JPS59153903A - タービンエンジンの動翼の密封装置 - Google Patents

タービンエンジンの動翼の密封装置

Info

Publication number
JPS59153903A
JPS59153903A JP59022706A JP2270684A JPS59153903A JP S59153903 A JPS59153903 A JP S59153903A JP 59022706 A JP59022706 A JP 59022706A JP 2270684 A JP2270684 A JP 2270684A JP S59153903 A JPS59153903 A JP S59153903A
Authority
JP
Japan
Prior art keywords
ring
radial
turbine
metal ring
ceramic
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.)
Granted
Application number
JP59022706A
Other languages
English (en)
Japanese (ja)
Other versions
JPH022442B2 (en:Method
Inventor
ジエラール・マルセル・フランソワ・マンデ
マルセル・ロベール・ソリニイ
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.)
NASHIONARU DECHIYUUDO E DO CON
NASHIONARU DECHIYUUDO E DO KONSUTORIYUKUSHION DE MOTOORU DABIASHION SOC
Original Assignee
NASHIONARU DECHIYUUDO E DO CON
NASHIONARU DECHIYUUDO E DO KONSUTORIYUKUSHION DE MOTOORU DABIASHION SOC
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 NASHIONARU DECHIYUUDO E DO CON, NASHIONARU DECHIYUUDO E DO KONSUTORIYUKUSHION DE MOTOORU DABIASHION SOC filed Critical NASHIONARU DECHIYUUDO E DO CON
Publication of JPS59153903A publication Critical patent/JPS59153903A/ja
Publication of JPH022442B2 publication Critical patent/JPH022442B2/ja
Granted 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
JP59022706A 1983-02-10 1984-02-09 タービンエンジンの動翼の密封装置 Granted JPS59153903A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8302101 1983-02-10
FR8302101A FR2540939A1 (fr) 1983-02-10 1983-02-10 Anneau d'etancheite pour un rotor de turbine d'une turbomachine et installation de turbomachine munie de tels anneaux

Publications (2)

Publication Number Publication Date
JPS59153903A true JPS59153903A (ja) 1984-09-01
JPH022442B2 JPH022442B2 (en:Method) 1990-01-18

Family

ID=9285777

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59022706A Granted JPS59153903A (ja) 1983-02-10 1984-02-09 タービンエンジンの動翼の密封装置

Country Status (5)

Country Link
US (1) US4596116A (en:Method)
EP (1) EP0119881B1 (en:Method)
JP (1) JPS59153903A (en:Method)
DE (1) DE3461319D1 (en:Method)
FR (1) FR2540939A1 (en:Method)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61132706A (ja) * 1984-11-30 1986-06-20 Toshiba Corp タ−ビンのシ−ル部間隙調整装置
JPS61135905A (ja) * 1984-11-22 1986-06-23 ソシエテ・ナシオナル・デテユード・エ・ドウ・コンストリユクシオン・ドウ・モトール・ダヴイアシオン、“エス．エヌ．ウ．セ．エム．アー．” ガスタービン用タービンリング部材
JPS61145303A (ja) * 1984-12-17 1986-07-03 ユナイテツド・テクノロジーズ・コーポレイシヨン 回転機械の改良された冷却可能なステータ組立体
JP2008303874A (ja) * 2007-05-30 2008-12-18 General Electric Co <Ge> 傾斜シールを有するシュラウド構成
JP2009168022A (ja) * 2008-01-11 2009-07-30 Snecma ２つのエンクロージャ間の連通を確立するためのバルブを備えたガスタービンエンジン
JP2012519803A (ja) * 2009-03-09 2012-08-30 スネクマ タービンリング組立体
WO2012132787A1 (ja) * 2011-03-30 2012-10-04 三菱重工業株式会社 ガスタービン
JP2013015138A (ja) * 2011-06-30 2013-01-24 General Electric Co <Ge> 低延性タービンシュラウド用弦状取り付け配置
JP2014177937A (ja) * 2013-03-14 2014-09-25 General Electric Co <Ge> 冷却ユニットを有するタービン・エンジン用ケーシング
JP2015505588A (ja) * 2012-01-26 2015-02-23 アルストム テクノロジー リミテッドＡＬＳＴＯＭ Ｔｅｃｈｎｏｌｏｇｙ Ｌｔｄ ターボ機械用のセグメント化された内環を備えるステータ構成部材
JP2017524088A (ja) * 2014-06-12 2017-08-24 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
JP2017524089A (ja) * 2014-06-12 2017-08-24 ゼネラル・エレクトリック・カンパニイ シュラウドハンガ組立体
JP2017150488A (ja) * 2016-02-26 2017-08-31 ゼネラル・エレクトリック・カンパニイ タービンシュラウドの密封冷却
JP2018520292A (ja) * 2015-05-22 2018-07-26 サフラン エアークラフト エンジンズ フランジによって支持されるタービンリングアセンブリ

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FR2580033A1 (en) * 1985-04-03 1986-10-10 Snecma Elastically suspended turbine ring for a turbine machine
FR2597921A1 (fr) * 1986-04-24 1987-10-30 Snecma Anneau de turbine sectorise
US4752184A (en) * 1986-05-12 1988-06-21 The United States Of America As Represented By The Secretary Of The Air Force Self-locking outer air seal with full backside cooling
FR2614073B1 (fr) * 1987-04-15 1992-02-14 Snecma Dispositif d'ajustement en temps reel du jeu radial entre un rotor et un stator de turbomachine
DE3830762C2 (de) * 1988-09-09 1994-08-18 Mtu Muenchen Gmbh Einrichtung zur Halterung eines Mantelringes in Gasturbinen
US5048288A (en) * 1988-12-20 1991-09-17 United Technologies Corporation Combined turbine stator cooling and turbine tip clearance control
GB8907706D0 (en) * 1989-04-05 1989-05-17 Rolls Royce Plc An axial flow compressor
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US5154575A (en) * 1991-07-01 1992-10-13 United Technologies Corporation Thermal blade tip clearance control for gas turbine engines
US5238365A (en) * 1991-07-09 1993-08-24 General Electric Company Assembly for thermal shielding of low pressure turbine
US5188507A (en) * 1991-11-27 1993-02-23 General Electric Company Low-pressure turbine shroud
FR2688539A1 (fr) * 1992-03-11 1993-09-17 Snecma Stator de turbomachine comprenant des dispositifs de reglage de jeu entre le stator et les aubes du rotor.
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US6190127B1 (en) * 1998-12-22 2001-02-20 General Electric Co. Tuning thermal mismatch between turbine rotor parts with a thermal medium
US6155780A (en) * 1999-08-13 2000-12-05 Capstone Turbine Corporation Ceramic radial flow turbine heat shield with turbine tip seal
JP2002309903A (ja) * 2001-04-10 2002-10-23 Mitsubishi Heavy Ind Ltd ガスタービンの蒸気配管構造
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US6925814B2 (en) * 2003-04-30 2005-08-09 Pratt & Whitney Canada Corp. Hybrid turbine tip clearance control system
US20040219011A1 (en) * 2003-05-02 2004-11-04 General Electric Company High pressure turbine elastic clearance control system and method
US6931859B2 (en) * 2003-12-17 2005-08-23 Honeywell International Inc. Variable turbine cooling flow system
US7293953B2 (en) * 2005-11-15 2007-11-13 General Electric Company Integrated turbine sealing air and active clearance control system and method
US8528339B2 (en) 2007-04-05 2013-09-10 Siemens Energy, Inc. Stacked laminate gas turbine component
FR2925939A1 (fr) * 2007-12-28 2009-07-03 Alstom Power Hydraulique Sa Machine hydraulique, installation de conversion d'energie comprenant une telle machine et procede d'ajustement d'une telle machine
US8568091B2 (en) * 2008-02-18 2013-10-29 United Technologies Corporation Gas turbine engine systems and methods involving blade outer air seals
US8047763B2 (en) * 2008-10-30 2011-11-01 General Electric Company Asymmetrical gas turbine cooling port locations
US8534995B2 (en) * 2009-03-05 2013-09-17 United Technologies Corporation Turbine engine sealing arrangement
FR2942845B1 (fr) * 2009-03-09 2011-04-01 Snecma Ensemble d'anneau de turbine
US8684674B2 (en) * 2010-10-29 2014-04-01 General Electric Company Anti-rotation shroud for turbine engines
US8790067B2 (en) * 2011-04-27 2014-07-29 United Technologies Corporation Blade clearance control using high-CTE and low-CTE ring members
US20130084160A1 (en) * 2011-09-30 2013-04-04 General Electric Company Turbine Shroud Impingement System with Bellows
US9726043B2 (en) 2011-12-15 2017-08-08 General Electric Company Mounting apparatus for low-ductility turbine shroud
US9169739B2 (en) * 2012-01-04 2015-10-27 United Technologies Corporation Hybrid blade outer air seal for gas turbine engine
US9541008B2 (en) * 2012-02-06 2017-01-10 General Electric Company Method and apparatus to control part-load performance of a turbine
US9200530B2 (en) 2012-07-20 2015-12-01 United Technologies Corporation Radial position control of case supported structure
US10072520B2 (en) 2013-02-18 2018-09-11 United Technologies Corporation Acoustic treatment to mitigate fan noise
US9598974B2 (en) 2013-02-25 2017-03-21 Pratt & Whitney Canada Corp. Active turbine or compressor tip clearance control
JP6114878B2 (ja) 2013-05-17 2017-04-12 ゼネラル・エレクトリック・カンパニイ Ｃｍｃシュラウド支持システム
CN105814282B (zh) 2013-12-12 2018-06-05 通用电气公司 Cmc护罩支撑系统
EP3102794B1 (en) * 2014-01-27 2019-12-18 United Technologies Corporation Blade outer air seal mount
US10400619B2 (en) 2014-06-12 2019-09-03 General Electric Company Shroud hanger assembly
EP3155236A1 (en) 2014-06-12 2017-04-19 General Electric Company Shroud hanger assembly
US9874104B2 (en) 2015-02-27 2018-01-23 General Electric Company Method and system for a ceramic matrix composite shroud hanger assembly
CA2924866A1 (en) * 2015-04-29 2016-10-29 Daniel K. Vetters Composite keystoned blade track
FR3036432B1 (fr) * 2015-05-22 2019-04-19 Safran Ceramics Ensemble d'anneau de turbine avec maintien axial
FR3045716B1 (fr) * 2015-12-18 2018-01-26 Safran Aircraft Engines Ensemble d'anneau de turbine avec maintien elastique a froid
FR3045717B1 (fr) * 2015-12-22 2020-07-03 Safran Aircraft Engines Dispositif de pilotage de jeu en sommets d'aubes rotatives de turbine
US10125788B2 (en) * 2016-01-08 2018-11-13 General Electric Company Ceramic tile fan blade containment
US10422241B2 (en) * 2016-03-16 2019-09-24 United Technologies Corporation Blade outer air seal support for a gas turbine engine
EP3228826B1 (de) * 2016-04-05 2021-03-17 MTU Aero Engines GmbH Dichtungssegmentanordnung mit steckverbindung, zugehörige gasturbine und herstellungsverfahren
US10428673B2 (en) 2016-05-02 2019-10-01 General Electric Company Aspirating face seal assembly and a method of operating the same
FR3055148B1 (fr) 2016-08-19 2020-06-05 Safran Aircraft Engines Ensemble d'anneau de turbine
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US10654577B2 (en) 2017-02-22 2020-05-19 General Electric Company Rainbow flowpath low pressure turbine rotor assembly
US11421627B2 (en) 2017-02-22 2022-08-23 General Electric Company Aircraft and direct drive engine under wing installation
FR3064022B1 (fr) * 2017-03-16 2019-09-13 Safran Aircraft Engines Ensemble d'anneau de turbine
FR3064023B1 (fr) * 2017-03-16 2019-09-13 Safran Aircraft Engines Ensemble d'anneau de turbine
FR3064024B1 (fr) 2017-03-16 2019-09-13 Safran Aircraft Engines Ensemble d'anneau de turbine
US10794214B2 (en) * 2017-05-08 2020-10-06 United Technologies Corporation Tip clearance control for gas turbine engine
US10815814B2 (en) * 2017-05-08 2020-10-27 Raytheon Technologies Corporation Re-use and modulated cooling from tip clearance control system for gas turbine engine
GB201712025D0 (en) * 2017-07-26 2017-09-06 Rolls Royce Plc Gas turbine engine
FR3076578B1 (fr) 2018-01-09 2020-01-31 Safran Aircraft Engines Ensemble d'anneau de turbine
FR3082872B1 (fr) * 2018-06-25 2021-06-04 Safran Aircraft Engines Dispositif de refroidissement d'un carter de turbomachine
FR3090731B1 (fr) 2018-12-19 2021-01-08 Safran Aircraft Engines Ensemble d’anneau de turbine à appuis rectilignes bombés.
FR3090732B1 (fr) 2018-12-19 2021-01-08 Safran Aircraft Engines Ensemble d’anneau de turbine avec flasques indexés.
FR3091550B1 (fr) 2019-01-08 2021-01-22 Safran Aircraft Engines Procédé de montage et de démontage d’un ensemble d’anneau de turbine
US10989059B2 (en) 2019-04-10 2021-04-27 Raytheon Technologies Corporation CMC BOAS arrangement
FR3106152B1 (fr) 2020-01-09 2022-01-21 Safran Aircraft Engines Ensemble d’anneau de turbine avec flasques indexés
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
FR3122210B1 (fr) 2021-04-21 2025-04-25 Safran Aircraft Engines Ensemble d’anneau de turbine monté sur entretoise
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CN116085068A (zh) * 2021-11-05 2023-05-09 通用电气公司 具有间隙控制系统的燃气涡轮发动机
US12338738B2 (en) * 2022-07-05 2025-06-24 General Electric Company Variable flowpath casings for blade tip clearance control
US12012859B2 (en) 2022-07-11 2024-06-18 General Electric Company Variable flowpath casings for blade tip clearance control
US11808157B1 (en) 2022-07-13 2023-11-07 General Electric Company Variable flowpath casings for blade tip clearance control
FR3141717A1 (fr) * 2022-11-08 2024-05-10 Safran Aircraft Engines anneau de turbine comportant une couche à haute résistance
US12320258B2 (en) * 2022-11-18 2025-06-03 Rtx Corporation Blade outer air seal with large radius of curvature mount hooks
FR3146706A1 (fr) 2023-03-13 2024-09-20 Safran Aircraft Engines Ensemble d’anneau de turbine à pions axiaux améliorés
FR3147317A1 (fr) 2023-03-29 2024-10-04 Safran Aircraft Engines Ensemble d’anneau de turbine avec une tôle d’étanchéité
FR3147318A1 (fr) 2023-03-29 2024-10-04 Safran Aircraft Engines Ensemble d’anneau de turbine avec une tôle d’étanchéité
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JPS55117011A (en) * 1979-02-28 1980-09-09 Mtu Muenchen Gmbh Device for minimizing blade tip clearance of axiallflow turbine and keeping said clearance constant
JPS5818502A (ja) * 1981-07-11 1983-02-03 ロ−ルス・ロイス・リミテツド ガス・タ−ビン機関用のシュラウド構造

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Cited By (18)

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Publication number Priority date Publication date Assignee Title
JPS61135905A (ja) * 1984-11-22 1986-06-23 ソシエテ・ナシオナル・デテユード・エ・ドウ・コンストリユクシオン・ドウ・モトール・ダヴイアシオン、“エス．エヌ．ウ．セ．エム．アー．” ガスタービン用タービンリング部材
JPS61132706A (ja) * 1984-11-30 1986-06-20 Toshiba Corp タ−ビンのシ−ル部間隙調整装置
JPS61145303A (ja) * 1984-12-17 1986-07-03 ユナイテツド・テクノロジーズ・コーポレイシヨン 回転機械の改良された冷却可能なステータ組立体
JP2008303874A (ja) * 2007-05-30 2008-12-18 General Electric Co <Ge> 傾斜シールを有するシュラウド構成
JP2009168022A (ja) * 2008-01-11 2009-07-30 Snecma ２つのエンクロージャ間の連通を確立するためのバルブを備えたガスタービンエンジン
JP2012519803A (ja) * 2009-03-09 2012-08-30 スネクマ タービンリング組立体
US9689272B2 (en) 2011-03-30 2017-06-27 Mitsubishi Heavy Industries, Ltd. Gas turbine and outer shroud
WO2012132787A1 (ja) * 2011-03-30 2012-10-04 三菱重工業株式会社 ガスタービン
JP2013015138A (ja) * 2011-06-30 2013-01-24 General Electric Co <Ge> 低延性タービンシュラウド用弦状取り付け配置
JP2015505588A (ja) * 2012-01-26 2015-02-23 アルストム テクノロジー リミテッドＡＬＳＴＯＭ Ｔｅｃｈｎｏｌｏｇｙ Ｌｔｄ ターボ機械用のセグメント化された内環を備えるステータ構成部材
JP2014177937A (ja) * 2013-03-14 2014-09-25 General Electric Co <Ge> 冷却ユニットを有するタービン・エンジン用ケーシング
JP2017524088A (ja) * 2014-06-12 2017-08-24 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
JP2017524089A (ja) * 2014-06-12 2017-08-24 ゼネラル・エレクトリック・カンパニイ シュラウドハンガ組立体
US11215081B2 (en) 2014-06-12 2022-01-04 General Electric Company Shroud hanger assembly
US11879349B2 (en) 2014-06-12 2024-01-23 General Electric Company Shroud hanger assembly
US12196099B2 (en) 2014-06-12 2025-01-14 General Electric Company Shroud hanger assembly
JP2018520292A (ja) * 2015-05-22 2018-07-26 サフラン エアークラフト エンジンズ フランジによって支持されるタービンリングアセンブリ
JP2017150488A (ja) * 2016-02-26 2017-08-31 ゼネラル・エレクトリック・カンパニイ タービンシュラウドの密封冷却

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US4596116A (en) 1986-06-24
FR2540939A1 (fr) 1984-08-17
JPH022442B2 (en:Method) 1990-01-18
EP0119881B1 (fr) 1986-11-12
EP0119881A1 (fr) 1984-09-26
FR2540939B1 (en:Method) 1985-03-22
DE3461319D1 (en) 1987-01-02

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