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Landing mode of fixed wing unmanned aerial vehicle with weight

A UAV and fixed-wing technology, applied in the field of fixed-wing UAV landing devices, can solve the problems of lack of efficient landing methods and inability to land

Inactive Publication Date: 2018-08-28
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 mode of fixed wing unmanned aerial vehicle with weight
  • Landing mode of fixed wing unmanned aerial vehicle with weight
  • Landing mode of fixed wing unmanned aerial vehicle with weight

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Experimental program
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Embodiment Construction

[0010] Below in conjunction with accompanying drawing, the present invention will be further described: a kind of landing mode of the fixed-wing unmanned aerial vehicle with weight, comprises two vertical rods 1 and fixed-wing unmanned aerial vehicle 2; Described two vertical rods are vertically fixed on On the ground, a support frame 11, a slideway 14, a rope 15, a weight 16 and a square body 13 are installed on the vertical bar 1; The two ends of the square body 13 and the slideway 14 are provided with raised structures to prevent the square body 13 from slipping out of the slideway 14; 13 is connected together with the support frame 11 by the breach that slideway 14 is provided with, and square body 13 can slide in slideway 14, and produces certain frictional force with slideway 14; The side of described rope 15 and square body 13 is connected Together, the end of the rope 15 is provided with a weight 16; when the square body 13 slides in the slideway 14, the weight 16 is d...

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Abstract

The invention discloses a landing mode of a fixed wing unmanned aerial vehicle with a weight, and belongs to the field of fixed wing unmanned aerial vehicle landing devices. A device comprises two vertical rods and the fixed wing unmanned aerial vehicle, the two vertical rods are vertically fixed onto the ground, a supporting frame, a slide, a rope, the weight and a square are mounted on each vertical rod, the slide is horizontally mounted at the upper end of the corresponding vertical rods, the square is arranged in the slide and connected together with the supporting frame through a notch formed in the slide, the supporting frame is of a U-shaped structure, a rubber rope is mounted on the supporting frame, two ends of the rubber rope are connected with two end points of the supporting frame, two fastening devices and two popping devices are mounted on the fixed wing unmanned aerial vehicle, the two fastening devices are mounted at the tail ends of two wings of the fixed wing unmannedaerial vehicle, and the popping devices are mounted in the wings of the fixed wing unmanned aerial vehicle. By the landing mode of the fixed wing unmanned aerial vehicle, the landing process of the fixed wing unmanned aerial vehicle is efficiently finished.

Description

technical field [0001] A landing method for a fixed-wing unmanned aerial vehicle with heavy objects 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 with heavy objects, including two vertical poles and a fixed-wing unmanned aerial vehicle; the two vertical poles are vertically fixed on the ground, and a support frame, a slide road, rope, weight and square body; the slidew...

Claims

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Application Information

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IPC IPC(8): B64F1/02
CPCB64F1/02B64U70/30
Inventor 黄华辉
Owner 佛山云澈科技有限公司