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Landing method of fixed-wing unmanned aerial vehicle

A UAV, fixed-wing technology, applied in aircraft parts, aircraft landers, ground devices, etc., can solve problems such as inability to land, lack of efficient landing methods, etc.

Inactive Publication Date: 2018-09-04
佛山云澈科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In certain environments, there will be situations where landing is not possible, and the existing fixed-wing UAVs lack an efficient way to land

Method used

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  • Landing method of fixed-wing unmanned aerial vehicle
  • Landing method of fixed-wing unmanned aerial vehicle
  • Landing method of fixed-wing unmanned aerial vehicle

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Experimental program
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Embodiment Construction

[0010] The present invention will be further described below in conjunction with accompanying drawing: a kind of landing mode of fixed-wing unmanned aerial vehicle, comprises two vertical rods 1 and fixed-wing unmanned aerial vehicle 2; Described two vertical rods are vertically fixed on the ground, in A support frame 11, a rope 15, a weight 16, a fixed plate 17, a track 14 and a sliding device 13 are installed on the vertical bar 1; 13. The two ends of the track 14 are provided with protruding structures to prevent the sliding device 13 from sliding out of the track 14; In contact with the track 14, the sliding device 13 can slide on the track 14, and generate a certain frictional force with the track 14; the fixed plate 17 is installed at the starting point of the track 14, and a circular hole is provided in the middle of the fixed plate 17; One end of the rope 15 is connected to the slideway device 13, and the other end passes through the round hole in the middle of the fix...

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Abstract

The invention discloses a landing method of a fixed-wing unmanned aerial vehicle, and belongs to the field of landing devices of fixed-wing unmanned aerial vehicles. The landing method of the fixed-wing unmanned aerial vehicle comprises two vertical rods and a fixed-wing unmanned aerial vehicle body. The two vertical rods are vertically fixed to the ground, the vertical rods are provided with supporting frames, ropes, weights, fixing plates, tracks and sliding devices. The tracks are horizontally installed at the upper ends of the vertical rods, and the peripheries of the tracks are partiallywrapped with the sliding devices. The sliding devices and the supporting frames are connected, and the inner walls of the sliding devices are in contact with the tracks. A rubber rope is installed oneach supporting frame, and two ends of each rubber rope are separately connected to two ends of each supporting frame. The fixed-wing unmanned aerial vehicle body is provided with two clamping buckling devices and two ejection devices, and the two clamping buckling devices are separately installed at the tail ends of two rings of the fixed-wing unmanned aerial vehicle body. The ejection devices are installed in the wings of the fixed-wing unmanned aerial vehicle body, and the ejection devices can pop up round rods to be connected with the clamping buckling devices to form closed structures after receiving a signal. The landing method of the fixed-wing unmanned aerial vehicle can effectively complete the landing process of the fixed-wing unmanned aerial vehicle.

Description

technical field [0001] A landing method for a fixed-wing unmanned aerial vehicle belongs to the field of landing devices for the fixed-wing unmanned aerial vehicle. Background technique [0002] The traditional fixed-wing UAV landing requires a runway to complete the deceleration process, which will take up a lot of resources. There will also be situations where landing cannot be performed under certain circumstances, and the existing fixed-wing drones lack an efficient landing method. Contents of the invention [0003] The purpose of the present invention is to solve the above problems and provide a brand-new landing method for fixed-wing unmanned aerial vehicles. [0004] A landing method for a fixed-wing unmanned aerial vehicle, comprising two vertical poles and a fixed-wing unmanned aerial vehicle; the two vertical poles are vertically fixed on the ground, and support frames, ropes, weights, Fixed plate, track and sliding device; the track is horizontally installed o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/00B64D45/06
CPCB64F1/00B64D45/06
Inventor 黄华辉
Owner 佛山云澈科技有限公司