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A folding self-locking device for UAV wings

A technology of wing folding and self-locking device, which is applied to the fuselage, aircraft parts, aircraft control and other directions, can solve the problems of not reducing the load capacity of the wing surface, increasing the design requirements of the wing surface folding, and reducing the field area of ​​the UAV. To achieve the effect of simple structure, good load characteristics and low weight

Active Publication Date: 2020-05-15
李伟忠
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Folding of the UAV's wing surface is still rare. However, the use of the folding wing surface can not only greatly reduce the battlefield area of ​​the UAV, but also has positive significance for the transportation and storage of the civilian use. The wing surface folding requires the wing surface After flattening, it is firm and reliable, and the load capacity of the wing surface cannot be reduced. The driving force should be simple and effective, reducing unnecessary driving load and overly complicated design, which will greatly increase the design requirements for wing surface folding.

Method used

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  • A folding self-locking device for UAV wings
  • A folding self-locking device for UAV wings
  • A folding self-locking device for UAV wings

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Embodiment Construction

[0023] The present invention will be further described below in conjunction with specific embodiments. The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not as a limitation to the present invention.

[0024] The working principle of the present invention is set forth in detail below: the fixed wing 21 and the foldable wing 22 are hinged together by a rotating shaft, the mounting plate 1 is fixedly installed on the fixed wing 21, and the fixed plate 4 is fixedly installed on the foldable machine on wing 22.

[0025] When unfolded after being folded, the small motor 10 simultaneously drives the small spur gear 8 and the small helical gear 7 to move. At this time, the helical gear 5 is driven to rotate on the rotating circle 303 of the locking plate 3. The gear 5 drives the locking plate 3 to rotate through the top wire 6, and then drives the fixed plate 4 to rotate. When the helical gear 5 rotates to 180 degrees, t...

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Abstract

The invention provides an unmanned aerial vehicle (UAV) wing folding self-locking device. The UAV wing folding self-locking device is suitable for a folding wing of a fixed-wing UAV. When a UAV is inuse, storage and carrying are inconvenient because of the wing, the UAV wing folding self-locking device is designed, the wing of the UAV can be folded, and a small space is occupied during storage; the wing can self-lock after unfolding and withstand high loads without affecting using of the wing. According to the UAV wing folding self-locking device, the designed adopts a stamping bending part as a main structure, using is easy, and mounting and maintenance are easy; and a direct current small motor is used for driving, controlling is simple, the cost is low, the weight is light, and the size is small, and not too much extra load is brought to the UAV. The UAV wing folding self-locking device is designed from the perspective of using, mounting and disassembling are integral, and maintenance is convenient.

Description

technical field [0001] The invention provides a wing folding self-locking device of an unmanned aerial vehicle, which belongs to the technical field of the design of the wing surface folding mechanism of an unmanned aerial vehicle. Background technique [0002] With the advancement of science and technology, there are more and more applications of drones. From military to civilian, more and more technologies are applied to the improved design of drones. Folding of the UAV's wing surface is still rare. However, the use of the folding wing surface can not only greatly reduce the battlefield area of ​​the UAV, but also has positive significance for the transportation and storage of the civilian use. The wing surface folding requires the wing surface After flattening, it is firm and reliable, and the load capacity of the airfoil cannot be reduced. The driving force should be simple and effective, reducing unnecessary driving load and overly complicated design, which will greatly...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/30
CPCB64C1/30
Inventor 刘占波
Owner 李伟忠