FR2885201B1 - Chambre de combustion aisement demontable a performance aerodynamique amelioree - Google Patents

Chambre de combustion aisement demontable a performance aerodynamique amelioree

Info

Publication number
FR2885201B1
FR2885201B1 FR0504283A FR0504283A FR2885201B1 FR 2885201 B1 FR2885201 B1 FR 2885201B1 FR 0504283 A FR0504283 A FR 0504283A FR 0504283 A FR0504283 A FR 0504283A FR 2885201 B1 FR2885201 B1 FR 2885201B1
Authority
FR
France
Prior art keywords
combustion chamber
aerodynamic performance
improved aerodynamic
easily dismantling
dismantling
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
FR0504283A
Other languages
English (en)
Other versions
FR2885201A1 (fr
Inventor
Christophe Pieussergues
Pierre Sablayrolles
Laurent Marnas
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 Moteurs SA
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
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Priority to FR0504283A priority Critical patent/FR2885201B1/fr
Priority to EP06112766.8A priority patent/EP1717516B1/fr
Priority to US11/410,068 priority patent/US7637111B2/en
Priority to JP2006120123A priority patent/JP2006307854A/ja
Priority to CA2544957A priority patent/CA2544957C/fr
Priority to RU2006114416/06A priority patent/RU2411412C2/ru
Priority to CNA2006100781482A priority patent/CN1854610A/zh
Publication of FR2885201A1 publication Critical patent/FR2885201A1/fr
Application granted granted Critical
Publication of FR2885201B1 publication Critical patent/FR2885201B1/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
    • F23R3/02—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
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • 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
    • F23R2900/00017—Assembling combustion chamber liners or subparts
FR0504283A 2005-04-28 2005-04-28 Chambre de combustion aisement demontable a performance aerodynamique amelioree Active FR2885201B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR0504283A FR2885201B1 (fr) 2005-04-28 2005-04-28 Chambre de combustion aisement demontable a performance aerodynamique amelioree
EP06112766.8A EP1717516B1 (fr) 2005-04-28 2006-04-19 Chambre de combustion aisément démontable à performance aérodynamique améliorée
JP2006120123A JP2006307854A (ja) 2005-04-28 2006-04-25 改善された空力性能を備えた、容易に取り外しできる燃焼チャンバ
US11/410,068 US7637111B2 (en) 2005-04-28 2006-04-25 Easily demountable combustion chamber with improved aerodynamic performance
CA2544957A CA2544957C (fr) 2005-04-28 2006-04-26 Chambre de combustion aisement demontable a performance aerodynamique amelioree
RU2006114416/06A RU2411412C2 (ru) 2005-04-28 2006-04-27 Демонтируемая камера сгорания с улучшенными аэродинамическими характеристиками
CNA2006100781482A CN1854610A (zh) 2005-04-28 2006-04-28 空气动力性能提高且易于拆卸的燃烧室

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0504283A FR2885201B1 (fr) 2005-04-28 2005-04-28 Chambre de combustion aisement demontable a performance aerodynamique amelioree

Publications (2)

Publication Number Publication Date
FR2885201A1 FR2885201A1 (fr) 2006-11-03
FR2885201B1 true FR2885201B1 (fr) 2010-09-17

Family

ID=35500968

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0504283A Active FR2885201B1 (fr) 2005-04-28 2005-04-28 Chambre de combustion aisement demontable a performance aerodynamique amelioree

Country Status (7)

Country Link
US (1) US7637111B2 (fr)
EP (1) EP1717516B1 (fr)
JP (1) JP2006307854A (fr)
CN (1) CN1854610A (fr)
CA (1) CA2544957C (fr)
FR (1) FR2885201B1 (fr)
RU (1) RU2411412C2 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8109098B2 (en) * 2006-05-04 2012-02-07 Siemens Energy, Inc. Combustor liner for gas turbine engine
FR2911668B1 (fr) * 2007-01-18 2009-03-20 Snecma Sa Chambre de combustion d'une turbomachine
FR2911669B1 (fr) * 2007-01-23 2011-09-16 Snecma Carenage pour chambre de combustion, chambre de combustion en etant equipee et turboreacteur les comportant.
FR2920525B1 (fr) * 2007-08-31 2014-06-13 Snecma Separateur pour alimentation de l'air de refroidissement d'une turbine
FR2964725B1 (fr) * 2010-09-14 2012-10-12 Snecma Carenage aerodynamique pour fond de chambre de combustion
US8938978B2 (en) * 2011-05-03 2015-01-27 General Electric Company Gas turbine engine combustor with lobed, three dimensional contouring
US8938976B2 (en) * 2011-05-20 2015-01-27 Siemens Energy, Inc. Structural frame for gas turbine combustion cap assembly
FR2976346B1 (fr) * 2011-06-08 2013-07-05 Turbomeca Chambre de combustion annulaire de turbomachine
FR2998038B1 (fr) * 2012-11-09 2017-12-08 Snecma Chambre de combustion pour une turbomachine
DE102015213629A1 (de) * 2015-07-20 2017-01-26 Rolls-Royce Deutschland Ltd & Co Kg Abdeckteil und Brennkammerbaugruppe für eine Gasturbine
US9995175B2 (en) * 2016-06-29 2018-06-12 General Electric Company System and method for gas bearing support of turbine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3422620A (en) * 1967-05-04 1969-01-21 Westinghouse Electric Corp Combustion apparatus
US3854285A (en) * 1973-02-26 1974-12-17 Gen Electric Combustor dome assembly
US4411134A (en) * 1981-10-26 1983-10-25 Moir David L Apparatus for the repair and replacement of transition ducts on jet engines and bracket therefor
FR2662784B1 (fr) * 1990-06-05 1992-08-14 Snecma Ensemble d'injection pour turbomachine, comprenant un bol de prevaporisation.
JP2597800B2 (ja) * 1992-06-12 1997-04-09 ゼネラル・エレクトリック・カンパニイ ガスタービンエンジン用燃焼器
DE69930455T2 (de) * 1998-11-12 2006-11-23 Mitsubishi Heavy Industries, Ltd. Gasturbinenbrennkammer
FR2825779B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Chambre de combustion munie d'un systeme de fixation de fond de chambre
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
US7415826B2 (en) * 2005-07-25 2008-08-26 General Electric Company Free floating mixer assembly for combustor of a gas turbine engine

Also Published As

Publication number Publication date
FR2885201A1 (fr) 2006-11-03
CN1854610A (zh) 2006-11-01
EP1717516B1 (fr) 2019-04-03
RU2411412C2 (ru) 2011-02-10
CA2544957C (fr) 2014-12-23
US7637111B2 (en) 2009-12-29
EP1717516A1 (fr) 2006-11-02
CA2544957A1 (fr) 2006-10-28
RU2006114416A (ru) 2007-11-10
US20060242939A1 (en) 2006-11-02
JP2006307854A (ja) 2006-11-09

Similar Documents

Publication Publication Date Title
FR2885201B1 (fr) Chambre de combustion aisement demontable a performance aerodynamique amelioree
FR2881813B1 (fr) Carenage de chambre de combustion de turbomachine
FR2897145B1 (fr) Chambre de combustion annulaire de turbomachine a fixations alternees.
FR2897144B1 (fr) Chambre de combustion de turbomachine a fentes tangentielles
FR2920523B1 (fr) Chambre de combustion de turbomachine a circulation helicoidale de l'air.
DE602006021273D1 (de) Verbrennungsmotor
BRPI0914905A2 (pt) câmara de combustão de motor de turbina a gás compreendendo pelo menos um defletor.
DE602006015519D1 (de) Verbrennungsmotor mit einem turbolader
DE602006003298D1 (de) Brennkraftmaschine
FR2935777B1 (fr) Chambre de combustion de turbomachine
FI20060561A0 (fi) Polttomoottorikone
FR2917487B1 (fr) Chambre de combustion de turbomachine a circulation helicoidale de l'air
DE602006002029D1 (de) Verbrennungsmotordämpfer
FI20060255A0 (fi) Polttomoottorikone
FR2909163B1 (fr) Carenage de chambre de combustion de turbomachine.
DE112006001575A5 (de) Brennkraftmaschine
FR2897923B1 (fr) Chambre de combustion annulaire a fond amovible
FR2891351B1 (fr) Chambre de combustion de moteur a turbine a gaz avec carenage
FR2925145B1 (fr) Chambre de combustion de turbomachine
DE602005005157D1 (de) Triebwerkanordnung
FI20060538A0 (fi) Polttomoottorikone
FI20060559A0 (fi) Polttomoottorikone
FR2920221B1 (fr) Chambre de combustion avec deflecteurs
DE112006002221A5 (de) Brennkraftmaschine
FR2887615B1 (fr) Carenage circulaire de chambre de combustion de turbomachine

Legal Events

Date Code Title Description
CD Change of name or company name
PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

CD Change of name or company name

Owner name: SNECMA, FR

Effective date: 20170713

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 16

PLFP Fee payment

Year of fee payment: 17

PLFP Fee payment

Year of fee payment: 18

PLFP Fee payment

Year of fee payment: 19

PLFP Fee payment

Year of fee payment: 20