An aircraft rudder pedal frame includes a base, a support framework and connection interfaces. Each connection interface is able to connect another part of the rudder pedal to the frame. The support framework connects each connection interface to the base. The support framework includes framework elements arranged in a lattice, at least one of the framework elements extending from each connection interface.


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    Titel :

    AIRCRAFT RUDDER PEDAL FRAME


    Beteiligte:
    GRANIER ERIC (Autor:in) / MATEUS VINCENT (Autor:in)

    Erscheinungsdatum :

    07.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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