FR2819010B1 - Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux - Google Patents

Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux

Info

Publication number
FR2819010B1
FR2819010B1 FR0100059A FR0100059A FR2819010B1 FR 2819010 B1 FR2819010 B1 FR 2819010B1 FR 0100059 A FR0100059 A FR 0100059A FR 0100059 A FR0100059 A FR 0100059A FR 2819010 B1 FR2819010 B1 FR 2819010B1
Authority
FR
France
Prior art keywords
turbomachine
high pressure
turbine
support area
ring support
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
FR0100059A
Other languages
English (en)
Other versions
FR2819010A1 (fr
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
Priority to FR0100059A priority Critical patent/FR2819010B1/fr
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Priority to RU2002123582/06A priority patent/RU2289699C2/ru
Priority to PCT/FR2002/000011 priority patent/WO2002053876A1/fr
Priority to JP2002554361A priority patent/JP4021768B2/ja
Priority to EP02290005A priority patent/EP1225309B1/fr
Priority to US10/204,403 priority patent/US6726446B2/en
Priority to DE60204489T priority patent/DE60204489T2/de
Priority to KR1020027011546A priority patent/KR100829154B1/ko
Priority to CA002400151A priority patent/CA2400151C/fr
Priority to UA2002097182A priority patent/UA73345C2/uk
Publication of FR2819010A1 publication Critical patent/FR2819010A1/fr
Application granted granted Critical
Publication of FR2819010B1 publication Critical patent/FR2819010B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR0100059A 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 Expired - Fee Related FR2819010B1 (fr)

Priority Applications (10)

Application Number Priority Date Filing Date Title
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
CA002400151A CA2400151C (fr) 2001-01-04 2002-01-03 Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux
JP2002554361A JP4021768B2 (ja) 2001-01-04 2002-01-03 クリアランス制御を有するガスタービンエンジンの高圧タービンのステータシュラウドのステイセクタ
EP02290005A EP1225309B1 (fr) 2001-01-04 2002-01-03 Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux
US10/204,403 US6726446B2 (en) 2001-01-04 2002-01-03 Stay sector of stator shroud of the high-pressure turbine of a gas turbine engine with clearance control
DE60204489T DE60204489T2 (de) 2001-01-04 2002-01-03 Stützträger für den Statorring einer Hochdruckturbine in einer Turbomachine mit Regulierung des Spiels
RU2002123582/06A RU2289699C2 (ru) 2001-01-04 2002-01-03 Промежуточный сегмент для удерживания статорного кольца турбины высокого давления в турбомашине, выполненный с возможностью коррекции величины зазоров
PCT/FR2002/000011 WO2002053876A1 (fr) 2001-01-04 2002-01-03 Secteur d"entretoise de support d"anneau de stator de la turbine haute pression d"une turbomachine avec rattrapage de jeux
KR1020027011546A KR100829154B1 (ko) 2001-01-04 2002-01-03 틈새 보상을 가진, 터빈 엔진의 고압 터빈의 고정자 링의지지 스페이서 섹터
UA2002097182A UA73345C2 (uk) 2001-01-04 2002-03-01 Проміжний сегмент для утримання статорного кільця турбіни високого тиску в турбомашині, виконаний з можливістю корекції величини зазорів

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
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
FR2819010A1 FR2819010A1 (fr) 2002-07-05
FR2819010B1 true FR2819010B1 (fr) 2004-05-28

Family

ID=8858504

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0100059A Expired - Fee Related 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

Country Status (10)

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

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FR2816352B1 (fr) * 2000-11-09 2003-01-31 Snecma Moteurs Ensemble de ventilation d'un anneau de stator
US8641045B2 (en) * 2003-05-01 2014-02-04 Advanced Technologies Group, Inc. Seal with stacked sealing elements
US7108479B2 (en) * 2003-06-19 2006-09-19 General Electric Company Methods and apparatus for supplying cooling fluid to turbine nozzles
FI116958B (fi) * 2003-07-01 2006-04-13 Nokia Corp Hallintasolmujen määrittäminen laitteenhallintajärjestelmässä
US20050091984A1 (en) * 2003-11-03 2005-05-05 Robert Czachor Heat shield for gas turbine engine
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
US7448846B2 (en) * 2005-08-06 2008-11-11 General Electric Company Thermally compliant turbine shroud mounting
US20070249823A1 (en) * 2006-04-20 2007-10-25 Chemagis Ltd. Process for preparing gemcitabine and associated intermediates
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
FR2942845B1 (fr) * 2009-03-09 2011-04-01 Snecma Ensemble d'anneau de turbine
JP5646517B2 (ja) * 2009-03-09 2014-12-24 スネクマ タービンリング組立体
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
US10344621B2 (en) * 2012-04-27 2019-07-09 General Electric Company System and method of limiting axial movement between components in a turbine assembly
EP2997234B1 (fr) 2013-05-17 2020-05-27 General Electric Company Système de support d'anneau d'étancheité cmc d'une turbine à gaz
CN105814282B (zh) 2013-12-12 2018-06-05 通用电气公司 Cmc护罩支撑***
WO2015109292A1 (fr) * 2014-01-20 2015-07-23 United Technologies Corporation Attache de retenue pour un joint de pale étanche à l'air extérieur
JP6363232B2 (ja) 2014-06-12 2018-07-25 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
CN106460543B (zh) * 2014-06-12 2018-12-21 通用电气公司 多件式护罩悬挂器组件
CN106460542B (zh) 2014-06-12 2018-11-02 通用电气公司 护罩挂架组件
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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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
EP1163430B1 (fr) * 1999-03-24 2003-08-20 Siemens Aktiengesellschaft Element de revetement et systeme comportant un element de revetement et une structure support
US6435820B1 (en) * 1999-08-25 2002-08-20 General Electric Company Shroud assembly having C-clip retainer

Also Published As

Publication number Publication date
FR2819010A1 (fr) 2002-07-05
KR20020075470A (ko) 2002-10-04
KR100829154B1 (ko) 2008-05-13
WO2002053876A1 (fr) 2002-07-11
US6726446B2 (en) 2004-04-27
CA2400151C (fr) 2009-10-06
DE60204489T2 (de) 2006-03-16
DE60204489D1 (de) 2005-07-14
UA73345C2 (uk) 2005-07-15
US20030031557A1 (en) 2003-02-13
JP4021768B2 (ja) 2007-12-12
EP1225309A1 (fr) 2002-07-24
CA2400151A1 (fr) 2002-07-11
JP2004517246A (ja) 2004-06-10
RU2289699C2 (ru) 2006-12-20
EP1225309B1 (fr) 2005-06-08

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse

Effective date: 20070930