| 发明名称 |
COATING PROCESS FOR GAS TURBINE ENGINE COMPONENT WITH COOLING HOLES |
| 摘要 |
A method of coating a component having a multiple of cooling holes includes removing at least a portion of a prior coating; directing a gas through at least one of the multiple of cooling holes; and applying a coat layer while directing the gas through at least one of the |
| 申请公布号 |
EP2935834(A1) |
申请公布日期 |
2015.10.28 |
| 申请号 |
EP20130865400 |
申请日期 |
2013.12.17 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BURD, STEVEN W.;BARRON, ALAN C. |
| 分类号 |
F02C7/12;B23P6/00;C23C4/00;C23C4/02;C23C4/18;C23C28/00;F01D5/00;F01D5/18;F01D5/28;F01D25/12 |
主分类号 |
F02C7/12 |
| 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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