UAV (unmanned aerial vehicle) ejection buffer protective device

A protection device and drone technology, applied in the field of drones, can solve the problems of drone imbalance, drone damage, poor take-off effect, etc., to achieve enhanced stability, stable launch process, and good use effect

Active Publication Date: 2019-06-21
CHENGDU AERONAUTIC POLYTECHNIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] UAVs are widely used in our lives because of their good effects, such as aerial photography, etc. However, most of the current UAV takeoff methods are to take off directly from the ground, and the takeoff effect is poor. When it is not stable, it is easy to cause the imbalance of the UAV and cause certain damage to the UAV. Therefore, we propose a buffer protection device for UAV ejection

Method used

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  • UAV (unmanned aerial vehicle) ejection buffer protective device
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  • UAV (unmanned aerial vehicle) ejection buffer protective device

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Embodiment Construction

[0015] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention.

[0016] refer to Figure 1-3 , a buffer protection device for unmanned aerial vehicle ejection, comprising a shell 3, a self-balancing device is installed on the lower surface of the shell 3, the self-balancing device includes a bottom plate 14, and both sides of the bottom plate 14 are symmetrically threaded with adjusting bolts 9, which can be adjusted. The balance of the device is fine-tuned to enhance the stability of use.

[0017] Both sides of the upper surface of the bottom plate 14 are symmetrically equipped with vertical support plates 7, the bottom between the two vertical support plates 7 is equipped with an arc-shaped plate 13, and the upper part between t...

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Abstract

The invention relates to the technical field of UAV (unmanned aerial vehicle), particularly an UAV ejection buffer protective device. The UAV ejection buffer protective device comprises a shell; the lower surface of the shell is provided with a self-balancing device; a moving column penetrates through the upper part of the internal side of the shell; an operation panel is arranged on the lower part of the external side of the shell; a storage battery, a first ring-shaped magnet, a second ring-shaped magnet shell and a clamping device are arranged on the lower surface of the internal side of the shell; a drawstring passes around a fixed pulley, penetrates through a through hole and is connected with a limiting block. The self-balancing device arranged in the invention can automatically maintain a horizontal plate in a horizontal state. The arranged first ring-shaped magnet and a second ring-shaped magnet can reduce contact friction. The arranged clamping device can clamp and fix the drawstring. The UAV can be ejected with the elasticity of a spring. The whole ejection process is smooth and stable. During ejection, the UAV is in a horizontal state, so that the stability of the ejection of the UAV is enhanced. The use effect is good, the practicality is strong, and popularization and utilization are worthwhile.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a buffer protection device for ejecting an unmanned aerial vehicle. Background technique [0002] UAVs are widely used in our lives because of their good effects, such as aerial photography, etc. However, most of the current take-off methods of UAVs are to take off directly from the ground, and the take-off effect is poor. When it is not stable, it is easy to cause the imbalance of the UAV and cause certain damage to the UAV. Therefore, we propose a buffer protection device for UAV ejection. Contents of the invention [0003] The purpose of the present invention is to solve the shortcomings in the prior art, and propose a buffer protection device for unmanned aerial vehicle ejection. [0004] In order to achieve the above object, the present invention adopts the following technical solutions: [0005] Design a buffer protection device for UAV ejection, includ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
Inventor 张伟瑞杜英杰周行烽赵大卫周孝贤
Owner CHENGDU AERONAUTIC POLYTECHNIC
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