发明名称 |
HYBRID THERMAL BARRIER COATING AND PROCESS OF MAKING SAME |
摘要 |
A thermal barrier coating is applied to a turbine engine component having a substrate. The thermal barrier coating has a first layer which has a strain tolerant columnar microstructure at an interface with the substrate for spallation resistance and a second layer which is porous conduction and radiation thermally resistant at an outer surface of the thermal barrier coating. |
申请公布号 |
EP2971240(A1) |
申请公布日期 |
2016.01.20 |
申请号 |
EP20130878078 |
申请日期 |
2013.12.30 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HAZEL, BRIAN T;LITTON, DAVID A.;MALONEY, MICHAEL J. |
分类号 |
C23C28/00;C23C4/11;C23C4/134;C23C28/04 |
主分类号 |
C23C28/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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