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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    Title :

    UNMANNED AIRCRAFT SYSTEM WITH SWAPPABLE COMPONENTS


    Additional title:

    UNBEMANNTES FLUGZEUGSYSTEM MIT AUSTAUSCHBAREN KOMPONENTEN
    SYSTÈME D'AÉRONEF SANS PILOTE AVEC COMPOSANTS POUVANT ÊTRE INTERCHANGÉS


    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 :

    2020-06-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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    PERRY PAUL / LASZLO ZOLTAN / PARKER SCOTT et al. | European Patent Office | 2020

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