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An aerial recovery device for unmanned aerial vehicles

A recovery device and drone technology, which is applied to aircraft parts, transportation and packaging, equipment for loading and unloading, etc., can solve the problems of unfavorable impact of drone activity radius and inability to achieve rapid recovery, and achieve rapid recovery work Effect

Active Publication Date: 2022-05-17
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Existing various platforms and various recovery methods cannot achieve fast recovery, and have a relatively large adverse effect on the radius of activity of the drone

Method used

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  • An aerial recovery device for unmanned aerial vehicles
  • An aerial recovery device for unmanned aerial vehicles
  • An aerial recovery device for unmanned aerial vehicles

Examples

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Embodiment Construction

[0019] The present invention will be further elaborated below in conjunction with the accompanying drawings. A UAV aerial recovery device includes a first linkage mechanism 2 and a second linkage mechanism 3. The first linkage mechanism 2 includes a fixed side 5, a sliding rail 6 and two sets of swing rods 7, the fixed side 5 is fixed at the tail of the main machine 1, one end of the two sets of swing rods 7 is connected to the fixed side 5, and the other end is connected to the slide rail 6, and the second linkage mechanism 2 includes a slider 8. The sub-machine docking device 9 and two sets of damping rods 10. The slider 8 is set on the slide rail 6 and can slide along the slide rail 6. One end of the two sets of damping rods 10 is connected to the slider 8, and the other One end is connected with the docking device 9 of the handset.

[0020] Both ends of the slide rail are provided with damping devices 11, preferably springs or liquids, to provide damping force. .

[0021...

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Abstract

The invention discloses an aerial recovery device for unmanned aerial vehicles, which comprises a first link mechanism and a second link mechanism. The first link mechanism includes a fixed side, a slide rail and two sets of swing bars, and the fixed side is fixed on a parent machine (1 ) tail, one end of two groups of swing rods is connected with the fixed side, and the other end is connected with the slide rail, the second link mechanism (2) includes a slider, sub-machine docking device and two groups of damping rods, and the slider is arranged on the slider The two sets of damping rods are connected to the slider at one end, and the other end is connected to the docking device of the sub-machine. The present invention adapts to the freight transport aircraft. The present invention relies on the slide rail and uses the hook mechanical device. Realize the deceleration and repositioning of the recovered UAV, combined with subsequent storage, can realize the recovery of fixed-wing UAVs faster than the existing recovery methods by virtue of the advantages of the high speed of the parent aircraft platform, and because the activity radius of the parent aircraft platform is relatively small Large, without negative restrictions on the radius of action of drones.

Description

technical field [0001] The invention relates to the technical field of aircraft space-based recovery, in particular to an aerial recovery device for unmanned aerial vehicles. Background technique [0002] At present, the specific recycling methods of fixed-wing UAVs include: parachuting, rope hook, hitting the net, etc. Platforms for implementing recovery actions include: land-based, sea-based and air-based. Among them, land-based and sea-based recovery methods include parachuting, rope hooks, hitting nets, etc. The space base is mainly recovered by means of parachuting from the helicopter platform. Existing various platforms and recovery methods cannot achieve rapid recovery, and have a relatively large adverse effect on the radius of activity of the drone. Contents of the invention [0003] The purpose of the present invention is to propose an aerial recovery device for unmanned aerial vehicles, which can quickly realize the recovery of unmanned aerial vehicles. [0...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D5/00B64D9/00B64D47/00
Inventor 任远春高怡宁李军府
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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