Method for producing an oxidation protection coating at least in regions on a component of a thermal gas turbine
AssigneeMTU Aero Engines AG
InventorsNils Weidlich, Frank Seidel, Ezgi Schoening
Life of this patent
Estimating the term…
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.
Claims10
A method for producing an oxidation protection coating at least in regions on a component of a thermal gas turbine, comprising the steps of:
- coating of the component at least in regions with a lacquer, which comprises at least one UV-curable binder and metal particles;
- curing of the lacquer by exposure to UV light;
- and
- thermally treating the component at least in the region of the cured lacquer for production of the oxidation protection coating.
Dependencies are inferred from the claim text.