CN103375816B - 用于将燃料供应到燃烧器的系统 - Google Patents

用于将燃料供应到燃烧器的系统 Download PDF

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Publication number
CN103375816B
CN103375816B CN201310149399.5A CN201310149399A CN103375816B CN 103375816 B CN103375816 B CN 103375816B CN 201310149399 A CN201310149399 A CN 201310149399A CN 103375816 B CN103375816 B CN 103375816B
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CN
China
Prior art keywords
liquid fuel
combustion chamber
chamber
channels
circumferentially
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
CN201310149399.5A
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English (en)
Chinese (zh)
Other versions
CN103375816A (zh
Inventor
B.W.罗米格
L.J.斯托亚
P.B.梅尔顿
T.E.约翰逊
G.A.博德曼
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
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN103375816A publication Critical patent/CN103375816A/zh
Application granted granted Critical
Publication of CN103375816B publication Critical patent/CN103375816B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • F23R3/346Feeding into different combustion zones for staged combustion
    • 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
    • F23R3/36Supply of different fuels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/22Fuel supply systems

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)
  • Spray-Type Burners (AREA)
CN201310149399.5A 2012-04-27 2013-04-26 用于将燃料供应到燃烧器的系统 Expired - Fee Related CN103375816B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/457,726 2012-04-27
US13/457726 2012-04-27
US13/457,726 US9200808B2 (en) 2012-04-27 2012-04-27 System for supplying fuel to a late-lean fuel injector of a combustor

Publications (2)

Publication Number Publication Date
CN103375816A CN103375816A (zh) 2013-10-30
CN103375816B true CN103375816B (zh) 2016-08-17

Family

ID=48182805

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310149399.5A Expired - Fee Related CN103375816B (zh) 2012-04-27 2013-04-26 用于将燃料供应到燃烧器的系统

Country Status (5)

Country Link
US (1) US9200808B2 (https=)
EP (1) EP2657611B1 (https=)
JP (1) JP6203528B2 (https=)
CN (1) CN103375816B (https=)
RU (1) RU2618765C2 (https=)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9297534B2 (en) 2011-07-29 2016-03-29 General Electric Company Combustor portion for a turbomachine and method of operating a turbomachine
US8904796B2 (en) * 2011-10-19 2014-12-09 General Electric Company Flashback resistant tubes for late lean injector and method for forming the tubes
US20130111918A1 (en) * 2011-11-07 2013-05-09 General Electric Company Combustor assembly for a gas turbomachine
US9097424B2 (en) * 2012-03-12 2015-08-04 General Electric Company System for supplying a fuel and working fluid mixture to a combustor
US8745986B2 (en) * 2012-07-10 2014-06-10 General Electric Company System and method of supplying fuel to a gas turbine
WO2014092185A1 (ja) * 2012-12-13 2014-06-19 川崎重工業株式会社 マルチ燃料対応のガスタービン燃焼器
US10139111B2 (en) * 2014-03-28 2018-11-27 Siemens Energy, Inc. Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine
EP2902708B1 (en) * 2014-06-12 2017-02-01 Kawasaki Jukogyo Kabushiki Kaisha Multi-fuel-supporting gas-turbine combustor
WO2016032436A1 (en) * 2014-08-26 2016-03-03 Siemens Energy, Inc. Cooling system for fuel nozzles within combustor in a turbine engine
FR3029271B1 (fr) * 2014-11-28 2019-06-21 Safran Aircraft Engines Paroi annulaire de deflection pour systeme d'injection de chambre de combustion de turbomachine offrant une zone etendue d'atomisation de carburant
JP2016109309A (ja) * 2014-12-02 2016-06-20 川崎重工業株式会社 ガスタービン用燃焼器、及びガスタービン
WO2016104725A1 (ja) * 2014-12-25 2016-06-30 川崎重工業株式会社 バーナ、燃焼器、及びガスタービン
US10054314B2 (en) * 2015-12-17 2018-08-21 General Electric Company Slotted injector for axial fuel staging
US20170260866A1 (en) * 2016-03-10 2017-09-14 Siemens Energy, Inc. Ducting arrangement in a combustion system of a gas turbine engine
US20170268776A1 (en) * 2016-03-15 2017-09-21 General Electric Company Gas turbine flow sleeve mounting
US11029030B2 (en) * 2016-08-03 2021-06-08 Siemens Energy Global GmbH & Co. KG Ducting arrangement with injector assemblies configured to form a shielding flow of air injected into a combustion stage in a gas turbine engine
WO2018026381A1 (en) * 2016-08-03 2018-02-08 Siemens Aktiengesellschaft Combustion system with injector assemblies arranged to recapture cooling air in a combustor wall to form a shielding flow of air in a combustion stage
US10502426B2 (en) 2017-05-12 2019-12-10 General Electric Company Dual fuel injectors and methods of use in gas turbine combustor
US20180340689A1 (en) * 2017-05-25 2018-11-29 General Electric Company Low Profile Axially Staged Fuel Injector
US10690349B2 (en) * 2017-09-01 2020-06-23 General Electric Company Premixing fuel injectors and methods of use in gas turbine combustor
US11187415B2 (en) * 2017-12-11 2021-11-30 General Electric Company Fuel injection assemblies for axial fuel staging in gas turbine combustors
US10816203B2 (en) * 2017-12-11 2020-10-27 General Electric Company Thimble assemblies for introducing a cross-flow into a secondary combustion zone
US11137144B2 (en) * 2017-12-11 2021-10-05 General Electric Company Axial fuel staging system for gas turbine combustors
US11022308B2 (en) 2018-05-31 2021-06-01 Honeywell International Inc. Double wall combustors with strain isolated inserts
US11933223B2 (en) * 2019-04-18 2024-03-19 Rtx Corporation Integrated additive fuel injectors for attritable engines
KR102164620B1 (ko) * 2019-06-19 2020-10-12 두산중공업 주식회사 연소기 및 이를 포함하는 가스터빈
US11333360B2 (en) * 2020-09-25 2022-05-17 General Electric Company Fuel injector for a turbomachine
US11846426B2 (en) 2021-06-24 2023-12-19 General Electric Company Gas turbine combustor having secondary fuel nozzles with plural passages for injecting a diluent and a fuel
CN114909675B (zh) * 2022-04-07 2024-03-01 中国联合重型燃气轮机技术有限公司 用于燃气涡轮机的燃烧室和燃气轮机
CN117109030B (zh) * 2022-05-16 2025-09-19 通用电气公司 燃烧器衬里中的热声阻尼器
CA3257195A1 (en) * 2022-05-23 2023-11-30 Casale Sa BURNER FOR REFORMING REACTOR
CN115059544A (zh) * 2022-07-01 2022-09-16 星辰萌想科技(北京)有限公司 一种具有双燃烧部的燃气轮机
CN115075946B (zh) * 2022-07-01 2024-11-01 星辰萌想科技(北京)有限公司 一种双燃烧部燃气轮机
DE102022208339A1 (de) 2022-08-10 2024-02-15 Rolls-Royce Deutschland Ltd & Co Kg Brennkammeranordnung zum Betrieb mit flüssigem und/oder gasförmigem Kraftstoff, Gasturbinenanordnung und Verfahren
US12188658B1 (en) 2023-07-07 2025-01-07 Ge Infrastructure Technology Llc Fuel injection assembly for a combustor
US12467630B2 (en) 2023-07-07 2025-11-11 Ge Vernova Infrastructure Technology Llc Fuel injection assembly having a boss with a serpentine cooling passage
US12429224B1 (en) * 2024-05-09 2025-09-30 Ge Infrastructure Technology Llc Axial fuel stage injector with fuel injection in same direction as high-pressure air flow
US12449128B1 (en) 2024-11-27 2025-10-21 Ge Vernova Infrastructure Technology Llc Boss for a fuel injection assembly having cooling circuit and combustor provided therewith

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5235813A (en) * 1990-12-24 1993-08-17 United Technologies Corporation Mechanism for controlling the rate of mixing in combusting flows
CN1118857A (zh) * 1994-04-02 1996-03-20 Abb管理有限公司 预混燃烧器
CN101235969A (zh) * 2007-01-31 2008-08-06 通用电气公司 具有同轴燃料-空气通道的逆流喷射机构

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2221621B1 (https=) * 1973-03-13 1976-09-10 Snecma
US3901445A (en) * 1974-11-08 1975-08-26 Pullman Inc Gas burner - lance construction
JPS6143637U (ja) * 1984-08-21 1986-03-22 三菱重工業株式会社 ガスタ−ビンの燃焼バ−ナ
US5749219A (en) * 1989-11-30 1998-05-12 United Technologies Corporation Combustor with first and second zones
US5207064A (en) 1990-11-21 1993-05-04 General Electric Company Staged, mixed combustor assembly having low emissions
GB9410233D0 (en) * 1994-05-21 1994-07-06 Rolls Royce Plc A gas turbine engine combustion chamber
JP3346034B2 (ja) * 1994-06-30 2002-11-18 石川島播磨重工業株式会社 ガスタービン用燃焼装置
JPH08145361A (ja) * 1994-11-16 1996-06-07 Ishikawajima Harima Heavy Ind Co Ltd ガスタービン用燃料噴射弁
JP3012166B2 (ja) * 1995-02-01 2000-02-21 川崎重工業株式会社 ガスタービン燃焼システム
US5622054A (en) * 1995-12-22 1997-04-22 General Electric Company Low NOx lobed mixer fuel injector
US6122916A (en) * 1998-01-02 2000-09-26 Siemens Westinghouse Power Corporation Pilot cones for dry low-NOx combustors
GB9813972D0 (en) * 1998-06-30 1998-08-26 Rolls Royce Plc A combustion chamber
JP2002523717A (ja) * 1998-08-20 2002-07-30 シーメンス アクチエンゲゼルシヤフト ハイブリッドバーナの運転方法
US6868676B1 (en) * 2002-12-20 2005-03-22 General Electric Company Turbine containing system and an injector therefor
JP2005147459A (ja) * 2003-11-13 2005-06-09 Hitachi Ltd ガスタービン燃焼器及びガスタービン燃焼器の燃料供給方法
JP4670035B2 (ja) * 2004-06-25 2011-04-13 独立行政法人 宇宙航空研究開発機構 ガスタービン燃焼器
JP2006090602A (ja) * 2004-09-22 2006-04-06 Japan Aerospace Exploration Agency ローブミキサー及び予混合器
US20060156734A1 (en) * 2005-01-15 2006-07-20 Siemens Westinghouse Power Corporation Gas turbine combustor
US7966822B2 (en) * 2005-06-30 2011-06-28 General Electric Company Reverse-flow gas turbine combustion system
US8387390B2 (en) * 2006-01-03 2013-03-05 General Electric Company Gas turbine combustor having counterflow injection mechanism
US20070151251A1 (en) * 2006-01-03 2007-07-05 Haynes Joel M Counterflow injection mechanism having coaxial fuel-air passages
JP5193695B2 (ja) * 2008-06-17 2013-05-08 新潟原動機株式会社 燃料噴射装置
CN102165258B (zh) * 2008-09-29 2014-01-22 西门子公司 燃料喷嘴
US20100223930A1 (en) * 2009-03-06 2010-09-09 General Electric Company Injection device for a turbomachine
RU86280U1 (ru) * 2009-04-10 2009-08-27 Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации Устройство сжигания топлива в камере сгорания
US8991192B2 (en) * 2009-09-24 2015-03-31 Siemens Energy, Inc. Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine
US8381532B2 (en) * 2010-01-27 2013-02-26 General Electric Company Bled diffuser fed secondary combustion system for gas turbines
EP2362148A1 (en) * 2010-02-23 2011-08-31 Siemens Aktiengesellschaft Fuel injector and swirler assembly with lobed mixer
US8752386B2 (en) * 2010-05-25 2014-06-17 Siemens Energy, Inc. Air/fuel supply system for use in a gas turbine engine
US8769955B2 (en) * 2010-06-02 2014-07-08 Siemens Energy, Inc. Self-regulating fuel staging port for turbine combustor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5235813A (en) * 1990-12-24 1993-08-17 United Technologies Corporation Mechanism for controlling the rate of mixing in combusting flows
CN1118857A (zh) * 1994-04-02 1996-03-20 Abb管理有限公司 预混燃烧器
CN101235969A (zh) * 2007-01-31 2008-08-06 通用电气公司 具有同轴燃料-空气通道的逆流喷射机构

Also Published As

Publication number Publication date
CN103375816A (zh) 2013-10-30
RU2013119328A (ru) 2014-11-10
RU2618765C2 (ru) 2017-05-11
JP6203528B2 (ja) 2017-09-27
EP2657611A2 (en) 2013-10-30
US20130283801A1 (en) 2013-10-31
US9200808B2 (en) 2015-12-01
EP2657611B1 (en) 2019-11-20
EP2657611A3 (en) 2017-11-22
JP2013231580A (ja) 2013-11-14

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