SE7714253L - PROCEDURE FOR PREPARING A COMPOSITE CONSTRUCTION - Google Patents

PROCEDURE FOR PREPARING A COMPOSITE CONSTRUCTION

Info

Publication number
SE7714253L
SE7714253L SE7714253A SE7714253A SE7714253L SE 7714253 L SE7714253 L SE 7714253L SE 7714253 A SE7714253 A SE 7714253A SE 7714253 A SE7714253 A SE 7714253A SE 7714253 L SE7714253 L SE 7714253L
Authority
SE
Sweden
Prior art keywords
fibers
matrix
composite
preparing
procedure
Prior art date
Application number
SE7714253A
Other languages
Swedish (sv)
Inventor
K M Prewo
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of SE7714253L publication Critical patent/SE7714253L/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • 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
    • C22C47/066—Weaving wires
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/02—Layer formed of wires, e.g. mesh
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2311/00—Metals, their alloys or their compounds
    • B32B2311/24—Aluminium
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2313/00—Elements other than metals
    • B32B2313/02—Boron

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Textile Engineering (AREA)
  • Laminated Bodies (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

QUICK BOND COMPOSITE AND PROCESS A tape of monolayer matrix for use in making up a multilayer matrix or composite which is bonded at a high pressure and temperature by pressing the composite between heated platens in air to cause densification, the tape consisting of collimated fibers held together by metal wire woven at right angles to the fibers. The aluminum matrix in which the fibers are embedded is provided by aluminum foils alternating with the collimated fibers in the multilayer matrix.
SE7714253A 1976-12-17 1977-12-15 PROCEDURE FOR PREPARING A COMPOSITE CONSTRUCTION SE7714253L (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US75157676A 1976-12-17 1976-12-17

Publications (1)

Publication Number Publication Date
SE7714253L true SE7714253L (en) 1978-06-18

Family

ID=25022621

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7714253A SE7714253L (en) 1976-12-17 1977-12-15 PROCEDURE FOR PREPARING A COMPOSITE CONSTRUCTION

Country Status (8)

Country Link
JP (1) JPS5376905A (en)
BE (1) BE861498A (en)
CA (1) CA1079011A (en)
DE (1) DE2756015A1 (en)
FR (1) FR2374162A1 (en)
GB (1) GB1562270A (en)
IL (1) IL53515A (en)
SE (1) SE7714253L (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2836418A1 (en) * 1978-08-19 1980-02-28 Helmut Dipl Phys Nussbaum Sandwich structure semi-finished constructional material - comprises tubes of fibrous material impregnated with synthetic resin and glued together
DE3000171C2 (en) * 1980-01-04 1982-04-29 Vereinigte Aluminium-Werke Ag, 5300 Bonn Fiber-reinforced composite material and process for its manufacture
GB2117020A (en) * 1982-03-18 1983-10-05 Hasegawa Chem Ind Reinforcement for plastics mouldings
FR2562101B1 (en) * 1984-03-27 1987-03-06 Brochier Sa MATERIAL BASED ON INORGANIC FIBERS, PARTICULARLY SILICON CARBIDE, FOR USE IN THE PRODUCTION OF COMPOSITE STRUCTURES
US4697324A (en) * 1984-12-06 1987-10-06 Avco Corporation Filamentary structural module for composites
US5337940A (en) * 1990-12-11 1994-08-16 Woods Harlan L Composite preform and method of manufacturing fiber reinforced composite

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1022533A (en) * 1962-05-24 1966-03-16 Nat Res Dev Composite metal structural components
FR1528298A (en) * 1967-06-20 1968-06-07 Nat Standard Co Method and structure for reinforcing metallic or non-metallic objects by a built-in mesh
US3942231A (en) * 1973-10-31 1976-03-09 Trw Inc. Contour formed metal matrix blade plies

Also Published As

Publication number Publication date
FR2374162A1 (en) 1978-07-13
FR2374162B1 (en) 1983-03-25
BE861498A (en) 1978-03-31
IL53515A (en) 1980-06-30
IL53515A0 (en) 1978-03-10
DE2756015A1 (en) 1978-11-02
CA1079011A (en) 1980-06-10
GB1562270A (en) 1980-03-12
JPS5376905A (en) 1978-07-07

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