UAV

Abstract

The present invention proposes an unmanned aerial vehicle, which includes a body, a plurality of rotors arranged on the body, push paddles arranged on the body, a main wing detachably connected to the body, and a controller for controlling flight; When the main wing is installed on the body, the controller switches to the first flight control mode under the remote control command or preset command, and controls the rotation of the propeller and the action of the rudder surface of the main wing, so that the unmanned aerial vehicle Fly in fixed-wing mode; when the main wing is separated from the body, the controller switches to the second flight control mode under remote control instructions or preset instructions, and controls the rotation of the plurality of rotors, so that the unmanned aerial vehicle Fly in multi-rotor mode. It integrates multi-rotor and fixed-wing models, and can change the type of flight to meet more needs.

Description

Technical field[0001]The present invention relates to an unmanned aircraft.Background technique[0002]Unmanned aircraft includes various types, such as multi-rotorless drones, fixed wing drones, etc. A multi-rotor drone is a multifocal aircraft capable of vertically down and decline, which is a aircraft that does not load operators in a plurality of rotors as power devices. The multi-rotor drone controls various attitudes by controlling each rotor speed, while achieving various gesture flights, such as hovering, front flight, side flying and flying, however, the energy consumption of multi-rotorless drone flight Large, life is short, and it is prone to losing balance when environmental factors such as strong winds. The fixed wing drone can generally provide reverse power by pushing air through the front or rear of the fuselage, while adjusting the airflow flying and attitude in high altitude, with a non-wing, the rudder surface provides a transverse flight required for drone flight. ...

AI Technical Summary

Problems solved by technology

[0003] The current multi-rotor UAVs and fixed-wing UAVs are independent aircrafts. Some users hope to use both multi-rotor UAVs and fixed-wing UAVs. However, the current UAVs cannot achieve this. Model change, under the demand of different models, only the required models can be purchased, and no matter what type of model, each has its own advantages and disadvantages

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