Auxiliary take-off equipment for unmanned aerial vehicle

A technology of drones and equipment, which is applied in the field of drone auxiliary take-off equipment, can solve the problem that the four-axis drone landing pad does not have the ejection take-off function, and achieve the effect of improving execution efficiency

Inactive Publication Date: 2020-09-18
孙伟
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Aiming at the deficiencies of the prior art, the present invention provides an auxiliary take-off device for drones, which solves the problem that the current four-axis drone landing pad does not have the function of ejection take-off

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  • Auxiliary take-off equipment for unmanned aerial vehicle
  • Auxiliary take-off equipment for unmanned aerial vehicle
  • Auxiliary take-off equipment for unmanned aerial vehicle

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Embodiment Construction

[0023] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0024] see figure 1 , figure 2 , image 3 , Figure 4 , Figure 5 , Figure 6 As shown, the present invention provides a technical solution: a UAV auxiliary take-off device, including a control module 1, a heating module 2, an evaporation module 3, a safety module 4 and a water pipe 5, and the heating module 2 includes a base plate 201, a ceramic frame support 202, ceramic frame 203, heating wire 204, ceramic ring 205 and ceramic ring support 206, the to...

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Abstract

The invention discloses auxiliary take-off equipment for an unmanned aerial vehicle. The equipment comprises a control module, a heating module, an evaporation module, a safety module and a water pipe. The heating module comprises a bottom plate, a ceramic frame support, a ceramic frame, a heating wire, a ceramic ring and a ceramic ring support, the ceramic frame is fixedly connected to the upperportion of the bottom plate through the ceramic frame support, and the heating wire is fixedly connected to the inner ring of the ceramic frame. The evaporation module is arranged; when the air pressure in a water storage barrel is too high, the water storage barrel can be effectively protected from bursting due to overlarge air pressure; in addition, the air pressure of the water storage barrel does not exceed the rated power, so that the phenomenon that the unmanned aerial vehicle is damaged due to the too large air pressure is prevented; a valve can be rapidly opened by arranging the control module, the unmanned aerial vehicle can take off more rapidly, and the execution efficiency can be effectively improved when an emergency task is executed.

Description

technical field [0001] The invention relates to the technical field of catapult take-off, in particular to an auxiliary take-off device for an unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as unmanned aerial vehicle, is an unmanned aircraft controlled by radio remote control equipment and its own program control device. UAV is actually a general term for unmanned aerial vehicles. From a technical point of view, it can be divided into: unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned Paraplane etc. Compared with manned aircraft, it has the advantages of small size, low cost, convenient use, low requirements for combat environment, and strong battlefield survivability. Contents of the invention [0003] Aiming at the deficiencies in the prior art, the present invention provides an auxiliary take-off device for unmanned aerial ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04B64F1/06F22B1/28F22B37/44
CPCB64F1/04B64F1/06F22B1/28F22B37/446
Inventor 孙伟
Owner 孙伟
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