Quick-assembling multi-rotor wing unmanned aerial vehicle structure

A multi-rotor unmanned aerial vehicle, fast technology, applied in the field of unmanned aerial vehicles, can solve the problems of long disassembly and assembly time, slow disassembly and assembly, etc., to achieve the effect of improving efficiency, shortening the manufacturing cycle and improving task efficiency

Pending Publication Date: 2017-08-29
BEIJING DIGSUR SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disassembly and assembly of the existing drones all rely on tools, which have the problems of slow disassembly and assembly and long disassembly and assembly time

Method used

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  • Quick-assembling multi-rotor wing unmanned aerial vehicle structure
  • Quick-assembling multi-rotor wing unmanned aerial vehicle structure
  • Quick-assembling multi-rotor wing unmanned aerial vehicle structure

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0064] The unmanned aerial vehicle structure described in embodiment 1 is the unmanned aerial vehicle structure of three axis six rotors, according to the quantity of wing, can also make such as Figure 9 The UAV structure of the six-axis six-rotor shown, such as Figure 10 The UAV structure of the four-axis quadrotor shown, such as Figure 11 The structure of the UAV with four axes and eight rotors is shown.

[0065] By adopting the above-mentioned technical scheme disclosed by the present invention, the following beneficial effects are obtained:

[0066] The structure of the UAV described in the present invention is a multi-rotor UAV that can be combined quickly and can realize different take-off weights, which shortens the manufacturing cycle of the UAV, reduces the cost of performing tasks, and improves task efficiency. The UAV structure of the present invention has the characteristics of tool-free installation, quick assembly and disassembly, quick assembly, and anti-ex...

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PUM

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Abstract

The invention discloses a quick-assembling multi-rotor wing unmanned aerial vehicle structure and relates to the technical field of unmanned aerial vehicles. The structure includes a vehicle body and a plurality of wings that are connected thereto. The vehicle body includes, successively from top to bottom, a vehicle body upper section, a vehicle body middle section, and a vehicle body lower section, wherein the vehicle body upper section includes a parachute cavity and a vehicle body upper shell; the vehicle body middle section includes a vehicle body middle shell, a vehicle arm fixing base and a vehicle arm connecting member A; a vehicle body upper plate, a vehicle body lower plate, a power supply section board, a battery, a parachute cavity fixing board, and a flight control device are arranged in an inner chamber of the vehicle body middle shell; the vehicle body lower section includes a vehicle body lower shell; the vehicle body upper shell, the vehicle body middle shell and the vehicle body lower shell are successively and detachably connected in order. The structure can be used for manufacturing multi-rotor wing unmanned aerial vehicles in different take-off weights, reduces manufacturing period, reduces mission execution cost and improves mission efficiency.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a fast combined multi-rotor unmanned aerial vehicle structure. Background technique [0002] UAVs have the characteristics of flexibility, light weight, small size, easy assembly and disassembly, the ability to mount different mission equipment according to needs, and short manufacturing cycle. They are widely used in military and civilian markets. [0003] However, with the rapid development of unmanned flight technology, the requirements for drones are getting higher and higher. The disassembly and assembly of existing drones are all by means of tools, which have the problems of slow disassembly and assembly and long disassembly and assembly time. Contents of the invention [0004] The purpose of the present invention is to provide a fast combined multi-rotor UAV structure, thereby solving the aforementioned problems in the prior art. [0005] In order to a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/00B64C27/08B64C27/32
CPCB64C1/00B64C27/08B64C27/32
Inventor 韩应付易世娇徐继勇孙长龙李明
Owner BEIJING DIGSUR SCI & TECH
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