Multi-rotary-wing single-motor driving structure and unmanned aerial vehicle

A single-motor-driven, multi-rotor technology, applied in the field of unmanned aerial vehicles, can solve the problems of difficult control of the synchronization of multiple rotors, accelerated power consumption of motors, and low work efficiency of the whole machine, and achieves less power loss, less parts loss, Small vibration effect

Inactive Publication Date: 2016-04-06
张家港锐泰智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] 2. Multiple motors work together, and the high-frequency vibration generated by them can easily affect the clarity of aerial photography;
[0007] 3. The synchronization of multiple rotors is difficult to control;
[0008] 4. Existing multi-axis aircraft use multiple motors to directly drive their respective propellers. In order to maintain balance during the flight of the aircraft, the flight control system needs to frequently change the motor speed
This frequent change of speed causes the motor to consume power faster
And each motor has working efficiency, the more motors there are, the lower the working efficiency of the whole machine will be

Method used

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  • Multi-rotary-wing single-motor driving structure and unmanned aerial vehicle

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Embodiment Construction

[0027] The technical solutions in the embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of the present invention.

[0028] ginseng figure 1 As shown, the multi-rotor single-motor drive structure includes a motor 1, two first rotors, two second rotors, and a first drive shaft 4 and a second drive shaft 5 arranged side by side. The first rotor and the second rotor Alternately arranged, the first drive shaft 4 is connected to the second drive shaft 5, the motor 1 is connected to the second drive shaft 5, the first drive shaft 4 is respectively connected to the two first rotors, and the s...

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Abstract

The invention discloses a multi-rotary-wing single-motor driving structure and an unmanned aerial vehicle. The driving structure comprises a motor, two first rotary wings, two second rotary wings, a first driving shaft and a second driving shaft, wherein the first driving shaft and the second driving shaft are arranged in parallel. The first rotary wings and the second rotary wings are arranged in a staggered mode. The first driving shaft is in transmission connection with the second driving shaft. The motor is in transmission connection with the second driving shaft. The first driving shaft is in transmission connection with the two first rotary wings. The second driving shaft is in transmission connection with the two second rotary wings. The two first rotary wings rotate synchronously in the first direction, meanwhile, the two second rotary wings rotate synchronously in the second direction, and the first direction and the second direction are opposite. According to the multi-rotary-wing single-motor driving structure, driving is conducted by one motor, the transmission series are small, and the transmission efficiency is high.

Description

technical field [0001] The present application relates to an unmanned aerial vehicle, in particular to a multi-rotor single-motor drive structure for an unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicles have the characteristics of small size, light weight, low cost, flexible operation and high safety, and can be widely used in aerial photography, monitoring, search and rescue, resource exploration and other fields. [0003] In the prior art, an unmanned aerial vehicle generally includes a plurality of rotors, each of which is driven by a motor, [0004] Its disadvantages are: [0005] 1. Due to the installation of multiple motors, the overall weight of the unmanned aerial vehicle is relatively heavy; [0006] 2. Multiple motors work together, and the high-frequency vibration generated by them can easily affect the clarity of aerial photography; [0007] 3. The synchronization of multiple rotors is difficult to control; [0008] 4. The existi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/12B64C27/08B64D27/24
CPCB64C27/12B64C27/08B64C2027/125B64D27/24
Inventor 杨华东赵江许剑
Owner 张家港锐泰智能科技有限公司
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