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UAV (unmanned aerial vehicle) vibration-absorbing landing bracket

A landing gear and UAV technology, applied in landing gear, aircraft parts, chassis and other directions, can solve the problems of UAV landing prone to rollover, the frame has no shock absorption function, and the shock absorption effect cannot be Good shock protection performance, improve stability, and enhance the effect of slip resistance

Inactive Publication Date: 2019-06-21
芜湖市极星航空科技有限公司
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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 provide a shock-absorbing landing gear for unmanned aerial vehicles to solve the problem that the unmanned aerial vehicle landing gear in the prior art has a relatively simple structure. The shock absorption effect will have a certain impact on the fuselage, and the drone is prone to rollover and other problems when it lands

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  • UAV (unmanned aerial vehicle) vibration-absorbing landing bracket

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Embodiment Construction

[0016] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0017] see Figure 1-5 In the embodiment of the present invention, a shock-absorbing landing gear for an unmanned aerial vehicle includes a drone body 2, and brackets 4 are installed on both sides of the bottom end of the drone body 2. The landing gear 7 and the shock-absorbing column 6 are composed of a telescopic sleeve 15, a telescopic rod 16 and a shock-absorbing spring 17. When the drone body 2 falls, the shock-absorbing column 6...

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Abstract

The invention discloses an UAV (unmanned aerial vehicle) vibration-absorbing landing bracket, comprising an UAV body, wherein two sides of the bottom end of the UAV body are provided with a support frame; the lower end of the support frame is connected with the landing bracket through a vibration-absorbing column; the vibration-absorbing column is composed of a telescopic sleeve, a telescopic rodand a vibration-absorbing spring group; the lower end of the landing bracket is provided with a bottom frame; a bracket accommodating sleeve is arranged outside the support frame; an anti-turning bracket is arranged outside the landing bracket; the anti-turning bracket is connected with the landing bracket through a rotating shaft; a reinforced pole is arranged between the landing brackets; an article-bearing net is arranged between the reinforced poles; each reinforced pole is provided with an elastic strap and a buckle; the two sides of the UAV body are provided with wings; a propeller is arranged on the wings. In the UAV (unmanned aerial vehicle) vibration-absorbing landing bracket disclosed by the invention, the landing bracket has a good vibration absorbing effect. When the UAV lands,effective vibration-absorbing protection is provided for the UAV body. The landing bracket has anti-turning performance, so that the UAV doesn't turn over during landing.

Description

technical field [0001] The present invention is in the technical field of unmanned aerial vehicle equipment, in particular to a shock-absorbing landing gear for unmanned aerial vehicles. Background technique [0002] Unmanned aircraft is referred to as "unmanned aerial vehicle", which is an unmanned aircraft operated by radio remote control equipment and self-provided program control device, or operated by on-board computer completely or intermittently. Compared with manned aircraft, Drones are often more suitable for tasks that are too "dumb, dirty or dangerous". The landing gear of the drone is a rack used to support the drone when it is landing. The existing drone landing gear structure is relatively simple, landing When the frame directly contacts the bottom surface, there is no shock absorption function, and the shock absorption effect cannot be well achieved. It will have a certain impact on the fuselage, and if the drone is not stable, it will easily roll over and so ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/62B64C25/64B64C25/04B64C25/10
Inventor 刘天天牛骏
Owner 芜湖市极星航空科技有限公司
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