An aircraft landing gear includes a strut mounted to an aircraft structure and moveable between extended and retracted positions. A bracing member includes a first bracing connecting rod hinged to the aircraft structure and a second bracing connecting rod hinged to the first bracing connecting rod and to the strut. A stabilizing member includes a first stabilizing connecting rod and a second stabilizing connecting rod hinged together. The second connecting stabilizing rod is hinged to the first bracing connecting rod. At least one spring is arranged to be resiliently subjected to a bending force when the hinges of the first and second stabilizing connecting rods move from their aligned position.
ATTERRISSEUR D'AERONEF EQUIPE D'UN DISPOSITIF DE VERROUILLAGE A RESSORT A LAME
AIRCRAFT LANDING GEAR PROVIDED WITH A LEAF SPRING LOCKING DEVICE
FLUGZEUGFAHRWERK MIT EINER BLATTFEDERVERRIEGELUNGSVORRICHTUNG
2024-05-08
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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