| 发明名称 |
GAS TURBINE ENGINE COMPONENT WITH FLOW SEPARATING RIB |
| 摘要 |
A component according to an exemplary aspect of the present disclosure includes, among other things, a wall that extends about a cooling cavity. The cooling cavity is a dual-fed cavity that is fed from at least two different locations. A rib separates the cooling cavity into a first portion and a second portion that is fluidly isolated from the first portion. |
| 申请公布号 |
US2015285081(A1) |
申请公布日期 |
2015.10.08 |
| 申请号 |
US201514665170 |
申请日期 |
2015.03.23 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SPANGLER Brandon W.;CAVALLO Gina |
| 分类号 |
F01D5/18;F01D5/14 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A component, comprising:
a wall that extends about a cooling cavity, wherein said cooling cavity is a dual-fed cavity that is fed from at least two different locations; and a rib that separates said cooling cavity into a first portion and a second portion that is fluidly isolated from said first portion. |
| 地址 |
Hartford CT US |
