Carbon fiber wing protecting frame for unmanned aerial vehicle

Abstract

The invention discloses a carbon fiber wing protecting frame for an unmanned aerial vehicle. The carbon fiber wing protecting frame comprises an unmanned aerial vehicle body, wherein the side wall ofthe unmanned aerial vehicle body is connected with four second wings which are arranged in an annular array mode, first wings are rotationally connected to one ends, far away from the unmanned plane body, of the second wings, arc-shaped machines are arranged at the edges of the first wings and the second wings, the interiors of the first wings and the interiors of the second wings are correspondingly provided with polyester filling layers, the first wings, the second wings, connecting plates and hinge rods are carbon fiber layers, the outer sides of the carbon fiber layers are coated with weaving layers, vortex coils are arranged on the upper surfaces of the first wings, electromagnetic coils parallel to the vortex coils are arranged on the lower surfaces of the first wings, the input endsof the electromagnetic coils are connected with transformers, and the transformers are connected with a micro-control computer. The carbon fiber wing protecting frame has the advantages that the stability of the unmanned aerial vehicle during flight is guaranteed, the unmanned aerial vehicle is protected, the weight is light, the strength is high, and the carbon fiber wing protecting frame is suitable for popularization.

Description

technical field [0001] The invention relates to the technical field of drones, in particular to a carbon fiber wing guard for drones. Background technique [0002] Most of the existing drone wings are fixed, which may cause damage to the wings when carrying the drone, so people have developed drones with folding wings. However, when the UAV with folding wings of the prior art is in use, its wing shakes seriously, which causes the UAV to fly unsteadily, which easily causes the UAV to crash and cause economic losses. In addition, the traditional unmanned Aircraft wing weight and pressure bearing capacity is weak. Contents of the invention [0003] The purpose of the present invention is to provide a carbon fiber wing guard for unmanned aerial vehicles, so as to solve the problems raised in the above-mentioned background technology. [0004] In order to solve the above technical problems, the present invention provides the following technical solutions: [0005] A carbon f...

AI Technical Summary

Problems solved by technology

[0002] Most of the existing drone wings are fixed, which may cause damage to the wings when carrying the drone, so people have developed drones with folding wings. However, when the UAV with folding wings of the prior art is in use, its wing shakes seriously, which causes the UAV to fly unsteadily, which easily causes the UAV to crash and cause economic losses. In addition, the traditional unmanned Wing weight and pressure capacity are weak

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