The embodiments is an unmanned aerial vehicle. The unmanned aerial vehicle includes: an airframe; and a fixed-wing assembly and a rotor assembly, both replaceably connected to the airframe. The fixed-wing assembly is connected to the airframe to form a vertical take-off and landing fixed-wing unmanned aerial vehicle and the rotor assembly is connected to the airframe to form a multi-rotor unmanned aerial vehicle, thereby implementing an unmanned aerial vehicle that can switch between the vertical take-off and landing fixed-wing unmanned aerial vehicle and the multi-rotor unmanned aerial vehicle.
Convertible unmanned aerial vehicle
2025-01-07
Patent
Electronic Resource
English
IPC: | B64U |
CONVERTIBLE LIFTING PROPELLER FOR UNMANNED AERIAL VEHICLE
European Patent Office | 2017
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