A main fitting includes an elongate piston and a cylinder configured to slidingly receive the piston. A first end of the piston extends from a first end of the cylinder, and a second end of the piston extends from a second end of the cylinder. The first end of the cylinder comprises a bearing surface engaging the piston to limit translation of the piston relative to the cylinder to a longitudinal direction.


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    Titel :

    LANDING GEAR MAIN FITTING WITH INTEGRAL SHOCK ABSORBER


    Beteiligte:
    PASIC ZORAN (Autor:in) / SACCOCCIA MICHAEL (Autor:in) / LEE RANDY (Autor:in)

    Erscheinungsdatum :

    02.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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