Rotary unmanned aerial vehicle launching device

A launching device and unmanned aerial vehicle technology, applied in the field of rotating unmanned aerial vehicle launching device, can solve the problems of large space occupation, high operating cost, complex structure, etc., and achieve small structural weight, reliable rack separation, and convenient storage and transportation Effect

Inactive Publication Date: 2020-04-03
BEIJING INST OF SPECIALIZED MACHINERY
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved by the present invention is to solve the disadvantages of the linear slide-rail UAV launching device involved in the background technology, which takes up a large space, needs to be boosted by external force to reduce the length of the UAV launching frame, has a complex structure, and has high operating costs. , making technological innovations to the traditional linear slide rail UAV take-off and launching device, making full use of the characteristics of circular motion reciprocating and cyclic motion, which can have enough acceleration space, and proposing a rotary UAV launch device based on circular motion

Method used

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  • Rotary unmanned aerial vehicle launching device
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Embodiment Construction

[0026] The present invention will be further described below in conjunction with the accompanying drawings.

[0027] Such as figure 1 As shown, a rotary launching device of the present invention is a technical innovation of the traditional linear slide rail type UAV take-off and launching device, making full use of the characteristics of circular motion, reciprocating cycle motion, and sufficient acceleration space. The launch device is composed of a rotary launch frame 1, a launch inclination control device 3, a separation device 5, a pulley device 2, and several unmanned aerial vehicles 4 to be launched. It has the characteristics of simple structure, small space occupation, and low launch cost. It can adapt to various launch methods such as UAV roadbed, sea-based, and vehicle-mounted mobile launch, and has high device versatility.

[0028] A rotary UAV launching device, which utilizes the characteristics of circular motion and reciprocating motion to make the UAV perform c...

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Abstract

The invention discloses a rotary unmanned aerial vehicle launching device, belongs to the technical field of aviation system unmanned aerial vehicle launching, and aims to realize technical innovationon a traditional linear slide rail type unmanned aerial vehicle launching device and obtain the rotary unmanned aerial vehicle launching device based on circular motion by making full use of the characteristic that the circular motion reciprocates circularly and has enough acceleration space. The launching device comprises a rotary launching frame, a launching inclination angle control device, aseparation device and a tackle device. The device has the advantages of being simple in structure, small in occupied space, low in launching cost and the like, can adapt to various launching modes such as unmanned aerial vehicle roadbeds, sea bases and vehicle-mounted mobile launching, and has high device universality.

Description

technical field [0001] The invention belongs to the technical field of aerial system unmanned aerial vehicle launching, and in particular relates to a rotary unmanned aerial vehicle launching device. Background technique [0002] Since the advent of drones in the 1920s, they have played an increasingly important role in warfare. Especially under the conditions of the modern information battlefield, drones are widely used to perform tasks such as reconnaissance, monitoring, situation assessment, and early warning strikes. As a key technology in the development of UAV technology, UAV launch and recovery technology is of great significance to promote the development of UAV technology. When UAVs perform combat missions, the two stages of take-off and landing are particularly critical, especially the choice of UAV launch technology, which directly determines whether the UAV can take off smoothly. There are many ways to take off UAVs, including hand throwing, ejection, rocket bo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04
CPCB64F1/04B64U70/00
Inventor 贾华宇李兆博巫伟男尹晓旭杨志
Owner BEIJING INST OF SPECIALIZED MACHINERY
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