B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 25/50 (2006.01)
Patent
CA 2142196
An aircraft landing locking pin (12) automati- cally repositions from an engage position, wherein a rotating portion (15) of the landing gear is prevented from rotating, to a released position, wherein the rotat- ing portion if free to rotate, in response to excessive side loading on the landing gear. The locking pin com- prises a spring loaded actuator (32, 34, 60) which urges a roller (19) of a lock pin assembly (20) in con- tact with a bushing (22). In response to a side loading on the landing gear in excess of a predetermined load- ing, the locking pin is automatically released wherein the roller is expelled from the bushing. The threshold loading is determined as a function of the spring force applied to the lock pin assembly via the actuator lin- kage. The locking pin automatically reengages when the lock pin assembly is aligned with the bushing.
Swabey Ogilvy Renault
United Technologies Corporation
LandOfFree
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