An aircraft landing gear assembly (10) having a reinstating geometry in which a lock (26) link can be moved to assume a first locking condition to inhibit movement of a stay (18) when a main strut (12) is in a deployed condition and a second locking condition to inhibit movement of the main strut (12) when in a stowed condition. An auxiliary unlock actuator (40, 52) is arranged to apply an unlocking force to the lock (26) when the lock (26) is holding the main strut (12) in the stowed condition, such that the actuator (40, 52) unlocks the lock (26) from the second locking condition.
AIRCRAFT LANDING GEAR ASSEMBLY
FLUGZEUGFAHRWERKSBAUGRUPPE
ENSEMBLE DE TRAIN D'ATTERRISSAGE D'AÉRONEF
2020-10-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |