FR2825781B1 - Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique - Google Patents

Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique

Info

Publication number
FR2825781B1
FR2825781B1 FR0107361A FR0107361A FR2825781B1 FR 2825781 B1 FR2825781 B1 FR 2825781B1 FR 0107361 A FR0107361 A FR 0107361A FR 0107361 A FR0107361 A FR 0107361A FR 2825781 B1 FR2825781 B1 FR 2825781B1
Authority
FR
France
Prior art keywords
turbomachine
cmc
combustion
metal housing
elastic mounting
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.)
Expired - Fee Related
Application number
FR0107361A
Other languages
English (en)
Other versions
FR2825781A1 (fr
Inventor
Pierre Camy
Benoit Carrere
Eric Conete
Alexandre Forestier
Georges Habarou
Didier Hernandez
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 FR0107361A priority Critical patent/FR2825781B1/fr
Priority to JP2002161063A priority patent/JP4031292B2/ja
Priority to EP02291365A priority patent/EP1265036B1/fr
Priority to DE60229466T priority patent/DE60229466D1/de
Priority to US10/162,189 priority patent/US6732532B2/en
Publication of FR2825781A1 publication Critical patent/FR2825781A1/fr
Application granted granted Critical
Publication of FR2825781B1 publication Critical patent/FR2825781B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F23R3/42—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
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00—Manufacture
    • F05B2230/60—Assembly methods
    • F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
    • F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
FR0107361A 2001-06-06 2001-06-06 Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique Expired - Fee Related FR2825781B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0107361A FR2825781B1 (fr) 2001-06-06 2001-06-06 Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique
JP2002161063A JP4031292B2 (ja) 2001-06-06 2002-06-03 金属ケーシング内のターボマシンのｃｍｃ燃焼室のための弾性的な取り付け
EP02291365A EP1265036B1 (fr) 2001-06-06 2002-06-04 Montage élastique de chambre de combustion CMC de turbomachine dans un carter métallique
DE60229466T DE60229466D1 (de) 2001-06-06 2002-06-04 Elastische Befestigung einer Turbinenbrennkammer aus keramischem Matrix-Verbundwerkstoff in einem metallischen Gehäuse
US10/162,189 US6732532B2 (en) 2001-06-06 2002-06-05 Resilient mount for a CMC combustion chamber of a turbomachine in a metal casing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0107361A FR2825781B1 (fr) 2001-06-06 2001-06-06 Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique

Publications (2)

Publication Number Publication Date
FR2825781A1 FR2825781A1 (fr) 2002-12-13
FR2825781B1 true FR2825781B1 (fr) 2004-02-06

Family

ID=8863985

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0107361A Expired - Fee Related FR2825781B1 (fr) 2001-06-06 2001-06-06 Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique

Country Status (5)

Country Link
US (1) US6732532B2 (fr)
EP (1) EP1265036B1 (fr)
JP (1) JP4031292B2 (fr)
DE (1) DE60229466D1 (fr)
FR (1) FR2825781B1 (fr)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2840974B1 (fr) * 2002-06-13 2005-12-30 Snecma Propulsion Solide Anneau d'etancheite pour cahmbre de combustion et chambre de combustion comportant un tel anneau
US6775985B2 (en) * 2003-01-14 2004-08-17 General Electric Company Support assembly for a gas turbine engine combustor
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
FR2860039B1 (fr) * 2003-09-19 2005-11-25 Snecma Moteurs Realisation de l'etancheite dans un turboreacteur pour le prelevement cabine par joints double sens a lamelles
FR2871846B1 (fr) 2004-06-17 2006-09-29 Snecma Moteurs Sa Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc
FR2871847B1 (fr) * 2004-06-17 2006-09-29 Snecma Moteurs Sa Montage d'un distributeur de turbine sur une chambre de combustion a parois en cmc dans une turbine a gaz
GB2422874A (en) * 2005-02-05 2006-08-09 Alstom Technology Ltd Gas turbine burner expansion bar structure
US7546743B2 (en) * 2005-10-12 2009-06-16 General Electric Company Bolting configuration for joining ceramic combustor liner to metal mounting attachments
FR2892181B1 (fr) * 2005-10-18 2008-02-01 Snecma Sa Fixation d'une chambre de combustion a l'interieur de son carter
US7523616B2 (en) * 2005-11-30 2009-04-28 General Electric Company Methods and apparatuses for assembling a gas turbine engine
US7493771B2 (en) * 2005-11-30 2009-02-24 General Electric Company Methods and apparatuses for assembling a gas turbine engine
US7637110B2 (en) * 2005-11-30 2009-12-29 General Electric Company Methods and apparatuses for assembling a gas turbine engine
FR2897418B1 (fr) 2006-02-10 2013-03-01 Snecma Chambre de combustion annulaire d'une turbomachine
US8863528B2 (en) * 2006-07-27 2014-10-21 United Technologies Corporation Ceramic combustor can for a gas turbine engine
FR2919380B1 (fr) * 2007-07-26 2013-10-25 Snecma Chambre de combustion d'une turbomachine.
US20090067917A1 (en) * 2007-09-07 2009-03-12 The Boeing Company Bipod Flexure Ring
JP5276345B2 (ja) * 2008-03-28 2013-08-28 三菱重工業株式会社 ガスタービン及びガスタービンの燃焼器挿入孔形成方法
US20120047909A1 (en) * 2010-08-24 2012-03-01 Nuovo Pignone S.P.A. Combustor liner concentric support and method
US8919134B2 (en) * 2011-01-26 2014-12-30 United Technologies Corporation Intershaft seal with support linkage
US9335051B2 (en) * 2011-07-13 2016-05-10 United Technologies Corporation Ceramic matrix composite combustor vane ring assembly
WO2013163510A1 (fr) 2012-04-27 2013-10-31 General Electric Company Éléments annulaires de liaison pour moteur à turbine à gaz
US9435266B2 (en) 2013-03-15 2016-09-06 Rolls-Royce North American Technologies, Inc. Seals for a gas turbine engine
US10436446B2 (en) 2013-09-11 2019-10-08 General Electric Company Spring loaded and sealed ceramic matrix composite combustor liner
US9404421B2 (en) 2014-01-23 2016-08-02 Siemens Energy, Inc. Structural support bracket for gas flow path
US20170059165A1 (en) 2015-08-28 2017-03-02 Rolls-Royce High Temperature Composites Inc. Cmc cross-over tube

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2268464A (en) * 1939-09-29 1941-12-30 Bbc Brown Boveri & Cie Combustion chamber
US2509503A (en) * 1946-02-12 1950-05-30 Lucas Ltd Joseph Combustion chamber for prime movers
GB1570875A (en) * 1977-03-16 1980-07-09 Lucas Industries Ltd Combustion equipment
CH633351A5 (de) * 1978-11-09 1982-11-30 Sulzer Ag Waermedehnungen nachgebende abdichtung einer ringbrennkammer fuer eine gasturbine.
US4688378A (en) * 1983-12-12 1987-08-25 United Technologies Corporation One piece band seal
US4821522A (en) * 1987-07-02 1989-04-18 United Technologies Corporation Sealing and cooling arrangement for combustor vane interface
US5291733A (en) * 1993-02-08 1994-03-08 General Electric Company Liner mounting assembly
DE19745683A1 (de) * 1997-10-16 1999-04-22 Bmw Rolls Royce Gmbh Aufhängung einer ringförmigen Gasturbinen-Brennkammer
JP4031590B2 (ja) * 1999-03-08 2008-01-09 三菱重工業株式会社 燃焼器の尾筒シール構造及びその構造を用いたガスタービン
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
US6334298B1 (en) * 2000-07-14 2002-01-01 General Electric Company Gas turbine combustor having dome-to-liner joint

Also Published As

Publication number Publication date
FR2825781A1 (fr) 2002-12-13
EP1265036A1 (fr) 2002-12-11
JP4031292B2 (ja) 2008-01-09
EP1265036B1 (fr) 2008-10-22
JP2003021334A (ja) 2003-01-24
US6732532B2 (en) 2004-05-11
US20020184890A1 (en) 2002-12-12
DE60229466D1 (de) 2008-12-04

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Legal Events

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CL Concession to grant licences
CD Change of name or company name
ST Notification of lapse

Effective date: 20110228