| 发明名称 |
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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| 申请公布号 |
US2011086179(A1) |
申请公布日期 |
2011.04.14 |
| 申请号 |
US20100971370 |
申请日期 |
2010.12.17 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHLICHTING KEVIN W.;MALONEY MICHAEL J.;LITTON DAVID A.;FRELING MELVIN;SMEGGIL JOHN G.;SNOW DAVID |
| 分类号 |
C23C4/12;C23C4/08;C23C4/10 |
主分类号 |
C23C4/12 |
| 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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