| 发明名称 |
PLATFORM COOLING CIRCUIT FOR A GAS TURBINE ENGINE COMPONENT |
| 摘要 |
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform having a first path side and a second path side and a platform cooling circuit disposed on one of the first path side and the second path side of the platform. The platform cooling circuit includes a first core cavity, a cavity in fluid communication with the first core cavity, and a cover plate positioned to cover at least the cavity. |
| 申请公布号 |
US2016115803(A1) |
申请公布日期 |
2016.04.28 |
| 申请号 |
US201514949922 |
申请日期 |
2015.11.24 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
PAPPLE Michael Leslie Clyde;BERGMAN Russell J.;ENNACER Mohammed;GREGG Shawn J.;MONGILLO Dominic J. |
| 分类号 |
F01D9/04;F01D25/12 |
主分类号 |
F01D9/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A component for a gas turbine engine, comprising:
a platform having a first path side and a second path side; and a platform cooling circuit disposed on one of said first path side and said second path side of said platform, wherein said platform cooling circuit includes:
a first core cavity;a cavity in fluid communication with said first core cavity; anda cover plate positioned to cover at least said cavity. |
| 地址 |
Hartford CT US |
