| 申请日期 | 2025-07-19 | 申请号 | US11465288 |
| 公开（公告）号 | US7229705B1 | 公开（公告）日 | 2007-06-12 |
| 公开国别 | US | 申请人省市代码 | 全国 |
| 申请人 | Mary B Johnson legal representative; Robert W Bruce | ||
| 简介 | The present invention is a turbine engine component comprising a superalloy substrate, a bond coat overlying the substrate having a thickness in the range of about 0.0005 inch to about 0.005 inch, a thin alumina scale overlying the bond coat, and a thermal barrier coating (TBC) overlying the thin alumina scale, the TBC having a thickness in the range of about 0.0025 inch to about 0.010 inch, and comprising at least mischmetal oxide. | ||
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