An unmanned aerial vehicle (UAV), comprising a fuselage outer shell defining a lateral axis, a longitudinal axis and a plurality of shell sides; fuselage center assembly positioned within a cavity defined by the fuselage outer shell; and a rotor arm and joint assembly. The plurality of the shell sides are concave with respect to the lateral axis or the longitudinal axis. The fuselage center assembly includes a lattice center defining a superior surface and an inferior surface as well as a plurality of channels, each channel having a proximal end and a distal end, wherein each proximal end is coupled to the superior surface and the inferior surface. The rotor arm has a proximal end and a distal end. A motor and rotor system is coupled to the distal end of the rotor arm. The rotor arm joint is coupled to the proximal end of the rotor arm, and the rotor arm joint further comprises an outer shell; and a plurality of quick release latches coupled to the outer shell and configured to coule the rotor arm joint to a plurality of corresponding latch receivers positioned.


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    Titel :

    AIRFRAME AND MOTOR ASSEMBLY FOR AN UNMANNED AIRCRAFT


    Beteiligte:
    DORNISCH MICHAEL (Autor:in) / TUBMAN MAX (Autor:in) / PANEK EVAN (Autor:in) / MCCAFFREY CONOR (Autor:in)

    Erscheinungsdatum :

    07.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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