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Fixed-wing unmanned aerial vehicle landing mode

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: 2018-08-17
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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  • Fixed-wing unmanned aerial vehicle landing mode
  • Fixed-wing unmanned aerial vehicle landing mode
  • Fixed-wing unmanned aerial vehicle landing mode

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Experimental program
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Embodiment Construction

[0009] The present invention will be further described below in conjunction with accompanying drawing: a kind of fixed-wing unmanned aerial vehicle landing mode, comprises two vertical rods 1 and fixed-wing unmanned aerial vehicle 2; Described two vertical rods are vertically fixed on the ground, A support frame 11 is installed on the bar 1, and the support frame 11 is a U-shaped structure, and a rubber rope 12 is installed on the support frame 11, and the two ends of the rubber rope 12 are respectively connected to two endpoints of the support frame 11; It is made of rubber and latex, and has the characteristics of large elongation, high toughness, and good resilience; the distance between the two rubber ropes 12 is smaller than the wingspan of the fixed-wing UAV 3; the fixed-wing has no Two buckle devices 21 and two pop-up devices 22 are installed on the man-machine 2, and the two buckle devices 21 are respectively installed on the ends of the two wings of the fixed-wing UAV ...

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Abstract

The invention discloses a fixed-wing unmanned aerial vehicle landing mode, and belongs to the field of a fixed-wing unmanned aerial vehicle landing device. The fixed-wing unmanned aerial vehicle landing mode comprises two vertical rods and a fixed-wing unmanned aerial vehicle. The two vertical rods are vertically fixed to the ground, supporting frames are installed on the vertical rods, and the supporting frames are of a U-shaped structure. Rubber ropes are installed on the supporting frames, and two ends of the rubber ropes are separately connected with two end points of the supporting frames. The rubber ropes are made of rubber and latex, and has the advantages of large elongation, high toughness and good resilience. The fixed-wing unmanned aerial vehicle is provided with two buckle devices and two ejecting devices, and the two buckle devices are separately installed at the tail ends of two wings of the fixed-wing unmanned aerial vehicle. The ejecting devices are installed in the wings of the fixed-wing unmanned aerial vehicle, and after receiving a signal, round rods can be ejected to be connected with the buckle devices to form closed structures. The brand new fixed-wing unmanned aerial vehicle landing mode efficiently completes 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 a support frame is installed on the vertical pole, and the support frame has a U-shaped structure , a rubber...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/02
CPCB64F1/02
Inventor 黄华辉
Owner 佛山云澈科技有限公司