Integrally-throwing small cluster unmanned aerial vehicle sowing device

A technology for small unmanned aerial vehicles and unmanned aerial vehicles, which can be applied to launch devices, motor vehicles, aircraft parts, etc. Realize the effect of high-altitude delivery, fast spreading and flexible methods, and reduce the risk of collision

Pending Publication Date: 2020-03-27
NORTHWESTERN POLYTECHNICAL UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the existing air launch technology mostly adopts the launching tube type. Due to the influence of the space of the launching tube and the safety constraints of the parent aircraft and small UAVs, it is impossibl

Method used

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  • Integrally-throwing small cluster unmanned aerial vehicle sowing device
  • Integrally-throwing small cluster unmanned aerial vehicle sowing device
  • Integrally-throwing small cluster unmanned aerial vehicle sowing device

Examples

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Embodiment Construction

[0021] This embodiment is a kind of overall delivery of small cluster unmanned aerial vehicle spreading device.

[0022] refer to Figure 1 to Figure 4 , the present embodiment puts the small cluster unmanned aerial vehicle spreading device as a whole, including the pod housing 1, the retarder parachute assembly 2, the lock release mechanism 3, the small unmanned aerial vehicle 4, the single launch tube 5, and the cluster loading pod 6; Among them, the cluster loading pod 6 is mounted on the lower part of the wing of the UAV carrier, and two sets of cluster loading pods 6 are arranged symmetrically according to the UAV carrier, or a single group is suspended on the belly of the UAV carrier. The pod housing 1 adopts a streamlined design.

[0023] The single launch tube 5 is arranged and combined in the cluster loading pod 6, the rear end of the single launch tube is connected to the lock release mechanism 3, the lock release mechanism 3 is fixed inside the cluster load pod 6 t...

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Abstract

The invention discloses a spreading device for integrally throwing small cluster unmanned aerial vehicles. The spreading device is composed of a cluster loading nacelle, a brake parachute assembly, alocking and releasing mechanism, a single launching canister and the small unmanned aerial vehicles. The cluster loading nacelle is hung on the lower portion of a wing of the unmanned aerial vehicle carrier, during launching, only the small unmanned aerial vehicle in the single launching canister needs to be unlocked at the designated height, other catapulting mechanisms are not needed, and the control process is simple. The cluster loading nacelle is integrally thrown, and the collision risk between the small unmanned aerial vehicle and a carrier aircraft in the launching process is reduced.A cluster loading nacelle short-interval quick unlocking and throwing mode is adopted, one-time multi-frame quick aerial launching of small cluster unmanned aerial vehicles can be achieved, and the launching efficiency is high. A cluster loading nacelle overall speed reduction mode is adopted, and the structure is simple; the aerial carrier can be launched in an airspace higher than the combat height of the small unmanned aerial vehicle; and when the small unmanned aerial vehicle reaches a safe distance from the cluster loading nacelle, the propeller is started, and the small unmanned aerial vehicle flies to a predetermined area for networking.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a small cluster unmanned aerial vehicle rapid delivery device that adopts cluster-loaded integral delivery pods and drogue parachutes for rapid dissemination. Background technique [0002] With the advancement of science and technology, the aerial UAV platform has developed from a single air vehicle to a multi-purpose UAV aerial mission platform that can carry a variety of sensors, special equipment and weapons. However, due to the small size of general UAVs, the weapon loading of mission equipment is greatly limited, and compared with traditional air combat platforms, various combat performances are quite different. However, the small UAV platform has the advantages of low manufacturing difficulty, low production cost, and short production cycle. Compared with manned UAVs, small UAVs are easier to manufacture and use in large quantities. [0003] In recent year...

Claims

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Application Information

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IPC IPC(8): B64D1/02B64D5/00B64D17/62B64D17/78B64C39/02
CPCB64D1/02B64D5/00B64D17/62B64D17/78B64C39/02
Inventor 闵荣田雪涛孙恒义席庆彪
Owner NORTHWESTERN POLYTECHNICAL UNIV
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