Unmanned aerial vehicle
A fixed-Wing assembly and the fixed-wing fuselage cooperate to make the flight range of the unmanned aerial vehicle relatively long, and to makeThe flight speed thereof relatively fast, thereby making the unmanned Aerial vehicle have the advantages of both a rotor aircraft and a fixed- wing aircraft.
Abstract
Disclosed is an unmanned aerial vehicle, comprising a fixed-wing fuselage (10), a fixed-wing power assembly (20) and multiple rotor power assemblies (30). The fixed-wing power assembly is provided on the fixed-wing fuselage. The multiple rotor power assemblies are provided on the fixed-wing fuselage. The fixed-wing fuselage comprises a front side close to a nose, and a rear side away from the nose, wherein a rear side of a fixed wing is provided with two secondary wings (15). The rotor power assemblies of the unmanned aerial vehicle can enable the unmanned aerial vehicle to take off and land vertically. A fixed-wing assembly and the fixed-wing fuselage cooperate to make the flight range of the unmanned aerial vehicle relatively long, and to make the flight speed thereof relatively fast, thereby making the unmanned aerial vehicle have the advantages of both a rotor aircraft and a fixed-wing aircraft, and able to suit complex environments, and improving the performance of the unmanned aerial vehicle.