BRPI1008982A2 - câmara anular de combustão destinada a equipar uma turbomáquina, e, turbomáquina - Google Patents

câmara anular de combustão destinada a equipar uma turbomáquina, e, turbomáquina

Info

Publication number: BRPI1008982A2
Authority: BR; Brazil
Prior art keywords: turbomachine; equipping; combustion chamber; annular combustion; annular
Prior art date: 2009-03-17

Application number

BRPI1008982A

Other languages

English (en)

Inventor

Romain Nicolas Lunel

Sébastien Alain Christophe BOURGEOIS

Thomas Olivier Marie Noel

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.)

2009-03-17

Filing date

2010-03-15

Publication date

2016-03-22

2010-03-15 Application filed by Snecma filed Critical Snecma

2016-03-22 Publication of BRPI1008982A2 publication Critical patent/BRPI1008982A2/pt

2021-01-26 Publication of BRPI1008982B1 publication Critical patent/BRPI1008982B1/pt

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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Fuel-Injection Apparatus (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)

BRPI1008982-9A 2009-03-17 2010-03-15 câmara anular de combustão destinada a equipar uma turbomáquina, e, turbomáquina BRPI1008982B1 (pt)

Applications Claiming Priority (3)

Application Number	Priority Date	Filing Date	Title
FR0951673		2009-03-17
FR0951673A FR2943403B1 (fr)	2009-03-17	2009-03-17	Chambre de combustion de turbomachine comprenant des moyens ameliores d'alimentation en air
PCT/EP2010/053249 WO2010105999A1 (fr)	2009-03-17	2010-03-15	Chambre de combustion de turbomachine comprenant des moyens ameliores d'alimentation en air

Publications (2)

Publication Number	Publication Date
BRPI1008982A2 true BRPI1008982A2 (pt)	2016-03-22
BRPI1008982B1 BRPI1008982B1 (pt)	2021-01-26

Family

ID=41165535

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI1008982-9A BRPI1008982B1 (pt)	2009-03-17	2010-03-15	câmara anular de combustão destinada a equipar uma turbomáquina, e, turbomáquina

Country Status (8)

Country	Link
US (1)	US9127841B2 (pt)
EP (1)	EP2409085B1 (pt)
CN (1)	CN102362120B (pt)
BR (1)	BRPI1008982B1 (pt)
CA (1)	CA2754419C (pt)
FR (1)	FR2943403B1 (pt)
RU (1)	RU2527932C2 (pt)
WO (1)	WO2010105999A1 (pt)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2964725B1 (fr)	2010-09-14	2012-10-12	Snecma	Carenage aerodynamique pour fond de chambre de combustion
FR3011317B1 (fr) *	2013-10-01	2018-02-23	Safran Aircraft Engines	Chambre de combustion pour turbomachine a admission d'air homogene au travers de systemes d'injection
FR3017255B1 (fr)	2014-02-03	2017-10-13	Snecma	Bougie d'allumage a semi-conducteur pour turbomachine d'aeronef, comprenant des ecopes d'evacuation d'eventuels reliquats de carburant
FR3035481B1 (fr) *	2015-04-23	2017-05-05	Snecma	Chambre de combustion de turbomachine comportant un dispositif de guidage de flux d'air de forme specifique
EP3252378A1 (en)	2016-05-31	2017-12-06	Siemens Aktiengesellschaft	Gas turbine annular combustor arrangement
US10619856B2 (en) *	2017-03-13	2020-04-14	Rolls-Royce Corporation	Notched gas turbine combustor cowl
US10907831B2 (en) *	2018-05-07	2021-02-02	Rolls-Royce Corporation	Ram pressure recovery fuel nozzle with a scoop
US10982852B2 (en)	2018-11-05	2021-04-20	Rolls-Royce Corporation	Cowl integration to combustor wall

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE3564024D1 (en) *	1984-02-29	1988-09-01	Lucas Ind Plc	Combustion equipment
US5142858A (en) *	1990-11-21	1992-09-01	General Electric Company	Compact flameholder type combustor which is staged to reduce emissions
RU2062405C1 (ru) *	1992-10-23	1996-06-20	Владимир Алексеевич Маев	Камера сгорания
US5623827A (en)	1995-01-26	1997-04-29	General Electric Company	Regenerative cooled dome assembly for a gas turbine engine combustor
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
US7222488B2 (en) *	2002-09-10	2007-05-29	General Electric Company	Fabricated cowl for double annular combustor of a gas turbine engine
US6779268B1 (en)	2003-05-13	2004-08-24	General Electric Company	Outer and inner cowl-wire wrap to one piece cowl conversion
FR2881813B1 (fr) *	2005-02-09	2011-04-08	Snecma Moteurs	Carenage de chambre de combustion de turbomachine
FR2909163B1 (fr)	2006-11-28	2011-02-25	Snecma	Carenage de chambre de combustion de turbomachine.
FR2910597B1 (fr) *	2006-12-22	2009-03-20	Snecma Sa	Carenage pour fond de chambre de combustion
FR2918444B1 (fr) *	2007-07-05	2013-06-28	Snecma	Deflecteur de fond de chambre, chambre de combustion le comportant et moteur a turbine a gaz en etant equipe
FR2941287B1 (fr)	2009-01-19	2011-03-25	Snecma	Paroi de chambre de combustion de turbomachine a une seule rangee annulaire d'orifices d'entree d'air primaire et de dilution
FR2964725B1 (fr)	2010-09-14	2012-10-12	Snecma	Carenage aerodynamique pour fond de chambre de combustion

2009
- 2009-03-17 FR FR0951673A patent/FR2943403B1/fr active Active
2010
- 2010-03-15 US US13/255,772 patent/US9127841B2/en active Active
- 2010-03-15 RU RU2011141837/06A patent/RU2527932C2/ru active
- 2010-03-15 CA CA2754419A patent/CA2754419C/fr active Active
- 2010-03-15 CN CN201080012736.0A patent/CN102362120B/zh active Active
- 2010-03-15 EP EP10708769.4A patent/EP2409085B1/fr active Active
- 2010-03-15 WO PCT/EP2010/053249 patent/WO2010105999A1/fr not_active Ceased
- 2010-03-15 BR BRPI1008982-9A patent/BRPI1008982B1/pt active IP Right Grant

Also Published As

Publication number	Publication date
EP2409085A1 (fr)	2012-01-25
FR2943403A1 (fr)	2010-09-24
CN102362120A (zh)	2012-02-22
BRPI1008982B1 (pt)	2021-01-26
EP2409085B1 (fr)	2015-02-25
CA2754419C (fr)	2017-04-04
RU2527932C2 (ru)	2014-09-10
US9127841B2 (en)	2015-09-08
RU2011141837A (ru)	2013-04-27
CA2754419A1 (fr)	2010-09-23
CN102362120B (zh)	2014-07-16
US20120055164A1 (en)	2012-03-08
FR2943403B1 (fr)	2014-11-14
WO2010105999A1 (fr)	2010-09-23

Similar Documents

Publication	Publication Date	Title
BRPI1011134A2 (pt)	2018-02-06	turbomáquina.
IT1400823B1 (it)	2013-07-02	Carcassa di turbina.
BRPI1008684A2 (pt)	2016-03-08	queimador de gás.
BRPI0909436A2 (pt)	2015-12-15	dsitribuidor de turbina para uma turbomáquina, turbina de turbomáquina e turbomáquina
BRPI1013342A2 (pt)	2016-03-29	conjunto de anel de turbina.
BRPI1008982A2 (pt)	2016-03-22	câmara anular de combustão destinada a equipar uma turbomáquina, e, turbomáquina
DE502008002661D1 (de)	2011-04-07	Gasdichte Kolbenringanordnung
BR112012002224A2 (pt)	2016-06-07	conjunto de estruturação para um bico de exaustão, bico de exaustão para uma nacela e nacela
BRPI0917460A2 (pt)	2015-12-01	parede interna de uma nacela de turbomáquina, e turbomáquina
GB2474344B (en)	2016-01-27	Turbomachine
GB2470282B (en)	2016-01-06	Flameless combustion systems for gas turbine engines
GB0903935D0 (en)	2009-04-22	Gas turbine engine
EP2469022A4 (en)	2015-01-07	RADIAL GAS DETENDER
BR112013021367A2 (pt)	2016-10-18	câmara anular de combustão de turbomáquina, compreendendo orifícios de diluição melhorados
FR2976346B1 (fr)	2013-07-05	Chambre de combustion annulaire de turbomachine
BR112012002447A2 (pt)	2016-03-01	câmara de combustão de turbomáquina ,e, turbomáquina.
PL2748532T3 (pl)	2017-11-30	Pierścieniowa ścianka komory spalania maszyny wirowej
FI20105766L (fi)	2011-01-08	Kaasumoottori
EP2519725A4 (en)	2015-03-25	CONSTRUCTION OF A GAS TURBINE ENGINE COMPONENT
GB2468848B (en)	2011-10-26	An assembly for a turbomachine
IT1397226B1 (it)	2013-01-04	Metodo di manutenzione di una camera di combustione di un impianto a turbina a gas.
FI20105531A0 (fi)	2010-05-14	Menetelmä ottopolttomoottorikoneen käyttämiseksi
FI20095856A7 (fi)	2011-02-21	Polttolaitos kiinteää biopolttoainetta varten
FR2944090B1 (fr)	2015-04-03	Turbomachine a chambre annulaire de combustion
FR2965604B1 (fr)	2013-04-19	Chambre de combustion de turbomachine

Legal Events

Date	Code	Title	Description
2019-01-15	B06F	Objections, documents and/or translations needed after an examination request according art. 34 industrial property law
2020-06-16	B06U	Preliminary requirement: requests with searches performed by other patent offices: suspension of the patent application procedure
2020-11-24	B09A	Decision: intention to grant
2021-01-26	B16A	Patent or certificate of addition of invention granted	Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 26/01/2021, OBSERVADAS AS CONDICOES LEGAIS.