An unmanned aerial vehicle (UAV) includes a fuselage assembly, a further portion that attaches with the fuselage assembly, and a propulsion assembly coupled with the further portion. The propulsion assembly is constructed and arranged to provide propulsion for the UAV. The fuselage assembly includes a fuselage body constructed and arranged to operate as a forward portion of the UAV, lateral stringers coupled with the fuselage body and extending laterally along the fuselage body, and a set of interchangeable covers to cover at least a portion of a payload bay opening defined by the fuselage body. Utilizing such a fuselage assembly offers a highly configurable mounting architecture to accommodate a wide variety of payloads.


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    Titel :

    UTILIZING A CUSTOMIZABLE FUSELAGE ASSEMBLY FOR AN UNMANNED AERIAL VEHICLE


    Weitere Titelangaben:

    VERWENDUNG EINER ANPASSBAREN RUMPFANORDNUNG FÜR EIN UNBEMANNTES LUFTFAHRZEUG
    UTILISATION D'UN ENSEMBLE DE FUSELAGE PERSONNALISABLE POUR UN VÉHICULE AÉRIEN SANS PILOTE



    Erscheinungsdatum :

    10.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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