GB1345541A - Fabricating composite parts - Google Patents

Fabricating composite parts

Info

Publication number
GB1345541A
GB1345541A GB1272771A GB1272771A GB1345541A GB 1345541 A GB1345541 A GB 1345541A GB 1272771 A GB1272771 A GB 1272771A GB 1272771 A GB1272771 A GB 1272771A GB 1345541 A GB1345541 A GB 1345541A
Authority
GB
United Kingdom
Prior art keywords
fibres
modules
resin
fibre
nodules
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
Application number
GB1272771A
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.)
International Business Machines Corp
Original Assignee
International Business Machines 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 International Business Machines Corp filed Critical International Business Machines Corp
Publication of GB1345541A publication Critical patent/GB1345541A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/001Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/12Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat
    • B29C70/14Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat oriented
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/345Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/12Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of short lengths, e.g. chopped filaments, staple fibres or bristles
    • B29K2105/128Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of short lengths, e.g. chopped filaments, staple fibres or bristles in the form of a mat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/16Fillers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

1345541 Composite fibre-resin parts INTERNATIONAL BUSINESS MACHINES CORP 3 May 1971 [8 May 1970] 12727/71 Heading B5A Composite parts having anisotropic mechanical properties are fabricated by making modules, in rod or tape form, of aligned fibres in a solid mouldable matrix material which bonds with the fibres, e.g. a thermosetting resin such as an epoxy resin with glass fibres; assembling in a mould cavity sufficient of these modules to form the completed part, the direction of fibre alignment being arranged to produce predetermined anisotropic properties, and moulding under heat and pressure to cause flow and cure, fibre alignment being maintained substantially as determined during assembly. The modules may be made by coating short fibres with resin, rotating them in an inner drum having a screen wire surface so that they fall through into radial cavities formed by vanes between this surface and an outer surface where they are compacted into nodules by heat and centrifugal force. Alternatively tapes can be formed continuously using a fourdrinier or sheet moulding machine, the fibres being aligned by feeding in a slurry through vanes and then sprayed with binder. The resin binder may be included in the slurry. Modules may be rigid bars or flexible tapes and may be cut to desired lengths, pre-formed to fit complex configurations and arranged in different directions and with differing fibre and/or matrix materials and extra filler such as metallic powder to impart desired characteristics such as wear resistance, conductivity or differing specific gravity to discrete portions of the final part. In an example a bail element is fabricated from nodules having glass fibres to form the core and graphite fibres to form wear surfaces.
GB1272771A 1970-05-08 1971-05-03 Fabricating composite parts Expired GB1345541A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US3568670A 1970-05-08 1970-05-08

Publications (1)

Publication Number Publication Date
GB1345541A true GB1345541A (en) 1974-01-30

Family

ID=21884205

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1272771A Expired GB1345541A (en) 1970-05-08 1971-05-03 Fabricating composite parts

Country Status (5)

Country Link
JP (1) JPS5114545B1 (en)
CA (1) CA922473A (en)
DE (1) DE2121719A1 (en)
FR (1) FR2088413B1 (en)
GB (1) GB1345541A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4737445A (en) * 1985-10-21 1988-04-12 Hoechst Aktiengesellschaft Photopolymerizable composition and photopolymerizable recording material containing said composition

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2622163C3 (en) * 1976-05-19 1983-05-26 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Profile support made of fiber-reinforced material
FR2440831A1 (en) * 1978-11-07 1980-06-06 Dassault Avions Panels with ancillary ribs of resin contg. high tensile fibres - are made by compression using moulds which exclude excess resin
FR2587649B1 (en) * 1985-09-20 1988-05-27 Renault PROCESS FOR PRODUCING ORIENTED FIBER COMPOSITE MATERIAL PRODUCTS, PARTICULARLY SPRING BLADES, PARTICULARLY FOR MOTOR VEHICLES AND PRODUCTS THEREOF
NL8702487A (en) * 1987-10-19 1989-05-16 Dsm Resins Bv METHOD FOR MANUFACTURE OF PRESS PRODUCTS
US5430932A (en) * 1994-03-15 1995-07-11 Insta Valve Co. Ltd Apparatus for installing a valve on or into an existing pipe
US20240198625A1 (en) * 2022-12-14 2024-06-20 Lockheed Martin Corporation Pi-shaped preform and bonded joints thereof

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2857189A (en) * 1955-01-14 1958-10-21 Rolls Royce Bushing of reinforced elastomer and method of manufacture
BE717862A (en) * 1967-10-24 1969-01-10

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4737445A (en) * 1985-10-21 1988-04-12 Hoechst Aktiengesellschaft Photopolymerizable composition and photopolymerizable recording material containing said composition

Also Published As

Publication number Publication date
FR2088413B1 (en) 1974-03-08
DE2121719A1 (en) 1971-12-02
CA922473A (en) 1973-03-13
FR2088413A1 (en) 1972-01-07
JPS5114545B1 (en) 1976-05-10

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee