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US07875370B2 Thermal barrier coating with a plasma spray top layer 有权
带有等离子喷涂顶层的隔热涂层

Thermal barrier coating with a plasma spray top layer
摘要:
A turbine engine component has a substrate, a thermal barrier coating deposited onto the substrate, and a sealing layer of ceramic material on an outer surface of the thermal barrier coating for limiting molten sand penetration.
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