DE60204489D1 - Stützträger für den Statorring einer Hochdruckturbine in einer Turbomachine mit Regulierung des Spiels - Google Patents

Stützträger für den Statorring einer Hochdruckturbine in einer Turbomachine mit Regulierung des Spiels

Info

Publication number
DE60204489D1
DE60204489D1 DE60204489T DE60204489T DE60204489D1 DE 60204489 D1 DE60204489 D1 DE 60204489D1 DE 60204489 T DE60204489 T DE 60204489T DE 60204489 T DE60204489 T DE 60204489T DE 60204489 D1 DE60204489 D1 DE 60204489D1
Authority
DE
Germany
Prior art keywords
turbomachine
game
regulation
pressure turbine
support beam
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
DE60204489T
Other languages
English (en)
Other versions
DE60204489T2 (de
Inventor
Jean-Baptiste Arilla
Alain Dominique Gendraud
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 DE60204489D1 publication Critical patent/DE60204489D1/de
Application granted granted Critical
Publication of DE60204489T2 publication Critical patent/DE60204489T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00Manufacture
    • F05B2230/60Assembly methods
    • F05B2230/604Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
    • F05B2230/606Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • F05D2230/64Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60204489T 2001-01-04 2002-01-03 Stützträger für den Statorring einer Hochdruckturbine in einer Turbomachine mit Regulierung des Spiels Expired - Lifetime DE60204489T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0100059 2001-01-04
FR0100059A FR2819010B1 (fr) 2001-01-04 2001-01-04 Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux

Publications (2)

Publication Number Publication Date
DE60204489D1 true DE60204489D1 (de) 2005-07-14
DE60204489T2 DE60204489T2 (de) 2006-03-16

Family

ID=8858504

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60204489T Expired - Lifetime DE60204489T2 (de) 2001-01-04 2002-01-03 Stützträger für den Statorring einer Hochdruckturbine in einer Turbomachine mit Regulierung des Spiels

Country Status (10)

Country Link
US (1) US6726446B2 (de)
EP (1) EP1225309B1 (de)
JP (1) JP4021768B2 (de)
KR (1) KR100829154B1 (de)
CA (1) CA2400151C (de)
DE (1) DE60204489T2 (de)
FR (1) FR2819010B1 (de)
RU (1) RU2289699C2 (de)
UA (1) UA73345C2 (de)
WO (1) WO2002053876A1 (de)

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FR2867224B1 (fr) * 2004-03-04 2006-05-19 Snecma Moteurs Dispositif de maintien axial de secteur d'entretoise pour anneau d'une turbine haute-pression de turbomachine
US7494317B2 (en) * 2005-06-23 2009-02-24 Siemens Energy, Inc. Ring seal attachment system
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US7607885B2 (en) * 2006-07-31 2009-10-27 General Electric Company Methods and apparatus for operating gas turbine engines
US7597533B1 (en) 2007-01-26 2009-10-06 Florida Turbine Technologies, Inc. BOAS with multi-metering diffusion cooling
US7665962B1 (en) 2007-01-26 2010-02-23 Florida Turbine Technologies, Inc. Segmented ring for an industrial gas turbine
FR2913051B1 (fr) * 2007-02-28 2011-06-10 Snecma Etage de turbine dans une turbomachine
KR100789311B1 (ko) * 2007-03-08 2007-12-28 한전케이피에스 주식회사 저압 터빈용 하부 그랜드 하우징 위치 조절 장치
FR2921410B1 (fr) * 2007-09-24 2010-03-12 Snecma Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des moyens permettant sa prehension
US7762509B2 (en) * 2007-10-18 2010-07-27 United Technologies Corp. Gas turbine engine systems involving rotatable annular supports
FR2923527B1 (fr) * 2007-11-13 2013-12-27 Snecma Etage de turbine ou de compresseur, en particulier de turbomachine
FR2931872B1 (fr) * 2008-05-28 2010-08-20 Snecma Turbine haute pression d'une turbomachine avec montage ameliore du boitier de pilotage des jeux radiaux d'aubes mobiles.
FR2935430B1 (fr) * 2008-08-26 2012-03-09 Snecma Turbine haute-pression de turbomachine amelioree, secteur de distributeur et moteur d'aeronef associes
FR2941488B1 (fr) * 2009-01-28 2011-09-16 Snecma Anneau de turbine a encoche anti-rotation
RU2522264C2 (ru) 2009-03-09 2014-07-10 Снекма Сборка обоймы турбины
FR2942845B1 (fr) * 2009-03-09 2011-04-01 Snecma Ensemble d'anneau de turbine
JP5384983B2 (ja) * 2009-03-27 2014-01-08 本田技研工業株式会社 タービンシュラウド
US8342798B2 (en) * 2009-07-28 2013-01-01 General Electric Company System and method for clearance control in a rotary machine
US8740552B2 (en) * 2010-05-28 2014-06-03 General Electric Company Low-ductility turbine shroud and mounting apparatus
JP5751950B2 (ja) * 2011-06-20 2015-07-22 三菱日立パワーシステムズ株式会社 ガスタービン及びガスタービンの補修方法
US9080458B2 (en) 2011-08-23 2015-07-14 United Technologies Corporation Blade outer air seal with multi impingement plate assembly
US9726043B2 (en) 2011-12-15 2017-08-08 General Electric Company Mounting apparatus for low-ductility turbine shroud
US9051849B2 (en) * 2012-02-13 2015-06-09 United Technologies Corporation Anti-rotation stator segments
FR2989724B1 (fr) * 2012-04-20 2015-12-25 Snecma Etage de turbine pour une turbomachine
CA2870765C (en) * 2012-04-27 2017-03-28 General Electric Company System and method of limiting axial movement between a hanger and a fairing assembly in a turbine assembly
US10378387B2 (en) 2013-05-17 2019-08-13 General Electric Company CMC shroud support system of a gas turbine
EP3080403B1 (de) 2013-12-12 2019-05-01 General Electric Company Trägersystem für cmc-mantel
EP3097273B1 (de) * 2014-01-20 2019-11-06 United Technologies Corporation Halteklammer für eine aussendichtung einer turbinenschaufel
JP6775425B2 (ja) 2014-06-12 2020-10-28 ゼネラル・エレクトリック・カンパニイ シュラウドハンガーアセンブリ
JP6574208B2 (ja) * 2014-06-12 2019-09-11 ゼネラル・エレクトリック・カンパニイ シュラウドハンガアセンブリ
CN106460560B (zh) 2014-06-12 2018-11-13 通用电气公司 护罩吊架组件
FR3024883B1 (fr) * 2014-08-14 2016-08-05 Snecma Module de turbomachine
US9874104B2 (en) 2015-02-27 2018-01-23 General Electric Company Method and system for a ceramic matrix composite shroud hanger assembly
US10392950B2 (en) 2015-05-07 2019-08-27 General Electric Company Turbine band anti-chording flanges
US9915153B2 (en) * 2015-05-11 2018-03-13 General Electric Company Turbine shroud segment assembly with expansion joints
US10436071B2 (en) * 2016-04-15 2019-10-08 United Technologies Corporation Blade outer air seal having retention snap ring
GB201708746D0 (en) * 2017-06-01 2017-07-19 Rolls Royce Plc Clearance control arrangement
FR3082872B1 (fr) * 2018-06-25 2021-06-04 Safran Aircraft Engines Dispositif de refroidissement d'un carter de turbomachine
US10934876B2 (en) * 2018-07-18 2021-03-02 Raytheon Technologies Corporation Blade outer air seal AFT hook retainer
FR3098238B1 (fr) * 2019-07-04 2021-06-18 Safran Aircraft Engines dispositif de refroidissement amélioré d’anneau de turbine d’aéronef
FR3109406B1 (fr) * 2020-04-17 2022-10-07 Safran Aircraft Engines Dispositif de refroidissement d’un carter de turbine
US11788425B2 (en) * 2021-11-05 2023-10-17 General Electric Company Gas turbine engine with clearance control system

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US5205708A (en) * 1992-02-07 1993-04-27 General Electric Company High pressure turbine component interference fit up
FR2743603B1 (fr) * 1996-01-11 1998-02-13 Snecma Dispositif de jonction de segments d'un distributeur circulaire a un carter de turbomachine
FR2766517B1 (fr) * 1997-07-24 1999-09-03 Snecma Dispositif de ventilation d'un anneau de turbomachine
FR2780443B1 (fr) * 1998-06-25 2000-08-04 Snecma Anneau de stator de turbine haute pression d'une turbomachine
WO2000057033A1 (de) * 1999-03-24 2000-09-28 Siemens Aktiengesellschaft Abdeckelement und anordnung mit einem abdeckelement und mit einer tragstruktur
US6435820B1 (en) * 1999-08-25 2002-08-20 General Electric Company Shroud assembly having C-clip retainer

Also Published As

Publication number Publication date
CA2400151A1 (fr) 2002-07-11
US20030031557A1 (en) 2003-02-13
KR100829154B1 (ko) 2008-05-13
WO2002053876A1 (fr) 2002-07-11
JP4021768B2 (ja) 2007-12-12
KR20020075470A (ko) 2002-10-04
FR2819010A1 (fr) 2002-07-05
UA73345C2 (uk) 2005-07-15
CA2400151C (fr) 2009-10-06
DE60204489T2 (de) 2006-03-16
US6726446B2 (en) 2004-04-27
EP1225309A1 (de) 2002-07-24
JP2004517246A (ja) 2004-06-10
EP1225309B1 (de) 2005-06-08
RU2289699C2 (ru) 2006-12-20
FR2819010B1 (fr) 2004-05-28

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR