BRPI0914905A2 - câmara de combustão de motor de turbina a gás compreendendo pelo menos um defletor. - Google Patents

câmara de combustão de motor de turbina a gás compreendendo pelo menos um defletor.

Info

Publication number: BRPI0914905A2
Authority: BR; Brazil
Prior art keywords: deflector; combustion chamber; gas turbine; turbine engine; engine combustion
Prior art date: 2008-06-10

Application number

BRPI0914905A

Other languages

English (en)

Inventor

Didier Hyppolyte Hernandez

Romain Nicolas Lunel

Sylvain Duval

Original Assignee

Snecma

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.)

2008-06-10

Filing date

2009-06-10

Publication date

2015-10-20

2009-06-10 Application filed by Snecma filed Critical Snecma

2015-10-20 Publication of BRPI0914905A2 publication Critical patent/BRPI0914905A2/pt

2020-05-05 Publication of BRPI0914905B1 publication Critical patent/BRPI0914905B1/pt

Links

238000002485 combustion reaction Methods 0.000 title 1

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)

BRPI0914905A 2008-06-10 2009-06-10 câmara de combustão de motor de turbina a gás compreendendo pelo menos um defletor BRPI0914905B1 (pt)

Applications Claiming Priority (2)

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
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
BRPI0914905A2 true BRPI0914905A2 (pt)	2015-10-20
BRPI0914905B1 BRPI0914905B1 (pt)	2020-05-05

Family

ID=40289257

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI0914905A BRPI0914905B1 (pt)	2008-06-10	2009-06-10	câmara de combustão de motor de turbina a gás compreendendo pelo menos um defletor

Country Status (9)

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

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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
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
US10378769B2 (en)	2016-09-30	2019-08-13	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
US10378772B2 (en)	2017-01-19	2019-08-13	General Electric Company	Combustor heat shield sealing
US10816199B2 (en)	2017-01-27	2020-10-27	General Electric Company	Combustor heat shield and attachment features
US11111858B2 (en)	2017-01-27	2021-09-07	General Electric Company	Cool core gas turbine engine
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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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
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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
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
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
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

2008
- 2008-06-10 FR FR0803226A patent/FR2932251B1/fr active Active
2009
- 2009-06-10 CA CA2727254A patent/CA2727254C/fr active Active
- 2009-06-10 WO PCT/EP2009/057147 patent/WO2010000583A2/fr not_active Ceased
- 2009-06-10 US US12/997,266 patent/US8756935B2/en active Active
- 2009-06-10 BR BRPI0914905A patent/BRPI0914905B1/pt active IP Right Grant
- 2009-06-10 RU RU2010154030/06A patent/RU2507452C2/ru active
- 2009-06-10 CN CN2009801216000A patent/CN102057224B/zh active Active
- 2009-06-10 EP EP09772283.9A patent/EP2307805B1/fr active Active
- 2009-06-10 JP JP2011512971A patent/JP5475757B2/ja active Active

Also Published As

Publication number	Publication date
RU2507452C2 (ru)	2014-02-20
FR2932251B1 (fr)	2011-09-16
CA2727254C (fr)	2016-08-23
BRPI0914905B1 (pt)	2020-05-05
JP5475757B2 (ja)	2014-04-16
EP2307805B1 (fr)	2017-03-15
CN102057224A (zh)	2011-05-11
WO2010000583A2 (fr)	2010-01-07
RU2010154030A (ru)	2012-07-20
US8756935B2 (en)	2014-06-24
CN102057224B (zh)	2013-04-24
CA2727254A1 (fr)	2010-01-07
EP2307805A2 (fr)	2011-04-13
JP2011523020A (ja)	2011-08-04
US20110113789A1 (en)	2011-05-19
FR2932251A1 (fr)	2009-12-11
WO2010000583A3 (fr)	2010-07-29

Legal Events

Date	Code	Title	Description
2019-01-22	B06F	Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
2019-07-16	B06T	Formal requirements before examination [chapter 6.20 patent gazette]
2020-03-10	B09A	Decision: intention to grant [chapter 9.1 patent gazette]
2020-05-05	B16A	Patent or certificate of addition of invention granted	Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 05/05/2020, OBSERVADAS AS CONDICOES LEGAIS.

Publication	Publication Date	Title
BRPI0914905A2 (pt)	2015-10-20	câmara de combustão de motor de turbina a gás compreendendo pelo menos um defletor.
GB0610800D0 (en)	2006-07-12	Combustion chamber for a gas turbine engine
GB2456147B (en)	2010-07-14	Fuel Injector Assembly for Gas Turbine Engines
GB2431435B (en)	2010-09-22	Gas turbine engine assembly
GB2436128B (en)	2008-08-13	Gas turbine engine
FR2897145B1 (fr)	2013-01-18	Chambre de combustion annulaire de turbomachine a fixations alternees.
BRPI0921971A2 (pt)	2016-01-05	filtro de admissão de ar para motores de combustão.
PL1902953T3 (pl)	2018-12-31	Silnik śmigłowca z turbiną gazową
BRPI1014115A2 (pt)	2016-04-12	ignitor, motor de combustão interna, e, método para formar um ignitor.
WO2014099074A3 (en)	2014-08-21	Gas turbine engine combustor with integrated combustor vane
FR2935777B1 (fr)	2013-03-08	Chambre de combustion de turbomachine
EP1924762A4 (en)	2009-10-28	COMBUSTION SYSTEMS FOR GAS TURBINE
GB2443194B (en)	2008-09-10	Gas turbine engine
GB2462245B (en)	2010-09-22	Gas turbine engine arrangement
FR2897144B1 (fr)	2008-05-02	Chambre de combustion de turbomachine a fentes tangentielles
BRPI0918437A2 (pt)	2015-11-24	êmbolo para um motor de combustão interna.
BRPI0917880A2 (pt)	2015-11-24	estrutura de entrada de ar para nacela de motor turbojato tencionada, nacela para um motor turbojato.
DE602004028297D1 (de)	2010-09-02	Umfangsbrennkammer für spitzenturbinenmotor
FR2881813B1 (fr)	2011-04-08	Carenage de chambre de combustion de turbomachine
BR112012002447A2 (pt)	2016-03-01	câmara de combustão de turbomáquina ,e, turbomáquina.
BRPI0918059A2 (pt)	2015-12-01	pistão para um motor de combustão interna.
WO2014099076A3 (en)	2014-09-12	Gas turbine engine combustor with integrated combustor vane
FR2923861B1 (fr)	2014-04-25	Circuit de carburant de turbomachine.
GB2441342B (en)	2009-03-18	Wall elements with apertures for gas turbine engine components
FR2885201B1 (fr)	2010-09-17	Chambre de combustion aisement demontable a performance aerodynamique amelioree