Landing gear drive system flexible interface
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United States of America Patent
Stats
-
Dec 15, 2020
Grant Date -
May 3, 2018
app pub date -
Dec 22, 2017
filing date -
Sep 5, 2013
priority date (Note) -
In Force
status (Latency Note)
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Abstract
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.
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