ES2182246T3 - Pieza de material compuesto de matriz metalica de alta rigidez y de gran estabilidad en una direccion longitudinal. - Google Patents

Pieza de material compuesto de matriz metalica de alta rigidez y de gran estabilidad en una direccion longitudinal.

Info

Publication number
ES2182246T3
ES2182246T3 ES98403009T ES98403009T ES2182246T3 ES 2182246 T3 ES2182246 T3 ES 2182246T3 ES 98403009 T ES98403009 T ES 98403009T ES 98403009 T ES98403009 T ES 98403009T ES 2182246 T3 ES2182246 T3 ES 2182246T3
Authority
ES
Spain
Prior art keywords
fibers
composite material
address
metal matrix
piece
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
ES98403009T
Other languages
English (en)
Inventor
Laetitia Billaud
Jocelyn Gaudin
Lutz Martine Nivet
Joel Poncy
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.)
Airbus Group SAS
Original Assignee
European Aeronautic Defence and Space Company EADS France
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 European Aeronautic Defence and Space Company EADS France filed Critical European Aeronautic Defence and Space Company EADS France
Application granted granted Critical
Publication of ES2182246T3 publication Critical patent/ES2182246T3/es
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
    • C22C47/08—Making alloys containing metallic or non-metallic fibres or filaments by contacting the fibres or filaments with molten metal, e.g. by infiltrating the fibres or filaments placed in a mould
    • 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
    • C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/14—Alloys containing metallic or non-metallic fibres or filaments characterised by the 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/249927—Fiber embedded in a metal matrix
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/249928—Fiber embedded in a ceramic, glass, or carbon matrix
    • Y10T428/249929—Fibers are aligned substantially parallel
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/249928—Fiber embedded in a ceramic, glass, or carbon matrix
    • Y10T428/249931—Free metal or alloy fiber
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3382—Including a free metal or alloy constituent
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/60—Nonwoven fabric [i.e., nonwoven strand or fiber material]
    • Y10T442/654—Including a free metal or alloy constituent

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Inorganic Fibers (AREA)

Abstract

UNA PIEZA ALARGADA, DE MATERIAL COMPUESTO CON MATRIZ METALICA, COMPRENDE RESPECTIVAMENTE ENTRE UN 35 % Y UN 45 % EN VOLUMEN DE UNA MATRIZ DE ALEACION CON BASE DE ALUMINIO O DE MAGNESIO Y ENTRE UN 65 % Y UN 55 % EN VOLUMEN DE FIBRAS CONTINUAS DE CARBONO, DISPUESTAS EN CAPAS PARALELAS A SU LONGITUD. AL MENOS APROXIMADAMENTE UN 90 % DE LAS FIBRAS DE CARBONO SON FIBRAS CON UN MODULO ULTRA ALTO. EN ENTRE 25 % Y UN 60 % DE LAS CAPAS, ESTAS FIBRAS ESTAN ORIENTADAS A 0° +/- 5° RESPECTO A LA DIRECCION LONGITUDINAL DE LA PIEZA CUANDO LA MATRIZ ES CON BASE DE ALUMINIO. EN LAS OTRAS CAPAS, LAS FIBRAS ESTAN ENTONCES ORIENTADAS ENTRE +/- 20° Y +/- 40° RESPECTO A ESTA DIRECCION. CUANDO LA MATRIZ ES CON BASE DE MAGNESIO, LAS FIBRAS CON MODULO ULTRA ALTO ESTAN ORIENTADAS A 0° +/- 5° EN AL MENOS UN 90 % DE LAS CAPAS. SE OBTIENE ASI UNA GRAN RIGIDEZ Y UNA GRAN ESTABILIDAD EN LA DIRECCION MENCIONADA, LO QUE FAVORECE LAS APLICACIONES EN LA INDUSTRIA ESPACIAL.
ES98403009T 1997-12-04 1998-12-01 Pieza de material compuesto de matriz metalica de alta rigidez y de gran estabilidad en una direccion longitudinal. Expired - Lifetime ES2182246T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9715306A FR2772049B1 (fr) 1997-12-04 1997-12-04 Piece en materiau composite a matrice metallique a haute rigidite et a grande stabilite dans une direction longitudinale

Publications (1)

Publication Number Publication Date
ES2182246T3 true ES2182246T3 (es) 2003-03-01

Family

ID=9514157

Family Applications (1)

Application Number Title Priority Date Filing Date
ES98403009T Expired - Lifetime ES2182246T3 (es) 1997-12-04 1998-12-01 Pieza de material compuesto de matriz metalica de alta rigidez y de gran estabilidad en una direccion longitudinal.

Country Status (8)

Country Link
US (1) US6197411B1 (es)
EP (1) EP0922779B1 (es)
JP (1) JP4283359B2 (es)
CA (1) CA2255402A1 (es)
DE (1) DE69807306T2 (es)
ES (1) ES2182246T3 (es)
FR (1) FR2772049B1 (es)
RU (1) RU2217522C2 (es)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10126926B4 (de) 2001-06-01 2015-02-19 Astrium Gmbh Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung
AT413704B (de) * 2004-06-23 2006-05-15 Arc Leichtmetallkompetenzzentrum Ranshofen Gmbh Kohlenstofffaserverstärktes leichtmetallteil und verfahren zur herstellung desselben
CN100503872C (zh) 2004-11-09 2009-06-24 岛根县 金属基碳纤维复合材料的制造方法
DE102005051269B3 (de) * 2005-10-26 2007-05-31 Infineon Technologies Ag Verbundwerkstoff und Bodenplatte
DE102006023041B4 (de) * 2006-05-17 2015-11-12 Bayerische Motoren Werke Aktiengesellschaft Partikelverstärkte Magnesium- oder Aluminiumlegierung
RU2613830C1 (ru) * 2015-10-07 2017-03-21 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Волокнистый композиционный материал
DE102015221078A1 (de) 2015-10-28 2017-05-04 Airbus Operations Gmbh Faserverstärktes Metallbauteil für ein Luft- oder Raumfahrzeug und Herstellungsverfahren für faserverstärkte Metallbauteile
ITUA20162826A1 (it) * 2016-04-22 2017-10-22 Freni Brembo Spa Corpo pinza di una pinza per freno a disco
CN107312984A (zh) * 2017-05-16 2017-11-03 苏州莱特复合材料有限公司 一种改性碳纤维增强镁基复合材料及其制备方法
CN107267826A (zh) * 2017-05-16 2017-10-20 苏州莱特复合材料有限公司 一种改性石墨烯增强镁基金属材料及其制备方法
CN108723309B (zh) * 2018-06-25 2021-01-01 临沂利信铝业有限公司 铝镁合金铸锭及其制备方法
CN110385437B (zh) * 2019-07-03 2021-09-10 西安理工大学 一种定向纤维原位增强钛及其合金支架的制备方法

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS613864A (ja) * 1984-06-15 1986-01-09 Toyota Motor Corp 炭素繊維強化マグネシウム合金
ATE115464T1 (de) * 1990-06-29 1994-12-15 Flexline Services Ltd Verfahren zur herstellung von verstärktem verbundmaterial und ein fasermaterial zur benutzung während dieses verfahrens.

Also Published As

Publication number Publication date
EP0922779B1 (fr) 2002-08-21
FR2772049A1 (fr) 1999-06-11
RU2217522C2 (ru) 2003-11-27
DE69807306D1 (de) 2002-09-26
FR2772049B1 (fr) 2000-02-18
JPH11256254A (ja) 1999-09-21
US6197411B1 (en) 2001-03-06
CA2255402A1 (fr) 1999-06-04
DE69807306T2 (de) 2003-04-17
JP4283359B2 (ja) 2009-06-24
EP0922779A1 (fr) 1999-06-16

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