An aircraft landing gear includes: a strut assembly hinged by its upper end to a structure element of the aircraft to pivot between deployed and retracted states; an interlocking system having a stay including an arm hinged to the strut assembly via a lifting pin carried by two lugs of a clevis of the strut assembly, this arm being terminated by a head through which the pin passes and which is located between the lugs; and a lifting jack having one end connected to a first end of the pin which is located outside the clevis, a first end stop carried by the pin at its first end beyond the jack, and a second end stop carried by the pin at its second end. The landing gear includes a system for translationally locking the lifting pin in the event of the pin breaking between its first end and the clevis.
AGENCEMENT DE BLOCAGE D'UN AXE D'ATTERRISSEUR D'AÉRONEF
ARRANGEMENT FOR LOCKING AN AIRCRAFT LANDING GEAR
ANORDNUNG ZUM VERRIEGELN EINES FLUGZEUGFAHRWERKS
2024-03-20
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |