发明名称 Drive system for aircraft landing gear
摘要 The invention is a drive system for rotating a wheel of an aircraft landing gear. The drive system includes a motor operable to rotate a drive pinion via a drive path, and a driven gear adapted to be mounted to the wheel. The drive system has a first configuration in which the drive pinion is capable of meshing with the driven gear to permit the motor to drive the driven gear via the drive path. The drive path has a plurality of shafts rotatable about respect shaft axes, including an output shaft. The output shaft is operable to pivot about the axis of rotation of another shaft axis spaced from the output shaft axis. Also, an aircraft landing gear having a wheel and the drive system, where the driven gear of the drive system is mounted to the wheel.
申请公布号 GB2533982(A) 申请公布日期 2016.07.13
申请号 GB20150008940 申请日期 2014.09.15
申请人 Airbus Operations Limited 发明人 Arnaud Didey;Fraser Wilson
分类号 B64C25/40 主分类号 B64C25/40
代理机构 代理人
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