| 发明名称 |
Thermal Barrier Coatings and Application Methods |
| 摘要 |
A gas turbine engine component has a metallic substrate. A coating is on the substrate. A barrier coat is applied while varying a speed of the component rotation so as to provide a corresponding microstructure to the barrier coat. |
| 申请公布号 |
US2010304037(A1) |
申请公布日期 |
2010.12.02 |
| 申请号 |
US20090475913 |
申请日期 |
2009.06.01 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
ZIMMERMAN BENJAMIN J.;LITTON DAVID A.;BLONDIN JOHN F. |
| 分类号 |
C23C10/00;B05D1/00;C23C4/08;C23C28/00;F01D5/28 |
主分类号 |
C23C10/00 |
| 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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