Light-weight foldable reconnaissance/attack integrated unmanned aerial vehicle

Abstract

The invention relates to the field of unmanned aerial vehicles and especially relates to a light-weight foldable reconnaissance / attack integrated unmanned aerial vehicle, which includes a fuselage, wings, a folding mechanism, flat vertical tails, reconnaissance cloud deck, and a dispensing mechanism. The fuselage includes a front section, a rear section, a central wing box, wing main beams, wing connection boxes, and a tail connection box. Each wing includes an inner section and an outer section. The two wings are arranged respectively at the left and the right of the fuselage symmetrically. The folding mechanism includes two set of wing folding mechanisms and a fuselage folding mechanism. The reconnaissance / attack integrated unmanned aerial vehicle can be quickly folded and expanded, is low in cost, has simple and easy-to-repair structure, and has excellent maneuverability and certain dispensing load. The unmanned aerial vehicle is used for military reconnaissance and quick and accurate strike tasks, and also can be applied to civil and scientific researching fields, such as atmospheric sounding and topographic mapping, etc.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a light-weight foldable integrated unmanned aerial vehicle for inspection and strike. Background technique [0002] UAVs are mostly fixed-wing aircraft, which take off by hand throw or take off in short distances. Most of them are electric, small in size and light in weight. Generally, metal materials and some advanced composite materials are used to reduce the structural weight, but their shapes are not regular enough, and most of them are larger than rotor drones, making it difficult to pack and carry. At the same time, the immediate repairability of most drones is poor, and the price is not cheap, generally above $5,000. UAVs in the prior art, such as a variable aspect ratio drone with a patent application number of CN201420040752.6, includes a fuselage, an outer wing, a middle wing, an empennage, and The power system also includes a connection mechanism between the o...

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a light-duty foldable unmanned aerial vehicle for inspection and combat, which can effectively solve the problems of the existing unmanned aerial vehicles in the prior art, which are expensive and difficult to maintain. In actual combat, it is difficult to quickly repair and then cannot be damaged again. The problem of putting into use and the existing drones are heavy, bulky, inconvenient to carry, and poor in maneuverability; the present invention provides a drone that can be quickly folded and unfolded, has low cost, simple structure and easy repair, and has excellent maneuverability. It can be used for military reconnaissance operations, fast and precise strike missions, and can also be used in civilian scientific research fields, such as atmospheric detection, surface surveying and mapping, etc.

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