FR2932251B1 - Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc - Google Patents

Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc

Info

Publication number
FR2932251B1
FR2932251B1 FR0803226A FR0803226A FR2932251B1 FR 2932251 B1 FR2932251 B1 FR 2932251B1 FR 0803226 A FR0803226 A FR 0803226A FR 0803226 A FR0803226 A FR 0803226A FR 2932251 B1 FR2932251 B1 FR 2932251B1
Authority
FR
France
Prior art keywords
deflectors
cmc
combustion chamber
gas turbine
turbine engine
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.)
Active
Application number
FR0803226A
Other languages
English (en)
Other versions
FR2932251A1 (fr
Inventor
Sylvain Duval
Didier Hippolyte Hernandez
Romain Nicolas Lunel
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 to FR0803226A priority Critical patent/FR2932251B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to RU2010154030/06A priority patent/RU2507452C2/ru
Priority to JP2011512971A priority patent/JP5475757B2/ja
Priority to US12/997,266 priority patent/US8756935B2/en
Priority to BRPI0914905A priority patent/BRPI0914905B1/pt
Priority to CN2009801216000A priority patent/CN102057224B/zh
Priority to CA2727254A priority patent/CA2727254C/fr
Priority to EP09772283.9A priority patent/EP2307805B1/fr
Priority to PCT/EP2009/057147 priority patent/WO2010000583A2/fr
Publication of FR2932251A1 publication Critical patent/FR2932251A1/fr
Application granted granted Critical
Publication of FR2932251B1 publication Critical patent/FR2932251B1/fr
Active 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

Landscapes

  • 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)
FR0803226A 2008-06-10 2008-06-10 Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc Active FR2932251B1 (fr)

Priority Applications (9)

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
JP2011512971A JP5475757B2 (ja) 2008-06-10 2009-06-10 Ｃｍｃデフレクタを備えるガスタービンエンジンの燃焼チャンバ
US12/997,266 US8756935B2 (en) 2008-06-10 2009-06-10 Gas turbine engine combustion chamber comprising CMC deflectors
BRPI0914905A BRPI0914905B1 (pt) 2008-06-10 2009-06-10 câmara de combustão de motor de turbina a gás compreendendo pelo menos um defletor
RU2010154030/06A RU2507452C2 (ru) 2008-06-10 2009-06-10 Камера сгорания газотурбинного двигателя, содержащая дефлекторы, изготовленные из композитного материала с керамической матрицей (смс)
CN2009801216000A CN102057224B (zh) 2008-06-10 2009-06-10 包括cmc偏转部的气体涡轮机燃烧室
CA2727254A CA2727254C (fr) 2008-06-10 2009-06-10 Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc
EP09772283.9A EP2307805B1 (fr) 2008-06-10 2009-06-10 Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc
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

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
FR2932251A1 FR2932251A1 (fr) 2009-12-11
FR2932251B1 true FR2932251B1 (fr) 2011-09-16

Family

ID=40289257

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0803226A Active FR2932251B1 (fr) 2008-06-10 2008-06-10 Chambre de combustion de moteur a turbine a gaz comportant des deflecteurs en cmc

Country Status (9)

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

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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
US9976746B2 (en) 2015-09-02 2018-05-22 General Electric Company Combustor assembly for a turbine engine
US10168051B2 (en) 2015-09-02 2019-01-01 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

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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
DE19515537A1 (de) * 1995-04-27 1996-10-31 Bmw Rolls Royce Gmbh Kopfteil einer Gasturbinen-Ringbrennkammer
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
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
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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
US7673460B2 (en) * 2005-06-07 2010-03-09 Snecma System of attaching an injection system to a turbojet combustion chamber base
FR2886714B1 (fr) * 2005-06-07 2007-09-07 Snecma Moteurs Sa Systeme d'injection anti-rotatif pour turbo-reacteur
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
FR2897107B1 (fr) * 2006-02-09 2013-01-18 Snecma Paroi transversale de chambre de combustion munie de trous de multiperforation
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
FR2903171B1 (fr) * 2006-06-29 2008-10-17 Snecma Sa Agencement a liaison par crabot pour chambre de combustion de 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
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

Also Published As

Publication number Publication date
RU2507452C2 (ru) 2014-02-20
US20110113789A1 (en) 2011-05-19
EP2307805A2 (fr) 2011-04-13
CA2727254C (fr) 2016-08-23
WO2010000583A2 (fr) 2010-01-07
BRPI0914905B1 (pt) 2020-05-05
CN102057224B (zh) 2013-04-24
US8756935B2 (en) 2014-06-24
JP5475757B2 (ja) 2014-04-16
RU2010154030A (ru) 2012-07-20
EP2307805B1 (fr) 2017-03-15
FR2932251A1 (fr) 2009-12-11
CN102057224A (zh) 2011-05-11
CA2727254A1 (fr) 2010-01-07
BRPI0914905A2 (pt) 2015-10-20
WO2010000583A3 (fr) 2010-07-29
JP2011523020A (ja) 2011-08-04

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