Method of manufacturing composite materials

• US 4,445,951 A
• Filed: 06/01/1982
• Issued: 05/01/1984
• Est. Priority Date: 07/01/1981
• Status: Expired due to Fees

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Lind, David J., Richards, Joyce
• Primary Examiner(s): Dawson, Robert A.
• Application Number:
  US06/383,619
• Time in Patent Office: 700 Days
• Field of Search: 156/93, 156/309.6, 428/102, 428/103, 428/104, 428/902, 428/367, 428/375, 428/396, 112/401, 112/412, 112/415
• US Class Current: 156/93
• CPC Class Codes: B29B 15/105 of reinforcement of definite length with a matrix in solid form, e.g. powder, fibre or sheet form calendering B29C70/506
• CPC Class Codes: B29C 70/34 and shaping or impregnating by compression , i.e. combined with compressing after the lay-up operation
• CPC Class Codes: B29C 70/465 and impregnating by melting a solid material, e.g. sheets, powders of fibres
• CPC Class Codes: B29K 2101/12 Thermoplastic materials
• CPC Class Codes: D04H 3/002 Inorganic yarns or filaments
• CPC Class Codes: D04H 3/10 with bonds between yarns or filaments made mechanically
• CPC Class Codes: D04H 3/115 by applying or inserting filamentary binding elements
• CPC Class Codes: D04H 3/12 with filaments or yarns secured together by chemical or thermo-activatable bonding agents, e.g. adhesives, applied or incorporated in liquid or solid form
• CPC Class Codes: Y10S 428/902 High modulus filament or fiber
• CPC Class Codes: Y10T 428/24033 including stitching and discrete fastener[s], coating or bond
• CPC Class Codes: Y10T 428/2405 Coating, impregnation, or bond in stitching zone only
• CPC Class Codes: Y10T 428/2918 including free carbon or carbide or therewith [not as steel]
• CPC Class Codes: Y10T 428/2933 Coated or with bond, impregnation or core
• CPC Class Codes: Y10T 428/2971 Impregnation

Abstract

A method of manufacturing a composite material in which layers of reinforcing filaments are stitched across with filaments of a thermoplastic polymer and then interposed between sheets of the same thermoplastic polymer as that used to stitch across the reinforcing filaments. The resultant stack is then heated under pressure for sufficient time for the thermoplastic polymer to impregnate the reinforcing filaments whereupon the thus formed composite is cooled under compression in order to avoid any distortion thereof.

Claims

1. A method of manufacturing a composite material comprising the successive steps of:

(1) stitching across at least one layer of reinforcing filaments with filaments of a thermoplastic polymer so that said thermoplastic polymer filaments maintain said reinforcing filaments in a given configuration,

(2) forming a structure of said at least one layer of the thus cross-stitched reinforcing filaments and sheets of the same thermoplastic polymer as that used in filament form to cross-stitch said reinforcing filaments so that one layer of cross-stitched filaments is interposed between two sheet of said thermoplastic polymer,

(3) compressing said structure at a temperature at which said thermoplastic polymer is mobile,

(4) maintaining said compression for sufficient time and temperature for the thermoplastic polymer of the sheets and filaments to impregnate said at least one layer of reinforcing filaments,

(5) cooling the thus formed composite material under compression in order to avoid any distortion thereof, and subsequently

(6) discontinuing said compression.

2. A method of manufacturing a composite material as claimed in claim 1 wherein said at least one layer of reinforcing filaments is in the form of tows.

3. A method of manufacturing a composite material as claimed in claim 1 wherein said at least one layer of reinforcing filaments is in the form of a woven cloth.

4. A method of manufacturing a composite material as claimed in claim 3 wherein at least some of the weft filaments of the cloth are constituted by the filaments of said thermoplastic polymer.

5. A method of manufacturing a composite material as claimed in claim 1 wherein said thermoplastic polymer is an aromatic polyether.

6. A method of manufacturing a composite material as claimed in claim 5 wherein said aromatic polyether is an aromatic polyetheretherketone.

7. A method of manufacturing a composite material as claimed in claim 1 wherein said reinforcing filaments are of carbon.