| 发明名称 |
GAS TURBINE GEARBOX INPUT SHAFT |
| 摘要 |
A gas turbine gearbox input shaft including a gear coupling engaged with an engine power gearbox and extending along a central engine axis thereof. The shaft may include a separable tuning segment coaxially joined to the gear coupling, and a spool coupling joined to the separable tuning segment opposite of the gear coupling, the spool coupling being engaged with an engine turbine spool. Methods of using the input shaft are also provided. |
| 申请公布号 |
US2017096941(A1) |
申请公布日期 |
2017.04.06 |
| 申请号 |
US201514876124 |
申请日期 |
2015.10.06 |
| 申请人 |
General Electric Company |
发明人 |
Antelo Randy Thomas;van der Merwe Gert J.;Fang Ning;Miller Steve D. |
| 分类号 |
F02C7/36;F02C3/04 |
主分类号 |
F02C7/36 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine gearbox input shaft, comprising:
a gear coupling engaged with an engine power gearbox and extending along a central engine axis thereof; a separable tuning segment coaxially joined to the gear coupling; and a spool coupling joined to the separable tuning segment opposite of the gear coupling, the spool coupling being engaged with an engine turbine spool. |
| 地址 |
Schenectady NY US |
