FR2897144B1 - Chambre de combustion de turbomachine a fentes tangentielles - Google Patents

Chambre de combustion de turbomachine a fentes tangentielles

Info

Publication number: FR2897144B1
Authority: FR; France
Prior art keywords: turbomachine; combustion chamber; tangential slots; tangential; slots
Prior art date: 2006-02-08
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

FR0650447A

Other languages

English (en)

Other versions

FR2897144A1 (fr

Inventor

Florian Bessagnet

Sousa Mario De

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.)

2006-02-08

Filing date

2006-02-08

Publication date

2008-05-02

2006-02-08 Application filed by SNECMA SAS filed Critical SNECMA SAS

2006-02-08 Priority to FR0650447A priority Critical patent/FR2897144B1/fr

2007-02-02 Priority to US11/670,510 priority patent/US7673457B2/en

2007-02-02 Priority to EP07101654A priority patent/EP1818616B1/fr

2007-02-07 Priority to RU2007104723/06A priority patent/RU2422730C2/ru

2007-02-08 Priority to CNA2007100075703A priority patent/CN101017000A/zh

2007-02-08 Priority to CA2577527A priority patent/CA2577527C/fr

2007-08-10 Publication of FR2897144A1 publication Critical patent/FR2897144A1/fr

2008-05-02 Application granted granted Critical

2008-05-02 Publication of FR2897144B1 publication Critical patent/FR2897144B1/fr

Status Expired - Fee Related legal-status Critical Current

2026-02-08 Anticipated expiration legal-status Critical

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
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2211/00—Thermal dilatation prevention or compensation
- 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

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)
Turbine Rotor Nozzle Sealing (AREA)
Portable Nailing Machines And Staplers (AREA)
Details Of Aerials (AREA)

FR0650447A 2006-02-08 2006-02-08 Chambre de combustion de turbomachine a fentes tangentielles Expired - Fee Related FR2897144B1 (fr)

Priority Applications (6)

Application Number	Priority Date	Filing Date	Title
FR0650447A FR2897144B1 (fr)	2006-02-08	2006-02-08	Chambre de combustion de turbomachine a fentes tangentielles
US11/670,510 US7673457B2 (en)	2006-02-08	2007-02-02	Turbine engine combustion chamber with tangential slots
EP07101654A EP1818616B1 (fr)	2006-02-08	2007-02-02	Chambre de combustion de turbomachine à fentes tangentielles
RU2007104723/06A RU2422730C2 (ru)	2006-02-08	2007-02-07	Кольцевая камера сгорания газотурбинного двигателя с тангенциальными щелями и газотурбинный двигатель, содержащий такую камеру сгорания
CNA2007100075703A CN101017000A (zh)	2006-02-08	2007-02-08	带有切向槽的涡轮发动机燃烧室
CA2577527A CA2577527C (fr)	2006-02-08	2007-02-08	Chambre de combustion de turbomachine a fentes tangentielles

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
FR0650447A FR2897144B1 (fr)	2006-02-08	2006-02-08	Chambre de combustion de turbomachine a fentes tangentielles

Publications (2)

Publication Number	Publication Date
FR2897144A1 FR2897144A1 (fr)	2007-08-10
FR2897144B1 true FR2897144B1 (fr)	2008-05-02

Family

ID=37102162

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR0650447A Expired - Fee Related FR2897144B1 (fr)	2006-02-08	2006-02-08	Chambre de combustion de turbomachine a fentes tangentielles

Country Status (6)

Country	Link
US (1)	US7673457B2 (fr)
EP (1)	EP1818616B1 (fr)
CN (1)	CN101017000A (fr)
CA (1)	CA2577527C (fr)
FR (1)	FR2897144B1 (fr)
RU (1)	RU2422730C2 (fr)

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FR2911668B1 (fr) *	2007-01-18	2009-03-20	Snecma Sa	Chambre de combustion d'une turbomachine
FR2914399B1 (fr) *	2007-03-27	2009-10-02	Snecma Sa	Carenage pour fond de chambre de combustion.
FR2918443B1 (fr) *	2007-07-04	2009-10-30	Snecma Sa	Chambre de combustion comportant des deflecteurs de protection thermique de fond de chambre et moteur a turbine a gaz en etant equipe
US20090090110A1 (en) *	2007-10-04	2009-04-09	Honeywell International, Inc.	Faceted dome assemblies for gas turbine engine combustors
FR2929689B1 (fr) *	2008-04-03	2013-04-12	Snecma Propulsion Solide	Chambre de combustion de turbine a gaz a parois interne et externe sectorisees
US20100186234A1 (en) *	2009-01-28	2010-07-29	Yehuda Binder	Electric shaver with imaging capability
US8511089B2 (en) *	2009-07-31	2013-08-20	Rolls-Royce Corporation	Relief slot for combustion liner
FR2964725B1 (fr) *	2010-09-14	2012-10-12	Snecma	Carenage aerodynamique pour fond de chambre de combustion
EP2781838B1 (fr) *	2011-11-16	2019-04-24	Mitsubishi Hitachi Power Systems, Ltd.	Chambre de combustion de turbine à gaz
US9133722B2 (en) *	2012-04-30	2015-09-15	General Electric Company	Transition duct with late injection in turbine system
US20160024959A1 (en) *	2013-03-13	2016-01-28	United Technologies Corporation	Variable vane drive system
FR3015639B1 (fr) *	2013-12-20	2018-08-31	Safran Aircraft Engines	Chambre de combustion dans une turbomachine
FR3017693B1 (fr) *	2014-02-19	2019-07-26	Safran Helicopter Engines	Chambre de combustion de turbomachine
DE102015212573A1 (de) *	2015-07-06	2017-01-12	Rolls-Royce Deutschland Ltd & Co Kg	Gasturbinenbrennkammer mit integriertem Turbinenvorleitrad sowie Verfahren zu deren Herstellung
DE102015213629A1 (de) *	2015-07-20	2017-01-26	Rolls-Royce Deutschland Ltd & Co Kg	Abdeckteil und Brennkammerbaugruppe für eine Gasturbine
DE102015224990A1 (de) *	2015-12-11	2017-06-14	Rolls-Royce Deutschland Ltd & Co Kg	Verfahren zur Montage einer Brennkammer eines Gasturbinentriebwerks
JP6763519B2 (ja) *	2016-03-31	2020-09-30	三菱パワー株式会社	燃焼器およびガスタービン
GB201613110D0 (en)	2016-07-29	2016-09-14	Rolls Royce Plc	A combustion chamber
US11015812B2 (en) *	2018-05-07	2021-05-25	Rolls-Royce North American Technologies Inc.	Combustor bolted segmented architecture
CN111561713B (zh) *	2020-04-16	2021-08-06	中国航发湖南动力机械研究所	直流燃烧室火焰筒
WO2021219445A1 (fr)	2020-04-30	2021-11-04	Tk Airport Solutions, S.A.	Procédé d'accostage automatisé d'une passerelle d'embarquement de passagers à un aéronef
CN115183277B (zh) *	2022-06-02	2024-05-17	中国航发四川燃气涡轮研究院	一种火焰筒

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GB648493A (en) *	1947-08-06	1951-01-03	Westinghouse Electric Int Co	Improvements in or relating to combustion apparatus for gas turbines
US3854285A (en) *	1973-02-26	1974-12-17	Gen Electric	Combustor dome assembly
US4433214A (en) *	1981-12-24	1984-02-21	Motorola, Inc.	Acoustical transducer with a slotted piston suspension
US5181377A (en) *	1991-04-16	1993-01-26	General Electric Company	Damped combustor cowl structure
FR2686683B1 (fr) *	1992-01-28	1994-04-01	Snecma	Turbomachine a chambre de combustion demontable.
CA2089272C (fr) *	1992-03-23	2002-09-03	James Norman Reinhold, Jr.	Chambre de combustion presentant une resistance aux chocs
CA2089302C (fr) *	1992-03-30	2004-07-06	Joseph Frank Savelli	Chambre de combustion annulaire double
DE4223733C2 (de) *	1992-07-18	1995-05-18	Gutehoffnungshuette Man	Verbindung von Mischrohr und Flammrohr einer Gasturbine
US5542246A (en) *	1994-12-15	1996-08-06	United Technologies Corporation	Bulkhead cooling fairing
EP0924458B1 (fr) *	1997-12-22	2002-08-28	Alstom	Brûleur
US6148600A (en) *	1999-02-26	2000-11-21	General Electric Company	One-piece sheet metal cowl for combustor of a gas turbine engine and method of configuring same
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
US6449952B1 (en) *	2001-04-17	2002-09-17	General Electric Company	Removable cowl for gas turbine combustor
US6655146B2 (en) *	2001-07-31	2003-12-02	General Electric Company	Hybrid film cooled combustor liner
US6513331B1 (en) *	2001-08-21	2003-02-04	General Electric Company	Preferential multihole combustor liner
US6672067B2 (en) *	2002-02-27	2004-01-06	General Electric Company	Corrugated cowl for combustor of a gas turbine engine and method for configuring same
US7222488B2 (en) *	2002-09-10	2007-05-29	General Electric Company	Fabricated cowl for double annular combustor of a gas turbine engine
US6895761B2 (en) *	2002-12-20	2005-05-24	General Electric Company	Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor
US6904757B2 (en) *	2002-12-20	2005-06-14	General Electric Company	Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor
US6779268B1 (en) *	2003-05-13	2004-08-24	General Electric Company	Outer and inner cowl-wire wrap to one piece cowl conversion
FR2855249B1 (fr) *	2003-05-20	2005-07-08	Snecma Moteurs	Chambre de combustion ayant une liaison souple entre un fond de chambre et une paroi de chambre
US7062920B2 (en) *	2003-08-11	2006-06-20	General Electric Company	Combustor dome assembly of a gas turbine engine having a free floating swirler
US7121095B2 (en) *	2003-08-11	2006-10-17	General Electric Company	Combustor dome assembly of a gas turbine engine having improved deflector plates
US7093441B2 (en) *	2003-10-09	2006-08-22	United Technologies Corporation	Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
US7765809B2 (en) *	2006-11-10	2010-08-03	General Electric Company	Combustor dome and methods of assembling such

2006
- 2006-02-08 FR FR0650447A patent/FR2897144B1/fr not_active Expired - Fee Related
2007
- 2007-02-02 EP EP07101654A patent/EP1818616B1/fr active Active
- 2007-02-02 US US11/670,510 patent/US7673457B2/en active Active
- 2007-02-07 RU RU2007104723/06A patent/RU2422730C2/ru active
- 2007-02-08 CA CA2577527A patent/CA2577527C/fr active Active
- 2007-02-08 CN CNA2007100075703A patent/CN101017000A/zh active Pending

Also Published As

Publication number	Publication date
CA2577527A1 (fr)	2007-08-08
US7673457B2 (en)	2010-03-09
RU2007104723A (ru)	2008-08-20
CN101017000A (zh)	2007-08-15
CA2577527C (fr)	2014-09-30
EP1818616A1 (fr)	2007-08-15
FR2897144A1 (fr)	2007-08-10
US20080010997A1 (en)	2008-01-17
EP1818616B1 (fr)	2012-12-26
RU2422730C2 (ru)	2011-06-27

Publication	Publication Date	Title
FR2897144B1 (fr)	2008-05-02	Chambre de combustion de turbomachine a fentes tangentielles
FR2897145B1 (fr)	2013-01-18	Chambre de combustion annulaire de turbomachine a fixations alternees.
FR2928994B1 (fr)	2010-04-02	Chambre de combustion de turbomachine.
EP1865262A4 (fr)	2014-08-06	Chambre de combustion de turbine a gaz
FR2903172B1 (fr)	2008-10-17	Agencement pour chambre de combustion de turbomachine ayant un defecteur a collerette
FR2903171B1 (fr)	2008-10-17	Agencement a liaison par crabot pour chambre de combustion de turbomachine
EP2075508A4 (fr)	2014-05-14	Chambre de combustion de turbine à gaz
FR2935777B1 (fr)	2013-03-08	Chambre de combustion de turbomachine
FR2897143B1 (fr)	2012-10-05	Chambre de combustion d'une turbomachine
GB0610800D0 (en)	2006-07-12	Combustion chamber for a gas turbine engine
FR2901349B1 (fr)	2008-09-05	Chambre de combustion d'une turbomachine
FR2908152B1 (fr)	2009-02-06	Aube en fleche de turbomachine
DE602007000064D1 (de)	2008-09-25	Ringförmige Brennkammer eines Turbotriebwerks
EP2187127A4 (fr)	2014-08-13	Chambre de combustion de turbine à gaz
EP2187128A4 (fr)	2015-07-29	Chambre de combustion
DE602007009436D1 (de)	2010-11-11	Ringförmige Brennkammer eines Turbotriebwerks
EP2230459A4 (fr)	2014-11-05	Chambre de combustion de turbine à gaz
FR2896537B1 (fr)	2011-07-29	Turbomachine a generateur-demarreur integre
DE602007007334D1 (de)	2010-08-05	Gasturbinenanordnung
BRPI0914905A2 (pt)	2015-10-20	câmara de combustão de motor de turbina a gás compreendendo pelo menos um defletor.
FR2920523B1 (fr)	2009-12-18	Chambre de combustion de turbomachine a circulation helicoidale de l'air.
EP2153051A4 (fr)	2013-06-19	Agencement de masquage pour moteur à turbine à gaz
FR2922629B1 (fr)	2009-12-25	Chambre de combustion a dilution optimisee et turbomachine en etant munie
FR2953907B1 (fr)	2012-11-02	Chambre de combustion pour turbomachine
FR2953909B1 (fr)	2013-02-15	Guidage d'une bougie dans une chambre de combustion de turbomachine

Legal Events

Date	Code	Title	Description
2014-11-21	ST	Notification of lapse	Effective date: 20141031