The invention relates to a novel multi-axis unmanned aerial vehicle. The novel multi-axis unmanned aerial vehicle comprises a vehicle body and is technically characterized in that a plurality of vertical motors are symmetrically installed on the two sides of the vehicle body, propeller blades are installed at the output ends of the vertical motors, each vertical motor is hinged to the traction end of a traction device, and the traction device can drive the vertical motors to swing at the same time by the same angle. According to the novel multi-axis unmanned aerial vehicle, a steering engine and a steering engine rocker arm are matched and a connecting rod and an installation plate are matched to control the angle of the vertical motors; when the multi-axis unmanned aerial vehicle moves horizontally, the vehicle body can move horizontally without generation of a dip angle due to the fact that angles are formed between the propeller blades installed at the output ends of the vertical motors and the horizontal plane, and accordingly, air resistance borne by the vehicle body is reduced, battery consumption is reduced, and the endurance mileage and flight time of the multi-axis unmanned aerial vehicle are increased.
Novel multi-axis unmanned aerial vehicle
2015-11-18
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2023
|Novel multi-axis unmanned aerial vehicle achieving low cruising energy consumption
Europäisches Patentamt | 2015
|Europäisches Patentamt | 2016
|Europäisches Patentamt | 2017
|