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DE69705907D1 - Herstellungsverfahren eines faserverstärkten metallischen Teils - Google Patents

Herstellungsverfahren eines faserverstärkten metallischen Teils

Info

Publication number
DE69705907D1
DE69705907D1 DE69705907T DE69705907T DE69705907D1 DE 69705907 D1 DE69705907 D1 DE 69705907D1 DE 69705907 T DE69705907 T DE 69705907T DE 69705907 T DE69705907 T DE 69705907T DE 69705907 D1 DE69705907 D1 DE 69705907D1
Authority
DE
Germany
Prior art keywords
fiber
manufacturing process
metallic part
reinforced metallic
reinforced
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
DE69705907T
Other languages
English (en)
Other versions
DE69705907T2 (de
Inventor
Edwin Stephen Twigg
Charles Richard Talbot
Phillip John Doorbar
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of DE69705907D1 publication Critical patent/DE69705907D1/de
Publication of DE69705907T2 publication Critical patent/DE69705907T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/02—Pretreatment of the fibres or filaments
    • C22C47/06—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
    • C22C47/062—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
    • C22C47/064—Winding wires
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49337—Composite blade

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
DE69705907T 1996-09-24 1997-09-09 Herstellungsverfahren eines faserverstärkten metallischen Teils Expired - Lifetime DE69705907T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9619890.8A GB9619890D0 (en) 1996-09-24 1996-09-24 A method of making a fibre reinforced metal component

Publications (2)

Publication Number Publication Date
DE69705907D1 true DE69705907D1 (de) 2001-09-06
DE69705907T2 DE69705907T2 (de) 2001-11-15

Family

ID=10800409

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69705907T Expired - Lifetime DE69705907T2 (de) 1996-09-24 1997-09-09 Herstellungsverfahren eines faserverstärkten metallischen Teils

Country Status (4)

Country Link
US (1) US5946801A (de)
EP (1) EP0831154B1 (de)
DE (1) DE69705907T2 (de)
GB (1) GB9619890D0 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2456637B (en) 1997-06-03 2010-01-13 Rolls Royce Plc A fibre reinforced metal rotor
FR2874232B1 (fr) * 1998-07-28 2007-06-15 Rolls Royce Plc Plc Rotor metallique renforce de fibres.
US6261699B1 (en) 1999-04-28 2001-07-17 Allison Advanced Development Company Fiber reinforced iron-cobalt composite material system
US6247638B1 (en) 1999-04-28 2001-06-19 Allison Advanced Development Company Selectively reinforced member and method of manufacture
US6232688B1 (en) 1999-04-28 2001-05-15 Allison Advanced Development Company High speed magnetic thrust disk
DE69930748T2 (de) 1999-11-04 2006-11-02 Avio S.P.A. Verfahren zur Herstellung eines Bauteiles aus Verbundwerkstoff
GB0119636D0 (en) * 2001-08-11 2001-10-03 Rolls Royce Plc a method of manufacturing a fibre reinforced metal component
DE10235818B4 (de) * 2002-08-05 2005-01-05 Mtu Aero Engines Gmbh Verfahren zur Herstellung einer Verstärkungsfaser, Verwendung derart hergestellter Verstärkungsfasern sowie Verfahren zur Herstellung eines Halbzeugs mit derart hergestellten Verstärkungsfasern
GB0324810D0 (en) * 2003-10-24 2003-11-26 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article
GB0327044D0 (en) * 2003-11-18 2004-04-07 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article and a cassette for use therein
GB0327043D0 (en) 2003-11-18 2004-04-07 Rolls Royce Plc A method of manufacturing an article by applying heat and pressure, a method of connecting a pipe to a sealed assembly and a connector for use therein
GB0327002D0 (en) * 2003-11-20 2003-12-24 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article
US7842375B2 (en) * 2005-05-17 2010-11-30 Rolls-Royce Corporation Fiber retention system for metal matrix composite preform
GB0515211D0 (en) * 2005-07-23 2005-08-31 Rolls Royce Plc A method of making titanium components
US7784182B2 (en) * 2006-11-08 2010-08-31 General Electric Company System for manufacturing a rotor having an MMC ring component and a unitary airfoil component
US7766623B2 (en) * 2006-11-08 2010-08-03 General Electric Company System for manufacturing a rotor having an MMC ring component and an airfoil component having monolithic airfoils
FR2925896B1 (fr) * 2007-12-28 2010-02-05 Messier Dowty Sa Procede de fabrication d'une piece metallique renforcee de fibres ceramiques
FR2925895B1 (fr) * 2007-12-28 2010-02-05 Messier Dowty Sa Procede de fabrication d'une piece metallique renforcee de fibres ceramiques
FR2933422B1 (fr) * 2008-07-04 2011-05-13 Messier Dowty Sa Procede de fabrication d'une piece metallique comportant des renforts internes formes de fibres ceramiques
GB201013440D0 (en) 2010-08-11 2010-09-22 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article
CN114737140B (zh) * 2022-04-14 2023-01-24 广东合拓新材料科技有限公司 一种抗拉强度高的铝单板材料及其制备方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3711936A (en) * 1970-12-28 1973-01-23 United Aircraft Corp Method for forming composite articles from alloy in temporary condition of superplasticity
JPS5923834A (ja) * 1982-07-30 1984-02-07 Chugai Ro Kogyo Kaisha Ltd 繊維強化合金
GB2196566B (en) * 1986-06-27 1990-03-07 Ex Cell O Corp Method of forming articles
US4907736A (en) * 1986-06-27 1990-03-13 Airfoil Textron Inc. Method of forming articles
US4782992A (en) * 1986-11-21 1988-11-08 Textron Inc. Method of forming articles
US4919594A (en) * 1987-05-15 1990-04-24 Allied-Signal Inc. Composite member, unitary rotor member including same, and method of making
US5337940A (en) * 1990-12-11 1994-08-16 Woods Harlan L Composite preform and method of manufacturing fiber reinforced composite
US5127802A (en) * 1990-12-24 1992-07-07 United Technologies Corporation Reinforced full-spar composite rotor blade
FR2699498B1 (fr) * 1992-12-23 1995-03-10 Eurocopter France Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication.
FR2713662B1 (fr) * 1993-12-08 1996-01-12 Snecma Procédé d'obtention d'une pièce circulaire métallique renforcée par des fibres.
FR2715883B1 (fr) * 1994-02-10 1996-03-29 Snecma Procédé d'obtention d'une pièce circulaire métallique renforcée par des fibres.

Also Published As

Publication number Publication date
EP0831154A1 (de) 1998-03-25
DE69705907T2 (de) 2001-11-15
EP0831154B1 (de) 2001-08-01
GB9619890D0 (en) 1996-11-06
US5946801A (en) 1999-09-07

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition