Process for coating an aircraft turbomachine part

摘要

Process for coating an aircraft turbomachine part with an anti-erosion coating The present invention relates to a process for coating a part (1) of an aircraft turbomachine with an anti-erosion coating, the process comprising: - depositing the anti-erosion coating by hot powdering on a part of a turbomachine of aircraft made of a composite material with an organic matrix or of a metallic material, said anti-erosion coating comprising a polyurethane or silicone polymer, said polymer having a glass transition temperature less than or equal to -30 ° C. Figure for the abstract: Fig. 1.