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.


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    Title :

    ATTERRISSEUR D'AERONEF EQUIPE D'UN DISPOSITIF DE VERROUILLAGE A RESSORT A LAME


    Additional title:

    AIRCRAFT LANDING GEAR PROVIDED WITH A LEAF SPRING LOCKING DEVICE
    FLUGZEUGFAHRWERK MIT EINER BLATTFEDERVERRIEGELUNGSVORRICHTUNG


    Contributors:

    Publication date :

    2024-05-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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