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FR2713663B1 - Procédé de fabrication de pièces axisymétriques en composite à matrice métallique. - Google Patents

Procédé de fabrication de pièces axisymétriques en composite à matrice métallique.

Info

Publication number
FR2713663B1
FR2713663B1 FR9315052A FR9315052A FR2713663B1 FR 2713663 B1 FR2713663 B1 FR 2713663B1 FR 9315052 A FR9315052 A FR 9315052A FR 9315052 A FR9315052 A FR 9315052A FR 2713663 B1 FR2713663 B1 FR 2713663B1
Authority
FR
France
Prior art keywords
matrix composite
metal matrix
axisymmetric parts
manufacturing axisymmetric
manufacturing
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
FR9315052A
Other languages
English (en)
Other versions
FR2713663A1 (fr
Inventor
Bachelet Eric
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR9315052A priority Critical patent/FR2713663B1/fr
Priority to US08/356,127 priority patent/US5460774A/en
Publication of FR2713663A1 publication Critical patent/FR2713663A1/fr
Application granted granted Critical
Publication of FR2713663B1 publication Critical patent/FR2713663B1/fr
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
    • 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
    • C22C49/02—Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
    • C22C49/10—Refractory metals
    • 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
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12007—Component of composite having metal continuous phase interengaged with nonmetal continuous phase
    • 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
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]

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)
  • Ceramic Products (AREA)
FR9315052A 1993-12-15 1993-12-15 Procédé de fabrication de pièces axisymétriques en composite à matrice métallique. Expired - Lifetime FR2713663B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9315052A FR2713663B1 (fr) 1993-12-15 1993-12-15 Procédé de fabrication de pièces axisymétriques en composite à matrice métallique.
US08/356,127 US5460774A (en) 1993-12-15 1994-12-15 Method of manufacturing axisymmetric components made of a composite material having a metallic matrix

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9315052A FR2713663B1 (fr) 1993-12-15 1993-12-15 Procédé de fabrication de pièces axisymétriques en composite à matrice métallique.

Publications (2)

Publication Number Publication Date
FR2713663A1 FR2713663A1 (fr) 1995-06-16
FR2713663B1 true FR2713663B1 (fr) 1996-01-12

Family

ID=9453942

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9315052A Expired - Lifetime FR2713663B1 (fr) 1993-12-15 1993-12-15 Procédé de fabrication de pièces axisymétriques en composite à matrice métallique.

Country Status (2)

Country Link
US (1) US5460774A (fr)
FR (1) FR2713663B1 (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5578384A (en) * 1995-12-07 1996-11-26 Ticomp, Inc. Beta titanium-fiber reinforced composite laminates
US5733390A (en) * 1993-10-18 1998-03-31 Ticomp, Inc. Carbon-titanium composites
US5906550A (en) * 1993-10-18 1999-05-25 Ticomp, Inc. Sports bat having multilayered shell
US6194081B1 (en) 1993-10-18 2001-02-27 Ticomp. Inc. Beta titanium-composite laminate
US5763079A (en) * 1995-05-23 1998-06-09 Atlantic Research Corporation Wire preforms for composite material manufacture and methods of making
US5843232A (en) * 1995-11-02 1998-12-01 General Electric Company Measuring deposit thickness in composite materials production
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US6039832A (en) * 1998-02-27 2000-03-21 The Boeing Company Thermoplastic titanium honeycomb panel
EP1099774B1 (fr) * 1999-11-04 2006-04-05 AVIO S.p.A. Procédé de fabriction d'un élément en matériau composite
US6457111B1 (en) 1999-12-14 2002-09-24 International Business Machines Corporation Method and system for allocation of a persistence indicator for an object in an object-oriented environment
US7785429B2 (en) * 2003-06-10 2010-08-31 The Boeing Company Tough, high-strength titanium alloys; methods of heat treating titanium alloys
DE10326818B4 (de) * 2003-06-15 2007-07-05 Mtu Aero Engines Gmbh Verbundwerkstoff, Verfahren zur Herstellung eines Verbundwerkstoffs und Verwendung desselben
US7118063B2 (en) * 2004-07-29 2006-10-10 Sequa Corporation Wire/fiber ring and method for manufacturing the same
FR2886290B1 (fr) * 2005-05-27 2007-07-13 Snecma Moteurs Sa Procede de fabrication d'une piece avec un insert en materiau composite a matrice metallique et fibres ceramiques
FR2972126B1 (fr) * 2011-03-01 2014-05-16 Snecma Procede de realisation d'une piece metallique telle qu'un renfort d'aube de turbomachine
FR2972125B1 (fr) * 2011-03-01 2013-04-12 Snecma Procede de realisation d'une piece metallique telle qu'un renfort d'aube de turbomachine
EP2796230A1 (fr) * 2013-04-22 2014-10-29 Gervaux Ltd Procédé de fabrication d'un composant métallique par utilisation d'enroulement de fil métallique et pressage isostatique à chaud
CN114411070A (zh) * 2021-11-19 2022-04-29 莫纶(珠海)新材料科技有限公司 一种纤维增强金属基复合材料及其制备方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2081237A1 (en) * 1970-03-20 1971-12-03 Onera (Off Nat Aerospatiale) Fibre impregnated composites - by forming a eutectic alloy in situ over the fibres
US3915776A (en) * 1971-07-12 1975-10-28 Kaempen Industries Method for making composite structures
NL7401813A (fr) * 1973-06-06 1974-12-10
US4876050A (en) * 1985-06-24 1989-10-24 Murdock, Inc. Process for dry fiber winding and impregnating of projectiles
US4867644A (en) * 1987-05-15 1989-09-19 Allied-Signal Inc. Composite member, unitary rotor member including same, and method of making
FR2684578B1 (fr) * 1991-12-04 1996-04-12 Snecma Procede de fabrication de pieces en materiau composite a matrice metallique
USH1261H (en) * 1992-05-15 1993-12-07 Gibson Baylor D On-line consolidation of filament wound thermoplastic parts

Also Published As

Publication number Publication date
FR2713663A1 (fr) 1995-06-16
US5460774A (en) 1995-10-24

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TP Transmission of property
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