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Unmanned aerial vehicle launching device

A technology of a launching device and an unmanned aerial vehicle, applied in the field of unmanned aerial vehicles, can solve the problems of difficult assembly, low exit speed, and small unilateral gap of the launch tube, and achieve the effects of easy installation, simple structure and high exit speed.

Active Publication Date: 2021-06-29
河南创仕航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, for single-tube launch, the exit velocity requirement is smaller
Single barrel launch cannot store a large amount of gas in advance
When installing the launch tube, the gap with one side of the launch tube is small, so it is not easy to assemble

Method used

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Embodiment Construction

[0021] 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.

[0022] Please also refer to the attached Figure 1-2 As shown, the present invention provides a UAV launching device 100

[0023] The drone launching device 100 includes a base 1 , a launch tube 2 , an air tank 3 , a connecting pipe 4 , a solenoid valve (not shown in the figure) and a supporting block (not shown in the figure).

[0024] The launch tube 2 includes a tube body 21 for accommodating an unmanned aerial vehicle (not shown in the figure) and a locki...

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PUM

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Abstract

An unmanned aerial vehicle launching device comprises a base, a launching cylinder, an air storage cylinder, a connecting pipe, an electromagnetic valve and a supporting block, the launching cylinder comprises a cylinder body used for containing an unmanned aerial vehicle and a locking clamping plate fixed to the cylinder body, one end of the cylinder body is fixed to the base, and the other end of the cylinder body is of an opening-shaped structure communicated with the outside; and the locking clamping plate is located at the end, close to the opening-shaped structure, of the barrel and used for forming a clamping fixing structure with the unmanned aerial vehicle. The air reservoir is fixed on the base; and the connecting pipe is fixed to the base, one end of the connecting pipe communicates with the launching cylinder, and the other end of the connecting pipe communicates with the air storage cylinder. The electromagnetic valve is installed in the launching cylinder and controls the launching cylinder and the air storage cylinder to be communicated or closed. The supporting block is arranged in the launching cylinder, and when the unmanned aerial vehicle is contained in the cylinder body, the supporting block and the locking clamping plate connectorly support and fix the unmanned aerial vehicle. Compared with the prior art, the device is simple in structure and easy to assemble.

Description

【Technical field】 [0001] The invention relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle launching device. 【Background technique】 [0002] In recent years, with the rapid development of UAVs, especially the application of UAV launching devices has become more and more widespread. UAVs generally use folding-wing UAVs. The wings can be folded to achieve portability and convenient storage. The UAV is pre-installed in the launch tube, and the launch tube is used to accommodate the drone launcher for launch. [0003] In related technologies, the UAV launch device includes a launch tube, which is generally a glass fiber tube. [0004] However, for single-barreled launch, the exit velocity requirement is smaller. Single-barrel launches cannot store large amounts of gas in advance. When the launch tube is installed, the gap with the one side of the launch tube is small, so it is not easy to assemble. [0005] Therefore, it is necessary...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 郭彬新翟彬薛明旭
Owner 河南创仕航空科技有限公司
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