A levered landing gear (110) including a first shock strut (200) having a longitudinal axis (LAX), a second shock strut (300) disposed concentrically with the first shock strut (200) along the longitudinal axis (LAX) such that the first shock strut (200) and the second shock strut (300) extend along a common extension axis (EX), and a truck lever (220) coupled to both the first shock strut (200) and the second shock strut (300) such that the second shock strut (300) pivots the truck lever (220) relative to the first shock strut (200).


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    Title :

    LEVERED LANDING GEAR WITH INNER SHOCK STRUT


    Additional title:

    HEBELFAHRWERK MIT INNEREM FEDERBEIN
    TRAIN D'ATTERRISSAGE À LEVIER À JAMBE DE FORCE INTERNE


    Contributors:

    Publication date :

    2020-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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