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.

    本发明公开了一种无人驾驶飞行器,该无人驾驶飞行器可包括机身和锚结构,该锚结构耦合到机身并且包括机翼保持结构和功率模块保持结构。无人驾驶飞行器还可包括机翼,该机翼可释放地耦合到机翼保持结构,从而将机翼耦合到机身;以及功率模块,该功率模块可释放地耦合到功率模块保持结构,从而将功率模块耦合到机身。


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    Titel :

    UNMANNED AIRCRAFT SYSTEM WITH SWAPPABLE COMPONENTS


    Weitere Titelangaben:

    具有可交换部件的无人驾驶飞机系统


    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 :

    26.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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