发明申请
US20070141385A1 Method of coating gas turbine components 审中-公开
燃气轮机组件的涂覆方法

Method of coating gas turbine components
摘要:
A method of forming a metal coating on surfaces of internal passages of a turbine blade, the turbine blade having an outer surface and comprising at least one internal passage. The method includes injecting a paint into at least one of the internal passages of the turbine blade, and heat treating the turbine blade such that an aluminide coating is deposited on the surface of the at least one internal passage.
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