| 发明名称 |
DISK LUG IMPINGEMENT FOR GAS TURBINE ENGINE AIRFOIL |
| 摘要 |
A component for a gas turbine engine includes a root with a neck that extends into a fir tree with at least one tooth, the root includes a feed passage in communication with a multiple of cooling passages that extend through the neck and fir tree. |
| 申请公布号 |
US2016040534(A1) |
申请公布日期 |
2016.02.11 |
| 申请号 |
US201514683408 |
申请日期 |
2015.04.10 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Gautschi Steven Bruce;Quach San;Propheter-Hinckley Tracy A. |
| 分类号 |
F01D5/18;F01D5/02;F01D5/30 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A component for a gas turbine engine, comprising:
a root including a neck and a fir tree, said fir tree including at least one tooth, said root includes a feed passage in communication with a tooth cooling passage that extends through said at least one tooth. |
| 地址 |
Hartford CT US |
