Unmanned aerial vehicle based on X-wing layout

Abstract

The invention relates to the technical field of unmanned aerial vehicles, and provides an unmanned aerial vehicle based on X-wing layout. The unmanned aerial vehicle comprises a vehicle body, a plurality of main wings and a plurality of tail rings, wherein the cross section of the vehicle body is in a circle shape, the plurality of main wings are symmetrically arranged along the longitudinal axisof the vehicle body, and the installation plane of the main wings is tangential to the vehicle body; the plurality of tail wings are symmetrically arranged along the longitudinal axis of the vehicle body, and the installation plane of the tail wings is tangential to the vehicle body; the installation direction of the tail wings is opposite to the installation direction of the main wings; each mainwing is connected with a foldable mechanism in the vehicle body through an adapter, and can rotate around the adapter which is used as the rotation center; all the main wings and the tail wings are foldable. The unmanned aerial vehicle has the advantages that by adopting the novel aerodynamics layout, compared with the traditional unmanned aerial vehicle, the maneuverability is stronger, and thebattlefield survival ability is strong; the unmanned aerial vehicle can be folded, so that the occupation space after folding is smaller than the occupation space of other conventional unmanned aerialvehicles, the disassembly of parts for box loading is not needed in the transportation process, and the disassembly and assembly time is shortened; the structure is simple, novel and reasonable, andthe application prospect is broad.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle based on an X-wing layout. Background technique [0002] UAVs can quickly reach the target area and perform single or multiple tasks such as patrol flight, reconnaissance and surveillance, damage assessment, aerial wireless relay and attack targets. Smart Ammo. [0003] Existing UAV design schemes include the following: [0004] (1) Conventional layout scheme. The wing and tail are connected to the middle of the fuselage by shafts and bearings. The main wing is a whole rectangular wing, which can rotate around the axis at the midpoint of the wing. After being folded, it coincides with the upper surface of the fuselage. The axis of the fuselage rotates forward and coincides with the lower surface of the fuselage; such as figure 1 -a shown; [0005] (2) Canard-forward swept wing layout scheme. The main wing and canard are connected ...

AI Technical Summary

Problems solved by technology

[0008] It can be seen from the above that the layout of the existing drones is left-right symmetrical along the longitudinal axis of the fuselage. This layout is usually difficult to meet the high maneuverability requirements of offensive and single-soldier drones. For example, this type Due to its aerodynamic characteristics, the layout of the UAV is difficult to be flexible when turning in the air

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