JP2015530518A5 - - Google Patents

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Publication number
JP2015530518A5
JP2015530518A5 JP2015533672A JP2015533672A JP2015530518A5 JP 2015530518 A5 JP2015530518 A5 JP 2015530518A5 JP 2015533672 A JP2015533672 A JP 2015533672A JP 2015533672 A JP2015533672 A JP 2015533672A JP 2015530518 A5 JP2015530518 A5 JP 2015530518A5
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JP
Japan
Prior art keywords
turbine
plane
oriented
gripping means
cylindrical surface
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
JP2015533672A
Other languages
English (en)
Japanese (ja)
Other versions
JP6246814B2 (ja
JP2015530518A (ja
Filing date
Publication date
Priority claimed from FR1259175A external-priority patent/FR2996251B1/fr
Application filed filed Critical
Publication of JP2015530518A publication Critical patent/JP2015530518A/ja
Publication of JP2015530518A5 publication Critical patent/JP2015530518A5/ja
Application granted granted Critical
Publication of JP6246814B2 publication Critical patent/JP6246814B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2015533672A 2012-09-28 2013-09-26 Ｃｍｃタービンブレード用の自己固定型ファスナ Active JP6246814B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1259175A FR2996251B1 (fr) 2012-09-28 2012-09-28 Attache auto-serrante pour aube de turbine en cmc
FR1259175 2012-09-28
PCT/FR2013/052278 WO2014049280A2 (fr) 2012-09-28 2013-09-26 Attache auto-serrante pour aube de turbine en cmc

Publications (3)

Publication Number Publication Date
JP2015530518A JP2015530518A (ja) 2015-10-15
JP2015530518A5 true JP2015530518A5 (enExample) 2017-06-01
JP6246814B2 JP6246814B2 (ja) 2017-12-13

Family

ID=48237017

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015533672A Active JP6246814B2 (ja) 2012-09-28 2013-09-26 Ｃｍｃタービンブレード用の自己固定型ファスナ

Country Status (9)

Country Link
US (1) US10227881B2 (enExample)
EP (1) EP2900927B2 (enExample)
JP (1) JP6246814B2 (enExample)
CN (1) CN104685162B (enExample)
BR (1) BR112015006761B1 (enExample)
CA (1) CA2886305C (enExample)
FR (1) FR2996251B1 (enExample)
RU (1) RU2664752C2 (enExample)
WO (1) WO2014049280A2 (enExample)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10428665B2 (en) * 2015-12-11 2019-10-01 General Electric Company CMC thermal clamps
CN106968716B (zh) * 2016-11-21 2017-12-19 北京航空航天大学 陶瓷基复合材料整体涡轮叶盘
US10808560B2 (en) * 2018-06-20 2020-10-20 Rolls-Royce Corporation Turbine vane assembly with ceramic matrix composite components
US12163547B2 (en) 2021-03-18 2024-12-10 General Electric Company Ceramic matrix composite fastener
CN113623020B (zh) * 2021-08-02 2022-07-08 无锡友鹏航空装备科技有限公司 一种密封性高的涡轮导向装置

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE470026A (enExample) * 1945-12-21
NL75780C (enExample) * 1948-09-17
DE818442C (de) * 1948-10-02 1951-10-25 Maschf Augsburg Nuernberg Ag Befestigung von Schaufeln, insbesondere aus keramischen Werkstoffen, fuer Kreiselradmaschinen
US2821357A (en) † 1950-05-09 1958-01-28 Maschf Augsburg Nuernberg Ag Connection of ceramic and metallic machine parts
GB914548A (en) * 1960-03-04 1963-01-02 Daimler Benz Ag Improvements relating to wheel discs with ceramic blades for axial-flow machines
US3713752A (en) 1971-10-28 1973-01-30 United Aircraft Corp Composite blade for a gas turbine engine
JPS5573806A (en) 1978-11-24 1980-06-03 Sumitomo Metal Ind Ltd Furnace building method of blast furnace hearth part
SU821709A1 (ru) * 1979-06-25 1981-04-15 Предприятие П/Я А-1877 Замковое соединение рабочихлОпАТОК C диСКОМ ТуРбиНы
DE3028701A1 (de) * 1980-07-29 1982-02-25 AEG-Kanis Turbinenfabrik GmbH, 8500 Nürnberg Schaufelschloss fuer turbinenbeschaufelung
FR2608674B1 (fr) * 1986-12-17 1991-04-19 Snecma Roue de turbine a aubes ceramique
US5074754A (en) * 1990-04-23 1991-12-24 United Technologies Corporation Rotor blade retention system
JP3216956B2 (ja) * 1994-06-08 2001-10-09 株式会社日立製作所 ガスタービン翼固定装置
DE19826897A1 (de) 1998-06-17 1999-12-23 Abb Patent Gmbh Schloß für Laufschaufeln eines Turbinenläufers
FR2943942B1 (fr) 2009-04-06 2016-01-29 Snecma Procede de fabrication d'une aube de turbomachine en materiau composite
US8251667B2 (en) * 2009-05-20 2012-08-28 General Electric Company Low stress circumferential dovetail attachment for rotor blades
US8727730B2 (en) * 2010-04-06 2014-05-20 General Electric Company Composite turbine bucket assembly

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