公开(公告)号：US20240287634A1

公开(公告)日：2024-08-29

申请号：US18581584

申请日：2024-02-20

Applicant: MTU Aero Engines AG

Inventor： Nils Weidlich ,  Frank Seidel ,  Ezgi Schoening

IPC: C21D1/72 ,  B05D3/04 ,  B05D3/06 ,  B05D7/16 ,  C21D1/26 ,  C21D1/74

CPC classification number: C21D1/72 ,  B05D3/0473 ,  B05D3/067 ,  B05D7/16 ,  C21D1/26 ,  C21D1/74 ,  B05D2601/28

Abstract: The invention relates to a method for producing at least in regions an oxidation protection coating on a component of a thermal gas turbine. In accordance with the invention, the method comprises the steps of coating the component at least in regions with a lacquer, which comprises at least one UV-curable binder and metal particles, curing the lacquer by exposure to UV light, and thermal treatment of the component at least in the region of the cured lacquer for production of the oxidation protection coating.