| 发明名称 |
SPEED SENSOR FOR A GAS TURBINE ENGINE |
| 摘要 |
A gas turbine engine includes a speed change mechanism. A fan drive shaft has a radially extending surface that is attached to the speed change mechanism. A speed sensor is located adjacent the radially extending surface. |
| 申请公布号 |
US2016298485(A1) |
申请公布日期 |
2016.10.13 |
| 申请号 |
US201514684501 |
申请日期 |
2015.04.13 |
| 申请人 |
United Technologies Corporation |
发明人 |
Sheridan William G.;Husband Jason |
| 分类号 |
F01D21/00;F02C3/107;F01D17/06 |
主分类号 |
F01D21/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a speed change mechanism; a fan drive shaft having a radially extending surface attached to the speed change mechanism; and a speed sensor located adjacent the radially extending surface. |
| 地址 |
Hartford CT US |
