| 发明名称 |
GAS TURBINE ENGINE AIRFOIL WITH WISHBONE BAFFLE COOLING SCHEME |
| 摘要 |
A gas turbine engine component includes a structure including spaced apart first and second exterior walls that extend in a first direction to an endwall. The first and second exterior walls are joined at the endwall to provide a cooling cavity. A wishbone baffle is arranged in the cooling cavity and includes first and second interior walls respectively adjacent to the first and second exterior walls. The first and second interior walls extend in the first direction to and are joined by an apex to provide a first cavity. The wishbone baffle separates the first cavity from a second cavity provided between the apex and the endwall. |
| 申请公布号 |
US2016208621(A1) |
申请公布日期 |
2016.07.21 |
| 申请号 |
US201414915513 |
申请日期 |
2014.08.27 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Spangler Brandon W.;Otero Edwin |
| 分类号 |
F01D5/18;B28B7/34;B28B1/30;F01D9/04;F01D25/12 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine component comprising:
a structure including spaced apart first and second exterior walls extending in a first direction to an endwall, the first and second exterior walls are joined at the endwall to provide a cooling cavity; and a wishbone baffle arranged in the cooling cavity and including first and second interior walls respectively adjacent to the first and second exterior walls, the first and second interior walls extending in the first direction to and joined by an apex to provide a first cavity, the wishbone baffle separates the first cavity from a second cavity provided between the apex and the endwall. |
| 地址 |
Hartford CT US |
