An unmanned aerial vehicle may include a fuselage and an anchor structure coupled to the fuselage and including a wing retention structure and a power module retention structure. The unmanned aerial vehicle may also include a wing releasably coupled to the wing retention structure, thereby coupling the wing to the fuselage, and a power module releasably coupled to the power module retention structure, thereby coupling the power module to the fuselage.


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    Titel :

    Unmanned aircraft system with swappable components


    Beteiligte:
    PERRY PAUL (Autor:in) / LASZLO ZOLTAN (Autor:in) / PARKER SCOTT (Autor:in) / GOLDSBERRY NATHAN (Autor:in) / WADE BRYAN (Autor:in) / WYROBEK KEENAN (Autor:in) / BOOMGAARD BRIAN (Autor:in) / LI ZHEFEI (Autor:in) / BLASER SVEN (Autor:in)

    Erscheinungsdatum :

    19.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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