An unmanned aerial vehicle 2 comprising: a fuselage 4; and a wing 6 comprising a central wing section 12 pivotably mounted to the fuselage 4 and a pair of outer wing sections 14a, 14b pivotably mounted to the central wing section 12; wherein the wing 6 has a folded configuration in which the central wing section 12 and the outer wing sections 14a, 14b are stacked on top of one another and are aligned with a longitudinal axis of the fuselage 4; and a deployed configuration in which the central wing section 12 is substantially perpendicular to the fuselage 4 and the outer wing sections 14a, 14b extend from the central wing section 12 away from the fuselage 4.
An unmanned aerial vehicle with folding wing arrangement
06.09.2017
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Wing folding mechanism, unmanned aerial vehicle and wing folding method of unmanned aerial vehicle
Europäisches Patentamt | 2023
|Unmanned aerial vehicle wing folding mechanism and unmanned aerial vehicle
Europäisches Patentamt | 2022
|Folding mechanism of folding-wing unmanned aerial vehicle
Europäisches Patentamt | 2021
|