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Mute propeller blade and rotor unmanned aerial vehicle with same

A blade, silent technology, applied in the field of drones, can solve the problems of high noise and slow flight speed, and achieve the effect of reducing noise, low cost and improving efficiency

Active Publication Date: 2016-11-16
湖北大秀智控科技发展有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide a silent blade and a rotor UAV containing it, so as to solve the technical problems of high noise and slow flight speed in the prior art

Method used

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  • Mute propeller blade and rotor unmanned aerial vehicle with same
  • Mute propeller blade and rotor unmanned aerial vehicle with same
  • Mute propeller blade and rotor unmanned aerial vehicle with same

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Embodiment Construction

[0040] The principles and features of the present invention are described below in conjunction with the accompanying drawings, and the examples given are only used to explain the present invention, and are not intended to limit the scope of the present invention.

[0041] The present invention provides a silent paddle, including a paddle body 5; in order to reduce the noise generated by the cutting airflow during the rotation of the paddle, as figure 1 As shown, in the present embodiment, the blade body 5 adopts bionics-bird wings, and a plurality of unequal sawtooth grooves 6 are arranged on the trailing edge of the blade body 5, and a plurality of unequal sawtooth grooves 6 are connected with the paddle A plurality of unequal-spaced sawtooth 7 is formed between the leaf body 5, thereby achieving the function of reducing noise, while cutting with a plurality of unequal-spaced sawtooth 7, on the one hand, the large eddy current generated during the rotation is cut and combed in...

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Abstract

The invention relates to a mute propeller blade. The mute propeller blade comprises a propeller blade body, wherein a plurality of unequal sawtooth grooves are formed in the tail edge of the propeller blade body; a plurality of unequidistant saw teeth are formed between the unequal sawtooth grooves and the propeller blade body; a micro array diaphragm structure is bonded to a force suction surface of the propeller blade body; the micro array diaphragm structure consists of a plurality of protrusions with different lengths; the protrusions with the different lengths are distributed in a sinusoidal waveform manner in the width direction of the propeller blade body; and each of the protrusions adopts a sawtooth-like structure, and a closed angle part of the sawtooth-like structure faces to the tail edge of the propeller blade body, and each of the protrusions of the sawtooth-like structure comprises a first sidewall and a second sidewall, wherein a certain inclined angle is at the jointed position of the first sidewall and the corresponding second sidewall. The invention also discloses a rotor unmanned aerial vehicle, and the rotor unmanned aerial vehicle comprises the mute propeller blade. The mute propeller blade disclosed by the invention has the beneficial effects that the noise reduction effect is good, the application range is extended, the efficiency of the unmanned aerial vehicle is improved, and the flying speed of the unmanned aerial vehicle is increased.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a silent blade and a rotor unmanned aerial vehicle containing the same. Background technique [0002] In today's society, as the technology of UAVs is getting more and more advanced, it can be seen in more and more occasions, such as military reconnaissance, assisting anti-terrorism, etc. UAVs have played a great role, reducing unnecessary losses and improving success rate. But in some cases, its noise problem has brought hidden dangers to its safety, such as the incident where a drone was discovered and shot down in military reconnaissance. The reason why drones are discovered is largely due to their relatively large noise, low-altitude flight, small size, and difficult to be detected by radar, but noise restricts their safety. In response to such problems, countries all over the world are now setting off an upsurge of research on low-noise drones. [0003] The noise o...

Claims

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Application Information

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IPC IPC(8): B64C27/473
CPCB64C27/473B64U50/19B64U10/10
Inventor 王杰刘银张珩
Owner 湖北大秀智控科技发展有限公司
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