| 发明名称 |
LOW TURN LOSS BAFFLE FLOW DIVERTER |
| 摘要 |
An airfoil according to an example of the present disclosure includes, among other things, an airfoil body having an internal passage for conveying a fluid flow. The internal passage includes first and second passage sections coupled at a turn section. A baffle includes a body arranged in the second passage section to define two cooling flow paths, and a first wedge region extends from the body into the first passage section such that the fluid flow is directed through the turn section between the first passage section and the two cooling flow paths. |
| 申请公布号 |
US2017044906(A1) |
申请公布日期 |
2017.02.16 |
| 申请号 |
US201514824195 |
申请日期 |
2015.08.12 |
| 申请人 |
United Technologies Corporation |
发明人 |
Mongillo Dominic J.;Spangler Brandon W. |
| 分类号 |
F01D5/18;F16L53/00;F01D25/12;F01D5/14;F01D9/04 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An airfoil, comprising:
an airfoil body having an internal passage for conveying a fluid flow, the internal passage including first and second passage sections coupled at a turn section; and a baffle including a body arranged in the second passage section to define two cooling flow paths, and a first wedge region extending from the body into the first passage section such that the fluid flow is directed through the turn section between the first passage section and the two cooling flow paths. |
| 地址 |
Hartford CT US |
