Patent ID: 9604425
Date: 2017-03-28
CPC Classifications: B29C,B29D,B29L,B64C,B64D,Y02T

Claim:
1. A method for producing a skin of a leading edge for an aircraft wing element, comprising an assembly of resistive heating elements designed to form an integral part of a system for de-icing and/or anti-icing of the leading edge, said method comprising: curing a stack in a mould between two moulding surfaces facing each other, said stack comprising: keeping on circulating an injection resin in said mould so as to generate and keep a counter-pressure at a periphery of the stack for pressurization of the injection resin contained in said stack until the injection resin of the stack has set; then stopping the circulating of the injection resin after the injection resin of the stack has set, leading to the injection resin being introduced between the stack and each of the two mould surfaces in order to apply a surface pressure on said stack until the said injection resin in said stack sets.