Modular heavy load composite wing unmanned aerial vehicle

Abstract

The application provides a modular large-load composite wing unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, the surfaces on both sides of the front end of the unmanned aerial vehicle body are provided with side wings, the surfaces on both sides of the rear end of the unmanned aerial vehicle body are provided with tail wings, the lower surface of the side wing is provided with a rotor arm, the upper surfaces at both ends of the rotor arm are provided with propellers, a connecting mechanism is arranged between the rotor arm and the side wing, the lower surfaces of the front ends of the rotor arms on both sides are fixedly provided with supporting plates, and the lower sides of the supporting plates and the tail wings are provided with buffer mechanisms. Through the clamping of the clamping block and the clamping groove and the elastic effect of the first spring, the installation and dismounting of the rotor arm and the side wing can be quickly realized. Without the aid of complex tools, the operation is simple and fast, the work efficiency is greatly improved, the operation difficulty and cost are reduced, and the demand for frequent replacement of the rotor arm in different task scenarios is better met.

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