| 发明名称 |
LIGHT WEIGHT PROPULSOR GEARBOX |
| 摘要 |
A propulsor gearbox assembly for a translational thrust propeller includes a housing defining an interior cavity, a planetary gear assembly contained within the interior cavity, an input shaft aligned on a first axis or rotation, and an output shaft aligned along a second axis of rotation. The first axis of rotation is coaxial with the second axis of rotation. |
| 申请公布号 |
US2016207619(A1) |
申请公布日期 |
2016.07.21 |
| 申请号 |
US201414915158 |
申请日期 |
2014.08.27 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
DARROW, JR. David A.;Tully Thomas L. |
| 分类号 |
B64C27/14;F16H57/04;F16H1/28 |
主分类号 |
B64C27/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A propulsor gearbox assembly for a translational thrust propeller, comprising:
a housing defining an interior cavity; a planetary gear assembly contained within the interior cavity; a gear-driven pump and a sump chamber contained within the interior cavity, wherein the gear-driven pump is configured to be driven by the planetary gear assembly; an input shaft aligned on a first axis or rotation; and an output shaft aligned along a second axis of rotation; wherein the first axis of rotation is coaxial with the second axis of rotation. |
| 地址 |
Stratford CT US |
