FR2871846B1 - Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc - Google Patents

Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc

Info

Publication number
FR2871846B1
FR2871846B1 FR0406597A FR0406597A FR2871846B1 FR 2871846 B1 FR2871846 B1 FR 2871846B1 FR 0406597 A FR0406597 A FR 0406597A FR 0406597 A FR0406597 A FR 0406597A FR 2871846 B1 FR2871846 B1 FR 2871846B1
Authority
FR
France
Prior art keywords
combustion chamber
gas turbine
turbine combustion
metallic casing
chamber supported
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 - Lifetime
Application number
FR0406597A
Other languages
English (en)
Other versions
FR2871846A1 (fr
Inventor
Caroline Aumont
Eric Conete
Sousa Mario Cesar De
Didier Hippolyte 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 FR0406597A priority Critical patent/FR2871846B1/fr
Priority to GB0511387A priority patent/GB2415496B/en
Priority to RU2005117832/06A priority patent/RU2310795C2/ru
Priority to JP2005169179A priority patent/JP2006003072A/ja
Priority to US11/153,353 priority patent/US7234306B2/en
Publication of FR2871846A1 publication Critical patent/FR2871846A1/fr
Application granted granted Critical
Publication of FR2871846B1 publication Critical patent/FR2871846B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2203/00—Non-metallic inorganic materials
    • F05C2203/08—Ceramics; Oxides

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)
FR0406597A 2004-06-17 2004-06-17 Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc Expired - Lifetime FR2871846B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0406597A FR2871846B1 (fr) 2004-06-17 2004-06-17 Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc
GB0511387A GB2415496B (en) 2004-06-17 2005-06-03 A gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members
RU2005117832/06A RU2310795C2 (ru) 2004-06-17 2005-06-09 Газовая турбина с камерой сгорания, выполненной из композитного материала
JP2005169179A JP2006003072A (ja) 2004-06-17 2005-06-09 Ｃｍｃ連結部材によって金属ケーシング内に支持されるｃｍｃ製ガスタービン燃焼室
US11/153,353 US7234306B2 (en) 2004-06-17 2005-06-16 Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0406597A FR2871846B1 (fr) 2004-06-17 2004-06-17 Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc

Publications (2)

Publication Number Publication Date
FR2871846A1 FR2871846A1 (fr) 2005-12-23
FR2871846B1 true FR2871846B1 (fr) 2006-09-29

Family

ID=34834207

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0406597A Expired - Lifetime FR2871846B1 (fr) 2004-06-17 2004-06-17 Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc

Country Status (5)

Country Link
US (1) US7234306B2 (fr)
JP (1) JP2006003072A (fr)
FR (1) FR2871846B1 (fr)
GB (1) GB2415496B (fr)
RU (1) RU2310795C2 (fr)

Families Citing this family (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2892181B1 (fr) * 2005-10-18 2008-02-01 Snecma Sa Fixation d'une chambre de combustion a l'interieur de son carter
US7578134B2 (en) * 2006-01-11 2009-08-25 General Electric Company Methods and apparatus for assembling gas turbine engines
US7802431B2 (en) * 2006-07-27 2010-09-28 Siemens Energy, Inc. Combustor liner with reverse flow for gas turbine engine
US8141370B2 (en) * 2006-08-08 2012-03-27 General Electric Company Methods and apparatus for radially compliant component mounting
FR2910597B1 (fr) * 2006-12-22 2009-03-20 Snecma Sa Carenage pour fond de chambre de combustion
US20090067917A1 (en) * 2007-09-07 2009-03-12 The Boeing Company Bipod Flexure Ring
US8726675B2 (en) * 2007-09-07 2014-05-20 The Boeing Company Scalloped flexure ring
FR2929689B1 (fr) 2008-04-03 2013-04-12 Snecma Propulsion Solide Chambre de combustion de turbine a gaz a parois interne et externe sectorisees
FR2929690B1 (fr) 2008-04-03 2012-08-17 Snecma Propulsion Solide Chambre de combustion sectorisee en cmc pour turbine a gaz
US9464808B2 (en) * 2008-11-05 2016-10-11 Parker-Hannifin Corporation Nozzle tip assembly with secondary retention device
US20100170258A1 (en) * 2009-01-06 2010-07-08 General Electric Company Cooling apparatus for combustor transition piece
FR2944089B1 (fr) * 2009-04-07 2015-05-22 Snecma Accrochage de chambre annulaire de combustion
US8745989B2 (en) 2009-04-09 2014-06-10 Pratt & Whitney Canada Corp. Reverse flow ceramic matrix composite combustor
US8226361B2 (en) * 2009-07-08 2012-07-24 General Electric Company Composite article and support frame assembly
US8206096B2 (en) * 2009-07-08 2012-06-26 General Electric Company Composite turbine nozzle
US8713945B2 (en) * 2010-06-29 2014-05-06 Nuovo Pignone S.P.A. Liner aft end support mechanisms and spring loaded liner stop mechanisms
US9234431B2 (en) * 2010-07-20 2016-01-12 Siemens Energy, Inc. Seal assembly for controlling fluid flow
US8973365B2 (en) * 2010-10-29 2015-03-10 Solar Turbines Incorporated Gas turbine combustor with mounting for Helmholtz resonators
US9335051B2 (en) * 2011-07-13 2016-05-10 United Technologies Corporation Ceramic matrix composite combustor vane ring assembly
FR2988777B1 (fr) * 2012-03-29 2014-04-25 Snecma Propulsion Solide Integration de pieces d'arriere-corps de moteur aeronautique
CA2896500A1 (fr) 2013-01-29 2014-08-07 Rolls-Royce Corporation Enveloppe de turbine
EP2971577B1 (fr) 2013-03-13 2018-08-29 Rolls-Royce Corporation Virole de turbine
US10436446B2 (en) 2013-09-11 2019-10-08 General Electric Company Spring loaded and sealed ceramic matrix composite combustor liner
US10539327B2 (en) * 2013-09-11 2020-01-21 United Technologies Corporation Combustor liner
JP6387551B2 (ja) * 2014-06-13 2018-09-12 ヤンマー株式会社 ガスタービンエンジン
US10190434B2 (en) 2014-10-29 2019-01-29 Rolls-Royce North American Technologies Inc. Turbine shroud with locating inserts
CA2915246A1 (fr) 2014-12-23 2016-06-23 Rolls-Royce Corporation Enveloppe de turbine
CA2915370A1 (fr) 2014-12-23 2016-06-23 Rolls-Royce Corporation Chemin de pale circulaire comportant des elements clavetes axialement
EP3045674B1 (fr) 2015-01-15 2018-11-21 Rolls-Royce Corporation Enveloppe de turbine avec inserts tubulaires de localisation de patins
CA2924855A1 (fr) 2015-04-29 2016-10-29 Rolls-Royce Corporation Sillage de pale a distorsion trapezoidale
CA2925588A1 (fr) 2015-04-29 2016-10-29 Rolls-Royce Corporation Sillage de pale brase destine a une turbine a gaz
US10436114B2 (en) * 2015-08-26 2019-10-08 Pratt & Whitney Canada Corp. Combustor cooling system
US11149646B2 (en) * 2015-09-02 2021-10-19 General Electric Company Piston ring assembly for a turbine engine
US10240476B2 (en) 2016-01-19 2019-03-26 Rolls-Royce North American Technologies Inc. Full hoop blade track with interstage cooling air
US10837638B2 (en) 2016-04-12 2020-11-17 Raytheon Technologies Corporation Heat shield with axial retention lock
US10816204B2 (en) * 2016-04-12 2020-10-27 Raytheon Technologies Corporation Heat shield with axial retention lock
US10287906B2 (en) 2016-05-24 2019-05-14 Rolls-Royce North American Technologies Inc. Turbine shroud with full hoop ceramic matrix composite blade track and seal system
US10415415B2 (en) 2016-07-22 2019-09-17 Rolls-Royce North American Technologies Inc. Turbine shroud with forward case and full hoop blade track
US10393380B2 (en) * 2016-07-12 2019-08-27 Rolls-Royce North American Technologies Inc. Combustor cassette liner mounting assembly
US10393381B2 (en) 2017-01-27 2019-08-27 General Electric Company Unitary flow path structure
US10253643B2 (en) 2017-02-07 2019-04-09 General Electric Company Airfoil fluid curtain to mitigate or prevent flow path leakage
US10378373B2 (en) 2017-02-23 2019-08-13 General Electric Company Flow path assembly with airfoils inserted through flow path boundary
US10385709B2 (en) 2017-02-23 2019-08-20 General Electric Company Methods and features for positioning a flow path assembly within a gas turbine engine
US10253641B2 (en) 2017-02-23 2019-04-09 General Electric Company Methods and assemblies for attaching airfoils within a flow path
US10247019B2 (en) 2017-02-23 2019-04-02 General Electric Company Methods and features for positioning a flow path inner boundary within a flow path assembly
US10385731B2 (en) * 2017-06-12 2019-08-20 General Electric Company CTE matching hanger support for CMC structures
US11280295B2 (en) 2019-03-12 2022-03-22 Rohr, Inc. Beaded finger attachment
FR3111964B1 (fr) 2020-06-26 2023-03-17 Safran Helicopter Engines Assemblage d’une pièce de chambre de combustion par recouvrement par une autre pièce
US11274603B1 (en) * 2020-08-21 2022-03-15 Bob Burkett Electric heating systems and methods for gas turbine engines and jet engines
FR3116862B1 (fr) * 2020-11-30 2022-12-23 Safran Ceram Module de combustion pour une turbomachine

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4191011A (en) * 1977-12-21 1980-03-04 General Motors Corporation Mount assembly for porous transition panel at annular combustor outlet
US4413477A (en) * 1980-12-29 1983-11-08 General Electric Company Liner assembly for gas turbine combustor
US5291732A (en) * 1993-02-08 1994-03-08 General Electric Company Combustor liner support assembly
JPH07217889A (ja) * 1994-01-31 1995-08-18 Mitsubishi Heavy Ind Ltd 燃焼器
JP2001012739A (ja) * 1999-06-30 2001-01-19 Mitsubishi Heavy Ind Ltd ガスタービン用燃焼器
FR2825784B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution
FR2825783B1 (fr) * 2001-06-06 2003-11-07 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine par pattes brasees
FR2825779B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Chambre de combustion munie d'un systeme de fixation de fond de chambre
FR2825785B1 (fr) * 2001-06-06 2004-08-27 Snecma Moteurs Liaison de chambre de combustion cmc de turbomachine en deux parties
FR2825781B1 (fr) * 2001-06-06 2004-02-06 Snecma Moteurs Montage elastique de chambre ce combustion cmc de turbomachine dans un carter metallique
FR2825780B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Architecure de chambre de combustion de turbomachine en materiau a matrice ceramique
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
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
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

Also Published As

Publication number Publication date
US20060032235A1 (en) 2006-02-16
GB2415496A (en) 2005-12-28
GB0511387D0 (en) 2005-07-13
GB2415496B (en) 2008-11-26
RU2005117832A (ru) 2006-12-20
RU2310795C2 (ru) 2007-11-20
JP2006003072A (ja) 2006-01-05
US7234306B2 (en) 2007-06-26
FR2871846A1 (fr) 2005-12-23

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