An unmanned aerial vehicle (UAV) includes a fuselage, a pair of wings attached to the fuselage, and a propulsion system mounted to the wings to provide propulsion to the UAV. The fuselage has an outer fuselage shell that is a first mechanical support structure for an airframe of the UAV. The pair of wings is attached to the fuselage and shaped to provide aerodynamic lift. The wings have outer wing shells that are second mechanical support structures for the airframe. The outer fuselage shell or the outer wing shells comprise one or more formed-metal sheets.
FORMED-METAL SHEET AIRFRAME FOR UAVS
LUFTFAHRZEUG MIT FORMMETALLBLECH FÜR UAVS
CELLULE À FEUILLE MÉTALLIQUE FAÇONNÉE POUR UAV
19.03.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64U |