JP2008169844A5 - - Google Patents

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Publication number
JP2008169844A5
JP2008169844A5 JP2008003923A JP2008003923A JP2008169844A5 JP 2008169844 A5 JP2008169844 A5 JP 2008169844A5 JP 2008003923 A JP2008003923 A JP 2008003923A JP 2008003923 A JP2008003923 A JP 2008003923A JP 2008169844 A5 JP2008169844 A5 JP 2008169844A5
Authority
JP
Japan
Prior art keywords
composite
epoxy resin
fiber reinforced
reinforced epoxy
airfoil
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
JP2008003923A
Other languages
English (en)
Japanese (ja)
Other versions
JP2008169844A (ja
Filing date
Publication date
Priority claimed from US11/652,473 external-priority patent/US7753653B2/en
Application filed filed Critical
Publication of JP2008169844A publication Critical patent/JP2008169844A/ja
Publication of JP2008169844A5 publication Critical patent/JP2008169844A5/ja
Ceased legal-status Critical Current

Links

JP2008003923A 2007-01-12 2008-01-11 複合材入口案内翼 Ceased JP2008169844A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/652,473 US7753653B2 (en) 2007-01-12 2007-01-12 Composite inlet guide vane

Publications (2)

Publication Number Publication Date
JP2008169844A JP2008169844A (ja) 2008-07-24
JP2008169844A5 true JP2008169844A5 (cg-RX-API-DMAC7.html) 2011-02-24

Family

ID=39247270

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008003923A Ceased JP2008169844A (ja) 2007-01-12 2008-01-11 複合材入口案内翼

Country Status (4)

Country Link
US (1) US7753653B2 (cg-RX-API-DMAC7.html)
EP (1) EP1947346B1 (cg-RX-API-DMAC7.html)
JP (1) JP2008169844A (cg-RX-API-DMAC7.html)
CN (1) CN101220818B (cg-RX-API-DMAC7.html)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1788197A1 (de) * 2005-11-21 2007-05-23 Siemens Aktiengesellschaft Turbinenschaufel für eine Dampfturbine
JP5192318B2 (ja) * 2007-09-28 2013-05-08 本田技研工業株式会社 整流部材ユニット及びその製造方法
DE102008058786A1 (de) * 2008-11-24 2010-05-27 Rolls-Royce Deutschland Ltd & Co Kg Hybrides Bauteil für ein Gasturbinentriebwerk
US8550776B2 (en) * 2010-07-28 2013-10-08 General Electric Company Composite vane mounting
US9429029B2 (en) 2010-09-30 2016-08-30 Pratt & Whitney Canada Corp. Gas turbine blade and method of protecting same
US20120082541A1 (en) * 2010-09-30 2012-04-05 Enzo Macchia Gas turbine engine casing
US20120082553A1 (en) * 2010-09-30 2012-04-05 Andreas Eleftheriou Metal encapsulated stator vane
US9587645B2 (en) 2010-09-30 2017-03-07 Pratt & Whitney Canada Corp. Airfoil blade
US20120082556A1 (en) * 2010-09-30 2012-04-05 Enzo Macchia Nanocrystalline metal coated composite airfoil
US9556742B2 (en) * 2010-11-29 2017-01-31 United Technologies Corporation Composite airfoil and turbine engine
US8690531B2 (en) 2010-12-30 2014-04-08 General Electroc Co. Vane with spar mounted composite airfoil
US8727721B2 (en) 2010-12-30 2014-05-20 General Electric Company Vane with spar mounted composite airfoil
FR2975734B1 (fr) * 2011-05-27 2013-05-31 Snecma Procede de renforcement d'une piece mecanique de turbomachine
CA2783854A1 (en) * 2011-07-28 2013-01-28 United Hydro Services, Llc Resurfaced wicket gate and methods
FR2983519B1 (fr) * 2011-12-01 2015-07-24 Snecma Propulsion Solide Aube de turbine a pale creuse en materiau composite, turbine ou compresseur ayant un distributeur ou redresseur forme de telles aubes et turbomachine les comprenant
US9427835B2 (en) 2012-02-29 2016-08-30 Pratt & Whitney Canada Corp. Nano-metal coated vane component for gas turbine engines and method of manufacturing same
US9115584B2 (en) * 2012-04-24 2015-08-25 General Electric Company Resistive band for turbomachine blade
US9322283B2 (en) 2012-09-28 2016-04-26 United Technologies Corporation Airfoil with galvanic corrosion preventive shim
US9335296B2 (en) 2012-10-10 2016-05-10 Westinghouse Electric Company Llc Systems and methods for steam generator tube analysis for detection of tube degradation
US9863366B2 (en) * 2013-03-13 2018-01-09 Rolls-Royce North American Technologies Inc. Exhaust nozzle apparatus and method for multi stream aircraft engine
EP3022396B1 (en) * 2013-07-15 2019-12-04 United Technologies Corporation Vibration-damped composite airfoils and manufacture methods
JP6392027B2 (ja) 2013-08-30 2018-09-19 株式会社東芝 タービン翼
FR3014964B1 (fr) * 2013-12-13 2018-09-28 Safran Aircraft Engines Redresseur a calage variable en materiaux composites
WO2016030608A1 (fr) * 2014-08-26 2016-03-03 Snecma Aube de redresseur en matériau composite à brides de fixation décalées pour moteur à turbine à gaz
US10589475B2 (en) * 2014-09-23 2020-03-17 General Electric Company Braided blades and vanes having dovetail roots
CN105587688A (zh) * 2014-10-20 2016-05-18 北京航天动力研究所 一种新型离心泵压出室结构
ES2797733T3 (es) * 2016-03-16 2020-12-03 MTU Aero Engines AG Paleta guía ajustable para turbina, turbina y método de fabricación
JP6630989B2 (ja) * 2016-03-25 2020-01-15 三菱重工エンジン＆ターボチャージャ株式会社 繊維強化部材のめっき方法
US11009036B2 (en) 2018-08-30 2021-05-18 Raytheon Technologies Corporation Fan blade having closed metal sheath
US11935662B2 (en) 2019-07-02 2024-03-19 Westinghouse Electric Company Llc Elongate SiC fuel elements
KR102523509B1 (ko) 2019-09-19 2023-04-18 웨스팅하우스 일렉트릭 컴퍼니 엘엘씨 콜드 스프레이 침착물의 현장 접착 테스트를 수행하기 위한 장치 및 사용 방법
DE102020119914A1 (de) * 2020-07-28 2022-02-03 KSB SE & Co. KGaA Gehäuse für strömungsführende Bauteile
US11352891B2 (en) 2020-10-19 2022-06-07 Pratt & Whitney Canada Corp. Method for manufacturing a composite guide vane having a metallic leading edge
US20240352862A1 (en) * 2023-04-21 2024-10-24 General Electric Company Airfoil assembly with a trunnion and spar

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3572971A (en) * 1969-09-29 1971-03-30 Gen Electric Lightweight turbo-machinery blading
US3600103A (en) * 1969-10-06 1971-08-17 United Aircraft Corp Composite blade
US3762835A (en) * 1971-07-02 1973-10-02 Gen Electric Foreign object damage protection for compressor blades and other structures and related methods
US3887297A (en) * 1974-06-25 1975-06-03 United Aircraft Corp Variable leading edge stator vane assembly
US4006999A (en) 1975-07-17 1977-02-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Leading edge protection for composite blades
US4022540A (en) 1975-10-02 1977-05-10 General Electric Company Frangible airfoil structure
US4594761A (en) * 1984-02-13 1986-06-17 General Electric Company Method of fabricating hollow composite airfoils
US5098797B1 (en) 1990-04-30 1997-07-01 Gen Electric Steel articles having protective duplex coatings and method of production
US5260099A (en) * 1990-04-30 1993-11-09 General Electric Company Method of making a gas turbine blade having a duplex coating
US5486096A (en) * 1994-06-30 1996-01-23 United Technologies Corporation Erosion resistant surface protection
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
DE19627860C1 (de) 1996-07-11 1998-01-08 Mtu Muenchen Gmbh Schaufel für Strömungsmaschine mit metallischer Deckschicht
GB2391270B (en) 2002-07-26 2006-03-08 Rolls Royce Plc Turbomachine blade
US7121727B2 (en) 2002-12-24 2006-10-17 General Electric Company Inlet guide vane bushing having extended life expectancy
DE10307610A1 (de) * 2003-02-22 2004-09-02 Rolls-Royce Deutschland Ltd & Co Kg Verdichterschaufel für ein Flugzeugtriebwerk
JP4860941B2 (ja) * 2005-04-27 2012-01-25 本田技研工業株式会社 整流部材ユニット及びその製造方法

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