JP2003293704A5 - - Google Patents

Download PDF

Info

Publication number
JP2003293704A5
JP2003293704A5 JP2003016827A JP2003016827A JP2003293704A5 JP 2003293704 A5 JP2003293704 A5 JP 2003293704A5 JP 2003016827 A JP2003016827 A JP 2003016827A JP 2003016827 A JP2003016827 A JP 2003016827A JP 2003293704 A5 JP2003293704 A5 JP 2003293704A5
Authority
JP
Japan
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
JP2003016827A
Other versions
JP4383060B2 (ja
JP2003293704A (ja
Filing date
Publication date
Priority claimed from US10/109,014 external-priority patent/US6733235B2/en
Application filed filed Critical
Publication of JP2003293704A publication Critical patent/JP2003293704A/ja
Publication of JP2003293704A5 publication Critical patent/JP2003293704A5/ja
Application granted granted Critical
Publication of JP4383060B2 publication Critical patent/JP4383060B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

JP2003016827A 2002-03-28 2003-01-27 タービンエンジン用のシュラウドセグメント及び組立体 Expired - Lifetime JP4383060B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/109014 2002-03-28
US10/109,014 US6733235B2 (en) 2002-03-28 2002-03-28 Shroud segment and assembly for a turbine engine

Publications (3)

Publication Number Publication Date
JP2003293704A JP2003293704A (ja) 2003-10-15
JP2003293704A5 true JP2003293704A5 (ja) 2006-03-16
JP4383060B2 JP4383060B2 (ja) 2009-12-16

Family

ID=28041007

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003016827A Expired - Lifetime JP4383060B2 (ja) 2002-03-28 2003-01-27 タービンエンジン用のシュラウドセグメント及び組立体

Country Status (6)

Country Link
US (1) US6733235B2 (ja)
EP (1) EP1350927B1 (ja)
JP (1) JP4383060B2 (ja)
CA (1) CA2416399C (ja)
DE (1) DE60314032T2 (ja)
ES (1) ES2287414T3 (ja)

Families Citing this family (113)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
ES2398727T3 (es) * 2009-03-09 2013-03-21 Snecma Conjunto de anillo de turbina
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
EP2977618B1 (en) 2011-12-31 2019-10-30 Rolls-Royce Corporation Gas turbine engine with a blade track assembly and corresponding assembly method
BR112015020325A2 (pt) 2013-02-25 2017-07-18 Gen Electric suspensor de cobertura com conjunto de retentor integral
EP2971587B1 (en) 2013-03-12 2020-02-05 Rolls-Royce Corporation Turbine blade track assembly
WO2014163674A1 (en) * 2013-03-13 2014-10-09 Freeman Ted J Dovetail retention system for blade tracks
US9506356B2 (en) * 2013-03-15 2016-11-29 Rolls-Royce North American Technologies, Inc. Composite retention feature
WO2014200575A2 (en) * 2013-04-12 2014-12-18 United Technologies Corporation Gas turbine engine rapid response clearance control system with air seal segment interface
CN105612313B (zh) 2013-05-17 2017-11-21 通用电气公司 燃气涡轮机的cmc护罩支撑系统
JP6643225B2 (ja) * 2013-06-11 2020-02-12 ゼネラル・エレクトリック・カンパニイ クリアランス制御リング組立体
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
EP3155236A1 (en) 2014-06-12 2017-04-19 General Electric Company Shroud hanger assembly
JP6574208B2 (ja) 2014-06-12 2019-09-11 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
EP3155231B1 (en) 2014-06-12 2019-07-03 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
EP3040617B1 (en) * 2014-12-31 2017-12-06 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
US9945242B2 (en) * 2015-05-11 2018-04-17 General Electric Company System for thermally isolating a turbine shroud
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
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
US10196919B2 (en) 2015-06-29 2019-02-05 Rolls-Royce North American Technologies Inc. Turbine shroud segment with load distribution springs
US10047624B2 (en) * 2015-06-29 2018-08-14 Rolls-Royce North American Technologies Inc. Turbine shroud segment with flange-facing perimeter seal
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
US10138750B2 (en) 2016-03-16 2018-11-27 United Technologies Corporation Boas segmented heat shield
US10161258B2 (en) 2016-03-16 2018-12-25 United Technologies Corporation Boas rail shield
US10422240B2 (en) 2016-03-16 2019-09-24 United Technologies Corporation Turbine engine blade outer air seal with load-transmitting cover plate
US10132184B2 (en) 2016-03-16 2018-11-20 United Technologies Corporation Boas spring loaded rail shield
US10513943B2 (en) 2016-03-16 2019-12-24 United Technologies Corporation Boas enhanced heat transfer surface
US10422241B2 (en) 2016-03-16 2019-09-24 United Technologies Corporation Blade outer air seal support for a gas turbine engine
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
US10107129B2 (en) 2016-03-16 2018-10-23 United Technologies Corporation Blade outer air seal with spring centering
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
US10443616B2 (en) 2016-03-16 2019-10-15 United Technologies Corporation Blade outer air seal with centrally mounted seal arc segments
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
FR3064024B1 (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
FR3064022B1 (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
US11021990B2 (en) * 2018-12-19 2021-06-01 General Electric Company Shroud sealing for a gas turbine engine
FR3090732B1 (fr) 2018-12-19 2021-01-08 Safran Aircraft Engines Ensemble d’anneau de turbine avec flasques indexés.
FR3090731B1 (fr) 2018-12-19 2021-01-08 Safran Aircraft Engines Ensemble d’anneau de turbine à appuis rectilignes bombés.
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
US11359507B2 (en) 2019-09-26 2022-06-14 Raytheon Technologies Corporation Double box composite seal assembly with fiber density arrangement 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
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
US11230937B2 (en) 2020-05-18 2022-01-25 Rolls-Royce North American Technologies Inc. Turbine shroud assembly with dovetail retention system
US11111796B1 (en) 2020-05-18 2021-09-07 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

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3085398A (en) * 1961-01-10 1963-04-16 Gen Electric Variable-clearance shroud structure for gas turbine engines
BE792224A (fr) * 1971-12-01 1973-03-30 Penny Robert N Element composite long ayant un coefficient de dilatation lineaire effectif predetermine
GB1484936A (en) * 1974-12-07 1977-09-08 Rolls Royce Gas turbine engines
DE3019920C2 (de) * 1980-05-24 1982-12-30 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur äußeren Ummantelung der Laufschaufeln von Axialturbinen für Gasturbinentriebwerke
US5071313A (en) 1990-01-16 1991-12-10 General Electric Company Rotor blade shroud segment
US5127793A (en) 1990-05-31 1992-07-07 General Electric Company Turbine shroud clearance control assembly
US5074748A (en) 1990-07-30 1991-12-24 General Electric Company Seal assembly for segmented turbine engine structures
US5228828A (en) * 1991-02-15 1993-07-20 General Electric Company Gas turbine engine clearance control apparatus
US5480281A (en) * 1994-06-30 1996-01-02 General Electric Co. Impingement cooling apparatus for turbine shrouds having ducts of increasing cross-sectional area in the direction of post-impingement cooling flow
US5562408A (en) 1995-06-06 1996-10-08 General Electric Company Isolated turbine shroud

Similar Documents

Publication Publication Date Title
BE2021C533I2 (ja)
BE2015C007I2 (ja)
BE2014C055I2 (ja)
BE2014C027I2 (ja)
BE2014C003I2 (ja)
BE2013C075I2 (ja)
BE2013C070I2 (ja)
BE2013C067I2 (ja)
BE2013C038I2 (ja)
BE2013C036I2 (ja)
BE2011C030I2 (ja)
JP2003293704A5 (ja)
JP2003232519A5 (ja)
BE2015C005I2 (ja)
BE2012C053I2 (ja)
JP2004208319A5 (ja)
JP2003335406A5 (ja)
JP2004001391A5 (ja)
JP2004007610A5 (ja)
JP2004226057A5 (ja)
JP2004228341A5 (ja)
JP2003284685A5 (ja)
BE2015C024I2 (ja)
AU2002245368A1 (ja)
AU2002255066A1 (ja)