Fixed wing type unmanned aerial vehicle with vertical takeoff and landing functions

Abstract

The invention discloses a fixed wing type unmanned aerial vehicle with vertical takeoff and landing functions. The fixed wing type unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein fixed wings are arranged at both sides of the unmanned aerial vehicle body; a first driving motor and a first rotary wing are arranged on each fixed wing, each first rotary wing is arranged on the corresponding first driving motor, a first battery and a first driver control assembly are arranged in the unmanned aerial vehicle body, and the first battery is used for driving a first driver to act. The fixed wing type unmanned aerial vehicle has the advantages that in the takeoff phase, the fixed wing type unmanned aerial vehicle is vertical to the horizontal surface through a first bending mechanism and a second bending mechanism, and then vertically takes off and lands; after takeoff, the first bending mechanism and the second bending mechanism are reset, the whole unmanned aerial vehicle is in a straight line shape, and the advancing function is realized through the rotary wings on the two bending mechanisms; under the mutual action of the rotary wings on the fixed wings, the whole power and steering of the unmanned aerial vehicle can be controlled.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a fixed-wing unmanned aerial vehicle capable of vertical take-off and landing. Background technique [0002] UAV is an unmanned aircraft operated by radio remote control equipment and self-contained program control device. There is no cockpit on board, but it is equipped with autopilot, program control device and other equipment. The personnel on the ground, on the ship or at the remote control station of the mother plane use radar and other equipment to track, locate, remote control, telemetry and digital transmission. It can take off like an ordinary aircraft under radio remote control or launch into the air with a booster rocket, and can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote control with a parachute or a block. ...

AI Technical Summary

Problems solved by technology

Catapult take-off requires a catapult frame, which is not easy to carry; hand-throwing take-off is a certain danger to the operator, and at the same time, the drone cannot be thrown by hand when its own weight is too large; runway taxi take-off and landing in the wild usually does not meet this condition; parachute will increase the flight weight At the same time, it is greatly affected by the wind, and it is impossible to land at the set position accurately. There are many factors that make it difficult to take off and land.

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