| 发明名称 |
Filter system for blade outer air seal |
| 摘要 |
<p>A gas turbine engine component (54) has a filter (86) mounted adjacent an impingement cavity (80) to filter particles out of a secondary cooling airflow outboard of a cooling channel (84) in communication with the secondary cooling airflow.</p> |
| 申请公布号 |
EP2093384(B1) |
申请公布日期 |
2015.04.29 |
| 申请号 |
EP20080253964 |
申请日期 |
2008.12.11 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
JOE, CHRISTOPHER R.;HUDSON, ERIC A.;SANTELER, KEITH A. |
| 分类号 |
F01D11/08;F01D5/18;F01D25/00;F01D25/12 |
主分类号 |
F01D11/08 |
| 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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