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Unmanned aerial vehicle launching device

A launching device and unmanned aerial vehicle technology, applied in the field of unmanned aerial vehicles, can solve the problems of complex release mechanism, poor ejection consistency, unsafety, etc., and achieve the effect of safe and reliable launch, simple and reliable structure, and good launch consistency

Active Publication Date: 2020-06-09
中船重工海空智能装备有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The disadvantages of the launch device for small drones in the prior art mainly lie in: 1. The release mechanism is complicated and unsafe; 2. The ejection consistency is not good

Method used

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  • Unmanned aerial vehicle launching device
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  • Unmanned aerial vehicle launching device

Examples

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Embodiment Construction

[0033] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0034] This embodiment provides a drone launching device, which is easy to operate and safe to launch, can achieve light weight, and has good ease of use, safety, durability and launch consistency.

[0035] like Figure 1-6 As shown, the launching device includes: traction system 1, buffer mechanism 2, ejection guide rail 3, release mechanism 4, front support 5, ejection trolley 6 and rear end support 7; traction system 1 includes: winch, traction rope, rubber band and Fixed pulley A; buffer mechanism 2 includes: buffer spring 21, support block 22, buffer pressure head 24, guide 23 and depression bar 25; ejection guide rail 3 includes: front guide rail 31 and rear guide rail 32; release mechanism 4 includes: car body Lock block 41, release block 42, fixed seat 43, compression spring 44 and release rope 45; front end support 5 includes: clamping part 51 an...

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Abstract

The invention discloses an unmanned aerial vehicle launching device, which comprises: a traction system, a buffer mechanism, an ejection guide rail, a release mechanism, a front end support, an ejection trolley and a rear end support. The traction system comprises a rubber band and a fixed pulley A; two ends of the ejection guide rail are respectively supported by front and rear end supports; thebuffer mechanism and the fixed pulley A are arranged at the front end of the ejection guide rail, and the buffer mechanism is located behind the fixed pulley A; the ejection trolley and the release mechanism are arranged at the rear end of the ejection guide rail, and the ejection trolley is located in front of the release mechanism; one end of the rubber band is installed at the front end of theejection trolley, and the other end of the rubber band bypasses the fixed pulley A and is fixed to the rear end of the ejection trolley. The unmanned aerial vehicle is installed on the ejection trolley. The release mechanism can lock the ejection trolley at the rear end of the ejection guide rail, during unlocking, the ejection trolley can slide to the front end along the ejection guide rail underthe action of a restoring force of the rubber band, the buffer mechanism is used for buffering and decelerating the ejection trolley, and the unmanned aerial vehicle can be launched out relative to the ejection trolley under the action of inertia force.

Description

technical field [0001] The invention relates to the technical field of drones, in particular to a launching device for drones. Background technique [0002] Small reconnaissance UAVs are divided into fixed-wing and multi-rotor UAVs by type, and use batteries as power. Among them, small fixed-wing UAVs are easy to deploy, flexible to use, easy to maintain, fast, long-range, and loaded. It has obvious advantages such as suitable capabilities, can enter the sky over the operation area to conduct surveillance and reconnaissance to obtain intelligence information, and has unique advantages such as real-time transmission of target images. It has been widely used in actual military operations and civilian fields, and can effectively complement satellite and manned reconnaissance Insufficient in strength, it is a kind of unmanned aerial vehicle with the largest number of equipment at home and abroad. [0003] In order to meet the needs of safe take-off of small reconnaissance drone...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 吴烁唐春胡宗智沈冬李波涛
Owner 中船重工海空智能装备有限公司
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