| 发明名称 |
DRIVE SYSTEM FOR AIRCRAFT LANDING GEAR |
| 摘要 |
A drive system for an aircraft landing gear is described. The drive system includes a drive pinion, a drive shaft arranged to rotate the drive pinion about a drive axis, and a casing which rotatably supports the drive shaft. The drive pinion is rotatably supported on the casing by a self-aligning bearing. The drive pinion is coupled to the drive shaft by a flexible coupling adapted to transfer torque between the drive pinion and the drive shaft and to permit tilting of the drive pinion relative to the drive axis. |
| 申请公布号 |
US2017029096(A1) |
申请公布日期 |
2017.02.02 |
| 申请号 |
US201515302886 |
申请日期 |
2015.04.09 |
| 申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
DIDEY Arnaud;WILSON Fraser;BRIANCOURT Stephen;TEAGUE Phillip |
| 分类号 |
B64C25/40;F16C23/08;F16D3/18;B64C25/34;B64C25/44 |
主分类号 |
B64C25/40 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A drive system for an aircraft landing gear, the drive system comprising:
a drive pinion; a drive shaft arranged to rotate the drive pinion about a drive axis; and a casing which rotatably supports the drive shaft, wherein the drive pinion is rotatably supported on the casing by a self-aligning bearing, and wherein the drive pinion is coupled to the drive shaft by a flexible coupling adapted to transfer torque between the drive pinion and the drive shaft and to permit tilting of the drive pinion relative to the drive axis. |
| 地址 |
Bristol GB |
