| 发明名称 |
DRIVE UNIT FOR AIRCRAFT RUNNING GEAR |
| 摘要 |
A drive unit (16) for an aircraft running gear (2) having at least a first wheel (4) and a second wheel (6) on a common wheel axis (A) is characterized in that the drive unit (16) is drivingly coupleable to the first and second wheels (4, 6) such that a direction of longitudinal extension (C) of the drive unit (16) is in a plane orthogonal to the common wheel axis (A). |
| 申请公布号 |
US2016009383(A1) |
申请公布日期 |
2016.01.14 |
| 申请号 |
US201514863905 |
申请日期 |
2015.09.24 |
| 申请人 |
L-3 Communications Magnet-Motor GmbH |
发明人 |
Oswald Johann;Heeg Manfred |
| 分类号 |
B64C25/40;F16H48/32;F16H48/34;F16H48/08 |
主分类号 |
B64C25/40 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A drive unit for an aircraft running gear having at least a first wheel and a second wheel on a common wheel axis, the drive unit comprising:
a differential gear; and a motor drivingly coupleable to the first and second wheels via the differential gear, wherein the drive unit is drivingly coupleable to the first and second wheels such that a direction of longitudinal extension of the drive unit is in a plane orthogonal to the common wheel axis. |
| 地址 |
Starnberg DE |
