DE69425418T2 - Verfahren zur Herstellung eines ringförmigenfaserverstärkten Metallkörpers - Google Patents

Verfahren zur Herstellung eines ringförmigenfaserverstärkten Metallkörpers

Info

Publication number
DE69425418T2
DE69425418T2 DE69425418T DE69425418T DE69425418T2 DE 69425418 T2 DE69425418 T2 DE 69425418T2 DE 69425418 T DE69425418 T DE 69425418T DE 69425418 T DE69425418 T DE 69425418T DE 69425418 T2 DE69425418 T2 DE 69425418T2
Authority
DE
Germany
Prior art keywords
producing
metal body
reinforced metal
annular fiber
annular
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
DE69425418T
Other languages
English (en)
Other versions
DE69425418D1 (de
Inventor
Jean-Claude Berthelemy
Daniel Georges Girault
Gilles Jean-Michel Bessenay
Ludovic Edmond Camille Molliex
Gerard Philippe Gauthier
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE69425418D1 publication Critical patent/DE69425418D1/de
Publication of DE69425418T2 publication Critical patent/DE69425418T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/17—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by forging
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21F—WORKING OR PROCESSING OF METAL WIRE
    • B21F17/00—Jacketing or reinforcing articles with wire
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00—Making machine elements
    • B21K1/28—Making machine elements wheels; discs
    • B21K1/36—Making machine elements wheels; discs with blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00—Making machine elements
    • B21K1/76—Making machine elements elements not mentioned in one of the preceding groups
    • B21K1/761—Making machine elements elements not mentioned in one of the preceding groups rings
    • 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
    • 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
    • C22C47/06—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
    • C22C47/068—Aligning 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
    • C22C47/20—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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/10—Geometry two-dimensional
    • F05B2250/14—Geometry two-dimensional elliptical
    • F05B2250/141—Geometry two-dimensional elliptical circular
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S72/00—Metal deforming
    • Y10S72/70—Deforming specified alloys or uncommon metal or bimetallic work

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Forging (AREA)
  • Powder Metallurgy (AREA)
DE69425418T 1993-12-08 1994-12-07 Verfahren zur Herstellung eines ringförmigenfaserverstärkten Metallkörpers Expired - Lifetime DE69425418T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9314698A FR2713662B1 (fr) 1993-12-08 1993-12-08 Procédé d'obtention d'une pièce circulaire métallique renforcée par des fibres.

Publications (2)

Publication Number Publication Date
DE69425418D1 DE69425418D1 (de) 2000-09-07
DE69425418T2 true DE69425418T2 (de) 2001-03-15

Family

ID=9453678

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69425418T Expired - Lifetime DE69425418T2 (de) 1993-12-08 1994-12-07 Verfahren zur Herstellung eines ringförmigenfaserverstärkten Metallkörpers

Country Status (5)

Country Link
US (2) US5562245A (de)
EP (1) EP0657554B1 (de)
JP (1) JP3194678B2 (de)
DE (1) DE69425418T2 (de)
FR (1) FR2713662B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004001262B4 (de) * 2004-01-08 2007-03-01 Mtu Aero Engines Gmbh Verfahren und Vorrichtung zum Ablegen von Fasern in Ausnehmungen, insbesondere bei der Herstellung von MMC-Bauteilen
US9656315B2 (en) 2012-03-13 2017-05-23 Trumpf Werkzeugmaschinen Gmbh + Co. Kg Producing composite fiber/metal workpieces

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2741383B1 (fr) * 1995-11-22 1997-12-12 Snecma Procede de fabrication d'un rotor composite a matrice metallique
GB9619890D0 (en) * 1996-09-24 1996-11-06 Rolls Royce Plc A method of making a fibre reinforced metal component
US5968671A (en) * 1997-10-31 1999-10-19 Joseph; Brian E. Brazed composites
US6178799B1 (en) 1999-10-12 2001-01-30 The Boeing Company Forming press and method for shaping angle-section workpieces
ATE322560T1 (de) * 1999-11-04 2006-04-15 Avio Spa Verfahren zur herstellung eines bauteiles aus verbundwerkstoff
US7153555B2 (en) * 2000-02-15 2006-12-26 Travel Tags, Inc. Plastic objects including lenticular lens sheets
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
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
FR2925895B1 (fr) * 2007-12-28 2010-02-05 Messier Dowty Sa Procede de fabrication d'une piece metallique renforcee de fibres ceramiques
FR2925897B1 (fr) * 2007-12-28 2010-07-30 Messier Dowty Sa Procede de fabrication de pieces avec insert en materiau composite a matrice metallique
HU227362B1 (en) * 2008-04-29 2011-04-28 Contitech Rubber Ind Kft Procedure for manufacturing fibre reinforced hoses
US8727203B2 (en) 2010-09-16 2014-05-20 Howmedica Osteonics Corp. Methods for manufacturing porous orthopaedic implants
US9745855B2 (en) 2011-12-05 2017-08-29 Apci, Llc Linear friction welding apparatus and method
CN102581557A (zh) * 2012-02-23 2012-07-18 滁州安迈达特种铝业有限公司 冰箱门把手的无缝堵头加工工艺
GB201700614D0 (en) * 2017-01-13 2017-03-01 Rolls Royce Plc A method of manufacturing a component
CN114918542B (zh) * 2022-03-04 2024-04-19 南京理工大学 一种高强铝合金的纳米颗粒增强激光填粉焊接方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2226863A1 (de) * 1972-06-02 1973-12-20 Felten & Guilleaume Kabelwerk Verfahren zur herstellung von durch einlagen von faserstrukturen verstaerkten metallwerkstoffen
US4012824A (en) * 1973-06-06 1977-03-22 Felten & Guilleaume Kabelwerke Ag Reinforced article and method of making the same
FR2366904A1 (fr) * 1976-10-11 1978-05-05 Armines Procede et appareillage pour la fabrication de tubes en materiaux composites
JPS57155336A (en) * 1981-03-20 1982-09-25 Honda Motor Co Ltd Production of fiber-reinforced composite body
US4782992A (en) * 1986-11-21 1988-11-08 Textron Inc. Method of forming articles
JP2545277B2 (ja) * 1988-11-18 1996-10-16 本田技研工業株式会社 コンロッドの閉塞鍛造装置
WO1991001324A1 (en) * 1989-07-19 1991-02-07 Calgene, Inc. Ovary-tissue transcriptional factors
US5184769A (en) * 1989-07-26 1993-02-09 Avco Corporation Tooling and method for consolidating a filamentary reinforced metal matrix composite
JP2659848B2 (ja) * 1990-05-29 1997-09-30 三菱重工業株式会社 短繊維系ｆｒｍの等温鍛造法
US5337940A (en) * 1990-12-11 1994-08-16 Woods Harlan L Composite preform and method of manufacturing fiber reinforced composite
US5098011A (en) * 1990-12-14 1992-03-24 Mcdonnell Douglas Corporation Method and tooling for fabricating monolithic metal or metal matrix composite structures
US5213252A (en) * 1992-05-15 1993-05-25 The United States Of America As Represented By The Secretary Of The Air Force Method to produce selectively reinforced titanium alloy articles
FR2715883B1 (fr) * 1994-02-10 1996-03-29 Snecma Procédé d'obtention d'une pièce circulaire métallique renforcée par des fibres.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004001262B4 (de) * 2004-01-08 2007-03-01 Mtu Aero Engines Gmbh Verfahren und Vorrichtung zum Ablegen von Fasern in Ausnehmungen, insbesondere bei der Herstellung von MMC-Bauteilen
US9656315B2 (en) 2012-03-13 2017-05-23 Trumpf Werkzeugmaschinen Gmbh + Co. Kg Producing composite fiber/metal workpieces

Also Published As

Publication number Publication date
EP0657554A1 (de) 1995-06-14
JPH07197108A (ja) 1995-08-01
US5642851A (en) 1997-07-01
FR2713662A1 (fr) 1995-06-16
FR2713662B1 (fr) 1996-01-12
JP3194678B2 (ja) 2001-07-30
US5562245A (en) 1996-10-08
DE69425418D1 (de) 2000-09-07
EP0657554B1 (de) 2000-08-02

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA MOTEURS, PARIS, FR

8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR