JP2013194739A5 - - Google Patents

Download PDF

Info

Publication number
JP2013194739A5
JP2013194739A5 JP2013054735A JP2013054735A JP2013194739A5 JP 2013194739 A5 JP2013194739 A5 JP 2013194739A5 JP 2013054735 A JP2013054735 A JP 2013054735A JP 2013054735 A JP2013054735 A JP 2013054735A JP 2013194739 A5 JP2013194739 A5 JP 2013194739A5
Authority
JP
Japan
Prior art keywords
thermal expansion
component
coefficient
aperture
metal
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
JP2013054735A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013194739A (ja
JP6118147B2 (ja
Filing date
Publication date
Priority claimed from US13/423,658 external-priority patent/US9175571B2/en
Application filed filed Critical
Publication of JP2013194739A publication Critical patent/JP2013194739A/ja
Publication of JP2013194739A5 publication Critical patent/JP2013194739A5/ja
Application granted granted Critical
Publication of JP6118147B2 publication Critical patent/JP6118147B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2013054735A 2012-03-19 2013-03-18 金属構成要素及びｃｍｃ構成要素のための接続システム、タービンブレード保持システム、並びに回転構成要素保持システム Active JP6118147B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/423,658 US9175571B2 (en) 2012-03-19 2012-03-19 Connecting system for metal components and CMC components, a turbine blade retaining system and a rotating component retaining system
US13/423,658 2012-03-19

Publications (3)

Publication Number Publication Date
JP2013194739A JP2013194739A (ja) 2013-09-30
JP2013194739A5 true JP2013194739A5 (enExample) 2016-04-28
JP6118147B2 JP6118147B2 (ja) 2017-04-19

Family

ID=47915443

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013054735A Active JP6118147B2 (ja) 2012-03-19 2013-03-18 金属構成要素及びｃｍｃ構成要素のための接続システム、タービンブレード保持システム、並びに回転構成要素保持システム

Country Status (5)

Country Link
US (1) US9175571B2 (enExample)
EP (1) EP2642076B1 (enExample)
JP (1) JP6118147B2 (enExample)
CN (1) CN103321687B (enExample)
RU (1) RU2623342C2 (enExample)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2990462B1 (fr) * 2012-05-14 2014-05-30 Snecma Dispositif d'attache d'aubes sur un disque de rotor de turbomachine
US9470092B2 (en) * 2013-01-02 2016-10-18 General Electric Company System and method for attaching a rotating blade in a turbine
US10280769B2 (en) * 2013-09-30 2019-05-07 United Technologies Corporation Nonmetallic airfoil with a compliant attachment
JP2017500473A (ja) 2013-11-25 2017-01-05 ゼネラル エレクトリック テクノロジー ゲゼルシャフト ミット ベシュレンクテル ハフツングＧｅｎｅｒａｌ Ｅｌｅｃｔｒｉｃ Ｔｅｃｈｎｏｌｏｇｙ ＧｍｂＨ ターボ機械用のモジュール構造に基づくブレードアセンブリ
US20170002661A1 (en) 2013-12-20 2017-01-05 General Electric Technology Gmbh Rotor blade or guide vane assembly
EP3105447A4 (en) * 2014-02-05 2017-12-13 United Technologies Corporation Disposable fan platform fairing
US9932831B2 (en) 2014-05-09 2018-04-03 United Technologies Corporation High temperature compliant metallic elements for low contact stress ceramic support
US10267156B2 (en) * 2014-05-29 2019-04-23 General Electric Company Turbine bucket assembly and turbine system
WO2016028306A1 (en) * 2014-08-22 2016-02-25 Siemens Energy, Inc. Modular turbine blade with separate platform support system
US10280768B2 (en) 2014-11-12 2019-05-07 Rolls-Royce North American Technologies Inc. Turbine blisk including ceramic matrix composite blades and methods of manufacture
US9909430B2 (en) * 2014-11-13 2018-03-06 Rolls-Royce North American Technologies Inc. Turbine disk assembly including seperable platforms for blade attachment
CA2915234A1 (en) 2015-01-13 2016-07-13 Rolls-Royce Corporation Turbine wheel with clamped blade attachment
GB201514139D0 (en) * 2015-08-11 2015-09-23 Rolls Royce Plc A datum feature for a composite component
AT518289B1 (de) * 2016-02-18 2018-06-15 Andritz Hydro Gmbh Peltonrad
US20180051880A1 (en) * 2016-08-18 2018-02-22 General Electric Company Combustor assembly for a turbine engine
US10294954B2 (en) 2016-11-09 2019-05-21 Rolls-Royce North American Technologies Inc. Composite blisk
US10577951B2 (en) 2016-11-30 2020-03-03 Rolls-Royce North American Technologies Inc. Gas turbine engine with dovetail connection having contoured root
US10563665B2 (en) 2017-01-30 2020-02-18 Rolls-Royce North American Technologies, Inc. Turbomachine stage and method of making same
CN106738497A (zh) * 2017-03-14 2017-05-31 青岛金科模具有限公司 花纹块及轮胎模具
CA3069310A1 (en) * 2017-07-07 2019-01-10 Magna Seating Inc. Pressure sensing system and seat cushion having the pressure sensing system
US10619514B2 (en) 2017-10-18 2020-04-14 Rolls-Royce Corporation Ceramic matrix composite assembly with compliant pin attachment features
US11802486B2 (en) 2017-11-13 2023-10-31 General Electric Company CMC component and fabrication using mechanical joints
WO2019108203A1 (en) * 2017-11-30 2019-06-06 Siemens Aktiengesellschaft Hybrid ceramic matrix composite components with intermediate cushion structure
US10801350B2 (en) * 2018-02-23 2020-10-13 Rolls-Royce Corporation Actively cooled engine assembly with ceramic matrix composite components
US11046620B2 (en) 2018-10-18 2021-06-29 Rolls-Royce Corporation Method of processing a ceramic matrix composite (CMC) component
US10752556B2 (en) * 2018-10-18 2020-08-25 Rolls-Royce High Temperature Composites Inc. Method of processing a ceramic matrix composite (CMC) component
US20220003202A1 (en) * 2018-11-01 2022-01-06 General Electric Company Wind turbine rotor blade joint constructed of dissimilar materials
FR3098542B1 (fr) * 2019-07-10 2023-11-24 Safran Ceram Ensemble de pièces de turbomachine
IT202100029963A1 (it) 2021-11-26 2023-05-26 Ge Avio Srl Motore a turbina a gas comprendente un complesso di pale rotanti.
CN116900247B (zh) * 2023-09-14 2023-12-05 中国航发北京航空材料研究院 陶瓷基复合材料与单晶高温合金复合构件的制备方法

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3923422A (en) * 1974-10-17 1975-12-02 United Technologies Corp Taper lining for composite blade root attachment
US4084922A (en) 1976-12-27 1978-04-18 Electric Power Research Institute, Inc. Turbine rotor with pin mounted ceramic turbine blades
US4273824A (en) * 1979-05-11 1981-06-16 United Technologies Corporation Ceramic faced structures and methods for manufacture thereof
JPS5748320U (enExample) * 1980-09-04 1982-03-18
DE3110096C2 (de) 1981-03-16 1983-05-19 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Turbinenlaufschaufel für Gasturbinentriebwerke
JP2924163B2 (ja) * 1990-10-31 1999-07-26 いすゞ自動車株式会社 ピストン及びその製造方法
US5240377A (en) 1992-02-25 1993-08-31 Williams International Corporation Composite fan blade
FR2697284B1 (fr) * 1992-10-27 1995-01-27 Europ Propulsion Procédé de fabrication d'une roue de turbine à aubes insérées et roue obtenue par le procédé.
DE4237031C1 (de) 1992-11-03 1994-02-10 Mtu Muenchen Gmbh Verstellbare Leitschaufel
FR2699497B1 (fr) * 1992-12-23 1995-03-10 Eurocopter France Dispositif de liaison pale-moyeu à attache feuilletée, pale de rotor munie d'une telle attache, et rotor équipé de telles pales.
US5405245A (en) 1993-11-29 1995-04-11 Solar Turbines Incorporated Ceramic blade attachment system
US5580219A (en) * 1995-03-06 1996-12-03 Solar Turbines Incorporated Ceramic blade attachment system
US5593275A (en) 1995-08-01 1997-01-14 General Electric Company Variable stator vane mounting and vane actuation system for an axial flow compressor of a gas turbine engine
US5735673A (en) 1996-12-04 1998-04-07 United Technologies Corporation Turbine engine rotor blade pair
US6086327A (en) 1999-01-20 2000-07-11 Mack Plastics Corporation Bushing for a jet engine vane
KR20010049364A (ko) 1999-06-14 2001-06-15 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹 시일 조립체
US6213719B1 (en) * 1999-07-28 2001-04-10 United Technologies Corporation Bar wedge preload apparatus for a propeller blade
US6431781B1 (en) 2000-06-15 2002-08-13 Honeywell International, Inc. Ceramic to metal joint assembly
US6670021B2 (en) 2001-11-14 2003-12-30 General Electric Company Monolithic ceramic attachment bushing incorporated into a ceramic matrix composite component and related method
US6725787B2 (en) 2002-03-11 2004-04-27 Weyerhaeuser Company Refractory vessel and lining therefor
GB2392477A (en) 2002-08-24 2004-03-03 Alstom Turbocharger
US6878246B2 (en) 2003-04-02 2005-04-12 Alcoa, Inc. Nickel foam pin connections for inert anodes
JP3858096B2 (ja) * 2003-07-09 2006-12-13 独立行政法人産業技術総合研究所 金属又はセラミックス含有発泡焼結体の製造方法
DE10358888B4 (de) 2003-12-16 2018-12-27 Schaeffler Technologies AG & Co. KG Brennkraftmaschine mit einer hydraulischen Vorrichtung zur Drehwinkelverstellung einer Nockenwelle gegenüber einer Kurbelwelle
DE10359730A1 (de) 2003-12-19 2005-07-14 Mtu Aero Engines Gmbh Turbomaschine, insbesondere Gasturbine
JP4731920B2 (ja) 2005-01-20 2011-07-27 本田技研工業株式会社 ロータ
US7563071B2 (en) 2005-08-04 2009-07-21 Siemens Energy, Inc. Pin-loaded mounting apparatus for a refractory component in a combustion turbine engine
US7523616B2 (en) 2005-11-30 2009-04-28 General Electric Company Methods and apparatuses for assembling a gas turbine engine
US7445427B2 (en) 2005-12-05 2008-11-04 General Electric Company Variable stator vane assembly and bushing thereof
US20090068008A1 (en) 2007-09-07 2009-03-12 Shimadzu Corporation Fastening structure and rotary vacuum pump
US8534989B2 (en) 2010-01-19 2013-09-17 Honeywell International Inc. Multi-piece turbocharger bearing

Similar Documents

Publication Publication Date Title
JP2013194739A5 (enExample)
RU2013111943A (ru) Система соединения металлических компонентов и кмкм-компонентов, система фиксации турбиной лопатки и система вращающегося компонента
JP2014521213A5 (enExample)
JP2017534766A5 (enExample)
TW200730715A (en) Fluid transfer controllers having a rotor assembly with multiple sets of rotor blades arranged in proximity and about the same hub component and further having barrier components configured to form passages for routing fluid through the multiple sets of
JP2009007981A5 (enExample)
WO2015002729A3 (en) Cell stabilization
Singh et al. Heatlines and thermal management analysis for natural convection within inclined porous square cavities
JP2009052554A5 (enExample)
JP2013044328A5 (enExample)
JP2012515773A5 (enExample)
WO2014099067A3 (en) Aluminum brazing of hollow titanium fan blades
JP2011127185A5 (enExample)
WO2014175940A3 (en) Gas turbine engine component manufacturing method and core for making same
CN106471248A8 (zh) 具有安装到塔架的热交换结构的风轮机
WO2018144171A3 (en) Method and system for phase change material component cooling
JP2017128606A5 (enExample)
WO2010006591A3 (de) Gasturbine und verfahren zum ändern der aerodynamischen gestalt einer gasturbinenschaufel
JP2013194713A5 (ja) 被冷却構造部材、タービン翼、及びタービン
WO2014197060A3 (en) Structural braze repair of superalloy component
JP2018087551A5 (enExample)
JP2020015505A5 (enExample)
JP2017502191A5 (enExample)
Cruzado et al. Wind tunnel studies of cantilever traffic signal structures
JP2007515644A5 (enExample)