JP2013194739A5 - - Google Patents
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- 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.)
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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 (https=) | 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 (https=) |
| EP (1) | EP2642076B1 (https=) |
| JP (1) | JP6118147B2 (https=) |
| CN (1) | CN103321687B (https=) |
| RU (1) | RU2623342C2 (https=) |
Families Citing this family (32)
| 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 |
| EP3052763B1 (en) * | 2013-09-30 | 2020-07-15 | United Technologies Corporation | A nonmetallic airfoil with a compliant attachment |
| KR20160085896A (ko) | 2013-11-25 | 2016-07-18 | 제네럴 일렉트릭 테크놀러지 게엠베하 | 터보기계를 위한 모듈러 구조에 근거한 블레이드 조립체 |
| WO2015091289A2 (en) | 2013-12-20 | 2015-06-25 | Alstom Technology Ltd | Rotor blade or guide vane assembly |
| WO2015130382A2 (en) * | 2014-02-05 | 2015-09-03 | 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 |
| EP3183429A1 (en) * | 2014-08-22 | 2017-06-28 | 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 |
| EP3649009B1 (en) * | 2017-07-07 | 2022-11-02 | 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. |
| CN115559972B (zh) * | 2022-11-03 | 2026-04-17 | 西安鑫垚陶瓷复合材料股份有限公司 | 用于金属-陶瓷基复材的连接组件、金属-陶瓷基复材构件 |
| 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 |
| CN121676056A (zh) * | 2026-02-09 | 2026-03-17 | 太行国家实验室 | 一种新型金属-cmc组合涡轮转子叶片及其设计方法 |
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|---|---|---|---|---|
| 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 (https=) * | 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 |
-
2012
- 2012-03-19 US US13/423,658 patent/US9175571B2/en active Active
-
2013
- 2013-03-13 EP EP13158942.6A patent/EP2642076B1/en active Active
- 2013-03-18 RU RU2013111943A patent/RU2623342C2/ru active
- 2013-03-18 JP JP2013054735A patent/JP6118147B2/ja active Active
- 2013-03-19 CN CN201310088260.4A patent/CN103321687B/zh active Active
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