| CPC B29C 43/203 (2013.01) [B29C 43/146 (2013.01); B32B 5/02 (2013.01); B32B 29/005 (2013.01); B32B 29/02 (2013.01); B32B 29/06 (2013.01); B29K 2101/12 (2013.01); B29K 2711/123 (2013.01); B32B 2255/12 (2013.01); B32B 2255/26 (2013.01); B32B 2262/101 (2013.01); B32B 2262/106 (2013.01); B32B 2307/54 (2013.01); B32B 2307/546 (2013.01); B32B 2307/558 (2013.01); B32B 2307/718 (2013.01); B32B 2307/72 (2013.01)] | 15 Claims |

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1. A method for the manufacture of a post-deformable high-pressure composite, characterized in that it comprises the following steps:
a) formation of a composite (1) by the arrangement of at least two layers of material, among which:
i. a plurality of Kraft paper sheets (3) coated with at least one type of thermoplastic resin, forming a laminate with two opposite flat surfaces; and
ii. a decorative coating (2) arranged on at least one of the flat surfaces of the laminate, the said decorative coating (2) being impregnated with at least one thermosetting resin or at least one thermoplastic resin;
b) hot compression moulding of the composite (1) formed in step a) by means of compression moulding at a temperature between 120° C. and 200° C. and at a pressure between 50 and 120 bar for 5 to 25 minutes;
c) the composite (1) formed in step b) remains in the compression moulding means until the latter cool to a temperature ranging from 17 to 22° C. and at a pressure between 50 and 120 bar;
wherein the Kraft paper sheets undergo a surface treatment with cold plasma produced by dielectric-barrier discharge at atmospheric pressure; and
wherein after step (i), synthetic fibres are additionally laid on at least one side of the laminate in a proportion between 5 and 20% of the total weight of the laminate.
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