JP2008169844A - 複合材入口案内翼 - Google Patents

複合材入口案内翼 Download PDF

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Publication number
JP2008169844A
JP2008169844A JP2008003923A JP2008003923A JP2008169844A JP 2008169844 A JP2008169844 A JP 2008169844A JP 2008003923 A JP2008003923 A JP 2008003923A JP 2008003923 A JP2008003923 A JP 2008003923A JP 2008169844 A JP2008169844 A JP 2008169844A
Authority
JP
Japan
Prior art keywords
composite
epoxy resin
fiber reinforced
airfoil
reinforced epoxy
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
JP2008169844A5 (enExample
Inventor
Ronald Cairo
ロナルド・カイロ
Jianqiang Chen
ジャンチアン・チェン
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2008169844A publication Critical patent/JP2008169844A/ja
Publication of JP2008169844A5 publication Critical patent/JP2008169844A5/ja
Ceased legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2253/00—Other material characteristics; Treatment of material
    • F05C2253/04—Composite, e.g. fibre-reinforced
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/90—Coating; Surface treatment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/95—Preventing corrosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/12—Light metals
    • F05D2300/121—Aluminium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6034—Orientation of fibres, weaving, ply angle

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
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 true JP2008169844A (ja) 2008-07-24
JP2008169844A5 JP2008169844A5 (enExample) 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 (enExample)
EP (1) EP1947346B1 (enExample)
JP (1) JP2008169844A (enExample)
CN (1) CN101220818B (enExample)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009085212A (ja) * 2007-09-28 2009-04-23 Honda Motor Co Ltd 整流部材ユニット及びその製造方法
WO2015029444A1 (ja) 2013-08-30 2015-03-05 株式会社 東芝 耐エロージョン性材料およびタービン翼
JPWO2017163408A1 (ja) * 2016-03-25 2019-01-31 三菱重工エンジン＆ターボチャージャ株式会社 めっき層付き繊維強化部材、及び繊維強化部材のめっき方法
JP2023535830A (ja) * 2020-07-28 2023-08-21 カーエスベー ソシエタス ヨーロピア ウント コンパニー コマンディート ゲゼルシャフト アウフ アクチェン 流導コンポーネント用ハウジング

Families Citing this family (30)

* 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
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
US20120082553A1 (en) * 2010-09-30 2012-04-05 Andreas Eleftheriou Metal encapsulated stator vane
US9429029B2 (en) 2010-09-30 2016-08-30 Pratt & Whitney Canada Corp. Gas turbine blade and method of protecting same
US9587645B2 (en) 2010-09-30 2017-03-07 Pratt & Whitney Canada Corp. Airfoil blade
US20120082541A1 (en) * 2010-09-30 2012-04-05 Enzo Macchia Gas turbine engine casing
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
WO2015009425A1 (en) * 2013-07-15 2015-01-22 United Technologies Corporation Vibration-damped composite airfoils and manufacture methods
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
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
JP7440621B2 (ja) 2019-09-19 2024-02-28 ウェスティングハウス エレクトリック カンパニー エルエルシー コールドスプレー堆積物のその場付着試験を行うための装置及びその使用方法
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

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1073002A (ja) * 1996-07-11 1998-03-17 Mtu Motoren & Turbinen Union Muenchen Gmbh 流体流装置用羽根及びその製造方法並びに修理方法
JP2006307698A (ja) * 2005-04-27 2006-11-09 Honda Motor Co Ltd 整流部材ユニット及びその製造方法

Family Cites Families (14)

* 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
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1073002A (ja) * 1996-07-11 1998-03-17 Mtu Motoren & Turbinen Union Muenchen Gmbh 流体流装置用羽根及びその製造方法並びに修理方法
JP2006307698A (ja) * 2005-04-27 2006-11-09 Honda Motor Co Ltd 整流部材ユニット及びその製造方法

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009085212A (ja) * 2007-09-28 2009-04-23 Honda Motor Co Ltd 整流部材ユニット及びその製造方法
WO2015029444A1 (ja) 2013-08-30 2015-03-05 株式会社 東芝 耐エロージョン性材料およびタービン翼
US10082035B2 (en) 2013-08-30 2018-09-25 Kabushiki Kaisha Toshiba Erosion resistant material and turbine blade
JPWO2017163408A1 (ja) * 2016-03-25 2019-01-31 三菱重工エンジン＆ターボチャージャ株式会社 めっき層付き繊維強化部材、及び繊維強化部材のめっき方法
JP2023535830A (ja) * 2020-07-28 2023-08-21 カーエスベー ソシエタス ヨーロピア ウント コンパニー コマンディート ゲゼルシャフト アウフ アクチェン 流導コンポーネント用ハウジング

Also Published As

Publication number Publication date
US20080170943A1 (en) 2008-07-17
CN101220818A (zh) 2008-07-16
EP1947346A1 (en) 2008-07-23
CN101220818B (zh) 2013-09-18
US7753653B2 (en) 2010-07-13
EP1947346B1 (en) 2014-04-30

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