JPH09151705A5 - - Google Patents

Info

Publication number
JPH09151705A5
JPH09151705A5 JP1996322181A JP32218196A JPH09151705A5 JP H09151705 A5 JPH09151705 A5 JP H09151705A5 JP 1996322181 A JP1996322181 A JP 1996322181A JP 32218196 A JP32218196 A JP 32218196A JP H09151705 A5 JPH09151705 A5 JP H09151705A5
Authority
JP
Japan
Prior art keywords
interlock
face
passages
air
segment
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.)
Pending
Application number
JP1996322181A
Other languages
English (en)
Japanese (ja)
Other versions
JPH09151705A (ja
Filing date
Publication date
Priority claimed from US08/561,767 external-priority patent/US5609469A/en
Application filed filed Critical
Publication of JPH09151705A publication Critical patent/JPH09151705A/ja
Publication of JPH09151705A5 publication Critical patent/JPH09151705A5/ja
Pending legal-status Critical Current

Links

JP8322181A 1995-11-22 1996-11-19 ロータ組立体用シュラウド Pending JPH09151705A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/561,767 US5609469A (en) 1995-11-22 1995-11-22 Rotor assembly shroud
US08/561,767 1995-11-22

Publications (2)

Publication Number Publication Date
JPH09151705A JPH09151705A (ja) 1997-06-10
JPH09151705A5 true JPH09151705A5 (enExample) 2004-11-11

Family

ID=24243371

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8322181A Pending JPH09151705A (ja) 1995-11-22 1996-11-19 ロータ組立体用シュラウド

Country Status (5)

Country Link
US (1) US5609469A (enExample)
EP (1) EP0775805B1 (enExample)
JP (1) JPH09151705A (enExample)
KR (1) KR100379728B1 (enExample)
DE (1) DE69623574T2 (enExample)

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US8439629B2 (en) 2007-03-01 2013-05-14 United Technologies Corporation Blade outer air seal
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US8177492B2 (en) * 2008-03-04 2012-05-15 United Technologies Corporation Passage obstruction for improved inlet coolant filling
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US8317461B2 (en) * 2008-08-27 2012-11-27 United Technologies Corporation Gas turbine engine component having dual flow passage cooling chamber formed by single core
US8365405B2 (en) * 2008-08-27 2013-02-05 United Technologies Corp. Preforms and related methods for repairing abradable seals of gas turbine engines
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US8167546B2 (en) * 2009-09-01 2012-05-01 United Technologies Corporation Ceramic turbine shroud support
US8727695B2 (en) * 2009-12-09 2014-05-20 Rolls-Royce Corporation Chamfer-fillet gap for thermal management
US8556575B2 (en) * 2010-03-26 2013-10-15 United Technologies Corporation Blade outer seal for a gas turbine engine
US8876458B2 (en) 2011-01-25 2014-11-04 United Technologies Corporation Blade outer air seal assembly and support
US8834106B2 (en) * 2011-06-01 2014-09-16 United Technologies Corporation Seal assembly for gas turbine engine
US20130170979A1 (en) * 2012-01-04 2013-07-04 General Electric Company Double ended brush seal assembly for a compressor
US9097129B2 (en) 2012-05-31 2015-08-04 United Technologies Corporation Segmented seal with ship lap ends
US8998572B2 (en) * 2012-06-04 2015-04-07 United Technologies Corporation Blade outer air seal for a gas turbine engine
US20140064942A1 (en) * 2012-08-31 2014-03-06 General Electric Company Turbine rotor blade platform cooling
US9587504B2 (en) 2012-11-13 2017-03-07 United Technologies Corporation Carrier interlock
US9255524B2 (en) 2012-12-20 2016-02-09 United Technologies Corporation Variable outer air seal fluid control
US9371738B2 (en) 2012-12-20 2016-06-21 United Technologies Corporation Variable outer air seal support
WO2014158589A1 (en) * 2013-03-13 2014-10-02 United Technologies Corporation Multi-axial brush seal
EP2971615B1 (en) 2013-03-15 2019-06-19 United Technologies Corporation Low leakage duct segment using expansion joint assembly
WO2015088656A1 (en) 2013-12-12 2015-06-18 United Technologies Corporation Wrapped dog bone seal
US9879557B2 (en) * 2014-08-15 2018-01-30 United Technologies Corporation Inner stage turbine seal for gas turbine engine
US10329934B2 (en) 2014-12-15 2019-06-25 United Technologies Corporation Reversible flow blade outer air seal
GB201508551D0 (en) 2015-05-19 2015-07-01 Rolls Royce Plc A heat exchanger for a gas turbine engine
US9803496B2 (en) 2015-07-01 2017-10-31 United Technologies Corporation Break-in system for gapping and leakage control
EP3173587B1 (de) * 2015-11-30 2021-03-31 MTU Aero Engines GmbH Gehäuse für eine strömungsmaschine, einbausicherung und strömungsmaschine
US10202864B2 (en) * 2016-02-09 2019-02-12 United Technologies Corporation Chevron trip strip
US10801345B2 (en) 2016-02-09 2020-10-13 Raytheon Technologies Corporation Chevron trip strip
US10422241B2 (en) 2016-03-16 2019-09-24 United Technologies Corporation Blade outer air seal support for a gas turbine engine
US10337346B2 (en) 2016-03-16 2019-07-02 United Technologies Corporation Blade outer air seal with flow guide manifold
US10513943B2 (en) 2016-03-16 2019-12-24 United Technologies Corporation Boas enhanced heat transfer surface
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
US10138749B2 (en) 2016-03-16 2018-11-27 United Technologies Corporation Seal anti-rotation feature
US10563531B2 (en) 2016-03-16 2020-02-18 United Technologies Corporation Seal assembly for gas turbine engine
US10138750B2 (en) 2016-03-16 2018-11-27 United Technologies Corporation Boas segmented heat shield
US10443424B2 (en) 2016-03-16 2019-10-15 United Technologies Corporation Turbine engine blade outer air seal with load-transmitting carriage
US10422240B2 (en) 2016-03-16 2019-09-24 United Technologies Corporation Turbine engine blade outer air seal with load-transmitting cover plate
US10107129B2 (en) 2016-03-16 2018-10-23 United Technologies Corporation Blade outer air seal with spring centering
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
US20170292395A1 (en) * 2016-04-07 2017-10-12 United Technologies Corporation Integrated brush seals
US10352183B2 (en) * 2016-04-25 2019-07-16 United Technologies Corporation High temperature seal and method
CN108533722B (zh) * 2018-04-13 2023-10-20 南京高速齿轮制造有限公司 适用于齿轮箱的刷式密封结构
US10815807B2 (en) * 2018-05-31 2020-10-27 General Electric Company Shroud and seal for gas turbine engine
US10738651B2 (en) * 2018-05-31 2020-08-11 General Electric Company Shroud for gas turbine engine
US10633995B2 (en) * 2018-07-31 2020-04-28 United Technologies Corporation Sealing surface for ceramic matrix composite blade outer air seal
US10787923B2 (en) * 2018-08-27 2020-09-29 Raytheon Technologies Corporation Axially preloaded seal
US10815810B2 (en) * 2019-01-10 2020-10-27 Raytheon Technologies Corporation BOAS assemblies with axial support pins
US11015473B2 (en) * 2019-03-18 2021-05-25 Raytheon Technologies Corporation Carrier for blade outer air seal
US11255208B2 (en) 2019-05-15 2022-02-22 Raytheon Technologies Corporation Feather seal for CMC BOAS
US11773751B1 (en) 2022-11-29 2023-10-03 Rolls-Royce Corporation Ceramic matrix composite blade track segment with pin-locating threaded insert
US12031443B2 (en) 2022-11-29 2024-07-09 Rolls-Royce Corporation Ceramic matrix composite blade track segment with attachment flange cooling chambers
US11713694B1 (en) 2022-11-30 2023-08-01 Rolls-Royce Corporation Ceramic matrix composite blade track segment with two-piece carrier
US11840936B1 (en) 2022-11-30 2023-12-12 Rolls-Royce Corporation Ceramic matrix composite blade track segment with pin-locating shim kit
US11732604B1 (en) 2022-12-01 2023-08-22 Rolls-Royce Corporation Ceramic matrix composite blade track segment with integrated cooling passages
US11885225B1 (en) 2023-01-25 2024-01-30 Rolls-Royce Corporation Turbine blade track with ceramic matrix composite segments having attachment flange draft angles
US12421870B1 (en) 2024-04-30 2025-09-23 Rolls-Royce Corporation Pin mounted ceramic matrix composite heat shields with impingement cooling

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