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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    Title :

    UNMANNED AIRCRAFT SYSTEM WITH SWAPPABLE COMPONENTS


    Additional title:

    具有可交换部件的无人驾驶飞机系统


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

    Publication date :

    2020-06-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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