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Sub-mother unmanned aerial vehicle unit based on folded combination form and combination method thereof

A combined form, sub-UAV technology, applied in the field of UAVs, to achieve the effect of reducing the occupied space, increasing the compactness, and increasing the loading capacity

Active Publication Date: 2020-01-03
SHANGHAI INST OF ELECTROMECHANICAL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This invention is mainly used for the connection of signals between multiple drones and the supply of energy, and does not involve the improvement of links such as the delivery of cluster drones

Method used

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  • Sub-mother unmanned aerial vehicle unit based on folded combination form and combination method thereof
  • Sub-mother unmanned aerial vehicle unit based on folded combination form and combination method thereof
  • Sub-mother unmanned aerial vehicle unit based on folded combination form and combination method thereof

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Effect test

Embodiment 1

[0037] The present invention discloses a mother-child UAV group based on folding and combination, including a mother UAV 1 and a sub-UAV 2; the two sub-UAVs 2 are respectively connected and located on the mother UAV 1 on both sides of the flanks.

[0038] The present invention combines one main, two auxiliary and three unmanned aerial vehicles into the form of a sub-maternal unmanned aerial vehicle, which can adopt different strategies of combined flight and independent flight according to the task requirements at different stages of task execution, and at the same time can reduce the size of the unmanned aerial vehicle The occupied space increases the number of drones dropped.

[0039] Specifically, such as Figure 1-3 Shown:

[0040] The flanks of the parent UAV 1 are provided with an actuating mechanism 11, and the belly of the child UAV 2 is provided with a slot mechanism 21, and the actuating mechanism 11 is matched and connected with the slot mechanism 21, further,

...

Embodiment 2

[0052] The present invention also provides a method for combining the sub-maternal unmanned aerial vehicle based on the folding combination form, using the sub-maternal unmanned aerial vehicle group based on the folding combination form described in Embodiment 1, including the following steps:

[0053] The step of connecting the mother and child drones: connecting the two child drones 2 to the two wings of the parent drone 1 through the actuating mechanism 11 and the slot mechanism 21, so that the two drones The child UAV 2 is located on the two wings of the parent UAV 1;

[0054] The wing connection step of the sub-drone: the two adjacent wings of the two sub-drone 2 are folded through the folding mechanism 21, and the actuating mechanism 11 and the slot mechanism at the wingtip are folded. 21 to connect;

[0055] Wing closing step of the sub-drone: the two outer wings of the two sub-drone 2 that are far away from each other are flipped toward the upper side of the fuselage ...

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Abstract

The invention relates to a sub-mother unmanned aerial vehicle unit based on a folded combination form in the technical field of unmanned aerial vehicles. The sub-mother unmanned aerial vehicle unit comprises a mother unmanned aerial vehicle and sub-unmanned aerial vehicles, wherein two sub-unmanned aerial vehicles are connected and located on the side wings of the two sides of the mother unmannedaerial vehicle respectively. The invention further provides the sub-mother unmanned aerial vehicle unit based on the folded combination form and a combination method thereof. Through the design of thefolding deformation combining technology, the contradiction between the number of putting of the cluster unmanned aerial vehicle and the limited space of an aerial carrier can be effectively solved.

Description

technical field [0001] The present invention relates to the technical field of unmanned aerial vehicle (UAV), in particular, to a mother-child unmanned aerial vehicle unit based on folding and combination form and its combination method. Background technique [0002] When a single UAV or manned aircraft performs missions, it faces many limitations such as sensor performance, reconnaissance range, detection angle, and ammunition load. Therefore, organizing multiple drones, or even multiple different types of unmanned or manned / unmanned aircraft to cooperate in combat is an important application mode on the future battlefield, so the concept of drone swarms came into being. Swarm drones have the advantages of self-decomposition, coordination, and segmental operations to complete tasks seamlessly, but the advantages of cluster drones need to be guaranteed by the scale of cluster drones. Therefore, the launch technology of swarm drones is one of the main problems of swarm drone...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D5/00B64C1/30B64C3/56B64C5/10
CPCB64D5/00B64C1/30B64C3/56B64C5/10B64U2101/00B64U80/82
Inventor 赵炜毕鹏张顺家史松伟吴昕芸杜泽弘李晓龙尹航陈航赵钱孔晓俊周俊忠
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG
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