Method of coating gas turbine components

Details Method of coating gas turbine components Method of coating gas turbine components

C - Chemistry, Metallurgy

23

C

C23C 30/00 (2006.01) B05D 3/02 (2006.01) B05D 7/14 (2006.01)

Patent

CA 2576572

A method of forming a metal coating on surfaces of internal passages of a turbine part (40) includes applying a nickel aluminum bond coating to an external surface of the turbine part, positioning the turbine part in a VPA chamber (88), coupling a gas manifold to at least one internal passage inlet, and coating at least a portion of the internal surface and the external of the turbine part by a vapor phase aluminiding (VPA) process using metal coating gases to form a coating on the internal surfaces of the turbine part.

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