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A split drone

A kind of unmanned aerial vehicle, split-type technology, applied in the direction of fuselage, aircraft assembly, aircraft parts, etc., can solve the problems of inconvenient, etc., and achieve the effect of simple plug structure and convenient plug operation

Active Publication Date: 2022-04-26
宝鸡特种飞行器工程研究院有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in order to deal with complex work tasks or combat tasks, a launch team often needs to configure many different folding drones, which is not convenient enough

Method used

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  • A split drone
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Examples

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Embodiment 1

[0029] Such as Figure 1 to Figure 5 As shown, the split drone of this embodiment includes a nose 1, a fuselage 2, a first plug board 3, a second plug board 4, a pressure plate 5, a main wing mechanism 6, an empennage mechanism 7 and a power unit 8 ;

[0030] Such as image 3 As shown, the first plug board 3 is installed on the machine head 1, and the second plug board 4 is installed on the fuselage 2; the left and right edges of the first plug board 3 are provided with first wing plates 3-1 for connection , the first wing plate 3-1 is provided with a first wedge block 3-2 and a second wedge block 3-3; the left and right edges of the second plug board 4 are provided with a second wing plate 4-1 for connection, the second The second wing plate 4-1 is provided with a third wedge block 4-2 and a wedge block group 4-3, and the wedge block group 4-3 includes two wedge blocks opposite to each other, so that the middle of the wedge block group 4-3 form a V-shaped slot;

[0031] S...

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Abstract

The invention discloses a split-type unmanned aerial vehicle, comprising a nose, a fuselage, a first plug board, a second plug board, a main wing mechanism, a tail mechanism and a power device; the first plug board and the second plug board One of the boards is installed on the machine head, and the other is installed on the fuselage, and the machine head and the fuselage are connected through the first plug board and the second plug board; the edge of the first plug board is provided with a The first wing plate is provided with a first wedge block and a second wedge block; the edge of the second plug board is provided with a second wing plate for connection, and a third wedge block is provided on the second wing plate And the wedge block group, the main wing mechanism, empennage mechanism and power plant are all installed in the fuselage. In the present invention, the UAV is designed as a split structure, and the nose and the fuselage are connected to each other through the first plug-in board and the second plug-in board, so that the same fuselage can be equipped with different heads to adapt to different drones. work tasks.

Description

technical field [0001] The invention relates to the field of aircraft equipment, in particular to a split unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicles refer to unmanned unmanned aircrafts, which are generally controlled by airborne programs or ground remote control facilities. The characteristics of small size and no fear of danger make drones have a very wide range of uses in both military and civilian fields, such as aerial photography, plant protection, disaster relief, exploration and anti-terrorism. Different application fields have different working environments. In order to adapt to complex working environments, the prior art UAVs have developed a variety of launch methods, such as runway launch, rocket-assisted launch, orbital catapult launch, Motherboard air launch and barrel launch, etc. Among them, the barrel launch is mainly used in folding wing drones. The launch tube stores the folded drone inside the barrel, and ignites the...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/00B64F5/10
CPCB64C1/00B64F5/10
Inventor 宋宵翔郭晓伟赵蓓蕾麻鹏科
Owner 宝鸡特种飞行器工程研究院有限公司
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