CN102057224B - 包括cmc偏转部的气体涡轮机燃烧室 - Google Patents

包括cmc偏转部的气体涡轮机燃烧室 Download PDF

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Publication number
CN102057224B
CN102057224B CN2009801216000A CN200980121600A CN102057224B CN 102057224 B CN102057224 B CN 102057224B CN 2009801216000 A CN2009801216000 A CN 2009801216000A CN 200980121600 A CN200980121600 A CN 200980121600A CN 102057224 B CN102057224 B CN 102057224B
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CN
China
Prior art keywords
deflector
sleeve
combustion chamber
cup
end wall
Prior art date
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CN2009801216000A
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English (en)
Chinese (zh)
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CN102057224A (zh
Inventor
西拉维·杜瓦尔
迪迪尔·希波吕忒·埃尔南德斯
罗曼·尼古拉斯·吕内尔
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Safran Aircraft Engines SAS
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SNECMA SAS
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Publication date
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Publication of CN102057224A publication Critical patent/CN102057224A/zh
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Publication of CN102057224B publication Critical patent/CN102057224B/zh
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    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
CN2009801216000A 2008-06-10 2009-06-10 包括cmc偏转部的气体涡轮机燃烧室 Active CN102057224B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0803226A FR2932251B1 (fr) 2008-06-10 2008-06-10 Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc
FR08/03226 2008-06-10
PCT/EP2009/057147 WO2010000583A2 (fr) 2008-06-10 2009-06-10 Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc

Publications (2)

Publication Number Publication Date
CN102057224A CN102057224A (zh) 2011-05-11
CN102057224B true CN102057224B (zh) 2013-04-24

Family

ID=40289257

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009801216000A Active CN102057224B (zh) 2008-06-10 2009-06-10 包括cmc偏转部的气体涡轮机燃烧室

Country Status (9)

Country Link
US (1) US8756935B2 (enExample)
EP (1) EP2307805B1 (enExample)
JP (1) JP5475757B2 (enExample)
CN (1) CN102057224B (enExample)
BR (1) BRPI0914905B1 (enExample)
CA (1) CA2727254C (enExample)
FR (1) FR2932251B1 (enExample)
RU (1) RU2507452C2 (enExample)
WO (1) WO2010000583A2 (enExample)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8943835B2 (en) * 2010-05-10 2015-02-03 General Electric Company Gas turbine engine combustor with CMC heat shield and methods therefor
FR2964177B1 (fr) 2010-08-27 2012-08-24 Snecma Chambre de combustion de moteur d?aeronef et procede de fixation d?un systeme d?injection dans une chambre de combustion de moteur d?aeronef
DE102013007443A1 (de) * 2013-04-30 2014-10-30 Rolls-Royce Deutschland Ltd & Co Kg Brennerdichtung für Gasturbinen-Brennkammerkopf und Hitzeschild
FR3026827B1 (fr) * 2014-10-01 2019-06-07 Safran Aircraft Engines Chambre de combustion de turbomachine
US10041676B2 (en) * 2015-07-08 2018-08-07 General Electric Company Sealed conical-flat dome for flight engine combustors
US20170059159A1 (en) 2015-08-25 2017-03-02 Rolls-Royce Corporation Cmc combustor shell with integral chutes
US10168051B2 (en) 2015-09-02 2019-01-01 General Electric Company Combustor assembly for a turbine engine
US9976746B2 (en) 2015-09-02 2018-05-22 General Electric Company Combustor assembly for a turbine engine
US11149646B2 (en) 2015-09-02 2021-10-19 General Electric Company Piston ring assembly for a turbine engine
GB2543803B (en) * 2015-10-29 2019-10-30 Rolls Royce Plc A combustion chamber assembly
US10317085B2 (en) * 2016-02-25 2019-06-11 General Electric Company Combustor assembly
US10371382B2 (en) * 2016-09-30 2019-08-06 General Electric Company Combustor heat shield and attachment features
US10495310B2 (en) 2016-09-30 2019-12-03 General Electric Company Combustor heat shield and attachment features
US10378769B2 (en) 2016-09-30 2019-08-13 General Electric Company Combustor heat shield and attachment features
US10378772B2 (en) 2017-01-19 2019-08-13 General Electric Company Combustor heat shield sealing
US11111858B2 (en) 2017-01-27 2021-09-07 General Electric Company Cool core gas turbine engine
US10816199B2 (en) 2017-01-27 2020-10-27 General Electric Company Combustor heat shield and attachment features
US10690347B2 (en) 2017-02-01 2020-06-23 General Electric Company CMC combustor deflector
US10837640B2 (en) 2017-03-06 2020-11-17 General Electric Company Combustion section of a gas turbine engine
US11402097B2 (en) 2018-01-03 2022-08-02 General Electric Company Combustor assembly for a turbine engine
FR3084731B1 (fr) 2019-02-19 2020-07-03 Safran Aircraft Engines Chambre de combustion pour une turbomachine
US11649964B2 (en) * 2020-12-01 2023-05-16 Raytheon Technologies Corporation Fuel injector assembly for a turbine engine
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Citations (4)

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Publication number Priority date Publication date Assignee Title
US5970716A (en) * 1997-10-02 1999-10-26 General Electric Company Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits
US5996335A (en) * 1995-04-27 1999-12-07 Bmw Rolls-Royce Gmbh Head part of an annular combustion chamber of a gas turbine having a holding part to secure a burner collar in a bayonet-catch type manner
US6212870B1 (en) * 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly
CN101016999A (zh) * 2006-02-09 2007-08-15 斯奈克玛 具有多孔洞的燃烧室横向壁

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US4180974A (en) * 1977-10-31 1980-01-01 General Electric Company Combustor dome sleeve
SU1002736A2 (ru) * 1981-09-29 1983-03-07 Центральный Научно-Исследовательский И Конструкторский Институт Топливной Аппаратуры Автотракторных И Стационарных Двигателей Камера сгорани
US5117637A (en) * 1990-08-02 1992-06-02 General Electric Company Combustor dome assembly
JPH08312961A (ja) * 1995-05-16 1996-11-26 Nissan Motor Co Ltd ガスタービンの燃焼器
FR2753779B1 (fr) * 1996-09-26 1998-10-16 Systeme d'injection aerodynamique d'un melange air carburant
JPH1166893A (ja) * 1997-08-22 1999-03-09 Mitsubishi Electric Corp 半導体記憶装置
US6397603B1 (en) * 2000-05-05 2002-06-04 The United States Of America As Represented By The Secretary Of The Air Force Conbustor having a ceramic matrix composite liner
US6442940B1 (en) * 2001-04-27 2002-09-03 General Electric Company Gas-turbine air-swirler attached to dome and combustor in single brazing operation
US6546732B1 (en) * 2001-04-27 2003-04-15 General Electric Company Methods and apparatus for cooling gas turbine engine combustors
US6581386B2 (en) * 2001-09-29 2003-06-24 General Electric Company Threaded combustor baffle
FR2832493B1 (fr) * 2001-11-21 2004-07-09 Snecma Moteurs Systeme d'injection multi-etages d'un melange air/carburant dans une chambre de combustion de turbomachine
FR2859272B1 (fr) * 2003-09-02 2005-10-14 Snecma Moteurs Systeme d'injection air/carburant, dans une chambre de combustion de turbomachine, ayant des moyens de generation de plasmas froids
RU2280814C1 (ru) * 2004-12-27 2006-07-27 Акционерное общество открытого типа Авиамоторный научно-технический комплекс "Союз" Кольцевая камера сгорания газотурбинного двигателя
FR2886714B1 (fr) * 2005-06-07 2007-09-07 Snecma Moteurs Sa Systeme d'injection anti-rotatif pour turbo-reacteur
US7673460B2 (en) * 2005-06-07 2010-03-09 Snecma System of attaching an injection system to a turbojet combustion chamber base
FR2893390B1 (fr) * 2005-11-15 2011-04-01 Snecma Fond de chambre de combustion avec ventilation
FR2894327B1 (fr) * 2005-12-05 2008-05-16 Snecma Sa Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
FR2897922B1 (fr) * 2006-02-27 2008-10-10 Snecma Sa Agencement pour une chambre de combustion de turboreacteur
FR2901349B1 (fr) * 2006-05-19 2008-09-05 Snecma Sa Chambre de combustion d'une turbomachine
FR2903170B1 (fr) * 2006-06-29 2011-12-23 Snecma Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
FR2903171B1 (fr) * 2006-06-29 2008-10-17 Snecma Sa Agencement a liaison par crabot pour chambre de combustion de turbomachine
US8863528B2 (en) * 2006-07-27 2014-10-21 United Technologies Corporation Ceramic combustor can for a gas turbine engine
FR2908867B1 (fr) * 2006-11-16 2012-06-15 Snecma Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
FR2941288B1 (fr) * 2009-01-16 2011-02-18 Snecma Dispositif d'injection d'un melange d'air et de carburant dans une chambre de combustion de turbomachine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5996335A (en) * 1995-04-27 1999-12-07 Bmw Rolls-Royce Gmbh Head part of an annular combustion chamber of a gas turbine having a holding part to secure a burner collar in a bayonet-catch type manner
US5970716A (en) * 1997-10-02 1999-10-26 General Electric Company Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits
US6212870B1 (en) * 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly
CN101016999A (zh) * 2006-02-09 2007-08-15 斯奈克玛 具有多孔洞的燃烧室横向壁

Also Published As

Publication number Publication date
EP2307805A2 (fr) 2011-04-13
JP2011523020A (ja) 2011-08-04
RU2010154030A (ru) 2012-07-20
BRPI0914905B1 (pt) 2020-05-05
US20110113789A1 (en) 2011-05-19
CA2727254C (fr) 2016-08-23
CA2727254A1 (fr) 2010-01-07
CN102057224A (zh) 2011-05-11
EP2307805B1 (fr) 2017-03-15
BRPI0914905A2 (pt) 2015-10-20
JP5475757B2 (ja) 2014-04-16
RU2507452C2 (ru) 2014-02-20
US8756935B2 (en) 2014-06-24
WO2010000583A3 (fr) 2010-07-29
FR2932251B1 (fr) 2011-09-16
WO2010000583A2 (fr) 2010-01-07
FR2932251A1 (fr) 2009-12-11

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