JP2016512584A5 - - Google Patents

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Publication number
JP2016512584A5
JP2016512584A5 JP2015558867A JP2015558867A JP2016512584A5 JP 2016512584 A5 JP2016512584 A5 JP 2016512584A5 JP 2015558867 A JP2015558867 A JP 2015558867A JP 2015558867 A JP2015558867 A JP 2015558867A JP 2016512584 A5 JP2016512584 A5 JP 2016512584A5
Authority
JP
Japan
Prior art keywords
section
turbine blade
composite
insert
hybrid turbine
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.)
Ceased
Application number
JP2015558867A
Other languages
English (en)
Japanese (ja)
Other versions
JP2016512584A (ja
Filing date
Publication date
Priority claimed from US13/774,581 external-priority patent/US9309772B2/en
Application filed filed Critical
Publication of JP2016512584A publication Critical patent/JP2016512584A/ja
Publication of JP2016512584A5 publication Critical patent/JP2016512584A5/ja
Ceased legal-status Critical Current

Links

JP2015558867A 2013-02-22 2014-02-11 複数の挿入体セクションを含むハイブリッドタービンブレード Ceased JP2016512584A (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/774,581 US9309772B2 (en) 2013-02-22 2013-02-22 Hybrid turbine blade including multiple insert sections
US13/774,581 2013-02-22
PCT/US2014/015767 WO2014130292A1 (en) 2013-02-22 2014-02-11 Hybrid turbine blade including multiple insert sections

Publications (2)

Publication Number Publication Date
JP2016512584A JP2016512584A (ja) 2016-04-28
JP2016512584A5 true JP2016512584A5 (enExample) 2017-03-16

Family

ID=50156974

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015558867A Ceased JP2016512584A (ja) 2013-02-22 2014-02-11 複数の挿入体セクションを含むハイブリッドタービンブレード

Country Status (7)

Country Link
US (1) US9309772B2 (enExample)
EP (1) EP2959112A1 (enExample)
JP (1) JP2016512584A (enExample)
CN (1) CN105008670B (enExample)
BR (1) BR112015018959A2 (enExample)
CA (1) CA2901235A1 (enExample)
WO (1) WO2014130292A1 (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014150364A1 (en) * 2013-03-15 2014-09-25 United Technologies Corporation Turbine engine hybrid rotor
US10196140B2 (en) 2016-04-12 2019-02-05 Sikorsky Aircraft Corporation Methods for separating rotor blade cuffs from rotor blade bodies
CN106282602B (zh) * 2016-08-23 2018-06-26 西安超码科技有限公司 一种铝熔体净化用分段式炭陶复合材料转子及其制备方法
CN106367615B (zh) * 2016-08-23 2018-05-29 西安超码科技有限公司 一种铝熔体净化用整体式炭陶复合材料转子及其制备方法
CN106762813B (zh) * 2017-03-31 2019-09-17 中国航发商用航空发动机有限责任公司 一种风扇叶片
US10934626B2 (en) * 2017-04-21 2021-03-02 General Electric Company Segmented environmental barrier coating systems and methods of forming the same
JP6800805B2 (ja) * 2017-05-08 2020-12-16 三菱重工業株式会社 複合材翼及び複合材翼の製造方法
EP3406424B1 (en) * 2017-05-22 2021-04-28 Ratier-Figeac SAS Aircraft blade and methods of forming and repairing an aircraft blade
US10677068B2 (en) * 2018-01-18 2020-06-09 Raytheon Technologies Corporation Fan blade with filled pocket
US11242866B2 (en) * 2018-08-01 2022-02-08 General Electric Company Casing having a non-axisymmetric composite wall
FR3085417B1 (fr) * 2018-08-29 2020-12-04 Safran Aircraft Engines Aube comprenant une structure en materiau composite et procede de fabrication associe
MX2021004858A (es) * 2018-11-01 2021-05-12 Gen Electric Metodo de instalacion y retencion de un buje en un perno de bloqueo de una union de aspa de rotor.
US11590746B2 (en) 2019-07-18 2023-02-28 The Boeing Company Elimination of surfacing film and primer from composite substrates
US12070770B2 (en) * 2019-07-18 2024-08-27 The Boeing Company Composite coatings having improved UV and paint stripping resistivity and methods for making same

Family Cites Families (20)

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Publication number Priority date Publication date Assignee Title
US3762835A (en) * 1971-07-02 1973-10-02 Gen Electric Foreign object damage protection for compressor blades and other structures and related methods
US4784575A (en) 1986-11-19 1988-11-15 General Electric Company Counterrotating aircraft propulsor blades
CA2042218A1 (en) 1990-07-20 1992-01-21 Jan C. Schilling Composite airfoil with increased shear capability
US5269658A (en) 1990-12-24 1993-12-14 United Technologies Corporation Composite blade with partial length spar
US5129787A (en) * 1991-02-13 1992-07-14 United Technologies Corporation Lightweight propulsor blade with internal spars and rigid base members
US5222297A (en) 1991-10-18 1993-06-29 United Technologies Corporation Composite blade manufacture
US5720597A (en) * 1996-01-29 1998-02-24 General Electric Company Multi-component blade for a gas turbine
JPH1054204A (ja) * 1996-05-20 1998-02-24 General Electric Co <Ge> ガスタービン用の多構成部翼
US6676080B2 (en) 2000-07-19 2004-01-13 Aero Composites, Inc. Composite airfoil assembly
US6607358B2 (en) 2002-01-08 2003-08-19 General Electric Company Multi-component hybrid turbine blade
CN100353030C (zh) 2003-04-19 2007-12-05 通用电气公司 多组件混合式涡轮叶片
US7575417B2 (en) * 2003-09-05 2009-08-18 General Electric Company Reinforced fan blade
US7334997B2 (en) 2005-09-16 2008-02-26 General Electric Company Hybrid blisk
GB2443482A (en) 2006-11-02 2008-05-07 Smiths Group Plc Propeller blade retention
FR2921099B1 (fr) * 2007-09-13 2013-12-06 Snecma Dispositif d'amortissement pour aube en materiau composite
DE102009036018A1 (de) * 2009-08-04 2011-02-17 Siemens Aktiengesellschaft Thermoplastendstufenschaufel
FR2954271B1 (fr) * 2009-12-21 2012-02-17 Snecma Pale d'helice d'aeronef
FR2962175B1 (fr) 2010-07-02 2012-08-10 Snecma Aube a longeron composite integre
GB2484107A (en) 2010-09-29 2012-04-04 Nenuphar Modular wind turbine blade for a vertical axis wind turbine
GB2484109A (en) 2010-09-29 2012-04-04 Nenuphar Vertical axis wind turbine having modular blades with support arm at joint

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