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US08147982B2 Porous protective coating for turbine engine components 有权
涡轮发动机部件的多孔保护涂层

Porous protective coating for turbine engine components
Abstract:
A method for coating a substrate of a turbine engine component, the method comprising cold spray depositing a metal-based material onto a surface of the substrate, and heating the deposited metal-based material to increase the porosity of the deposited metal-based material.
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