Aircraft landing gear swivel locking pin having automatic releas

Aeronautics and astronautics – Aircraft propulsion and steering on land or water

Patent

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Details

244102R, B64C 2550

Patent

active

053338162

ABSTRACT:
An aircraft landing locking pin (12) automatically repositions from an engage position, wherein a rotating portion (15) of the landing gear is prevented from rotating, to a released position, wherein the rotating portion if free to rotate, in response to excessive side loading on the landing gear. The locking pin comprises a spring loaded actuator (32,34,60) which urges a roller (19) of a lock pin assembly (20) in contact with a bushing (22). In response to a side loading on the landing gear in excess of a predetermined loading, 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 linkage. The locking pin automatically reengages when the lock pin assembly is aligned with the bushing.

REFERENCES:
patent: 1896234 (1933-02-01), Hathorn
patent: 2338572 (1944-01-01), Corwin
patent: 3006579 (1961-10-01), Frederick
patent: 3361390 (1968-01-01), Wilkes
patent: 4155522 (1979-05-01), Sealey

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