DE602005001979D1 - Aufhängung einer Gasturbinenbrennkammer mit integriertem Turbinenleitapparat - Google Patents

Aufhängung einer Gasturbinenbrennkammer mit integriertem Turbinenleitapparat

Info

Publication number
DE602005001979D1
DE602005001979D1 DE602005001979T DE602005001979T DE602005001979D1 DE 602005001979 D1 DE602005001979 D1 DE 602005001979D1 DE 602005001979 T DE602005001979 T DE 602005001979T DE 602005001979 T DE602005001979 T DE 602005001979T DE 602005001979 D1 DE602005001979 D1 DE 602005001979D1
Authority
DE
Germany
Prior art keywords
suspension
combustion chamber
integrated
gas turbine
nozzle
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
DE602005001979T
Other languages
English (en)
Other versions
DE602005001979T2 (de
Inventor
Caroline Aumont
Eric Conette
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
Publication of DE602005001979D1 publication Critical patent/DE602005001979D1/de
Application granted granted Critical
Publication of DE602005001979T2 publication Critical patent/DE602005001979T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
DE602005001979T 2004-06-17 2005-06-02 Aufhängung einer Gasturbinenbrennkammer mit integriertem Turbinenleitapparat Active DE602005001979T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0406595 2004-06-17
FR0406595A FR2871845B1 (fr) 2004-06-17 2004-06-17 Montage de chambre de combustion de turbine a gaz avec distributeur integre de turbine haute pression

Publications (2)

Publication Number Publication Date
DE602005001979D1 true DE602005001979D1 (de) 2007-09-27
DE602005001979T2 DE602005001979T2 (de) 2008-05-08

Family

ID=34942372

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005001979T Active DE602005001979T2 (de) 2004-06-17 2005-06-02 Aufhängung einer Gasturbinenbrennkammer mit integriertem Turbinenleitapparat

Country Status (8)

Country Link
US (1) US7237388B2 (de)
EP (1) EP1607582B1 (de)
JP (1) JP2006002773A (de)
CA (1) CA2509797C (de)
DE (1) DE602005001979T2 (de)
ES (1) ES2290865T3 (de)
FR (1) FR2871845B1 (de)
RU (1) RU2368790C2 (de)

Families Citing this family (59)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7805946B2 (en) * 2005-12-08 2010-10-05 Siemens Energy, Inc. Combustor flow sleeve attachment system
US7934382B2 (en) * 2005-12-22 2011-05-03 United Technologies Corporation Combustor turbine interface
US7578134B2 (en) * 2006-01-11 2009-08-25 General Electric Company Methods and apparatus for assembling gas turbine engines
JPWO2007114520A1 (ja) * 2006-03-30 2009-08-20 日本電気株式会社 物品管理システムおよび物品管理方法
US7681403B2 (en) 2006-04-13 2010-03-23 General Electric Company Forward sleeve retainer plate and method
US20100225902A1 (en) * 2006-09-14 2010-09-09 General Electric Company Methods and apparatus for robotically inspecting gas turbine combustion components
US7765809B2 (en) * 2006-11-10 2010-08-03 General Electric Company Combustor dome and methods of assembling such
FR2914707B1 (fr) * 2007-04-05 2009-10-30 Snecma Propulsion Solide Sa Procede d'assemblage avec recouvrement de deux pieces ayant des coefficients de dilatation differents et assemblage ainsi obtenu
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
FR2929690B1 (fr) 2008-04-03 2012-08-17 Snecma Propulsion Solide Chambre de combustion sectorisee en cmc pour turbine a gaz
EP2180143A1 (de) * 2008-10-23 2010-04-28 Siemens Aktiengesellschaft Gasturbinenleitschaufelnanordnung und Gasturbine
US8875520B2 (en) * 2008-12-31 2014-11-04 Rolls-Royce North American Technologies, Inc. Gas turbine engine device
US9074005B2 (en) * 2009-01-02 2015-07-07 Washington State University Compositions and methods for modulating plant disease resistance and immunity
US8745989B2 (en) * 2009-04-09 2014-06-10 Pratt & Whitney Canada Corp. Reverse flow ceramic matrix composite combustor
US8206096B2 (en) * 2009-07-08 2012-06-26 General Electric Company Composite turbine nozzle
US8226361B2 (en) * 2009-07-08 2012-07-24 General Electric Company Composite article and support frame assembly
US8646276B2 (en) * 2009-11-11 2014-02-11 General Electric Company Combustor assembly for a turbine engine with enhanced cooling
FR2956695B1 (fr) * 2010-02-25 2012-11-16 Turbomeca Support de palier arriere souple avec butee pour turbomachine
US9234431B2 (en) * 2010-07-20 2016-01-12 Siemens Energy, Inc. Seal assembly for controlling fluid flow
FR2964145B1 (fr) 2010-08-26 2018-06-15 Safran Helicopter Engines Procede d'accrochage de blindage sur carter de turbine et ensemble d'accrochage pour sa mise en oeuvre
US8448444B2 (en) 2011-02-18 2013-05-28 General Electric Company Method and apparatus for mounting transition piece in combustor
US9335051B2 (en) * 2011-07-13 2016-05-10 United Technologies Corporation Ceramic matrix composite combustor vane ring assembly
JP6162949B2 (ja) * 2011-12-16 2017-07-12 ゼネラル・エレクトリック・カンパニイ Ｃｍｃライナの強化冷却のための一体化バッフルシステム
US20130152591A1 (en) * 2011-12-16 2013-06-20 General Electric Company System of integrating baffles for enhanced cooling of cmc liners
FR2988777B1 (fr) * 2012-03-29 2014-04-25 Snecma Propulsion Solide Integration de pieces d'arriere-corps de moteur aeronautique
US9108736B2 (en) 2012-06-05 2015-08-18 United Technologies Corporation Nacelle inner flow structure leading edge latching system
WO2014120310A2 (en) * 2012-11-02 2014-08-07 Metallic Hi Temperature Seal Systems, Llc. High temperature seal assembly
FR3002272A1 (fr) * 2013-02-19 2014-08-22 Snecma Secteur de distributeur a anti-rotation pour secteur adjacent
US9982628B2 (en) 2013-03-06 2018-05-29 United Technologies Corporation Exhaust system having a flow path liner supported by structural duct segments
US9488110B2 (en) 2013-03-08 2016-11-08 General Electric Company Device and method for preventing leakage of air between multiple turbine components
EP3299583B1 (de) * 2013-09-10 2019-10-30 United Technologies Corporation Hochdruckturbinenleitschaufelträger mit mitteln zur verdrehsicherung und druckstosskompensation
JP6228685B2 (ja) 2013-09-11 2017-11-08 ゼネラル・エレクトリック・カンパニイ ばねで荷重されシールされるセラミックマトリックス複合材燃焼器ライナ
FR3010774B1 (fr) * 2013-09-16 2018-01-05 Safran Aircraft Engines Turbomachine a chambre de combustion maintenue par une couronne de fixation metallique
EP3052862A4 (de) * 2013-10-04 2016-11-02 United Technologies Corp Brennkammertafel mit mehreren befestigungen
FR3017928B1 (fr) * 2014-02-27 2019-07-26 Safran Aircraft Engines Turbomachine a bride externe de chambre de combustion de type "sandwich"
JP6429764B2 (ja) * 2015-12-24 2018-11-28 三菱重工航空エンジン株式会社 ガスタービン
US10378771B2 (en) 2016-02-25 2019-08-13 General Electric Company Combustor assembly
US10281153B2 (en) * 2016-02-25 2019-05-07 General Electric Company Combustor assembly
EP3228833B1 (de) 2016-04-05 2018-08-01 MTU Aero Engines GmbH Verbindungsanordnung für bauteile aus keramischen faserverbundwerkstoffen eines turbinenzwischengehäuses
EP3228820B1 (de) * 2016-04-08 2020-07-22 Ansaldo Energia Switzerland AG Turbomotor mit einer schaufelträgereinheit
US20170370583A1 (en) * 2016-06-22 2017-12-28 General Electric Company Ceramic Matrix Composite Component for a Gas Turbine Engine
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
US10378770B2 (en) * 2017-01-27 2019-08-13 General Electric Company Unitary flow path structure
US20180223691A1 (en) * 2017-02-03 2018-08-09 United Technologies Corporation Case flange with stress reducing features
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
US10253641B2 (en) 2017-02-23 2019-04-09 General Electric Company Methods and assemblies for attaching airfoils within a flow path
US10385776B2 (en) 2017-02-23 2019-08-20 General Electric Company Methods for assembling a unitary flow path structure
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
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
CN108869041B (zh) * 2017-05-12 2020-07-14 中国联合重型燃气轮机技术有限公司 用于燃气轮机的前端转向勺状件
US10385731B2 (en) 2017-06-12 2019-08-20 General Electric Company CTE matching hanger support for CMC structures
US10746035B2 (en) 2017-08-30 2020-08-18 General Electric Company Flow path assemblies for gas turbine engines and assembly methods therefore
FR3080145B1 (fr) * 2018-04-17 2020-05-01 Safran Aircraft Engines Distributeur en cmc avec reprise d'effort par une pince etanche
EP3674081B1 (de) * 2018-12-31 2022-02-23 Ansaldo Energia Switzerland AG Hochtemperaturbeständige fliesen und herstellungsverfahren dafür
CN113685844B (zh) * 2021-08-24 2022-11-25 中国航发湖南动力机械研究所 一种燃烧室全环试验件小弯管装配工装
CN116105177A (zh) * 2023-03-10 2023-05-12 中国航发湖南动力机械研究所 一种陶瓷基火焰筒

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR692826A (fr) * 1929-06-04 1930-11-12 Dispositif de fixation de distributeurs de turbines
US2420135A (en) * 1944-06-07 1947-05-06 Elliott Co Support for expansible members
GB1089660A (en) * 1966-04-25 1967-11-01 Rolls Royce Gas turbine engine combustion equipment
US4566851A (en) * 1984-05-11 1986-01-28 United Technologies Corporation First stage turbine vane support structure
US5188507A (en) * 1991-11-27 1993-02-23 General Electric Company Low-pressure turbine shroud
DE4323706A1 (de) * 1993-07-15 1995-01-19 Abb Management Ag Gasturbine
FR2728016B1 (fr) 1994-12-07 1997-01-17 Snecma Distributeur monobloc non-sectorise d'un stator de turbine de turbomachine
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
FR2825780B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Architecure de chambre de combustion de turbomachine en materiau a matrice ceramique
FR2825783B1 (fr) * 2001-06-06 2003-11-07 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine par pattes brasees
FR2825784B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Accrochage de chambre de combustion cmc de turbomachine utilisant les trous de dilution
FR2825785B1 (fr) * 2001-06-06 2004-08-27 Snecma Moteurs Liaison de chambre de combustion cmc de turbomachine en deux parties
FR2825787B1 (fr) * 2001-06-06 2004-08-27 Snecma Moteurs Montage de chambre de combustion cmc de turbomachine par viroles de liaison souples
FR2831600B1 (fr) * 2001-10-25 2004-01-02 Snecma Moteurs Dispositif d'arret en rotation d'un secteur porteur d'aubes fixes dans une virole d'une turbomachine

Also Published As

Publication number Publication date
ES2290865T3 (es) 2008-02-16
EP1607582B1 (de) 2007-08-15
US20060032237A1 (en) 2006-02-16
CA2509797A1 (fr) 2005-12-17
RU2005119717A (ru) 2006-12-27
FR2871845B1 (fr) 2009-06-26
FR2871845A1 (fr) 2005-12-23
EP1607582A1 (de) 2005-12-21
JP2006002773A (ja) 2006-01-05
US7237388B2 (en) 2007-07-03
RU2368790C2 (ru) 2009-09-27
CA2509797C (fr) 2012-04-24
DE602005001979T2 (de) 2008-05-08

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Legal Events

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8364 No opposition during term of opposition