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A silent propeller and its rotor drone

A paddle and silent technology, applied in the field of drones, can solve the problems of slow flight speed and loud noise, and achieve the effects of low cost, noise reduction and efficiency improvement

Active Publication Date: 2018-08-21
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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  • A silent propeller and its rotor drone
  • A silent propeller and its rotor drone
  • A silent propeller and its rotor drone

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Embodiment Construction

[0036] 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.

[0037] 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 to 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 int...

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PUM

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Abstract

The invention relates to a silent blade, which includes a blade body; a plurality of unequal sawtooth grooves are formed on the trailing edge of the blade body, and a plurality of unequal distances are formed between the plurality of unequal sawtooth grooves and the blade body. Sawtooth; the suction surface of the blade body is bonded with a microarray diaphragm structure; the microarray diaphragm structure is composed of several protrusions of different lengths; several protrusions of different lengths are arranged in a sinusoidal waveform in the width direction of the blade body. cloth; the protrusions are in a zigzag-like structure, and the sharp corners of the zigzag-like structure are all facing the trailing edge of the blade body; the protrusions in the zig-zag structure include a first side wall and a second side wall; the first side wall and the The second side wall forms a certain angle at the intersection. A rotor drone is also disclosed, and the rotor drone includes the above-mentioned silent blades. The beneficial effects of the invention are: good noise reduction effect, expanded use range, improved efficiency and flying speed of the drone.

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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Patent Type & Authority Patents(China)
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