JPH09112206A5 - - Google Patents

Info

Publication number
JPH09112206A5
JPH09112206A5 JP1996297854A JP29785496A JPH09112206A5 JP H09112206 A5 JPH09112206 A5 JP H09112206A5 JP 1996297854 A JP1996297854 A JP 1996297854A JP 29785496 A JP29785496 A JP 29785496A JP H09112206 A5 JPH09112206 A5 JP H09112206A5
Authority
JP
Japan
Prior art keywords
shroud
thermal
spring
radial surface
cantilevers
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
JP1996297854A
Other languages
English (en)
Japanese (ja)
Other versions
JPH09112206A (ja
JP3965607B2 (ja
Filing date
Publication date
Priority claimed from US08/546,631 external-priority patent/US5639210A/en
Application filed filed Critical
Publication of JPH09112206A publication Critical patent/JPH09112206A/ja
Publication of JPH09112206A5 publication Critical patent/JPH09112206A5/ja
Application granted granted Critical
Publication of JP3965607B2 publication Critical patent/JP3965607B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

JP29785496A 1995-10-23 1996-10-23 ロータ組立体用シュラウド Expired - Fee Related JP3965607B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/546,631 US5639210A (en) 1995-10-23 1995-10-23 Rotor blade outer tip seal apparatus
US08/546,631 1995-10-23

Publications (3)

Publication Number Publication Date
JPH09112206A JPH09112206A (ja) 1997-04-28
JPH09112206A5 true JPH09112206A5 (enExample) 2004-10-21
JP3965607B2 JP3965607B2 (ja) 2007-08-29

Family

ID=24181306

Family Applications (1)

Application Number Title Priority Date Filing Date
JP29785496A Expired - Fee Related JP3965607B2 (ja) 1995-10-23 1996-10-23 ロータ組立体用シュラウド

Country Status (5)

Country Link
US (1) US5639210A (enExample)
EP (1) EP0770761B1 (enExample)
JP (1) JP3965607B2 (enExample)
KR (1) KR100405881B1 (enExample)
DE (1) DE69634869T2 (enExample)

Families Citing this family (71)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5791872A (en) * 1997-04-22 1998-08-11 Rolls-Royce Inc. Blade tip clearence control apparatus
US5846048A (en) * 1997-05-22 1998-12-08 Mitsubishi Heavy Industries, Ltd. Gas turbine stationary blade unit
US6402466B1 (en) * 2000-05-16 2002-06-11 General Electric Company Leaf seal for gas turbine stator shrouds and a nozzle band
US6409471B1 (en) * 2001-02-16 2002-06-25 General Electric Company Shroud assembly and method of machining same
US6877952B2 (en) * 2002-09-09 2005-04-12 Florida Turbine Technologies, Inc Passive clearance control
EP1599949A1 (en) * 2003-02-27 2005-11-30 Mi-Kyung Oh A monitoring system of the inner state of tires and a method for operating the system
EP1707749B1 (en) * 2005-03-28 2012-02-22 United Technologies Corporation Blade outer seal assembly
US7721433B2 (en) * 2005-03-28 2010-05-25 United Technologies Corporation Blade outer seal assembly
US20090096174A1 (en) * 2007-02-28 2009-04-16 United Technologies Corporation Blade outer air seal for a gas turbine engine
DE102007031711A1 (de) * 2007-07-06 2009-01-08 Rolls-Royce Deutschland Ltd & Co Kg Gehäusedeckbandsegment-Aufhängung
US8308428B2 (en) 2007-10-09 2012-11-13 United Technologies Corporation Seal assembly retention feature and assembly method
US8240980B1 (en) 2007-10-19 2012-08-14 Florida Turbine Technologies, Inc. Turbine inter-stage gap cooling and sealing arrangement
US8439639B2 (en) * 2008-02-24 2013-05-14 United Technologies Corporation Filter system for blade outer air seal
US8585357B2 (en) * 2009-08-18 2013-11-19 Pratt & Whitney Canada Corp. Blade outer air seal support
US20120177484A1 (en) * 2011-01-07 2012-07-12 General Electric Company Elliptical Sealing System
US8876484B2 (en) 2011-08-05 2014-11-04 Hamilton Sundstrand Corporation Turbine blade pocket pin stress relief
US9726043B2 (en) 2011-12-15 2017-08-08 General Electric Company Mounting apparatus for low-ductility turbine shroud
US20130170979A1 (en) * 2012-01-04 2013-07-04 General Electric Company Double ended brush seal assembly for a compressor
US9228447B2 (en) * 2012-02-14 2016-01-05 United Technologies Corporation Adjustable blade outer air seal apparatus
EP2634373A1 (en) * 2012-02-28 2013-09-04 Siemens Aktiengesellschaft Arrangement for a turbomachine
US9885368B2 (en) 2012-05-24 2018-02-06 Carrier Corporation Stall margin enhancement of axial fan with rotating shroud
US9200530B2 (en) 2012-07-20 2015-12-01 United Technologies Corporation Radial position control of case supported structure
WO2014186015A2 (en) * 2013-03-11 2014-11-20 United Technologies Corporation Actuator for gas turbine engine blade outer air seal
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
EP3030755B1 (en) * 2013-08-07 2022-04-20 Raytheon Technologies Corporation Clearance control assembly with specific assembly of a clearance control ring
FR3009579B1 (fr) * 2013-08-07 2015-09-25 Snecma Carter de turbine en deux materiaux
EP3055514B1 (en) * 2013-10-07 2020-04-08 United Technologies Corporation Gas turbine engine blade outer air seal thermal control system
JP5889266B2 (ja) * 2013-11-14 2016-03-22 三菱重工業株式会社 タービン
US9266618B2 (en) 2013-11-18 2016-02-23 Honeywell International Inc. Gas turbine engine turbine blade tip active clearance control system and method
US10323535B2 (en) * 2013-12-10 2019-06-18 United Technologies Corporation Blade tip clearance systems
JP6529013B2 (ja) 2013-12-12 2019-06-12 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
US9945248B2 (en) 2014-04-01 2018-04-17 United Technologies Corporation Vented tangential on-board injector for a gas turbine engine
EP2949873A1 (en) 2014-05-27 2015-12-02 Siemens Aktiengesellschaft Turbomachine with an ingestion shield and use of the turbomachine
US10465558B2 (en) 2014-06-12 2019-11-05 General Electric Company Multi-piece shroud hanger assembly
US10400619B2 (en) 2014-06-12 2019-09-03 General Electric Company Shroud hanger assembly
WO2015191169A1 (en) 2014-06-12 2015-12-17 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
FR3045717B1 (fr) * 2015-12-22 2020-07-03 Safran Aircraft Engines Dispositif de pilotage de jeu en sommets d'aubes rotatives de turbine
US10422241B2 (en) 2016-03-16 2019-09-24 United Technologies Corporation Blade outer air seal support for a gas turbine engine
US10138750B2 (en) * 2016-03-16 2018-11-27 United Technologies Corporation Boas segmented heat shield
US10107129B2 (en) 2016-03-16 2018-10-23 United Technologies Corporation Blade outer air seal with spring centering
US10422240B2 (en) 2016-03-16 2019-09-24 United Technologies Corporation Turbine engine blade outer air seal with load-transmitting cover plate
US10161258B2 (en) 2016-03-16 2018-12-25 United Technologies Corporation Boas rail shield
US10415414B2 (en) 2016-03-16 2019-09-17 United Technologies Corporation Seal arc segment with anti-rotation feature
US10513943B2 (en) 2016-03-16 2019-12-24 United Technologies Corporation Boas enhanced heat transfer surface
US10132184B2 (en) 2016-03-16 2018-11-20 United Technologies Corporation Boas spring loaded rail shield
US10443616B2 (en) 2016-03-16 2019-10-15 United Technologies Corporation Blade outer air seal with centrally mounted seal arc segments
US10337346B2 (en) 2016-03-16 2019-07-02 United Technologies Corporation Blade outer air seal with flow guide manifold
US10443424B2 (en) 2016-03-16 2019-10-15 United Technologies Corporation Turbine engine blade outer air seal with load-transmitting carriage
US10563531B2 (en) 2016-03-16 2020-02-18 United Technologies Corporation Seal assembly for gas turbine engine
US10138749B2 (en) 2016-03-16 2018-11-27 United Technologies Corporation Seal anti-rotation feature
US10344612B2 (en) * 2017-01-13 2019-07-09 United Technologies Corporation Compact advanced passive tip clearance control
FR3062169B1 (fr) * 2017-01-20 2019-04-19 Safran Aircraft Engines Carter de module de turbomachine d'aeronef, comprenant un caloduc associe a un anneau d'etancheite entourant une roue mobile aubagee du module
US10450957B2 (en) * 2017-01-23 2019-10-22 United Technologies Corporation Gas turbine engine with heat pipe system
US20190218928A1 (en) * 2018-01-17 2019-07-18 United Technologies Corporation Blade outer air seal for gas turbine engine
US10704408B2 (en) * 2018-05-03 2020-07-07 Rolls-Royce North American Technologies Inc. Dual response blade track system
DE102018210599A1 (de) 2018-06-28 2020-01-02 MTU Aero Engines AG Strömungsmaschinenbauteilanordnung
FR3086323B1 (fr) * 2018-09-24 2020-12-11 Safran Aircraft Engines Carter interne de turmomachine a isolation thermique amelioree
US11215056B2 (en) * 2020-04-09 2022-01-04 Raytheon Technologies Corporation Thermally isolated rotor systems and methods
US11220928B1 (en) * 2020-08-24 2022-01-11 Rolls-Royce Corporation Turbine shroud assembly with ceramic matrix composite components and cooling features
US12188359B2 (en) * 2022-09-30 2025-01-07 Rtx Corporation Blade outer air seal with retainer ring
US12006829B1 (en) 2023-02-16 2024-06-11 General Electric Company Seal member support system for a gas turbine engine
US12486779B2 (en) 2023-03-08 2025-12-02 General Electric Company Seal support assembly for a turbine engine
US12116896B1 (en) 2023-03-24 2024-10-15 General Electric Company Seal support assembly for a turbine engine
US12372002B2 (en) 2023-03-24 2025-07-29 General Electric Company Seal support assembly for a turbine engine
US12416243B2 (en) 2023-03-24 2025-09-16 General Electric Company Seal support assembly for a turbine engine
US12215587B2 (en) 2023-03-24 2025-02-04 General Electric Company Seal support assembly for a turbine engine
US12421861B2 (en) 2023-03-24 2025-09-23 General Electric Company Seal support assembly for a turbine engine
US12241375B2 (en) 2023-03-24 2025-03-04 General Electric Company Seal support assembly for a turbine engine
US12215588B2 (en) 2023-03-27 2025-02-04 General Electric Company Seal assembly for a gas turbine engine
US12326089B2 (en) 2023-04-24 2025-06-10 General Electric Company Seal assembly for a gas turbine engine

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB216737A (en) * 1923-08-02 1924-06-05 Karl Baumann Improvements relating to elastic fluid turbines
DE518106C (de) * 1924-02-18 1931-02-24 Jan Kieswetter Einrichtung zum Ausgleich verschiedener Waermeausdehnungen zwischen einer aeusseren Gehaeusewand und einer Zwischenwand des gleichen Gehaeuses, insbesondere bei Dampf- oder Gasturbinen
US2634090A (en) * 1950-07-28 1953-04-07 Westinghouse Electric Corp Turbine apparatus
GB1484936A (en) * 1974-12-07 1977-09-08 Rolls Royce Gas turbine engines
GB1484288A (en) * 1975-12-03 1977-09-01 Rolls Royce Gas turbine engines
US4177004A (en) * 1977-10-31 1979-12-04 General Electric Company Combined turbine shroud and vane support structure
GB2047354B (en) * 1979-04-26 1983-03-30 Rolls Royce Gas turbine engines
DE3018621C2 (de) * 1980-05-16 1982-06-03 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Außengehäuse für Axialverdichter oder -turbinen von Strömungsmaschinen, insbesondere Gasturbinentriebwerken
GB2087979B (en) * 1980-11-22 1984-02-22 Rolls Royce Gas turbine engine blade tip seal
GB2257754B (en) * 1983-02-26 1993-09-29 Rolls Royce Improvements in or relating to axial flow gas turbines
JPS59218307A (ja) * 1983-05-26 1984-12-08 Hitachi Ltd ガスタ−ビンのケ−シング
FR2548733B1 (fr) * 1983-07-07 1987-07-10 Snecma Dispositif d'etancheite d'aubages mobiles de turbomachine
FR2574473B1 (fr) * 1984-11-22 1987-03-20 Snecma Anneau de turbine pour une turbomachine a gaz
FR2577281B1 (fr) * 1985-02-13 1987-03-20 Snecma Carter de turbomachine associe a un dispositif pour ajuster le jeu entre aubes mobiles et carter
GB2206651B (en) * 1987-07-01 1991-05-08 Rolls Royce Plc Turbine blade shroud structure
GB8903000D0 (en) * 1989-02-10 1989-03-30 Rolls Royce Plc A blade tip clearance control arrangement for a gas turbine engine
GB2236147B (en) * 1989-08-24 1993-05-12 Rolls Royce Plc Gas turbine engine with turbine tip clearance control device and method of operation
US5104287A (en) * 1989-09-08 1992-04-14 General Electric Company Blade tip clearance control apparatus for a gas turbine engine
US5116199A (en) * 1990-12-20 1992-05-26 General Electric Company Blade tip clearance control apparatus using shroud segment annular support ring thermal expansion
US5080557A (en) * 1991-01-14 1992-01-14 General Motors Corporation Turbine blade shroud assembly
US5228828A (en) * 1991-02-15 1993-07-20 General Electric Company Gas turbine engine clearance control apparatus
US5167487A (en) * 1991-03-11 1992-12-01 General Electric Company Cooled shroud support
US5154575A (en) * 1991-07-01 1992-10-13 United Technologies Corporation Thermal blade tip clearance control for gas turbine engines
US5205115A (en) * 1991-11-04 1993-04-27 General Electric Company Gas turbine engine case counterflow thermal control
GB9210642D0 (en) * 1992-05-19 1992-07-08 Rolls Royce Plc Rotor shroud assembly
US5261228A (en) * 1992-06-25 1993-11-16 General Electric Company Apparatus for bleeding air

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