US6884026B2
(en)
*
|
2002-09-30 |
2005-04-26 |
General Electric Company |
Turbine engine shroud assembly including axially floating shroud segment
|
US6808363B2
(en)
*
|
2002-12-20 |
2004-10-26 |
General Electric Company |
Shroud segment and assembly with circumferential seal at a planar segment surface
|
US6893214B2
(en)
*
|
2002-12-20 |
2005-05-17 |
General Electric Company |
Shroud segment and assembly with surface recessed seal bridging adjacent members
|
US6896484B2
(en)
*
|
2003-09-12 |
2005-05-24 |
Siemens Westinghouse Power Corporation |
Turbine engine sealing device
|
US6997673B2
(en)
*
|
2003-12-11 |
2006-02-14 |
Honeywell International, Inc. |
Gas turbine high temperature turbine blade outer air seal assembly
|
US6951112B2
(en)
*
|
2004-02-10 |
2005-10-04 |
General Electric Company |
Methods and apparatus for assembling gas turbine engines
|
US7052235B2
(en)
|
2004-06-08 |
2006-05-30 |
General Electric Company |
Turbine engine shroud segment, hanger and assembly
|
GB2416194B
(en)
*
|
2004-07-15 |
2006-08-16 |
Rolls Royce Plc |
A spacer arrangement
|
US20060078429A1
(en)
*
|
2004-10-08 |
2006-04-13 |
Darkins Toby G Jr |
Turbine engine shroud segment
|
US7387758B2
(en)
*
|
2005-02-16 |
2008-06-17 |
Siemens Power Generation, Inc. |
Tabbed ceramic article for improved interlaminar strength
|
US7494317B2
(en)
*
|
2005-06-23 |
2009-02-24 |
Siemens Energy, Inc. |
Ring seal attachment system
|
US7523616B2
(en)
*
|
2005-11-30 |
2009-04-28 |
General Electric Company |
Methods and apparatuses for assembling a gas turbine engine
|
US7637110B2
(en)
*
|
2005-11-30 |
2009-12-29 |
General Electric Company |
Methods and apparatuses for assembling a gas turbine engine
|
US7686575B2
(en)
*
|
2006-08-17 |
2010-03-30 |
Siemens Energy, Inc. |
Inner ring with independent thermal expansion for mounting gas turbine flow path components
|
US7625177B2
(en)
*
|
2006-08-31 |
2009-12-01 |
Pratt & Whitney Canada Cororation |
Simple axial retention feature for abradable members
|
US9039358B2
(en)
*
|
2007-01-03 |
2015-05-26 |
United Technologies Corporation |
Replaceable blade outer air seal design
|
FR2913717A1
(fr)
|
2007-03-15 |
2008-09-19 |
Snecma Propulsion Solide Sa |
Ensemble d'anneau de turbine pour turbine a gaz
|
US8061977B2
(en)
*
|
2007-07-03 |
2011-11-22 |
Siemens Energy, Inc. |
Ceramic matrix composite attachment apparatus and method
|
US8206092B2
(en)
*
|
2007-12-05 |
2012-06-26 |
United Technologies Corp. |
Gas turbine engines and related systems involving blade outer air seals
|
US9297335B2
(en)
*
|
2008-03-11 |
2016-03-29 |
United Technologies Corporation |
Metal injection molding attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct
|
WO2010103213A1
(fr)
*
|
2009-03-09 |
2010-09-16 |
Snecma |
Ensemble d'anneau de turbine
|
FR2952965B1
(fr)
*
|
2009-11-25 |
2012-03-09 |
Snecma |
Isolation d'un rebord circonferentiel d'un carter externe de turbomachine vis-a-vis d'un secteur d'anneau correspondant
|
JP5517742B2
(ja)
*
|
2010-05-21 |
2014-06-11 |
三菱重工業株式会社 |
分割体、これを用いたタービン分割環およびこれを備えたガスタービン
|
US8740552B2
(en)
*
|
2010-05-28 |
2014-06-03 |
General Electric Company |
Low-ductility turbine shroud and mounting apparatus
|
US8985944B2
(en)
*
|
2011-03-30 |
2015-03-24 |
General Electric Company |
Continuous ring composite turbine shroud
|
US20130004306A1
(en)
*
|
2011-06-30 |
2013-01-03 |
General Electric Company |
Chordal mounting arrangement for low-ductility turbine shroud
|
US9726043B2
(en)
|
2011-12-15 |
2017-08-08 |
General Electric Company |
Mounting apparatus for low-ductility turbine shroud
|
WO2013102171A2
(en)
|
2011-12-31 |
2013-07-04 |
Rolls-Royce Corporation |
Blade track assembly, components, and methods
|
JP6363111B2
(ja)
*
|
2013-02-25 |
2018-07-25 |
ゼネラル・エレクトリック・カンパニイ |
一体型の分割式cmcシュラウドハンガ及びリテーナシステム
|
US9759082B2
(en)
|
2013-03-12 |
2017-09-12 |
Rolls-Royce Corporation |
Turbine blade track assembly
|
US9458726B2
(en)
|
2013-03-13 |
2016-10-04 |
Rolls-Royce Corporation |
Dovetail retention system for blade tracks
|
US9506356B2
(en)
*
|
2013-03-15 |
2016-11-29 |
Rolls-Royce North American Technologies, Inc. |
Composite retention feature
|
US10370999B2
(en)
|
2013-04-12 |
2019-08-06 |
United Technologies Corporation |
Gas turbine engine rapid response clearance control system with air seal segment interface
|
WO2014186099A1
(en)
|
2013-05-17 |
2014-11-20 |
General Electric Company |
Cmc shroud support system of a gas turbine
|
US20160123172A1
(en)
|
2013-06-11 |
2016-05-05 |
General Electric Company |
Passive control of gas turbine clearances using ceramic matrix composites inserts
|
EP2835500A1
(de)
|
2013-08-09 |
2015-02-11 |
Siemens Aktiengesellschaft |
Einsatzelement und Gasturbine
|
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
|
CN106460560B
(zh)
|
2014-06-12 |
2018-11-13 |
通用电气公司 |
护罩吊架组件
|
CA2951431C
(en)
|
2014-06-12 |
2019-03-26 |
General Electric Company |
Multi-piece shroud hanger assembly
|
CA2951638A1
(en)
*
|
2014-06-12 |
2015-12-17 |
General Electric Company |
Shroud hanger assembly
|
US9945256B2
(en)
*
|
2014-06-27 |
2018-04-17 |
Rolls-Royce Corporation |
Segmented turbine shroud with seals
|
US10184356B2
(en)
*
|
2014-11-25 |
2019-01-22 |
United Technologies Corporation |
Blade outer air seal support structure
|
CA2915246A1
(en)
*
|
2014-12-23 |
2016-06-23 |
Rolls-Royce Corporation |
Turbine shroud
|
US10941942B2
(en)
|
2014-12-31 |
2021-03-09 |
Rolls-Royce North American Technologies Inc. |
Retention system for gas turbine engine assemblies
|
US9874104B2
(en)
|
2015-02-27 |
2018-01-23 |
General Electric Company |
Method and system for a ceramic matrix composite shroud hanger assembly
|
US10100649B2
(en)
*
|
2015-03-31 |
2018-10-16 |
Rolls-Royce North American Technologies Inc. |
Compliant rail hanger
|
US9845692B2
(en)
*
|
2015-05-05 |
2017-12-19 |
General Electric Company |
Turbine component connection with thermally stress-free fastener
|
US9932901B2
(en)
|
2015-05-11 |
2018-04-03 |
General Electric Company |
Shroud retention system with retention springs
|
US9828879B2
(en)
*
|
2015-05-11 |
2017-11-28 |
General Electric Company |
Shroud retention system with keyed retention clips
|
US9945242B2
(en)
*
|
2015-05-11 |
2018-04-17 |
General Electric Company |
System for thermally isolating a turbine shroud
|
FR3036435B1
(fr)
*
|
2015-05-22 |
2020-01-24 |
Safran Ceramics |
Ensemble d'anneau de turbine
|
US10221713B2
(en)
*
|
2015-05-26 |
2019-03-05 |
Rolls-Royce Corporation |
Shroud cartridge having a ceramic matrix composite seal segment
|
US10094234B2
(en)
|
2015-06-29 |
2018-10-09 |
Rolls-Royce North America Technologies Inc. |
Turbine shroud segment with buffer air seal system
|
US10047624B2
(en)
*
|
2015-06-29 |
2018-08-14 |
Rolls-Royce North American Technologies Inc. |
Turbine shroud segment with flange-facing perimeter seal
|
US10196919B2
(en)
|
2015-06-29 |
2019-02-05 |
Rolls-Royce North American Technologies Inc. |
Turbine shroud segment with load distribution springs
|
US10215056B2
(en)
|
2015-06-30 |
2019-02-26 |
Rolls-Royce Corporation |
Turbine shroud with movable attachment features
|
US10030541B2
(en)
|
2015-07-01 |
2018-07-24 |
Rolls-Royce North American Technologies Inc. |
Turbine shroud with clamped flange attachment
|
US10767863B2
(en)
|
2015-07-22 |
2020-09-08 |
Rolls-Royce North American Technologies, Inc. |
Combustor tile with monolithic inserts
|
US10443417B2
(en)
|
2015-09-18 |
2019-10-15 |
General Electric Company |
Ceramic matrix composite ring shroud retention methods-finger seals with stepped shroud interface
|
US10094244B2
(en)
|
2015-09-18 |
2018-10-09 |
General Electric Company |
Ceramic matrix composite ring shroud retention methods-wiggle strip spring seal
|
US9945257B2
(en)
*
|
2015-09-18 |
2018-04-17 |
General Electric Company |
Ceramic matrix composite ring shroud retention methods-CMC pin-head
|
US10458263B2
(en)
*
|
2015-10-12 |
2019-10-29 |
Rolls-Royce North American Technologies Inc. |
Turbine shroud with sealing features
|
US10415414B2
(en)
|
2016-03-16 |
2019-09-17 |
United Technologies Corporation |
Seal arc segment with anti-rotation feature
|
US10337346B2
(en)
|
2016-03-16 |
2019-07-02 |
United Technologies Corporation |
Blade outer air seal with flow guide manifold
|
US10443616B2
(en)
|
2016-03-16 |
2019-10-15 |
United Technologies Corporation |
Blade outer air seal with centrally mounted seal arc segments
|
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
|
US10422241B2
(en)
|
2016-03-16 |
2019-09-24 |
United Technologies Corporation |
Blade outer air seal support for a gas turbine engine
|
US10161258B2
(en)
|
2016-03-16 |
2018-12-25 |
United Technologies Corporation |
Boas rail shield
|
US10513943B2
(en)
|
2016-03-16 |
2019-12-24 |
United Technologies Corporation |
Boas enhanced heat transfer surface
|
US10138749B2
(en)
|
2016-03-16 |
2018-11-27 |
United Technologies Corporation |
Seal anti-rotation feature
|
US10443424B2
(en)
|
2016-03-16 |
2019-10-15 |
United Technologies Corporation |
Turbine engine blade outer air seal with load-transmitting carriage
|
US10138750B2
(en)
|
2016-03-16 |
2018-11-27 |
United Technologies Corporation |
Boas segmented heat shield
|
US10563531B2
(en)
*
|
2016-03-16 |
2020-02-18 |
United Technologies Corporation |
Seal assembly for gas turbine engine
|
US10132184B2
(en)
|
2016-03-16 |
2018-11-20 |
United Technologies Corporation |
Boas spring loaded rail shield
|
US20170276000A1
(en)
*
|
2016-03-24 |
2017-09-28 |
General Electric Company |
Apparatus and method for forming apparatus
|
US10458268B2
(en)
*
|
2016-04-13 |
2019-10-29 |
Rolls-Royce North American Technologies Inc. |
Turbine shroud with sealed box segments
|
FR3055147B1
(fr)
|
2016-08-19 |
2020-05-29 |
Safran Aircraft Engines |
Ensemble d'anneau de turbine
|
FR3055146B1
(fr)
|
2016-08-19 |
2020-05-29 |
Safran Aircraft Engines |
Ensemble d'anneau de turbine
|
FR3055148B1
(fr)
|
2016-08-19 |
2020-06-05 |
Safran Aircraft Engines |
Ensemble d'anneau de turbine
|
US10577970B2
(en)
|
2016-09-13 |
2020-03-03 |
Rolls-Royce North American Technologies Inc. |
Turbine assembly with ceramic matrix composite blade track and actively cooled metallic carrier
|
US10697314B2
(en)
*
|
2016-10-14 |
2020-06-30 |
Rolls-Royce Corporation |
Turbine shroud with I-beam construction
|
US10577951B2
(en)
|
2016-11-30 |
2020-03-03 |
Rolls-Royce North American Technologies Inc. |
Gas turbine engine with dovetail connection having contoured root
|
US11225880B1
(en)
|
2017-02-22 |
2022-01-18 |
Rolls-Royce Corporation |
Turbine shroud ring for a gas turbine engine having a tip clearance probe
|
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
|
US10480337B2
(en)
|
2017-04-18 |
2019-11-19 |
Rolls-Royce North American Technologies Inc. |
Turbine shroud assembly with multi-piece seals
|
US10704407B2
(en)
|
2017-04-21 |
2020-07-07 |
Rolls-Royce High Temperature Composites Inc. |
Ceramic matrix composite blade track segments
|
US10801349B2
(en)
|
2017-08-25 |
2020-10-13 |
Raytheon Technologies Corporation |
Ceramic matrix composite blade outer air seal
|
US10557365B2
(en)
|
2017-10-05 |
2020-02-11 |
Rolls-Royce Corporation |
Ceramic matrix composite blade track with mounting system having reaction load distribution features
|
FR3076578B1
(fr)
|
2018-01-09 |
2020-01-31 |
Safran Aircraft Engines |
Ensemble d'anneau de turbine
|
US11035243B2
(en)
|
2018-06-01 |
2021-06-15 |
Raytheon Technologies Corporation |
Seal assembly for gas turbine engines
|
US10907487B2
(en)
|
2018-10-16 |
2021-02-02 |
Honeywell International Inc. |
Turbine shroud assemblies for gas turbine engines
|
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.
|
US11021990B2
(en)
*
|
2018-12-19 |
2021-06-01 |
General Electric Company |
Shroud sealing for a gas turbine engine
|
FR3091550B1
(fr)
|
2019-01-08 |
2021-01-22 |
Safran Aircraft Engines |
Procédé de montage et de démontage d’un ensemble d’anneau de turbine
|
US11761343B2
(en)
|
2019-03-13 |
2023-09-19 |
Rtx Corporation |
BOAS carrier with dovetail attachments
|
US11015485B2
(en)
|
2019-04-17 |
2021-05-25 |
Rolls-Royce Corporation |
Seal ring for turbine shroud in gas turbine engine with arch-style support
|
US11352897B2
(en)
|
2019-09-26 |
2022-06-07 |
Raytheon Technologies Corporation |
Double box composite seal assembly for gas turbine engine
|
US11220924B2
(en)
|
2019-09-26 |
2022-01-11 |
Raytheon Technologies Corporation |
Double box composite seal assembly with insert for gas turbine engine
|
US11359507B2
(en)
|
2019-09-26 |
2022-06-14 |
Raytheon Technologies Corporation |
Double box composite seal assembly with fiber density arrangement for gas turbine engine
|
US11149563B2
(en)
|
2019-10-04 |
2021-10-19 |
Rolls-Royce Corporation |
Ceramic matrix composite blade track with mounting system having axial reaction load distribution features
|
US11053817B2
(en)
*
|
2019-11-19 |
2021-07-06 |
Rolls-Royce Corporation |
Turbine shroud assembly with ceramic matrix composite blade track segments and full hoop carrier
|
FR3106152B1
(fr)
|
2020-01-09 |
2022-01-21 |
Safran Aircraft Engines |
Ensemble d’anneau de turbine avec flasques indexés
|
US11111796B1
(en)
|
2020-05-18 |
2021-09-07 |
Rolls-Royce North American Technologies Inc. |
Turbine shroud assembly with dovetail retention system
|
US11230937B2
(en)
|
2020-05-18 |
2022-01-25 |
Rolls-Royce North American Technologies Inc. |
Turbine shroud assembly with dovetail retention system
|
US11873762B2
(en)
|
2020-06-16 |
2024-01-16 |
Rolls-Royce Corporation |
High temperature heat shield assemblies
|
KR102316629B1
(ko)
|
2020-06-23 |
2021-10-25 |
두산중공업 주식회사 |
터빈 블레이드 팁 간극 제어장치 및 이를 포함하는 가스 터빈
|
US11674403B2
(en)
|
2021-03-29 |
2023-06-13 |
General Electric Company |
Annular shroud assembly
|
FR3122210A1
(fr)
|
2021-04-21 |
2022-10-28 |
Safran Aircraft Engines |
Ensemble d’anneau de turbine monté sur entretoise
|
FR3123943B1
(fr)
|
2021-06-14 |
2024-01-26 |
Safran Aircraft Engines |
Ensemble d’anneau de turbine monté sur entretoise
|