| 发明名称 |
AIRFOIL COOLING CIRCUIT AND CORRESPONDING AIRFOIL |
| 摘要 |
An airfoil cooling circuit for a gas turbine engine having at least one internal cavity with a lobed cross-sectional shape. |
| 申请公布号 |
US2015110611(A1) |
申请公布日期 |
2015.04.23 |
| 申请号 |
US201314399572 |
申请日期 |
2013.05.28 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
Bergholz Robert Frederick |
| 分类号 |
F01D5/14;F01D25/12;F01D5/18 |
主分类号 |
F01D5/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An airfoil cooling circuit for a gas turbine engine comprising:
at least one internal cavity; wherein said cavity has a lobed cross-sectional shape. |
| 地址 |
Schenectady NY US |
