发明名称 LANDING GEAR DRIVE SYSTEM FLEXIBLE INTERFACE
摘要 A drive system for an aircraft landing gear, the drive system comprising: a pinion gear (110); a drive shaft (120) arranged to rotate the pinion gear about a drive axis; a driven gear arranged to mesh with the pinion gear to be rotatable by the pinion gear, the driven gear being connectable to a wheel of the landing gear to be capable of rotating the wheel about a wheel axis; and a flexible interface comprising a crowned spline joint (501) between the drive shaft and the pinion gear. The crowned spline joint is arranged to permit tilting of the pinion gear relative to the drive axis. In some embodiments a first spline joint between the drive shaft and the pinion gear is arranged to permit tilting of the pinion gear relative to the drive axis; and a second spline joint is arranged to permit translation of the pinion gear along the drive axis relative to the drive shaft.
申请公布号 WO2015033160(A1) 申请公布日期 2015.03.12
申请号 WO2014GB52701 申请日期 2014.09.05
申请人 AIRBUS OPERATIONS LIMITED 发明人 DIDEY, ARNAUD;WILSON, FRASER
分类号 B64C25/40;F16D3/06;F16D3/18;F16D3/223 主分类号 B64C25/40
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