| 发明名称 |
ROTOR BLADE PLATFORM COOLING PASSAGE |
| 摘要 |
A rotor blade according to an exemplary aspect of the present disclosure includes, among other things, a platform, an airfoil that extends from the platform and a platform cooling passage extending inside of the platform. The platform cooling passage includes an inlet disposed through a non-gas path surface of the platform and an outlet disposed through a mate face of the platform. |
| 申请公布号 |
US2016305254(A1) |
申请公布日期 |
2016.10.20 |
| 申请号 |
US201415100413 |
申请日期 |
2014.11.17 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SNYDER Daniel A.;BEATTIE Jeffrey S. |
| 分类号 |
F01D5/18;F04D29/58;F04D29/32 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A rotor blade, comprising:
a platform; an airfoil that extends from said platform; a platform cooling passage extending inside of said platform; and said platform cooling passage including an inlet disposed through a non-gas path surface of said platform and an outlet disposed through a mate face of said platform. |
| 地址 |
Hartford CT US |
