Retraction system for mooring unmanned aerial vehicle and method for deploying and retracting mooring unmanned aerial vehicle with same

A UAV, tethered technology, applied in the field of aircraft to achieve the effect of ensuring take-off and landing

Inactive Publication Date: 2016-10-12
任雪峰
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, in the prior art, there is no system, device and method that can effectively solve the problem of tethered UAV ...

Method used

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  • Retraction system for mooring unmanned aerial vehicle and method for deploying and retracting mooring unmanned aerial vehicle with same
  • Retraction system for mooring unmanned aerial vehicle and method for deploying and retracting mooring unmanned aerial vehicle with same
  • Retraction system for mooring unmanned aerial vehicle and method for deploying and retracting mooring unmanned aerial vehicle with same

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Embodiment Construction

[0028] The technical solution of the present invention will be described in further detail below in conjunction with the accompanying drawings.

[0029] Such as figure 1 and 2 As shown, the retractable system for tethered UAV of the present invention includes a retractable compartment 20 for accommodating the tethered UAV 10, which includes an inner space. Specifically, the retractable compartment 20 includes: a lifting platform 210 , a slidable compartment cover 220 , cables 230 and a cable retractable device 240 for retracting the cables 230 .

[0030] Wherein, the lifting platform 210 is disposed in the inner space of the retractable cabin 20 for making the tethered drone 10 rest thereon. Specifically, the lifting platform 210 includes: a lifting platform body 211, whose top surface is used to place the moored drone 10; a lifting platform bracket 212, which is used to support the lifting platform body 211; a guide, which is located in the storage compartment The bottom ...

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Abstract

The invention relates to a retraction system for a mooring unmanned aerial vehicle. The retraction system comprises an retraction cabin for containing the mooring unmanned aerial vehicle, a cable for communication and power transmission and a cable take-up and pay-off device used for taking up and paying off the cable, wherein the retraction cabin comprises a lifting platform and a slidable cabin cover, the lifting platform is arranged inside the retraction cabin, the mooring unmanned aerial vehicle can stay on the lifting platform, the slidable cabin cover is arranged on the top of the retraction cabin and used for opening and closing the retraction cabin, and the cable take-up and pay-off device is arranged in the retraction system and connected with the mooring unmanned aerial vehicle through the cable. The invention further provides a method for deploying and retracting the mooring unmanned aerial vehicle through the retraction system. The method comprises the releasing step and the retracting step. The system and method can effectively solve the deploying and retracting problems of the mooring unmanned aerial vehicle.

Description

technical field [0001] The invention relates to the field of aircraft. More specifically, the present invention relates to a system for retracting and deploying a tethered UAV and a method for retracting and deploying the tethered UAV. Background technique [0002] Tethered UAV is a kind of UAV that is developing rapidly nowadays. Since the flight and control of tethered drones require loads of high voltage and high current, most tethered drones are not equipped with a power supply unit, or the power supply of the power supply unit is very small. Usually, the tethered UAV relies on one or more cables to connect with the ground power supply system and relies on the ground power supply system to provide it with the power required for endurance. Therefore, the tethered drone will always drag the cable during flight, hence the name of the tethered drone. [0003] The retractable technology of the tethered UAV is an important part of the technology of the tethered UAV, which p...

Claims

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Application Information

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IPC IPC(8): B64F1/00B64F1/12
CPCB64F1/007B64F1/12B64U50/34B64U80/70
Inventor 任雪峰
Owner 任雪峰
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