DE69207206D1 - Verfahren zur herstellung eines faserverstärkten blattes - Google Patents

Verfahren zur herstellung eines faserverstärkten blattes

Info

Publication number
DE69207206D1
DE69207206D1 DE69207206T DE69207206T DE69207206D1 DE 69207206 D1 DE69207206 D1 DE 69207206D1 DE 69207206 T DE69207206 T DE 69207206T DE 69207206 T DE69207206 T DE 69207206T DE 69207206 D1 DE69207206 D1 DE 69207206D1
Authority
DE
Germany
Prior art keywords
producing
fiber reinforced
leaf
reinforced leaf
fiber
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.)
Expired - Lifetime
Application number
DE69207206T
Other languages
English (en)
Other versions
DE69207206T2 (de
Inventor
John Graff
John Violette
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69207206D1 publication Critical patent/DE69207206D1/de
Application granted granted Critical
Publication of DE69207206T2 publication Critical patent/DE69207206T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0025Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B29C70/865Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/26Fabricated blades
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making
    • Y10T29/49337Composite blade

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
DE69207206T 1991-10-18 1992-10-06 Verfahren zur herstellung eines faserverstärkten blattes Expired - Lifetime DE69207206T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/780,696 US5222297A (en) 1991-10-18 1991-10-18 Composite blade manufacture
PCT/US1992/008488 WO1993008017A1 (en) 1991-10-18 1992-10-06 Composite blade manufacture

Publications (2)

Publication Number Publication Date
DE69207206D1 true DE69207206D1 (de) 1996-02-08
DE69207206T2 DE69207206T2 (de) 1996-06-27

Family

ID=25120384

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69207206T Expired - Lifetime DE69207206T2 (de) 1991-10-18 1992-10-06 Verfahren zur herstellung eines faserverstärkten blattes

Country Status (5)

Country Link
US (1) US5222297A (de)
EP (1) EP0610273B1 (de)
BR (1) BR9206514A (de)
DE (1) DE69207206T2 (de)
WO (1) WO1993008017A1 (de)

Families Citing this family (143)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5527155A (en) * 1992-08-21 1996-06-18 Mcdonnell Douglas Corp. Injection molded fan blade
US5598760A (en) * 1994-07-15 1997-02-04 Sucic; Steve EOP scribe device
JPH08177767A (ja) * 1994-12-20 1996-07-12 Zexel Corp ベーン型圧縮機のベーン及びその製造方法
GB2306353B (en) * 1995-10-28 1998-10-07 Rolls Royce Plc A method of manufacturing a blade
US5833998A (en) * 1995-11-06 1998-11-10 The Procter & Gamble Company Topical compositions for regulating the oily/shiny appearance of skin
US5720597A (en) * 1996-01-29 1998-02-24 General Electric Company Multi-component blade for a gas turbine
US6003754A (en) * 1997-10-21 1999-12-21 Allison Advanced Development Co. Airfoil for a gas turbine engine and method of manufacture
US6231941B1 (en) * 1998-07-14 2001-05-15 The Boeing Company Radius fillers for a resin transfer molding process
IT1303558B1 (it) * 1998-09-03 2000-11-14 Cavalli S R L Procedimento per la realizzazione di volanti per veicoli, inparticolare volanti rivestiti in materiale pregiato, e volanti
US6305905B1 (en) 1999-05-05 2001-10-23 United Technologies Corporation Bolted-on propeller blade
US6296037B1 (en) * 1999-08-10 2001-10-02 Newell Window Furnishings, Inc. Foam core vane for door and window covering
US6250886B1 (en) * 1999-09-03 2001-06-26 Chittom International, Inc. Axial flow fan and fan blade
DE19959598A1 (de) * 1999-12-10 2001-06-13 Rolls Royce Deutschland Verfahren zum Herstellen einer Schaufel einer Strömungsmaschine
US6676080B2 (en) 2000-07-19 2004-01-13 Aero Composites, Inc. Composite airfoil assembly
US7226559B2 (en) * 2000-12-08 2007-06-05 Toyota Motor Sales, U.S.A., Inc. Method for molding structures
US6764280B2 (en) 2001-03-06 2004-07-20 Bell Helicopter Textron Inc. Multi-bladed tail rotor hub design for coriolis relief
US6439849B1 (en) 2001-05-03 2002-08-27 Bell Helicopter Textron, Inc. Dual trunnion hub-to-mast assembly
US6659722B2 (en) 2001-05-07 2003-12-09 Bell Helicopter Textron, Inc. Composite rotor blade and method of manufacture
US6705011B1 (en) 2003-02-10 2004-03-16 United Technologies Corporation Turbine element manufacture
US6877532B2 (en) * 2003-05-29 2005-04-12 Invision Investments, Inc. Purging system for a liquid dispensing nozzle
US7165945B2 (en) * 2003-08-22 2007-01-23 Sikorsky Aircraft Corporation Braided spar for a rotor blade and method of manufacture thereof
FR2861143B1 (fr) * 2003-10-20 2006-01-20 Snecma Moteurs Aube de turbomachine, notamment aube de soufflante et son procede de fabrication
AU2004288913B2 (en) * 2003-11-06 2009-09-17 Hexcel Corporation Interlock double weave fabric and methods of making and using the same
GB0424481D0 (en) * 2004-11-05 2004-12-08 Rolls Royce Plc Composite aerofoil
US7247002B2 (en) * 2004-12-02 2007-07-24 Siemens Power Generation, Inc. Lamellate CMC structure with interlock to metallic support structure
US7278830B2 (en) * 2005-05-18 2007-10-09 Allison Advanced Development Company, Inc. Composite filled gas turbine engine blade with gas film damper
US7547194B2 (en) * 2006-07-31 2009-06-16 General Electric Company Rotor blade and method of fabricating the same
GB2449058B (en) * 2007-01-20 2011-08-10 Smiths Aerospace Group Ltd Blades
ES2319152B1 (es) * 2007-07-17 2010-01-11 Fco.Javier Garcia Castro Procedimiento para la fabricacion de palas eolicas.
US8206118B2 (en) * 2008-01-04 2012-06-26 United Technologies Corporation Airfoil attachment
US8221084B2 (en) * 2008-02-28 2012-07-17 Textron Innovations Inc. Single-piece propeller and method of making
WO2009112017A2 (de) * 2008-03-14 2009-09-17 Thoenes Dichtungstechnik Gmbh Verfahren zur herstellung eines rotorblattes für eine windkraftanlage sowie ein nach diesem verfahren hergestelltes rotorblatt
ES2557998T5 (es) * 2008-04-15 2019-06-24 Siemens Ag Pala de turbina eólica con un conductor de rayos integrado y método para la fabricación de la misma
FR2933379B1 (fr) * 2008-07-07 2010-08-20 Aerazur Procede d'assemblage d'un tapis de degivrage et d'un blindage metallique sur une structure
FR2933634B1 (fr) * 2008-07-10 2010-08-27 Snecma Aube redresseur de soufflante en composite 3d
GB2466793B (en) 2009-01-07 2011-11-09 Ge Aviat Systems Ltd Composite spars
FR2942513B1 (fr) * 2009-02-20 2011-05-27 Airbus France Aube pour recepteur de turbomachine, comprenant une partie pale integrant un fusible mecanique
US7963747B2 (en) 2009-04-02 2011-06-21 General Electric Company Braided wind turbine blades and method of making same
US8075274B2 (en) * 2009-05-13 2011-12-13 Hamilton Sundstrand Corporation Reinforced composite fan blade
DE102009024845A1 (de) * 2009-06-09 2010-12-16 Howaldtswerke-Deutsche Werft Gmbh Propeller
DK2295235T3 (da) * 2009-08-20 2013-07-29 Siemens Ag Fiberforstærket plaststruktur og fremgangsmåde til fremstilling af den fiberforstærkede plaststruktur
GB2470618B (en) * 2009-09-14 2011-08-24 Alexander Fergusson An improved method of and apparatus for making a composite material
US20110116906A1 (en) * 2009-11-17 2011-05-19 Smith Blair A Airfoil component wear indicator
US20110129348A1 (en) * 2009-11-30 2011-06-02 United Technologies Corporation Core driven ply shape composite fan blade and method of making
JP2011137386A (ja) * 2009-12-25 2011-07-14 Mitsubishi Heavy Ind Ltd 風車回転翼および風車回転翼の製造方法
US20110176927A1 (en) * 2010-01-20 2011-07-21 United Technologies Corporation Composite fan blade
US8499450B2 (en) 2010-01-26 2013-08-06 United Technologies Corporation Three-dimensionally woven composite blade with spanwise weft yarns
US8500407B1 (en) 2010-03-28 2013-08-06 The Boeing Company Composite blade root-end drill-through lug and attachment method
US8540481B2 (en) * 2010-04-13 2013-09-24 Rolls-Royce Corporation Rotor blade assembly
US20130115440A1 (en) * 2010-05-28 2013-05-09 Bernd Hoevel Composites
DK2402148T3 (da) * 2010-06-30 2014-10-13 Siemens Ag Støbningsfremgangsmåde til fremstilling af et arbejdsemne
FR2962175B1 (fr) * 2010-07-02 2012-08-10 Snecma Aube a longeron composite integre
US8662855B2 (en) 2010-08-31 2014-03-04 United Technologies Corporation Integrally woven composite fan blade using progressively larger weft yarns
FR2964426B1 (fr) * 2010-09-06 2014-02-14 Snecma Aube mobile en materiau composite
FR2970943B1 (fr) 2011-01-31 2014-02-28 Eurocopter France Pale et procede de fabrication de ladite pale
DK2481559T3 (da) * 2011-02-01 2019-07-29 Siemens Gamesa Renewable Energy As Forberedelse af en vindmøllevinge til korrekt positionering i et efterfølgende samlingstrin
US8790087B2 (en) 2011-04-28 2014-07-29 Hamilton Sundstrand Corporation Interlocking blade sheath
WO2012151348A1 (en) * 2011-05-03 2012-11-08 Iowa State University Research Foundation, Inc. Fabric winding machine
FR2976552A1 (fr) * 2011-06-16 2012-12-21 Jacky Greziller Composition structurelle et mode de realisation d'une helice composite a longerons integres.
FR2977235B1 (fr) 2011-06-30 2013-07-12 Eurocopter France Pale de rotor, et aeronef
FR2980537B1 (fr) * 2011-09-26 2015-04-24 Snecma Aube pour turbomachine et procede de fabrication d'une telle aube
US9168998B2 (en) 2011-11-23 2015-10-27 The Boeing Company Composite propeller spar
EP2599713A1 (de) * 2011-11-30 2013-06-05 Ratier-Figeac SAS Propellerblattholm mit Wabenkern
EP2599714B1 (de) * 2011-11-30 2014-10-08 Hamilton Sundstrand Corporation Propellerblatt mit entsprechendem Klebstoff an der Holmverbindung
FR2983457B1 (fr) 2011-12-01 2014-01-10 Eurocopter France Pale de rotor
US10215027B2 (en) * 2012-01-04 2019-02-26 United Technologies Corporation Aluminum fan blade construction with welded cover
FR2985939B1 (fr) * 2012-01-25 2014-02-14 Snecma Procede de fabrication d'une pale d'helice a structure composite, comprenant un ajustement de position entre deux parties
CN104105581B (zh) 2012-01-25 2016-08-17 斯奈克玛 由复合材料制造螺旋桨叶片的方法
FR2985940B1 (fr) * 2012-01-25 2014-10-24 Snecma Procede de fabrication d'une pale d'helice en materiau composite
US9352823B2 (en) * 2012-04-04 2016-05-31 Hamilton Sundstrand Corporation Propeller blade with reinforced spar core
US20130280079A1 (en) * 2012-04-18 2013-10-24 Hamilton Sundstrand Corporation Propeller blade with metallic foam spar core
EP2660143B1 (de) * 2012-04-30 2021-07-07 Ratier-Figeac Propellerblatt mit leichtgewichtigem Einsatz und Schotten
US9416668B2 (en) * 2012-04-30 2016-08-16 United Technologies Corporation Hollow fan bladed with braided fabric tubes
EP2660145A1 (de) * 2012-04-30 2013-11-06 Ratier-Figeac Propellerblatt mit leichtgewichtigem Einsatz
EP2660146B1 (de) * 2012-04-30 2018-01-31 Hamilton Sundstrand Corporation Propellerblatt mit modifizierter Holmlaminierung
EP2660144A1 (de) * 2012-04-30 2013-11-06 Hamilton Sundstrand Corporation Propellerflügel mit veränderter Holmsteifigkeit
EP2669192B8 (de) * 2012-05-29 2017-03-01 Ratier-Figeac SAS Propellerblatt
US9139287B2 (en) * 2012-06-26 2015-09-22 Hamilton Sundstrand Corporation Propeller blade with carbon foam spar core
US8876482B2 (en) * 2012-09-11 2014-11-04 United Technologies Corporation Electrical grounding for blade sheath
US9322283B2 (en) 2012-09-28 2016-04-26 United Technologies Corporation Airfoil with galvanic corrosion preventive shim
US9309772B2 (en) 2013-02-22 2016-04-12 General Electric Company Hybrid turbine blade including multiple insert sections
US11719161B2 (en) * 2013-03-14 2023-08-08 Raytheon Technologies Corporation Low noise turbine for geared gas turbine engine
US10323521B2 (en) 2013-03-15 2019-06-18 United Technologies Corporation Hybrid fan blade biscuit construction
EP2971527B1 (de) * 2013-03-15 2020-08-05 United Technologies Corporation Hybride gebläseschaufelkonstruktion mit flachdübel
EP3004561A2 (de) 2013-05-29 2016-04-13 General Electric Company Metallplatte für eine verbundstofftragfläche
US9682773B2 (en) 2013-06-25 2017-06-20 The Boeing Company Systems and methods for blade attachment
JP6557223B2 (ja) * 2013-07-08 2019-08-07 サフラン エアークラフト エンジンズ 航空機用複合プロペラブレード
US10648340B2 (en) 2013-08-28 2020-05-12 Sikorsky Aircraft Corporation High modulus hybrid material rotor blade spar
GB2518640B (en) * 2013-09-26 2016-01-20 Ge Aviat Systems Ltd Propeller blade assembly
US9709030B2 (en) * 2013-12-16 2017-07-18 General Electric Company Methods of manufacturing rotor blade components for a wind turbine
WO2015108616A1 (en) 2014-01-16 2015-07-23 General Electric Company Composite blade root stress reducing shim
US9920629B2 (en) * 2014-02-20 2018-03-20 Hamilton Sundstrand Corporation Propeller blade and method
US20150266572A1 (en) * 2014-03-21 2015-09-24 Hamilton Sundstrand Corporation Propeller blade having compliant spar core
WO2016025386A1 (en) 2014-08-15 2016-02-18 Sikorsky Aircraft Corporation Rotor blade spar formation with automated fiber placement
US10099434B2 (en) * 2014-09-16 2018-10-16 General Electric Company Composite airfoil structures
US9936646B2 (en) * 2014-11-12 2018-04-10 Deere & Company Light weight needle construction for delivering twine in a large square baler
FR3032648B1 (fr) * 2015-02-16 2017-03-03 Herakles Procede de fabrication d'une aube de turbomachine en materiau composite
EP4030063A1 (de) 2015-12-14 2022-07-20 Hunter Fan Company Deckenlüfter
US10677259B2 (en) 2016-05-06 2020-06-09 General Electric Company Apparatus and system for composite fan blade with fused metal lead edge
US10239604B2 (en) * 2016-05-21 2019-03-26 Bell Helicopter Textron Inc. Structurally biased proprotor blade assembly
CN109109400B (zh) * 2016-06-13 2021-03-02 亿航智能设备(广州)有限公司 一种复合材料及飞行器
EP3257743B1 (de) 2016-06-14 2020-05-20 Ratier-Figeac SAS Propellerschaufeln
EP3318483B1 (de) * 2016-11-08 2020-12-30 Ratier-Figeac SAS Verstärktes propellerblatt
US10626884B2 (en) 2016-12-09 2020-04-21 Hamilton Sundstrand Corporation Systems and methods for making airfoils
EP3399085B1 (de) 2017-05-05 2022-07-13 Ratier-Figeac SAS Mehrschichtiger geflochtener artikel, sein herstellungsverfahren, ein flugzeugbauteil mit diesem geflecht und ein verfahren zur herstellung eines propellerflügels
EP3431388A1 (de) 2017-07-17 2019-01-23 Ratier-Figeac SAS Propellerschaufeln
US10640197B1 (en) * 2017-10-31 2020-05-05 Wisk Aero Llc Composite airfoil with rolled fiberglass reinforced leading edge
EP3552953B1 (de) 2018-04-10 2020-04-22 Ratier-Figeac SAS Propellerblattfusskupplung
EP3556544B1 (de) * 2018-04-17 2021-07-28 Ratier-Figeac SAS Propellerblattholm
USD957617S1 (en) 2018-07-10 2022-07-12 Hunter Fan Company Ceiling fan blade
USD903092S1 (en) 2018-07-10 2020-11-24 Hunter Fan Company Ceiling fan blade
USD880680S1 (en) 2018-07-10 2020-04-07 Hunter Fan Company Ceiling fan blade
USD905227S1 (en) 2018-07-10 2020-12-15 Hunter Fan Company Ceiling fan blade
USD957618S1 (en) 2018-07-10 2022-07-12 Hunter Fan Compnay Ceiling fan blade
USD880684S1 (en) 2018-07-10 2020-04-07 Hunter Fan Company Ceiling fan blade
USD906511S1 (en) 2018-07-10 2020-12-29 Hunter Fan Company Ceiling fan blade
USD905226S1 (en) 2018-07-10 2020-12-15 Hunter Fan Company Ceiling fan blade
USD880683S1 (en) 2018-07-10 2020-04-07 Hunter Fan Company Ceiling fan blade
USD903091S1 (en) 2018-07-10 2020-11-24 Hunter Fan Company Ceiling fan blade
USD902377S1 (en) 2018-07-10 2020-11-17 Hunter Fan Company Ceiling fan blade
USD880682S1 (en) 2018-07-10 2020-04-07 Hunter Fan Company Ceiling fan blade
US11111930B2 (en) 2018-07-10 2021-09-07 Hunter Fan Company Ceiling fan blade
USD957619S1 (en) 2018-07-10 2022-07-12 Hunter Fan Company Ceiling fan blade
USD880681S1 (en) 2018-07-10 2020-04-07 Hunter Fan Company Ceiling fan blade
USD980408S1 (en) 2018-07-10 2023-03-07 Hunter Fan Company Ceiling fan blade
USD905845S1 (en) 2018-07-10 2020-12-22 Hunter Fan Company Ceiling fan blade
US10760428B2 (en) 2018-10-16 2020-09-01 General Electric Company Frangible gas turbine engine airfoil
US11111815B2 (en) 2018-10-16 2021-09-07 General Electric Company Frangible gas turbine engine airfoil with fusion cavities
US11149558B2 (en) 2018-10-16 2021-10-19 General Electric Company Frangible gas turbine engine airfoil with layup change
US10746045B2 (en) 2018-10-16 2020-08-18 General Electric Company Frangible gas turbine engine airfoil including a retaining member
US11434781B2 (en) 2018-10-16 2022-09-06 General Electric Company Frangible gas turbine engine airfoil including an internal cavity
US10837286B2 (en) 2018-10-16 2020-11-17 General Electric Company Frangible gas turbine engine airfoil with chord reduction
EP3659909B1 (de) * 2018-11-27 2023-03-22 Ratier-Figeac SAS Propellerschaufeln
FR3107300B1 (fr) * 2020-02-18 2022-07-08 Safran Aircraft Engines Pale composite pour rotor de turbomachine
EP3907063B1 (de) * 2020-05-04 2024-04-24 Ratier-Figeac SAS Mehrschichtiger geflochtener artikel
IT202000012412A1 (it) * 2020-05-26 2021-11-26 Baruffi Eng S R L Metodo di realizzazione di un manufatto in materiale composito
US11946391B2 (en) * 2021-03-11 2024-04-02 General Electric Company Turbine engine with composite airfoil having a non-metallic leading edge protective wrap
US11674399B2 (en) 2021-07-07 2023-06-13 General Electric Company Airfoil arrangement for a gas turbine engine utilizing a shape memory alloy
US11668317B2 (en) 2021-07-09 2023-06-06 General Electric Company Airfoil arrangement for a gas turbine engine utilizing a shape memory alloy
FR3136011B1 (fr) * 2022-05-31 2024-04-26 Safran Aircraft Engines Aube comprenant une structure en matériau composite et procédé de fabrication associé
US11608158B1 (en) * 2022-07-25 2023-03-21 Joon Bu Park Negative Poisson's ratio materials for propellers and turbines
CN115388715A (zh) * 2022-07-30 2022-11-25 安徽梦克斯航空科技有限公司 一种轻质弹翼结构及成型方法
US11982205B1 (en) * 2022-12-28 2024-05-14 General Electric Company Airfoil having a spar assembly for a turbine engine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511862A (en) * 1950-06-20 Propeller
US2599718A (en) * 1949-09-12 1952-06-10 Max M Munk Laminated propeller
GB1319235A (en) * 1969-07-18 1973-06-06 Dowty Rotol Ltd Devices of fibrous-reinforced plastics material
US3970495A (en) * 1974-07-24 1976-07-20 Fiber Science, Inc. Method of making a tubular shaft of helically wound filaments
GB2032832B (en) * 1978-09-16 1982-07-28 Dowty Rotol Ltd Foam-containing structures
US4648921A (en) * 1980-10-02 1987-03-10 United Technologies Corporation Method of making fiber reinforced articles
GB2105633B (en) * 1981-08-28 1985-07-31 Dowty Rotol Ltd Foam-containing structures
US4524499A (en) * 1981-11-16 1985-06-25 Trw Inc. Method of fabricating an aircraft propeller assembly with composite blades
US4470862A (en) * 1982-05-27 1984-09-11 United Technologies Corporation Manufacture of fiber reinforced articles
US4919594A (en) * 1987-05-15 1990-04-24 Allied-Signal Inc. Composite member, unitary rotor member including same, and method of making
US4789304A (en) * 1987-09-03 1988-12-06 United Technologies Corporation Insulated propeller blade
US5049036A (en) * 1988-09-09 1991-09-17 Airfoil Textron Inc Composite blade with divergent root and method for making same
US5018271A (en) * 1988-09-09 1991-05-28 Airfoil Textron Inc. Method of making a composite blade with divergent root
US5013216A (en) * 1988-09-09 1991-05-07 Airfoil Textron Inc. Composite blade perform with divergent root
JPH03104799A (ja) * 1989-09-20 1991-05-01 Fuji Heavy Ind Ltd 複合材ブレードの製造方法
US5042968A (en) * 1989-11-02 1991-08-27 United Technologies Corporation Propeller blade subassembly and method for making a propeller blade subassembly
US5123814A (en) * 1990-07-27 1992-06-23 The Marley Cooling Tower Company Industrial cooling tower fan blade having abrasion resistant leading edge
US5127802A (en) * 1990-12-24 1992-07-07 United Technologies Corporation Reinforced full-spar composite rotor blade

Also Published As

Publication number Publication date
WO1993008017A1 (en) 1993-04-29
US5222297A (en) 1993-06-29
EP0610273B1 (de) 1995-12-27
DE69207206T2 (de) 1996-06-27
EP0610273A1 (de) 1994-08-17
BR9206514A (pt) 1995-10-31

Similar Documents

Publication Publication Date Title
DE69207206D1 (de) Verfahren zur herstellung eines faserverstärkten blattes
DE59404424D1 (de) Verfahren zur herstellung eines photochromen gegenstandes
ATA3291A (de) Verfahren zur herstellung eines cellulosischen formkoerpers
DE69330005D1 (de) Verfahren zur herstellung eines gekrummten, splittersicheren glaslaminats
DE69030971D1 (de) Verfahren zur herstellung eines wasserabsorbierenden harzes
DE69408142T3 (de) Verfahren zur herstellung eines mineralfaserprodukts
DE3670788D1 (de) Verfahren zur herstellung eines hohlen faserverstaerkten gegenstandes.
DE69408987T2 (de) Verfahren zur herstellung eines mineralfaserproduktes
DE69622570T2 (de) Verfahren zur herstellung eines gepolten elektrooptischen glasfasersegments
ATA3191A (de) Verfahren zur herstellung eines cellulosischen formkoerpers
ATE148101T1 (de) Verfahren zur herstellung eines biphenylderivates
DE69125789D1 (de) Verfahren zur herstellung einer polyoxyalkylenverbindungen
DE69009655D1 (de) Verfahren zur Herstellung eines Wickelkabels.
DE69110286D1 (de) Verfahren zur herstellung eines überzuges.
DE69024817D1 (de) Verfahren zur herstellung eines punktartig teilweise bedeckten elementes
DE69323814T2 (de) Verfahren zur herstellung eines textil-verbundwerkstoff
DE58902103D1 (de) Verfahren zur herstellung eines gewickelten thermoplastischen rohres.
DE69314312D1 (de) Verfahren zur herstellung eines polymer
DE59201852D1 (de) Verfahren zur herstellung eines stiftes.
DE69214578D1 (de) Verfahren zur Herstellung eines Toner-Harzes
DE69220960D1 (de) Verfahren zur herstellung eines verbundwerkstoff
ATA34392A (de) Verfahren zur herstellung eines haarnährmittels
DE69417773T2 (de) Verfahren zur Herstellung eines p-Fuchsons
DE68905764D1 (de) Verfahren zur herstellung eines faserkopplers.
DE69210585D1 (de) Verfahren zur herstellung eines dichtungsrings

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
R071 Expiry of right

Ref document number: 610273

Country of ref document: EP