Method of coating gas turbine components

Coating processes – Interior of hollow article coating – Coating by vapor – gas – mist – or smoke

Reexamination Certificate

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C427S239000, C427S250000, C427S294000, C427S295000, C427S376300

Reexamination Certificate

active

07838070

ABSTRACT:
A method of forming a metal coating on surfaces of internal passages of a turbine blade includes, in an exemplary embodiment, the steps of positioning the turbine blade in a CVD chamber, coupling a reagent gas manifold to at least one internal passage inlet, and coating the surfaces of the at least one internal passage by a CVD process using metal coating reagent gases to form a metal coating on the surfaces of the at least one internal passage.

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