Quick release assembly for aircraft landing gear
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United States of America Patent
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-
Sep 1, 2015
Grant Date -
May 31, 2012
app pub date -
Oct 14, 2011
filing date -
Oct 18, 2010
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A torque link member for aircraft landing gear includes a first end for connecting to a lower portion or an upper portion of the aircraft landing gear and a second end for connecting to another torque link member. A locking pin is disposed on one of the upper portion, the lower portion, the first end or the second end. The locking pin is axially movable between an engaged position wherein the pin protrudes for interengagement with a cooperating aperture on the first end, the second end, the upper portion, the lower portion, or the second end of the other torque link member, and a disengaged position. The locking pin is biased toward the engaged position and movable against the biasing to the disengaged position.
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