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Unmanned aerial vehicle balancing device

A balancing device and UAV technology, which is applied in the direction of aircraft stability, aircraft parts, transportation and packaging of devices controlled by gravity. damage

Inactive Publication Date: 2021-09-10
宁波阿瑞斯自动化技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the prior art, the impact between the UAV and the ground cannot be well buffered when it lands, resulting in damage to the UAV, and the UAV tends to tilt and lose its balance when it lands, causing the UAV to topple and fall. bad drone

Method used

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Embodiment Construction

[0028] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in combination with specific embodiments and with reference to the accompanying drawings. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the present invention. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concept of the present invention.

[0029] Such as Figure 1-8 As shown, a drone balancing device proposed by the present invention includes a drone body 1, a riser 2 is symmetrically installed on the bottom of the drone body 1, and a plurality of chutes 11 are symmetrically provided on the opposite face of the riser 2 , the chute 11 is provided with a second slide bar 20, the second slide bar 20 is provided with a second slide block 19, and the second sli...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle balancing device which comprises an unmanned aerial vehicle body, vertical plates are symmetrically arranged at the bottom of the unmanned aerial vehicle body, a plurality of sliding grooves are symmetrically formed in the opposite faces of the two vertical plates, second sliding rods are arranged in the sliding grooves, and the second sliding rods are sleeved with second sliding blocks. According to the device, through mutual cooperative use of sliding blocks, springs, sliding rods, supporting rods, buffer cylinders, buffer pull rods, baffles, bearings, connecting shafts and bases, the device can buffer scores generated between the unmanned aerial vehicle and the ground when the unmanned aerial vehicle lands, and the unmanned aerial vehicle is prevented from being damaged due to impact force; meanwhile, through cooperation of the balance plate, the balance block, the gear, the toothed rail, the servo motor and the gravity sensor, the balance stability of the unmanned aerial vehicle can be kept, the situation that the unmanned aerial vehicle topples over and is broken is avoided, certain loss is avoided, and the practicability is higher.

Description

technical field [0001] The invention relates to the technical field of drones, in particular to a balancing device for drones. Background technique [0002] UAVs are unmanned aircraft operated by radio-controlled equipment and self-contained program controls, or operated entirely or intermittently autonomously by an on-board computer. In the prior art, the impact between the UAV and the ground cannot be well buffered when it lands, resulting in damage to the UAV, and the UAV tends to tilt and lose its balance when it lands, causing the UAV to topple and fall. Bad drone. Therefore, we propose a drone balancing device. Contents of the invention [0003] (1) Purpose of the invention [0004] In order to solve the technical problems existing in the background technology, the present invention proposes a UAV balance device, which has the characteristics of buffering the impact force generated between the ground and the UAV and keeping the UAV balanced and not easy to dump. ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/62B64C17/02
CPCB64C25/62B64C17/02
Inventor 张磊
Owner 宁波阿瑞斯自动化技术有限公司
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