Multi-rotor-wing unmanned aerial vehicle mooring system

A multi-rotor unmanned and aircraft technology, which is applied to ground devices, aircraft parts, and ground devices for mooring aircraft, to achieve the effects of low cost, stable hovering, and convenient use

Active Publication Date: 2013-06-12
CHINA ELECTRONICS TECH GRP NO 7 RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Compared with the general technology, the multi-rotor UAV mooring system of the present invention has the characteristics of simple structure, high reliability, stable hovering, convenient use and low cost. The mooring method is applied to the multi-rotor UAV to solve the problem of Solved the common problems of the tethered platform in terms of stability, erection convenience, flexibility of use and cost of use

Method used

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  • Multi-rotor-wing unmanned aerial vehicle mooring system

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Embodiment Construction

[0011] In order to further illustrate the technical means adopted by the present invention and the achieved effects, the technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings and preferred embodiments.

[0012] see figure 1 , is a structural schematic diagram of the mooring system of the multi-rotor unmanned aerial vehicle of the present invention. The multi-rotor unmanned aircraft mooring system of the present invention includes a multi-rotor unmanned aircraft as a mooring platform, a mooring cable and a ground device, and the mooring cable connects the multi-rotor unmanned aircraft and the ground device; The rotor unmanned aircraft includes a tethered power supply unit, the tether cable includes a power transmission cable, the ground unit includes a ground power supply unit, and the tethered power supply unit is connected to the ground power supply unit through the power transmission cable in...

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Abstract

The invention discloses a multi-rotor-wing unmanned aerial vehicle mooring system, which comprises a multi-rotor-wing unmanned aerial vehicle serving as a mooring platform, a mooring line and a ground device, wherein the mooring line is connected with the multi-rotor-wing unmanned aerial vehicle and the ground device; the multi-rotor-wing unmanned aerial vehicle comprises a mooring supply unit; the mooring line comprises a power transmission cable; the ground device comprises a ground power supply device; and the mooring supply unit is connected with the ground power supply device via the power transmission cable in the mooring line. The multi-rotor-wing unmanned aerial vehicle mooring system disclosed by the invention has the characteristics of simple structure, high reliability, stability in hovering, convenience in use and low cost, the mooring mode is applied to the multi-rotor-wing unmanned aerial vehicle, and the problems of the mooring platform on the aspects of stability, erection convenience, use flexibility and use cost are solved. In addition, through the power transmission cable in the mooring line, a ground power supply can continuously supply power to the mooring platform, and the long-time hovering flight of the aerial vehicle is realized.

Description

technical field [0001] The invention relates to the technical field of mooring systems, in particular to a mooring system for a multi-rotor unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicles such as balloons, airships, and ducted aircraft have the characteristics of vertical take-off and landing and stable hovering, and are widely used as tethered platforms in the fields of reconnaissance, communication, and aerial photography. Although tethered balloons or tethered airships can stay in the air for a long time, they have a large volume, expensive filling gas, and high maintenance costs. The ducted aircraft must use multiple tethers, which is costly, complicated to erect and open, and requires a large erection site; when multiple tethers are tethered to fly, the horizontal orientation of the fuselage is fixed, and it cannot be flexible according to the actual needs of the mission. Rotate the horizontal orientation, unless the aircraft is lowered,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/36H01B9/00B64F3/02
Inventor 付松源彭革新杨涛程晓洁武广友
Owner CHINA ELECTRONICS TECH GRP NO 7 RES INST
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