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DE69807306D1 - Metallmatrixverbundkörper mit hoher Steifigkeit und hoher Stabilität in Längsrichtung - Google Patents

Metallmatrixverbundkörper mit hoher Steifigkeit und hoher Stabilität in Längsrichtung

Info

Publication number
DE69807306D1
DE69807306D1 DE69807306T DE69807306T DE69807306D1 DE 69807306 D1 DE69807306 D1 DE 69807306D1 DE 69807306 T DE69807306 T DE 69807306T DE 69807306 T DE69807306 T DE 69807306T DE 69807306 D1 DE69807306 D1 DE 69807306D1
Authority
DE
Germany
Prior art keywords
longitudinal direction
matrix composite
metal matrix
composite body
high rigidity
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 - Fee Related
Application number
DE69807306T
Other languages
English (en)
Other versions
DE69807306T2 (de
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 Defence and Space SAS
Original Assignee
Airbus Group SAS
Aerospatiale Matra
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 Airbus Group SAS, Aerospatiale Matra filed Critical Airbus Group SAS
Publication of DE69807306D1 publication Critical patent/DE69807306D1/de
Application granted granted Critical
Publication of DE69807306T2 publication Critical patent/DE69807306T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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)
DE69807306T 1997-12-04 1998-12-01 Metallmatrixverbundkörper mit hoher Steifigkeit und hoher Stabilität in Längsrichtung Expired - Fee Related DE69807306T2 (de)

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 (2)

Publication Number Publication Date
DE69807306D1 true DE69807306D1 (de) 2002-09-26
DE69807306T2 DE69807306T2 (de) 2003-04-17

Family

ID=9514157

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69807306T Expired - Fee Related DE69807306T2 (de) 1997-12-04 1998-12-01 Metallmatrixverbundkörper mit hoher Steifigkeit und hoher Stabilität in Längsrichtung

Country Status (8)

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

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
WO2006051782A1 (ja) 2004-11-09 2006-05-18 Shimane Prefectural Government 金属基炭素繊維複合材料およびその製造方法
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
CA2086328A1 (en) * 1990-06-29 1991-12-30 Gui Gerard De Jager Process for manufacturing reinforced composites and filament material for use in said process

Also Published As

Publication number Publication date
DE69807306T2 (de) 2003-04-17
FR2772049B1 (fr) 2000-02-18
EP0922779A1 (de) 1999-06-16
US6197411B1 (en) 2001-03-06
JP4283359B2 (ja) 2009-06-24
EP0922779B1 (de) 2002-08-21
ES2182246T3 (es) 2003-03-01
RU2217522C2 (ru) 2003-11-27
CA2255402A1 (fr) 1999-06-04
JPH11256254A (ja) 1999-09-21
FR2772049A1 (fr) 1999-06-11

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Legal Events

Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: EUROPEAN AERONAUTIC DEFENCE AND SPACE CO. - EADS F

8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee