A structure made of composite material for a propulsive aircraft assembly includes at least one thermal zone designed to receive electrical energy. Each thermal zone includes at least one resistive skin having an inner film produced in a thermoplastic material made conductive by the inclusion of carbon nanotubes, such that each resistive skin is designed to dissipate, by Joule effect, at least a portion of the electrical energy received by the thermal zone, an intermediate ply produced in a satin fabric impregnated with a thermoplastic material, and an outer film produced in a thermoplastic material.
STRUCTURE FOR PROPULSIVE AIRCRAFT ASSEMBLY, ASSOCIATED PROPULSIVE SYSTEM AND ASSEMBLY
2018-06-28
Patent
Electronic Resource
English