Method of producing a formable composite material

Abstract: The invention provides a method of providing a formable composite material comprising providing a reinforcing material (9) having a plurality of superimposed layers (1-6), each layer consisting of a plurality of unidirectional non-woven yarns or threads (10) laid side-by-side, the yarns or threads in at least some of the different layers extending in different directions, said layers being stitched (12) together, and before said stitching incorporating in or with the reinforcing material (9) a matrix material (7, 8)

Description: The present invention relates to a method of producing formable composite materials, e.g., for forming reinforced plastics or other articles. It is known to produce formable composite materials, in the form of so-called "pre-pregs", which comprise a mat of woven or non-woven glass fibres or other reinforcing material impregnated with a synthetic resin matrix material. Such known formable composite materials suffer from the disadvantages that the distribution of the fibres in a non-woven mat is random and cannot be controlled, so that the strength characteristics of an article formed therefrom can be unpredictable, that in woven mats the weft and warp are crimped where they intersect one another which reduces the strength thereof, and that they have a limited shelf life. EP-A-33244 discloses a method in accordance with the preamble of Claim 1. The present invention has as its object to provide a continuous method of producing a formable composite material in which the reinforcing material is multi-axial and can be "engineered" to suit particular applications and which, according to a preferred embodiment, has an indefinite shelf life. The invention provides a method of producing a formable composite material as set out in claim 1. Prefered embodiments are defined in the dependent claims. Preferably, said layers are stitched together by knitting therethrough and the yarns or threads in each of said layers are held by said stitching in fixed relation to one another. The matrix material may be a plastics material, e.g. a thermoplastic or thermosetting resin, or a metal, ceramics or other material which during subsequent forming of the composite material e.g., under heat and pressure, will consolidate to form a matrix around the reinforcing material. A sheet, film, ribbon tape or tissue of woven or non-woven material, e.g. a foamed material or a polyester or other thermoset plastics material, may be interposed between two or more of said layers and/or applied to at least one outer surface of the reinforcing material, and stitched in with said layers, to impart required properties to the composite material. According to a preferred embodiment of the present invention, said matrix material is at least one film, sheet, ribbon, tape or tissue of thermoplastic material which is interposed between at least two of said layers and/or is applied to one or both outer surfaces of the superimposed layers, and is stitched in with said layers. Advantageously a said film, sheet, ribbon, tape or tissue of thermoplastic material is interposed between each of the adjacent layers of the reinforcing material. Such a composite material can have an indefinite shelf life, is easy to store and to handle, and is simple to use since the composite material simply needs heating prior to forming to soften the thermoplastic material and allow flow to wet the reinforcing material prior to or during forming of the composite material. Moreover, with the composite material produced by this embodiment equal distribution of the thermoplastic matrix material throughout the reinforcing material is ensured. According to an alternative embodiment, the reinforcing material is impregnated e.g., sprayed, with synthetic resin matrix material, e.g., a thermoplastic or thermosetting resin material, prior to said stitching. In this way formable composite materials can be produced which have the advantage that the orientation of the yarns or threads in the reinforcing material is known, the yarns or threads are straight with no crimps therein, and that accordingly the strength characteristics of an article formed from the composite material are of a maximum and can be predicted. According to another embodiment of the present invention, a coating of synthetic resin matrix material, e.g., thermosetting resin material, is applied to one or both outer surfaces of the reinforcing material prior to said stitching. Said coating may be tacky and may be covered with a release paper, either before or after said stitching, until the composite material is required for use when the release paper may be removed. According to a further embodiment of the present invention said yarns or threads of reinforcing material in at least some of said layers have incorporated or interspersed therewith said matrix material. According to one embodiment, the yarns or threads of reinforcing material have interspersed therebetween yarns or threads of thermoplastic resin material. In another embodiment, at least some of the yarns or threads of reinforcing material are coated or impregnated with a matrix material, e.g., are coated or impregnated with a matrix material in powder form which is retained in place by an outer coating or sheath, e.g., of thermoplastics material. The powder matrix material may be a thermoplastic or thermosetting resin material or a ceramic or metal material. For example, the reinforcing material may be of carbon fibre and the powder matrix material of carbon to provide a carbon/carbon composite. This again provides a composite material which is easy to handle, which can have an indefinite shelf life and which is easy to use. The term "yarns or threads" as used herein and in the claims hereof means yarns, threads, monofilaments, rovings, tows or the like, of continuous or discontinuous fibres, as conventionally used. Said yarns or threads of the reinforcing material are preferably of glass e.g., glass fibre, although they can, if desired, be of other suitable reinforcing materials such as carbon fibre, aramid fibre, ceramic fibre, polyethylene fibre, polyester fibre, metal or mixtures thereof. The yarns or threads in at least two of said layers preferably extend at 90° to one another. Advantageously, the yarns or threads in at least one further layer extend at an angle of from 45° to 90° with respect to the yarns or threads in at least one of said at least two layers. Thus, for example, said layers may comprise at least a layer in which the yarns or threads extend in a first direction, a layer in which the yarns or threads extend in a second direction at 90° to the first direction, a layer in which the yarns or threads extend in a third direction at 45° to the first direction, and a layer in which the yarns or threads extend in a fourth direction at 45° to the first direction and 90° to the third direction. Such a material may be isotropic. In at least one of said layers the yarns or threads may be laid at different densities in different parts of the layer to provide different strength characteristics in different parts of the composite material. In this way the composite material can be "engineered" to suit particular requirements. The yarn or thread used in said stitching is engineered or selected to assist in imparting required properties or characteristics to the composite material, e.g., desired mechanical or electrical properties. For example, the yarn or thread may be a thermoplastic material which will become part of the matrix when the composite material is formed, e.g., under heat and pressure. Different layers of said reinforcing material and/or the matrix material in or between different layers of said reinforcing material may have different properties, e.g., different mechanical, physical or electrical properties, such as different mechanical strengths or different electrical conductivities and/or electrical resistances and/or dielectric properties, to provide a "hybrid" composite material having required properties. If desired, additional pieces or "patches" of reinforcing material may be introduced between two or more of said layers prior to said stitching to provide additional reinforcement or thickness at selected positions in the composite material, thus enabling the composite material to be further "engineered" to suit its final application. The present invention will be more particularly described with reference to the accompanying drawings, in which: Fig.1 diagramatically illustrates a method of producing a composite material according to a preferred embodiment, and Fig.2 is a greatly enlarged cross-section of a yarn or thread used in another embodiment. Referring to Fig. 1 of the drawings it will be seen that in the method illustrated a reinforcing material 9 is produced having a plurality of layers 1-6 superimposed upon one another. Each of the layers 1-6 comprises a plurality of unidirectional non-woven yarns or threads 10 and the yarns or threads 10 in at least some of the different layers extend in different directions as shown. Thus, as illustrated, the yarns or threads 10 in the layer 1 extend longitudinally of the reinforcing material, the yarns or threads 10 in the layer 2 extend at right angles to the yarns or threads 10 in the layer 1, the yarns or threads 10 in the layer 3 extend at 45° with respect to the yarns or threads in the layers 1 and 2, and so on as shown. It will be understood that the embodiment shown is for illustration only and that the reinforcing material can comprise any required number of layers with the yarns or threads in the different layers oriented as required. Interposed between at least two of the layers 1-6, and preferably between each of the adjacent layers 1-6, is a film or sheet of thermoplastic material 8. In addition, a sheet or film of thermoplastic material 7 is applied to one or both outer surfaces of the reinforcing material 9. The layers 1-6 of the reinforcing material 9, together with the films or sheets of thermoplastic material 7, 8, are stitched together by knitting therethrough as illustrated at 11 to form stitching 12. The stitching is such that the yarns or threads 10 in each of the layers 1-6 are held in fixed position relative to one another. Yarns or threads 13 of thermoplastic material can be interspersed or co-mingled with the yarns or threads 10 in one or more of the layers 1-6 as illustrated at 14, either to provide additional thermoplastic material in the composite material or to replace the thermoplastic sheet or film material 7 and/or 8. If desired, pieces or patches 15 of reinforcing material can be inserted between any of the adjacent layers 1-6 prior to said stitching, to provide additional reinforcement or thickness of a required size and shape and at required locations in the finished composite material. Because the yarns or threads 10 in the different layers 1-6 are multi-axial and the yarns or threads 10 in the different layers are firmly held by the stitching 12, the composite material produced by the method of the present invention can be formed to complex shapes without creasing or wrinkling. In the embodiment illustrated in Fig. 2 at least some of the yarns or threads 10 and/or the yarns or threads 13 comprise a core of reinforcing yarn or thread 16, a layer of matrix material 17 around the yarn or thread 16 and a sheath or coating 18 around the layer of matrix material 17. The core 16 may be a reinforcing yarn or thread of glass fibre, aramid fibre, carbon fibre, ceramic fibre, metal, polyester fibre, polyethylene fibre or other reinforcing material, or mixtures of two or more thereof. The matrix material 17 may be in powder or other suitable form and may comprise a thermoplastic or thermosetting resin material, ceramic, carbon, metal or other suitable matrix forming material. The sheath or coating 18 may be a thermoplastics or other suitable material. In accordance with this embodiment composite materials of various different combinations of reinforcing and matrix materials can be produced, such as glass fibre/thermosetting resin or carbon/carbon. Yarns or threads 10 according to this embodiment can be used in place of or in conjunction with the films or sheets 7 and/or 8 and/or the yarns or threads 13.

Claims: A method of producing a formable composite material comprising a reinforcing material (9) having a plurality of superimposed layers (1-6), each layer (1-6) consisting of a plurality of unidirectional non-woven yarns or threads (10) laid side-by-side, the yarns or threads (10) in at least some of the different layers extending in different directions and incorporating in or with the reinforcing material a matrix material (7,8,13) the method characterised in that the reinforcing material is made by laying said plurality of yarns or threads (10) of a layer side-by-side, each succeeding layer being superimposed on the preceding layer, and stitching the layers of yarns or threads together to hold the yarns or threads in fixed relation to one another, after incorporation of the matrix material (7,8,13), and wherein the method is such that the properties of the layers of said reinforcing material and the matrix material in or between different layers of said reinforcing material and the yarn or thread used in said stitching are selected and at least one of said layers of yarns or threads may be laid at different densities in different parts of the layer, whereby to produce a formable composite material having required properties. A method according to claim 1, wherein said layers (1-6) are stitched together by knitting therethrough. A method according to claim 1 or 2, wherein said matrix material (7,8,13) is a thermoplastic or thermosetting resin material, or a metal or ceramics material. A method according to any one of the preceding claims wherein a sheet, film, tissue, ribbon or tape of woven or non-woven material is interposed between at least two of said layers, and/or is applied to at least one outer surface of the reinforcing material (9), and is stitched in with said layers (1-6). A method according to claim 4, where said sheet, film, tissue ribbon or tape is of a foamed material or a polyester or other thermosetting plastics material. A method according to any one of the preceding claims, wherein said matrix material (7,8) is a film, sheet, ribbon or tape of thermoplastics material which is interposed between at least two of said layers (1-6) and/or is applied to one or both outer surfaces of the superimposed layers and is stitched in with said layers (1-6). A method according to claim 6 wherein a said film, sheet, ribbon or tape of thermoplastics material is interposed between each of the adjacent layers (1-6) of the reinforcing material. A method according to any one of claims 1 to 5, comprising impregnating said reinforcing material with synthetic resin matrix material (7,8). A method according to any one of claims 1 to 5, comprising applying a coating of synthetic resin matrix material to at least one outer surface of the reinforcing material (9). A method according to claim 9, wherein said coating is tacky and a release paper is applied thereover. A method according to claim 8 or 10, wherein said synthetic resin material is a thermosetting resin material. A method according to any one of the preceding claims wherein said yarns or threads (10) are made of glass. A method according to any one of claims 1 to 11, wherein said yarns or threads (10) are of glass fibre, carbon fibre, aramid fibre, ceramic fibre, metal, polyethylene or mixtures thereof. A method according to any one of the preceding claims wherein said yarns or threads (10) have incorporated or interspersed therewith yarns or threads (13) of thermoplastic resin material. A method according to any one of the preceding claims, wherein at least some of said yarns or threads (10,13) comprise a core (16) of reinforcing yarn or thread, a layer of matrix material (17) around the core and an outer sheath or layer (18) around the layer of matrix material (17). A method according to any one of the preceding claims where the yarns or threads (10) in at least two of said layers (1-6) extend at 90° to one another. A method according to claim 16, wherein the yarns or threads in at least one further layer extend at an angle of from 45° to 90° with respect to the yarns or threads (10) in at least one of said at least two layers (1-6). A method according to claim 17 wherein said layers comprise at least a layer in which the yams or threads (10) extend in a first direction, a layer in which the yarns or threads extend in a second direction at 90° to the first direction, a layer in which the yarns or threads (10) extend in a third direction at 45° to the first direction, and a layer in which the yarns or threads extend in a fourth direction at 45° to the first direction and 90° to the third direction. A method according to claim 18 wherein the reinforcing material is isotropic. A method according to any one of the preceding claims, comprising inserting pieces or patches of reinforcing material (15) at selected positions between said layers (1-6) prior to said stitching.

Inventors: VANE JEFFREY ALBERT, VANE, JEFFREY ALBERT
Applicants: TECH TEXTILES INT LTD, TECH TEXTILES INTERNATIONAL LIMITED
Application year: 1989
Main classification: B29C70
IPC codes: B29C70, B32B5, D04H13, D04B21, B32B17, B32B27