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A roller-type multi-stage damping reed pipe UAV anti-drop device

An unmanned aerial vehicle, a roller-type technology, applied in the field of unmanned aerial vehicles, can solve problems such as easy rollover, and achieve the effect of easy disassembly and replacement, avoiding damage to the body and equipment, and light weight

Inactive Publication Date: 2018-07-31
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to reduce the strong impact of the unmanned aerial vehicle landing on the ground in the prior art, and to overcome the problem of being unable to land on undulating roads and easily turning over when landing, the present invention proposes a roller-type multi-stage damping reed switch UAV anti-drop device

Method used

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  • A roller-type multi-stage damping reed pipe UAV anti-drop device
  • A roller-type multi-stage damping reed pipe UAV anti-drop device
  • A roller-type multi-stage damping reed pipe UAV anti-drop device

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Embodiment Construction

[0023] This embodiment is a roller-type multi-stage damping reed switch UAV anti-drop device.

[0024] refer to Figure 1 to Figure 6 , this embodiment takes the rotor drone as an example. The roller type multi-stage damping reed pipe UAV anti-drop device is composed of a long reed pipe, a short reed pipe, a universal wheel bracket, and a hinge support on the fuselage floor. The long reed pipe and the short reed pipe are three-stage damping reed pipes respectively. Structure, the damping reed tube is a thin-walled cylindrical ferromagnetic tube, and a magnetic bar and a spring are installed in the ferromagnetic tube. The long reed pipe and the short reed pipe are two structurally identical parts, and the length of the short reed pipe is one third of the length of the long reed pipe. The fuselage floor hinge supports are divided into multiple groups, with the outer normal of the fuselage floor passing through the center of gravity of the fuselage as the reference outer normal...

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Abstract

The invention discloses a roller type multistage damping reed pipe anti-falling device for an unmanned aerial vehicle. A three-level damping reed pipe telescopic structure is adopted, damping reed pipes are in a thin-shell cylinder shape, and magnetic rods and springs are installed in the damping reed pipes. The two damping reed pipes have unequal lengths, and the length of the short reed pipe is one-third that of the long reed pipe. The long reed pipe and the short reed pipe are connected to a hinge support of a fuselage base plate, and the tail end of the short reed pipe is connected to the side wall of a first stage of the long reed pipe. A universal wheel support is connected with the long reed pipe, a rubber wheel is installed below the support, and a pressure ball bearing rotates to achieve 360-degree rotation of the rubber wheel. When the rotor unmanned aerial vehicle lands, the anti-falling device delays ground contact time by compressing the springs to reduce impact force and converts kinetic energy into elastic potential energy, magnetic damping can alleviate vibration, and energy is dissipated. The universal wheel support is matched with the rubber wheel to prevent rollover caused by a horizontal speed, and the goal of protecting the unmanned aerial vehicle is achieved. The anti-falling device can also serve as an undercarriage to make the unmanned aerial vehicle capable of landing directly.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a roller-type multi-stage damping reed pipe anti-drop device for unmanned aerial vehicles. Background technique [0002] Multi-rotor unmanned aerial vehicles (UAVs) are the frontier and hot issues of research at home and abroad in recent years, and they are widely used in agriculture, commerce and surveying fields. Multi-rotor drones have the characteristics of flexible maneuverability and quick response in aerial photography and item loading and transportation applications. However, the proficiency of UAV operators is uneven, or there are occasional mechanical failures, which cause abnormal landings, which may easily cause damage to the aircraft structure and equipment. Therefore, the design of the shock-absorbing landing gear with certain damping is particularly important to protect the safety of the airframe and equipment. [0003] The landing gear of the mu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C25/62
CPCB64C25/62
Inventor 吴艳辉赵征汪一舟是介
Owner NORTHWESTERN POLYTECHNICAL UNIV
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