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.
UTILIZING A CUSTOMIZABLE FUSELAGE ASSEMBLY FOR AN UNMANNED AERIAL VEHICLE
VERWENDUNG EINER ANPASSBAREN RUMPFANORDNUNG FÜR EIN UNBEMANNTES LUFTFAHRZEUG
UTILISATION D'UN ENSEMBLE DE FUSELAGE PERSONNALISABLE POUR UN VÉHICULE AÉRIEN SANS PILOTE
10.07.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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