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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    Titel :

    LEVERED LANDING GEAR WITH INNER SHOCK STRUT


    Weitere Titelangaben:

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


    Beteiligte:

    Erscheinungsdatum :

    2020-12-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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