| 发明名称 |
TURBINE BLADE STAKING PIN |
| 摘要 |
A staking pin for a gas turbine engine is disclosed. The staking pin may include a solid portion extending part of a length of the staking pin, and a hollow portion extending an additional part of the length of the staking pin. The staking pin may be constructed of Alloy X material having an average grain diameter of between about 0.0449 and 0.1270 mm. |
| 申请公布号 |
US2014286782(A1) |
申请公布日期 |
2014.09.25 |
| 申请号 |
US201313752532 |
申请日期 |
2013.01.29 |
| 申请人 |
Solar Turbines Incorporated |
发明人 |
Mulford Adam Curtis;Jarmakani Hussam |
| 分类号 |
F01D5/30 |
主分类号 |
F01D5/30 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A staking pin for a gas turbine engine, comprising:
a solid portion extending part of a length of the staking pin; and a hollow portion extending an additional part of the length of the staking pin, wherein the staking pin is constructed of Alloy X material having an average grain diameter of between about 0.0449 and 0.1270 mm. |
| 地址 |
US |
