| 发明名称 |
Thermal barrier coating with a plasma spray top layer |
| 摘要 |
<p>A turbine engine component (10) has a substrate (12), a thermal barrier coating (14) deposited onto the substrate (12), and a sealing layer (16) of ceramic material on an outer surface of the thermal barrier coating (14) for limiting molten sand penetration.</p> |
| 申请公布号 |
EP1889940(A2) |
申请公布日期 |
2008.02.20 |
| 申请号 |
EP20070253170 |
申请日期 |
2007.08.13 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHLICHTING, KEVIN W.;LITTON, DAVID A.;MALONEY, MICHAEL J.;FRELING, MELVIN;SMEGGIL, JOHN G.;SNOW, DAVID |
| 分类号 |
C23C4/18;C23C4/02;C23C4/12;C23C28/00;C23C28/04 |
主分类号 |
C23C4/18 |
| 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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