Multi-rotor unmanned aerial vehicle based on universal rotor set

A technology of a multi-rotor unmanned aerial vehicle and a rotor group, which is applied in the field of unmanned aerial vehicles

Inactive Publication Date: 2017-08-29
NANJING UNIV OF INFORMATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

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And each rotor can only

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  • Multi-rotor unmanned aerial vehicle based on universal rotor set
  • Multi-rotor unmanned aerial vehicle based on universal rotor set
  • Multi-rotor unmanned aerial vehicle based on universal rotor set

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Embodiment Construction

[0023] The present invention will be further explained below in conjunction with the accompanying drawings and specific embodiments. It should be understood that the following specific embodiments are only used to illustrate the present invention but not to limit the scope of the present invention.

[0024] figure 1 It is a structural schematic diagram of the present invention, as can be seen in conjunction with the accompanying drawings, this multi-rotor UAV based on the universal rotor group includes a frame, a flight control system 1, GPS 2, a controller and a universal rotor group 7, the frame It includes a center plate and several balanced rotor groups 4 extending uniformly from the periphery of the center plate. Several legs 6 are uniformly arranged on the lower circumference of the center plate, and the universal rotor group 7 is arranged on the vertical side of the center plate. Below, the flight control system 1 and GPS 2 are arranged above the center board, and the ...

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Abstract

The invention discloses a multi-rotor unmanned aerial vehicle based on a universal rotor set. The multi-rotor unmanned aerial vehicle based on the universal rotor set comprises a rack, a flight control system, a GPS (Global Positioning System), a controller and the universal rotor set, wherein the rack comprises a center plate and a plurality of balance rotor sets uniformly extending from the periphery of the center plate; a plurality of lead frames are uniformly arranged on the periphery below the lower part of the center plate; the universal rotor set is arranged vertically below the center plate; the flight control system and the GPS are arranged above the center plate; and the flight control system is used for controlling the universal rotor set to be adjusted in different directions and speeds. The multi-rotor unmanned aerial vehicle based on the universal rotor set has the beneficial effects that the practicability is high, the flight speed and direction of the unmanned aerial vehicle are controlled through the universal rotor set; the balance of the unmanned aerial vehicle is kept through the multiple groups of balance rotors; the power consumption rate is reduced; the cruising power and flexibility are promoted; the practicability and convenience of the unmanned aerial vehicle are improved; and the multi-rotor unmanned aerial vehicle based on the universal rotor set has practical significance and can be produced in quantity to achieve the purpose of popularization.

Description

technical field [0001] The invention relates to a multi-rotor unmanned aerial vehicle based on a universal rotor group, and belongs to the technical field of unmanned aerial vehicles. Background technique [0002] At present, multi-rotor unmanned aerial vehicles have been widely used in fields such as field construction, exploration, transportation, tourism, rescue, especially work on rivers and lakes. send etc. It has a unique advantage that it can be lifted vertically; it is not restricted by terrain and roads, and can quickly reach the scene where work and rescue are needed, even in places that are inaccessible, for close observation; The department sends video and image data for the technical personnel of the relevant department to analyze and judge the scene, or quickly transport materials to the scene, and achieved good results. [0003] However, the current multi-rotor UAVs basically have an even number of rotors. The quad-rotors, hex-rotors, and octa-rotors all rel...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/82
CPCB64C27/08B64C27/82B64C2027/8236B64U10/10
Inventor 张彪陈冲张磊涛曹政陈明健
Owner NANJING UNIV OF INFORMATION SCI & TECH
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