| 发明名称 |
COOLING HOLE ARRANGEMENT FOR ENGINE COMPONENT |
| 摘要 |
A component for a gas turbine engine according to an exemplary aspect of this disclosure includes a surface having a plurality of cooling holes. The surface includes a first region and a second region each having a plurality of cooling holes. The cooling holes within the first region are arranged differently than the cooling holes in the second region. |
| 申请公布号 |
US2015300258(A1) |
申请公布日期 |
2015.10.22 |
| 申请号 |
US201514689168 |
申请日期 |
2015.04.17 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Mongillo Dominic J.;Quach San;Gautschi Steven Bruce;Donnell Brandon S.;Tracy Anita L.;Girma Yafet |
| 分类号 |
F02C7/18;F01D25/12;F02C3/04 |
主分类号 |
F02C7/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A component for a gas turbine engine, comprising:
a surface having a plurality of cooling holes, the surface including a first region and a second region each having a plurality of cooling holes, the cooling holes within the first region being arranged differently than the cooling holes in the second region. |
| 地址 |
Hartford CT US |
