| 发明名称 |
GEAR GEOMETRY WITH FLUID RESERVOIR AND FLUID PATHS |
| 摘要 |
A helicopter is provided and includes an engine, a rotor, a gear train configured to transmit torque from the engine to the rotor such that the rotor is rotatable about an axis of rotation, a primary lubrication system, which is configured to supply the gear train with a fluid and a secondary lubrication system disposed in a gear of the gear train, including a fluid reservoir, which is configured to receive and store the fluid and to continue to supply the gear train with the fluid following a failure of the primary lubrication system. |
| 申请公布号 |
US2015260274(A1) |
申请公布日期 |
2015.09.17 |
| 申请号 |
US201313930488 |
申请日期 |
2013.06.28 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
SAMMATARO Stephen R.;PATRY Ryan |
| 分类号 |
F16H57/04;B64C27/12 |
主分类号 |
F16H57/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A helicopter, comprising:
an engine; a rotor; a gear train configured to transmit torque from the engine to the rotor such that the rotor is rotatable about an axis of rotation; a primary lubrication system, which is configured to supply the gear train with a fluid; and a secondary lubrication system disposed in a gear of the gear train, including a fluid reservoir, which is configured to receive and store the fluid and to continue to supply the gear train with the fluid following a failure of the primary lubrication system. |
| 地址 |
Stratford CT US |
