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Unmanned aerial vehicle with landing buffer function

A UAV and functional technology, applied in the field of UAV, can solve the problems of landing, can not slide and buffer, and the shock absorption effect is not good, and achieve the effect of reducing impact, simple structure, and reducing impact force.

Pending Publication Date: 2020-04-17
江苏艾格信航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to solve the shortcomings in the prior art that the shock absorption effect is not good and the landing cannot be slid and buffered, and a kind of unmanned aerial vehicle with a landing buffer function is proposed

Method used

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  • Unmanned aerial vehicle with landing buffer function
  • Unmanned aerial vehicle with landing buffer function
  • Unmanned aerial vehicle with landing buffer function

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Embodiment Construction

[0014] 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.

[0015] refer to Figure 1-4 , a kind of unmanned aerial vehicle with landing buffering function, comprises unmanned aerial vehicle main body 1, and the bottom of unmanned aerial vehicle main body 1 is provided with rotating shaft 7, and the two sides of rotating shaft 7 are rotationally connected with two fixed plates 5, each fixed Both ends of the plate 5 are provided with a connecting column 3, one end of the connecting column 3 is provided with a shock absorbing column 11, the shock absorbing column 11 is provided with a fixed plate 16, one end of the shock absorbing column 11 is provided with a piston 12, and the outside of the piston 12 A cushioning device shell...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles and particularly relates to an unmanned aerial vehicle with a landing buffer function. The unmanned aerial vehicle comprises aunmanned aerial vehicle body, wherein a rotating shaft is arranged at the bottom of the unmanned aerial vehicle main body; the two sides of the rotating shaft are rotationally connected with two fixing plates; connecting columns are arranged at the two ends of each fixing plate; a damping column is arranged at one end of the connecting column; a fixed disc is arranged on the damping column; a piston is arranged at one end of the damping column; a buffer device shell is arranged outside the piston; the sliding device is arranged at one end of the buffer device shell; and an air pipe is arrangedat the top of the sliding device. The unmanned aerial vehicle landing buffering device has the advantages that the unmanned aerial vehicle landing buffering device is reasonable in design and simplein structure, landing buffering functions can be realized by the unmanned aerial vehicle landing buffering device, impact during landing can be greatly reduced, the unmanned aerial vehicle can be protected, and the unmanned aerial vehicle landing buffering device is suitable for popularization.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a landing buffer function. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. It is a general term for unmanned aerial vehicles. It was first used in the military field. With the improvement of production capacity, the rapid development of various industries, and the development and promotion of drone technology, drones have gradually entered the public's perspective and have been widely used in aerial photography, agriculture, forestry, surveying and mapping and other fields. During the use of the man-machine, the landing process is particularly important, because to avoid damage to the drone, a good buffer device is needed to offset the impact of the drone when it lands, which is limited by the accuracy of ...

Claims

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Application Information

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IPC IPC(8): B64C25/62B64D45/06
CPCB64C25/62B64D45/06
Inventor 陈晓峰
Owner 江苏艾格信航空科技有限公司
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