| 发明名称 |
Flow directing cover for engine component |
| 摘要 |
An assembly for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, an airfoil including a radial end, a first passageway having an outlet at the radial end, and a second passageway having an inlet at the radial end. The assembly further includes a cover having at least one turning cavity configured to direct fluid expelled from the outlet of the first passageway into the inlet of the second passageway. |
| 申请公布号 |
US2016312632(A1) |
申请公布日期 |
2016.10.27 |
| 申请号 |
US201514693359 |
申请日期 |
2015.04.22 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Hagan Benjamin F.;Waite Ryan Alan;Dube Bryan P.;Thornton Lane |
| 分类号 |
F01D9/06 |
主分类号 |
F01D9/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An assembly for a gas turbine engine, comprising:
an airfoil including a radial end, a first passageway having an outlet at the radial end, and a second passageway having an inlet at the radial end; and a cover including at least one turning cavity configured to direct fluid expelled from the outlet of the first passageway into the inlet of the second passageway. |
| 地址 |
Hartford CT US |
