STRUCTURE FOR AN AIRCRAFT PROPULSION ASSEMBLY, ASSOCIATED SYSTEM AND PROPULSION ASSEMBLY

摘要

The invention relates to a structure (16) made of composite material for an aircraft propulsion unit, the structure (16) comprising at least one thermal zone (24) able to receive electrical energy, the structure (16) being characterized in each thermal zone (24) comprises at least one resistive film (26) comprising an inner film (30) made of a thermoplastic material made conductive by inclusion of carbon nanotubes, so that each resistive film (26) is suitable for dissipating, by Joule effect, at least a portion of the electrical energy received by the thermal zone (24), an intermediate fold (28) made of a satin fabric impregnated with a thermoplastic material, and an outer film (32) made in a thermoplastic material.