DE602004003114D1 - Verfahren zur Herstellung eines Artikels aus einem faserverstärktem Verbundmetal - Google Patents

Verfahren zur Herstellung eines Artikels aus einem faserverstärktem Verbundmetal

Info

Publication number
DE602004003114D1
DE602004003114D1 DE602004003114T DE602004003114T DE602004003114D1 DE 602004003114 D1 DE602004003114 D1 DE 602004003114D1 DE 602004003114 T DE602004003114 T DE 602004003114T DE 602004003114 T DE602004003114 T DE 602004003114T DE 602004003114 D1 DE602004003114 D1 DE 602004003114D1
Authority
DE
Germany
Prior art keywords
article
fiber
producing
reinforced composite
composite metal
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.)
Active
Application number
DE602004003114T
Other languages
English (en)
Other versions
DE602004003114T2 (de
Inventor
Edwin S Twigg
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
Publication of DE602004003114D1 publication Critical patent/DE602004003114D1/de
Application granted granted Critical
Publication of DE602004003114T2 publication Critical patent/DE602004003114T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • C22C47/02—Pretreatment of the fibres or filaments
    • C22C47/04—Pretreatment of the fibres or filaments by coating, e.g. with a protective or activated covering
    • 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
    • C22C47/14—Making alloys containing metallic or non-metallic fibres or filaments by powder metallurgy, i.e. by processing mixtures of metal powder and fibres or filaments
    • 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
    • C22C47/20—Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing 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
    • 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
    • B22F2999/00—Aspects linked to processes or compositions used in 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
    • Y10T29/49337—Composite blade
    • 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
    • Y10T29/49826—Assembling or joining
    • Y10T29/49885—Assembling or joining with coating before or during assembling
    • 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
    • Y10T29/49826—Assembling or joining
    • Y10T29/49908—Joining by deforming

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)
DE602004003114T 2003-10-24 2004-10-01 Verfahren zur Herstellung eines Artikels aus einem faserverstärktem Verbundmetal Active DE602004003114T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0324810 2003-10-24
GBGB0324810.1A GB0324810D0 (en) 2003-10-24 2003-10-24 A method of manufacturing a fibre reinforced metal matrix composite article

Publications (2)

Publication Number Publication Date
DE602004003114D1 true DE602004003114D1 (de) 2006-12-21
DE602004003114T2 DE602004003114T2 (de) 2007-03-08

Family

ID=29595727

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004003114T Active DE602004003114T2 (de) 2003-10-24 2004-10-01 Verfahren zur Herstellung eines Artikels aus einem faserverstärktem Verbundmetal

Country Status (5)

Country Link
US (1) US7343677B2 (de)
EP (1) EP1527842B1 (de)
JP (1) JP4805563B2 (de)
DE (1) DE602004003114T2 (de)
GB (1) GB0324810D0 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0327002D0 (en) * 2003-11-20 2003-12-24 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article
US20060107516A1 (en) * 2004-11-24 2006-05-25 Touchstone Research Laboratory, Ltd. Intermittently connected metal matrix composite bars
FR2901497B1 (fr) * 2006-05-24 2009-03-06 Snecma Sa Procede de fabrication d'un disque de rotor de turbomachine
GB2438633B (en) * 2006-05-31 2010-12-01 Tisics Ltd Reinforced splines and their manufacture
WO2008044320A1 (fr) * 2006-10-13 2008-04-17 Mole's Act Co., Ltd. Procédé de chauffage par conduction de pièces, procédé de production de corps liés, procédé de production de corps frittés, et dispositif de chauffage par conduction de pièces
DE102007012845A1 (de) * 2007-03-17 2008-09-18 Ks Kolbenschmidt Gmbh Erzeugung eines partiellen Faserverbundgefüges in einem Bauteil über eine Laserumschmelzbehandlung
FR2919284B1 (fr) * 2007-07-26 2010-09-24 Snecma Piece mecanique comportant un insert en materiau composite.
FR2925896B1 (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
FR2935990B1 (fr) * 2008-09-17 2011-05-13 Aircelle Sa Procede de fabrication d'une piece en materiau composite a matrice metallique
FR2952944B1 (fr) 2009-11-25 2014-05-02 Messier Dowty Sa Procede de fabrication d'une piece metallique composite a renforts internes en fibres, preforme de mise en oeuvre et piece metallique obtenue
FR2953859B1 (fr) * 2009-12-16 2013-12-20 Snecma Procede de fabrication d'un insert de forme droite en materiau composite a matrice metallique
GB201005270D0 (en) 2010-03-30 2010-05-12 Rolls Royce Plc A method and apparatus for manufacturing a rotor disc
GB201013440D0 (en) 2010-08-11 2010-09-22 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article
CN105705724B (zh) 2013-12-13 2019-02-01 哈里伯顿能源服务公司 井下使用的纤维增强工具
US10145179B2 (en) 2013-12-13 2018-12-04 Halliburton Energy Services, Inc. Fiber-reinforced tools for downhole use

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61114848A (ja) * 1984-11-12 1986-06-02 工業技術院長 金属基複合材料の製造法
JPS61159540A (ja) * 1985-01-07 1986-07-19 Nippon Gakki Seizo Kk 繊維強化金属材の製法
US4809903A (en) * 1986-11-26 1989-03-07 United States Of America As Represented By The Secretary Of The Air Force Method to produce metal matrix composite articles from rich metastable-beta titanium alloys
US5261940A (en) * 1986-12-23 1993-11-16 United Technologies Corporation Beta titanium alloy metal matrix composites
JPH079005B2 (ja) * 1988-06-09 1995-02-01 株式会社神戸製鋼所 Ａ▲ｌ▼基複合材の成形方法
US5260137A (en) * 1990-06-07 1993-11-09 Avco Corporation Infiltrated fiber-reinforced metallic and intermetallic alloy matrix composites
US5425494A (en) * 1990-06-07 1995-06-20 Alliedsignal Inc. Method for forming infiltrated fiber-reinforced metallic and intermetallic alloy matrix composites
US5099573A (en) * 1990-06-27 1992-03-31 Compressor Components Textron Inc. Method of making hollow articles
US5305520A (en) * 1990-09-01 1994-04-26 Rolls-Royce Plc Method of making fibre reinforced metal component
US5337940A (en) * 1990-12-11 1994-08-16 Woods Harlan L Composite preform and method of manufacturing fiber reinforced composite
GB9122913D0 (en) * 1991-10-29 1991-12-11 British Petroleum Co Plc Process for the preparation of fibre reinforced metal matrix composites
DE4319727C2 (de) * 1993-06-15 1996-08-29 Mtu Muenchen Gmbh Verfahren zur Herstellung eines Schaufelringes für einen trommelartig aufgebauten Rotor, insbesondere Verdichterrotor einer Turbomaschine
US5501906A (en) * 1994-08-22 1996-03-26 Minnesota Mining And Manufacturing Company Ceramic fiber tow reinforced metal matrix composite
US6214134B1 (en) * 1995-07-24 2001-04-10 The United States Of America As Represented By The Secretary Of The Air Force Method to produce high temperature oxidation resistant metal matrix composites by fiber density grading
GB9619890D0 (en) * 1996-09-24 1996-11-06 Rolls Royce Plc A method of making a fibre reinforced metal component
FR2754478B1 (fr) * 1996-10-16 1998-11-20 Snecma Procede de fabrication d'une aube creuse de turbomachine
JP3216579B2 (ja) * 1997-07-23 2001-10-09 関西日本電気株式会社 陰極部材の製造方法およびこの陰極部材を用いた電子管
DE10005250B4 (de) * 1999-02-09 2004-10-28 Mtu Aero Engines Gmbh Verfahren zur Herstellung von faserverstärkten metallischen Bauteilen
US6247638B1 (en) * 1999-04-28 2001-06-19 Allison Advanced Development Company Selectively reinforced member and method of manufacture
ATE322560T1 (de) * 1999-11-04 2006-04-15 Avio Spa 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
JP2003138352A (ja) * 2001-10-29 2003-05-14 Mitsubishi Heavy Ind Ltd 金属基複合材料の成形方法

Also Published As

Publication number Publication date
EP1527842B1 (de) 2006-11-08
JP2005171379A (ja) 2005-06-30
US20050086789A1 (en) 2005-04-28
US7343677B2 (en) 2008-03-18
DE602004003114T2 (de) 2007-03-08
JP4805563B2 (ja) 2011-11-02
GB0324810D0 (en) 2003-11-26
EP1527842A1 (de) 2005-05-04

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Legal Events

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8364 No opposition during term of opposition