) * 1998-06-10 2000-03-21 Siemens Westinghouse Power Corporation Main stage fuel mixer with premixing transition for dry low Nox (DLN) combustors
US6598383B1 (en) * 1999-12-08 2003-07-29 General Electric Co. Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels
JP2002349854A (ja) * 2001-05-30 2002-12-04 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器のパイロットノズルおよび供給路変換器
JP3495730B2 (ja) * 2002-04-15 2004-02-09 三菱重工業株式会社 ガスタービンの燃焼器
JP3684208B2 (ja) 2002-05-20 2005-08-17 株式会社東芝 ガスタービン制御装置
US7546735B2 (en) * 2004-10-14 2009-06-16 General Electric Company Low-cost dual-fuel combustor and related method
JP4728176B2 (ja) * 2005-06-24 2011-07-20 株式会社日立製作所 バーナ、ガスタービン燃焼器及びバーナの冷却方法

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55500647A (ja) * 1978-09-15 1980-09-11
JPS57186026A (en) * 1981-04-17 1982-11-16 Gen Electric Gas turbine fuel device
JPH04314933A (ja) * 1991-01-18 1992-11-06 General Electric Co <Ge> ガスタービンエンジン燃料マニホルド
JPH085075A (ja) * 1994-06-13 1996-01-12 Westinghouse Electric Corp <We> ガスタービン

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011137452A (ja) * 2009-12-31 2011-07-14 General Electric Co <Ge> 振動数調整可能なブラケットレス流体マニホルド
CN102741614A (zh) * 2010-03-30 2012-10-17 三菱重工业株式会社 燃烧器及燃气轮机
CN102741614B (zh) * 2010-03-30 2014-11-12 三菱重工业株式会社 燃烧器及燃气轮机
CN112780416A (zh) * 2021-01-29 2021-05-11 安徽应流航空科技有限公司 一种主燃油分配结构

Also Published As

Publication number Publication date
EP2182195B1 (en) 2016-02-17
JP4764392B2 (ja) 2011-08-31
US20100192584A1 (en) 2010-08-05
EP2182195A4 (en) 2014-06-18
JP2009052513A (ja) 2009-03-12
CN101784776A (zh) 2010-07-21
KR101121373B1 (ko) 2012-03-09
EP2182195A1 (en) 2010-05-05
US8544276B2 (en) 2013-10-01
KR20100029274A (ko) 2010-03-16

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