Landing gear drive system flexible interface
AssigneeAirbus Operations GmbH
InventorArnaud Didey
Life of this patent
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AssigneeAirbus Operations GmbH
InventorArnaud Didey
Estimating the term…
A drive system for an aircraft landing gear, the drive system including a pinion gear, a drive shaft 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. The flexible interface includes a plurality of driven gear coupling members, each driven gear coupling member having a first connection portion attached to the driven gear, a second connection portion adapted to be attached to the wheel at an offset distance from the wheel axis, and a joint between the first connection portion and the second connection portion, the joint permitting relative movement between the first connection portion and the second connection portion.
A drive system for an aircraft landing gear, the drive system comprising:
Dependencies are inferred from the claim text.