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FR2970555B1 - Capot d'extremite pour dispositif de combustion de turbine a gaz - Google Patents

Capot d'extremite pour dispositif de combustion de turbine a gaz Download PDF

Info

Publication number
FR2970555B1
FR2970555B1 FR1250490A FR1250490A FR2970555B1 FR 2970555 B1 FR2970555 B1 FR 2970555B1 FR 1250490 A FR1250490 A FR 1250490A FR 1250490 A FR1250490 A FR 1250490A FR 2970555 B1 FR2970555 B1 FR 2970555B1
Authority
FR
France
Prior art keywords
gas turbine
end cover
combustion device
turbine combustion
cover
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
FR1250490A
Other languages
English (en)
Other versions
FR2970555A1 (fr
Inventor
Donald Mark Bailey
Donald Timothy Lemon
Kwanwoo Kim
Patrick Benedict MELTON
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
Publication of FR2970555A1 publication Critical patent/FR2970555A1/fr
Application granted granted Critical
Publication of FR2970555B1 publication Critical patent/FR2970555B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00—Feeding or distributing other fuel to combustion apparatus
    • F23K5/02—Liquid fuel
    • F23K5/14—Details thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K2900/00—Special features of, or arrangements for fuel supplies
    • F23K2900/05142—Special materials for liquid fuel supply lines
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices

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)
  • Feeding And Controlling Fuel (AREA)
  • Gas Burners (AREA)
FR1250490A 2011-01-18 2012-01-18 Capot d'extremite pour dispositif de combustion de turbine a gaz Expired - Fee Related FR2970555B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/008,399 US8820086B2 (en) 2011-01-18 2011-01-18 Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal
US13/008.399 2011-01-18

Publications (2)

Publication Number Publication Date
FR2970555A1 FR2970555A1 (fr) 2012-07-20
FR2970555B1 true FR2970555B1 (fr) 2018-04-20

Family

ID=46397782

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1250490A Expired - Fee Related FR2970555B1 (fr) 2011-01-18 2012-01-18 Capot d'extremite pour dispositif de combustion de turbine a gaz

Country Status (5)

Country Link
US (1) US8820086B2 (fr)
JP (1) JP2012149878A (fr)
CN (1) CN102607065B (fr)
DE (1) DE102012100371A1 (fr)
FR (1) FR2970555B1 (fr)

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* Cited by examiner, † Cited by third party
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WO2012112889A2 (fr) 2011-02-18 2012-08-23 Ethier Jason Dispositifs d'écoulement de fluide ayant une géométrie verticalement simple et procédés de fabrication de ces derniers
US9062629B2 (en) * 2011-11-15 2015-06-23 Walbro Engine Management, L. L.C. Carburetor fuel supply system
US9062630B2 (en) 2011-11-15 2015-06-23 Walbro Engine Management, L.L.C. Carburetor fuel supply system
US9347668B2 (en) * 2013-03-12 2016-05-24 General Electric Company End cover configuration and assembly
US9534787B2 (en) 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
US9671112B2 (en) 2013-03-12 2017-06-06 General Electric Company Air diffuser for a head end of a combustor
US9759425B2 (en) 2013-03-12 2017-09-12 General Electric Company System and method having multi-tube fuel nozzle with multiple fuel injectors
US9651259B2 (en) 2013-03-12 2017-05-16 General Electric Company Multi-injector micromixing system
US9366439B2 (en) 2013-03-12 2016-06-14 General Electric Company Combustor end cover with fuel plenums
US9765973B2 (en) 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
US9528444B2 (en) 2013-03-12 2016-12-27 General Electric Company System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US9650959B2 (en) * 2013-03-12 2017-05-16 General Electric Company Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
US9625157B2 (en) 2014-02-12 2017-04-18 General Electric Company Combustor cap assembly
US9845956B2 (en) * 2014-04-09 2017-12-19 General Electric Company System and method for control of combustion dynamics in combustion system
US10030580B2 (en) 2014-04-11 2018-07-24 Dynamo Micropower Corporation Micro gas turbine systems and uses thereof
US9546600B2 (en) * 2014-08-12 2017-01-17 General Electric Company Nozzle having an orifice plug for a gas turbomachine
US10100730B2 (en) * 2015-03-11 2018-10-16 Pratt & Whitney Canada Corp. Secondary air system with venturi
CN104776447B (zh) * 2015-03-27 2017-08-25 北京华清燃气轮机与煤气化联合循环工程技术有限公司 一种用于燃气轮机燃烧室的组合式端盖
US10087845B2 (en) 2015-11-30 2018-10-02 General Electric Company Pressure damping device for fuel manifold
US9879536B2 (en) 2015-12-21 2018-01-30 General Electric Company Surface treatment of turbomachinery
US20180363905A1 (en) * 2016-01-13 2018-12-20 General Electric Company Fuel nozzle assembly for reducing multiple tone combustion dynamics
US10788215B2 (en) * 2016-12-21 2020-09-29 General Electric Company Fuel nozzle assembly with flange orifice
JP7096182B2 (ja) * 2019-02-27 2022-07-05 三菱重工業株式会社 ガスタービン燃焼器及びガスタービン
CN112066414B (zh) * 2019-06-10 2022-04-12 中国航发商用航空发动机有限责任公司 燃烧室、燃气轮机以及抑制振荡燃烧的方法
US11466859B2 (en) * 2020-12-18 2022-10-11 Pratt & Whitney Canada Corp. Gap filler for a fuel system gallery
FR3121956A1 (fr) * 2021-04-15 2022-10-21 Safran Helicopter Engines Canalisation de turbomachine a moyen de restriction de debit amovible
US11525403B2 (en) * 2021-05-05 2022-12-13 Pratt & Whitney Canada Corp. Fuel nozzle with integrated metering and flashback system

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US5259184A (en) * 1992-03-30 1993-11-09 General Electric Company Dry low NOx single stage dual mode combustor construction for a gas turbine
JP2759722B2 (ja) * 1992-05-20 1998-05-28 川崎重工業株式会社 ガスタ−ビンの燃焼制御装置
US5269468A (en) * 1992-06-22 1993-12-14 General Electric Company Fuel nozzle
JP3082823B2 (ja) * 1994-02-23 2000-08-28 三菱重工業株式会社 耐熱、耐食処理を施したガスタービン用燃焼器ノズル
US5415000A (en) * 1994-06-13 1995-05-16 Westinghouse Electric Corporation Low NOx combustor retro-fit system for gas turbines
US6010592A (en) * 1994-06-23 2000-01-04 Kimberly-Clark Corporation Method and apparatus for increasing the flow rate of a liquid through an orifice
JPH1082527A (ja) * 1996-09-05 1998-03-31 Toshiba Corp ガスタービン燃焼器
US6763663B2 (en) * 2001-07-11 2004-07-20 Parker-Hannifin Corporation Injector with active cooling
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US6883329B1 (en) * 2003-01-24 2005-04-26 Power Systems Mfg, Llc Method of fuel nozzle sizing and sequencing for a gas turbine combustor
US7134287B2 (en) 2003-07-10 2006-11-14 General Electric Company Turbine combustor endcover assembly
US7003958B2 (en) * 2004-06-30 2006-02-28 General Electric Company Multi-sided diffuser for a venturi in a fuel injector for a gas turbine
US7287382B2 (en) * 2004-07-19 2007-10-30 John Henriquez Gas turbine combustor end cover
US20070075158A1 (en) * 2005-09-22 2007-04-05 Pelletier Robert R Nozzle assembly
US8122721B2 (en) * 2006-01-04 2012-02-28 General Electric Company Combustion turbine engine and methods of assembly
US7757491B2 (en) * 2008-05-09 2010-07-20 General Electric Company Fuel nozzle for a gas turbine engine and method for fabricating the same
US20090320483A1 (en) * 2008-06-26 2009-12-31 General Electric Company Variable Orifice Plug for Turbine Fuel Nozzle
US20100050640A1 (en) * 2008-08-29 2010-03-04 General Electric Company Thermally compliant combustion cap device and system
FR2939171B1 (fr) * 2008-11-28 2010-12-31 Snecma Turbomachine a systemes d'injection de carburant distincts, utilisant des joints d'etancheite identiques.
US8220272B2 (en) * 2008-12-04 2012-07-17 General Electric Company Combustor housing for combustion of low-BTU fuel gases and methods of making and using the same
US8225610B2 (en) * 2008-12-08 2012-07-24 General Electric Company Fuel delivery system and method of assembling the same
US9140454B2 (en) * 2009-01-23 2015-09-22 General Electric Company Bundled multi-tube nozzle for a turbomachine
US20100192587A1 (en) * 2009-02-03 2010-08-05 William Kirk Hessler Combustor assembly for use in a gas turbine engine and method of assembling same

Also Published As

Publication number Publication date
US8820086B2 (en) 2014-09-02
FR2970555A1 (fr) 2012-07-20
CN102607065B (zh) 2015-08-05
DE102012100371A1 (de) 2012-07-19
JP2012149878A (ja) 2012-08-09
US20120180488A1 (en) 2012-07-19
CN102607065A (zh) 2012-07-25

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