Unmanned aerial vehicle with landing protection function

A protection function and technology for drones, applied in the field of drones, can solve problems such as wasted storage space, damage to the body of the drone, and the drone is not provided with a buffering and shock-absorbing device, and achieves good buffering and shock-absorbing effects. The effect of saving storage space and improving practicality

Inactive Publication Date: 2021-11-02
誉荣广州网络科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] During the landing process of the UAV, the UAV often collides with the ground due to careless operation of the operator or due to terrain and airflow. The high impact force between the drone and the ground will cause the UAV to be unable to land smoothly, thus causing a certain degree of damage to the fuselage of the UAV, and the existing UAVs with buffer and shock absorption functions generally have buffer and shock absorption devices. Unable to store, resulting in waste of storage space

Method used

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  • Unmanned aerial vehicle with landing protection function
  • Unmanned aerial vehicle with landing protection function
  • Unmanned aerial vehicle with landing protection function

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Embodiment Construction

[0023] The present invention is described in further detail now in conjunction with accompanying drawing. These drawings are all simplified schematic diagrams, which only illustrate the basic structure of the present invention in a schematic manner, so they only show the configurations related to the present invention.

[0024] Such as figure 1 As shown, a UAV with a landing protection function includes a main body 1, a support buffer mechanism and a storage mechanism, and the support buffer mechanism and the storage mechanism are both arranged on the main body 1;

[0025] When the device is in use, the main body 1 is used to realize the flight of the device, the shock generated when the main body 1 falls is buffered and damped by the support buffer mechanism, and the support buffer mechanism is stored by the storage mechanism.

[0026] Such as Figure 2-4As shown, there are two support and buffer mechanisms, and the two support and buffer mechanisms are respectively arrange...

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Abstract

The invention relates to a unmanned aerial vehicle with a landing protection function. Theunmanned aerial vehicle comprises a main body, two supporting and buffering mechanisms and a storage mechanism; the supporting and buffering mechanisms and the storage mechanism are arranged on the main body, the two supporting and buffering mechanisms are arranged at the two ends of the main body correspondingly, and each supporting and buffering mechanism comprises a supporting assembly and a buffering assembly; each supporting assembly comprises a supporting unit and a connecting unit,each buffering assembly comprises a buffering unit, a pushing unit and a positioning unit, and the storage mechanism comprises a moving assembly and a locking assembly.According to the unmanned aerial vehicle with the landing protection function, flight is achieved through the main body, and vibration generated during landing of the main body is buffered and damped through the supporting and buffering mechanisms; storage is achieved through the storage mechanism, the device is provided with multiple buffering and damping structures, the better buffering and damping effect is achieved, therefore, the main body is better protected, storage can be achieved through the storage mechanism, the storage space is saved, meanwhile, the device is protected, and practicability is improved.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle with a landing protection function. Background technique [0002] Unmanned aircraft, referred to as unmanned aerial vehicle, is an unmanned aircraft controlled by radio remote control equipment and self-contained program control device, or operated completely or intermittently by the on-board computer. [0003] During the landing process of the UAV, the UAV often collides with the ground due to careless operation of the operator or due to terrain and airflow. The high impact force between the drone and the ground will cause the UAV to be unable to land smoothly, thus causing a certain degree of damage to the fuselage of the UAV, and the existing UAVs with buffer and shock absorption functions generally have buffer and shock absorption devices. It cannot be stored, resulting in a waste of storage space. Contents of the invention [0004] The technical problem to be solved by the present invention i...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/62B64C25/26
CPCB64C25/62B64C25/26
Inventor 谢传忠
Owner 誉荣广州网络科技有限公司
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