| 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 | US9169005(B2) | 申请公布日期 | 2015.10.27 |
| 申请号 | US201013643855 | 申请日期 | 2010.04.28 |
| 申请人 | L-3 Communications Magnet-Motor GmbH | 发明人 | Oswald Johann;Heeg Manfred |
| 分类号 | B64C25/40 | 主分类号 | B64C25/40 |
| 代理机构 | Brinks Gilson & Lione | 代理人 | Brinks Gilson & Lione |
| 主权项 | 1. A drive unit for an aircraft running gear having a running gear leg and at least a first wheel and a second wheel on a common wheel axis, characterized in that 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 and substantially parallel to a main longitudinal axis of the running gear leg, and further characterized in that the drive unit comprises: a first motor drivingly coupleable to the first wheel via a first gear structure, and a second motor drivingly coupleable to the second wheel via a second gear structure, wherein the first and second motors are arranged in tandem along the direction of longitudinal extension of the drive unit. | ||
| 地址 | Starnberg DE | ||