Invention Application
US20150336850A1 Thermal Barrier Coating for CMAS Resistance and Low Thermal Conductivity 审中-公开
用于CMAS电阻和低导热性的热障涂层

Thermal Barrier Coating for CMAS Resistance and Low Thermal Conductivity
Abstract:
A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.
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