阅读说明：本技术 一种基于旋涡阵列的降噪方法 (Noise reduction method based on vortex array ) 是由 马瑞轩 张树海 罗勇 王益民 武从海 李虎 刘旭亮 韩帅斌 王勋年 于 2021-11-16 设计创作，主要内容包括：本发明适用于飞行器噪声抑制技术领域,提供了一种基于旋涡阵列的降噪方法,本发明采用气流产生的旋涡阵列来消除噪声,取代了现有技术中采用实体降噪装置降噪的方式,从而无需事先了解噪声特性,并且可以根据实时采集到的噪声信号适应性地调整产生的旋涡阵列的参数,操作更加方便,使用范围更广。由于产生旋涡阵列的材料直接来源于空气等流体介质,环保无污染。(The invention is suitable for the technical field of noise suppression of aircrafts, and provides a noise reduction method based on a vortex array. The material for generating the vortex array is directly derived from fluid media such as air, so that the method is environment-friendly and pollution-free.)

1. A noise reduction method based on vortex arrays is characterized in that the noise reduction is carried out by adopting the vortex arrays, and the vortex arrays are generated by airflow.

2. A method of noise reduction based on vortex arrays according to claim 1, wherein the vortex arrays comprise at least one of the following arrays: the noise reduction array comprises a high-frequency noise reduction array, a medium-frequency noise reduction array and a low-frequency noise reduction array.

3. A method for noise reduction based on vortex arrays according to claim 2, wherein when there are two or more sets of vortex arrays, the arrays are staggered.

4. A vortex array based noise reduction method according to claim 3,

the high-frequency noise reduction array comprises three vortices A1, A2 and A3, and is arranged in an equilateral triangle, A1 rotates anticlockwise, A3 rotates clockwise, and A2 rotates clockwise;

the medium-frequency noise reduction array comprises three vortices B1, B2 and B3, the vortices are arranged in an equilateral triangle, B1 rotates anticlockwise, B3 rotates clockwise, and B2 rotates clockwise;

the low-frequency noise reduction array comprises three vortices C1, C2 and C3, and is arranged in an equilateral triangle, C1 rotates anticlockwise, C3 rotates clockwise, and C2 rotates clockwise;

the coordinates of each vortex are respectively，，，，，，，，(ii) a WhereinR1 is the vortex core radius of each vortex in the high-frequency noise reduction array;R2 is the vortex core radius of each vortex in the medium frequency noise reduction array;Rand 3 is the vortex core radius of each vortex in the low-frequency noise reduction array.

5. A noise reduction method based on a vortex array is characterized by comprising the following steps:

s10, acquiring noise parameters and analyzing noise attributes;

the noise attribute comprises that the noise is one or more of low-frequency noise, intermediate-frequency noise and high-frequency noise;

s20, selecting a corresponding vortex array according to the noise attribute and/or the noise reduction target;

according to the noise attribute, if the noise contains low-frequency noise, the vortex array selected contains a low-frequency noise reduction array; if the noise contains intermediate frequency noise, the vortex array selected contains an intermediate frequency noise reduction array; if the noise contains high-frequency noise, the vortex array selected contains a high-frequency noise reduction array;

the noise reduction target comprises at least one of low-frequency noise reduction, medium-frequency noise reduction and high-frequency noise reduction;

the vortex array is generated by an air flow;

s30, starting the vortex generator to generate a corresponding vortex array.

6. The vortex array based noise reduction method according to claim 5, wherein the step S10 further includes obtaining the frequency of the noise, obtaining the center frequency of the dominant frequency band of each of the low frequency noise, the intermediate frequency noise and the high frequency noise, and recording the center frequency as the frequency band of the dominant frequency band in sequencef _l 、f _m Andf _h corresponding wavelengths are respectivelyλ _l 、λ _m Andλ _h the spectral density of acoustic energy at the corresponding frequency band isE _l 、E _m AndE _h 。

7. a vortex array based noise reduction method according to claim 6, wherein the distribution of each vortex in the vortex array is as follows:

，

wherein the content of the first and second substances,u，ρ，prespectively being swirlingSpeed, density and intensity;rthe distance from any point in space to the center of the vortex;Ris the radius of the vortex core of the vortex,M _v in order to be the strength of the vortex,γis the index of the adiabatic heat of the gas,αconstant, V and P are polynomial distribution functions.

8. The vortex array based noise reduction method of claim 7, wherein the low frequency noise reduction array comprises three vortices，，A1, A3 rotates counterclockwise, a2 rotates clockwise, and:

， ；

wherein the content of the first and second substances,R ₁for the radius of the vortex core of the vortex in the high frequency noise reduction array,M _v1 and (3) the strength of the vortex in the high-frequency noise reduction array is shown, wherein pi is the circumferential rate.

9. The vortex array based noise reduction method of claim 7, wherein the IF noise reduction array comprises three vortices，，B1, B3 rotates counterclockwise, B2 rotates clockwise, and:

， ；

wherein the content of the first and second substances,R ₂for the radius of the vortex core of the vortices in the low frequency noise reduction array,M _v2 and the strength of the vortex in the medium-frequency noise reduction array is shown, and pi is the circumferential rate.

10. The vortex array based noise reduction method of claim 7, wherein the high frequency noise reduction array comprises three vortices，，C1, C3 rotates counterclockwise, C2 rotates clockwise, and:

， ；

wherein the content of the first and second substances,R ₃for the radius of the vortex core of the vortices in the low frequency noise reduction array,M _v3 swirl enhancement of vortices in arrays for noise reduction for low frequency noiseDegree, pi is the circumferential ratio.

Technical Field

The invention relates to the technical field of noise suppression of aircrafts, in particular to a noise reduction method based on a vortex array.

Background

The unsteady, non-uniform motion of the fluid medium can produce aerodynamic noise. Aerodynamic noise is ubiquitous in many areas of aviation, navigation, and ground transportation. As an important mark of the national aviation level and comprehensive national strength, large civil aircrafts such as ARJ21, C919, CR929 and the like in China are in the mass production or research and development stage at present, and in order to successfully obtain airworthiness licenses and enter the international and domestic markets, the noise level of the aircrafts must meet the relevant airworthiness requirements. The pneumatic noise of the military aircraft not only causes structural fatigue and influences the penetration capability of the military aircraft, but also brings great negative effects to the mental states of drivers and passengers, and greatly reduces the comprehensive fighting performance including sound stealth. Therefore, the pneumatic noise suppression device has important significance for national economy and national defense construction.

There are two major noise reduction approaches to aerodynamic noise. Firstly, the intensity of the noise source is restrained, the sound production efficiency of the noise source is directly reduced by optimizing the pneumatic appearance, or the flow characteristic of a local flow field near the sound source is changed by injecting micro jet or adopting a sawtooth and other bionic structures, so that the aim of reducing the pneumatic noise is fulfilled. The method has strong noise reduction pertinence and can reduce the pneumatic noise in a global large range. However, it is difficult to systematically know the position of the noise source and the flow characteristics near the noise source in advance in the actual engineering, so that for the problem of pneumatic noise reduction in the complex engineering problem, a second approach is mostly adopted, i.e., the propagation path of noise is controlled, the optimal noise reduction in a local area is realized, and in the implementation process, sound energy is mainly absorbed through a sound absorption structure and materials such as a porous medium and an impedance gradual change material to reduce the noise. However, most of the attached sound absorption materials and structures are flammable and harmful substances, which can cause hidden dangers to the health and safety of airborne personnel and can influence the overall aerodynamic characteristics of the aircraft.

Disclosure of Invention

In order to solve the technical problems in the prior art, the invention provides a noise reduction method based on a vortex array, which directly adopts a vortex generator to generate vortex array airflow meeting requirements so as to reduce the noise of jet flow of an engine.

A noise reduction method based on vortex arrays is characterized in that the noise reduction is carried out by adopting the vortex arrays, and the vortex arrays are generated by airflow.

Further, the vortex array includes at least one of the following arrays: the noise reduction array comprises a high-frequency noise reduction array, a medium-frequency noise reduction array and a low-frequency noise reduction array.

Further, when two or more sets of vortex arrays exist, the arrays are arranged in a staggered mode.

Further, the high-frequency noise reduction array comprises three vortices A1, A2 and A3, and is arranged in an equilateral triangle, A1, A3 rotates anticlockwise, and A2 rotates clockwise;

the medium-frequency noise reduction array comprises three vortices B1, B2 and B3, the vortices are arranged in an equilateral triangle, B1 rotates anticlockwise, B3 rotates clockwise, and B2 rotates clockwise;

the low-frequency noise reduction array comprises three vortices C1, C2 and C3, and is arranged in an equilateral triangle, C1 rotates anticlockwise, C3 rotates clockwise, and C2 rotates clockwise;

the coordinates of each vortex are respectively，，，，，，，，(ii) a WhereinR1 is the vortex core radius of each vortex in the high-frequency noise reduction array;R2 is the vortex core radius of each vortex in the medium frequency noise reduction array;Rand 3 is the vortex core radius of each vortex in the low-frequency noise reduction array.

A noise reduction method based on vortex arrays comprises the following steps:

s10, acquiring noise parameters and analyzing noise attributes;

the noise attribute comprises that the noise is one or more of low-frequency noise, intermediate-frequency noise and high-frequency noise;

s20, selecting a corresponding vortex array according to the noise attribute and/or the noise reduction target;

according to the noise attribute, if the noise contains low-frequency noise, the selected noise reduction array contains a low-frequency noise reduction array; if the noise contains intermediate frequency noise, the selected noise reduction array contains an intermediate frequency noise reduction array; if the noise contains high-frequency noise, the selected noise reduction array contains a high-frequency noise reduction array;

the noise reduction target comprises at least one of low-frequency noise reduction, medium-frequency noise reduction and high-frequency noise reduction;

the vortex array is generated by an air flow;

s30, starting the vortex generator to generate a corresponding vortex array.

Further, in step S10, the method further includes obtaining a frequency of the noise, obtaining center frequencies of frequency bands that are dominant in each of the low frequency noise, the intermediate frequency noise, and the high frequency noise, and recording the center frequencies as the center frequencies in sequencef _l 、f _m Andf _h corresponding wavelengths are respectivelyλ _l 、λ _m Andλ _h the spectral density of acoustic energy at the corresponding frequency band isE _l 、E _m AndE _h 。

further, in the vortex array, the distribution of each vortex is as follows:

，

wherein the content of the first and second substances,u，ρ，pvelocity, density and intensity of the vortex, respectively;rthe distance from any point in space to the center of the vortex;Ris the radius of the vortex core of the vortex,M _v in order to be the strength of the vortex,γis the index of the adiabatic heat of the gas,αconstant, V and P are polynomial distribution functions.

Further, the low frequency noise reduction array includes three vortices，，A1, A3 rotates counterclockwise, a2 rotates clockwise, and:

， ；

wherein the content of the first and second substances,R ₁for the radius of the vortex core of the vortex in the high frequency noise reduction array,M _v1 and (3) the strength of the vortex in the high-frequency noise reduction array is shown, wherein pi is the circumferential rate.

Further, the medium frequency noise reduction array comprises three vortices，，B1, B3 rotates counterclockwise, B2 rotates clockwise, and:

， ；

wherein the content of the first and second substances,R ₂for the radius of the vortex core of the vortices in the low frequency noise reduction array,M _v2 and the strength of the vortex in the medium-frequency noise reduction array is shown, and pi is the circumferential rate.

Further, the high frequency noise reduction array includes three vortices，，C1, C3 rotates counterclockwise, C2 rotates clockwise, and:

， ；

wherein the content of the first and second substances,R ₃for the radius of the vortex core of the vortices in the low frequency noise reduction array,M _v3 and the intensity of the vortex in the low-frequency noise reduction array is shown, wherein pi is the circumferential rate.

Compared with the prior art, the noise reduction method based on the vortex array at least has the following beneficial effects:

1. the invention carries out noise reduction based on the vortex array of the airflow, does not need a solid noise reduction device, and does not need to know the characteristics of a noise source in advance;

2. the parameters of the vortex array based on the airflow can be adaptively adjusted according to the collected noise signals, so that the vortex array based on the airflow is more convenient to use, has a wider application range and has a better noise reduction effect;

3. the vortex array based on airflow is environment-friendly and pollution-free due to the fact that the vortex array is derived from fluid media such as air;

4. the invention provides a method for reducing noise by adopting an airflow to generate a vortex array, provides a directional guide for the field of noise reduction and noise reduction, and lays a foundation for the research of the field;

5. the invention also provides an optimized array arrangement form for noise reduction by adopting the equilateral triangle array, and the noise reduction effect of the arrangement structure is optimal.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the embodiments of the present invention or in the description of the prior art will be briefly described below, and it is obvious that the drawings described below are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.

FIG. 1 is a schematic diagram of a vortex array arrangement according to an embodiment of the present invention.

Detailed Description

The following description provides many different embodiments, or examples, for implementing different features of the invention. The particular examples set forth below are illustrative only and are not intended to be limiting.

Example 1

A noise reduction method based on a vortex array is used for noise reduction, and the vortex array is generated by airflow. The noise reduction method of the invention generates the vortex array through the airflow when the noise reduction is needed, so that the noise reduction effect of the noise reduction device in the prior art is achieved, and compared with the existing noise reduction material, the vortex array is directly generated by air, so that the noise reduction method is environment-friendly, pollution-free, high-temperature resistant and more suitable for noise reduction of an aircraft under extreme flight conditions; most importantly, various parameters of the vortex array formed by the airflow can be adjusted according to the actual noise condition, the noise characteristic does not need to be known in advance like the prior art, and the application range is wider.

The vortex array of the present invention can be generated by a vortex generator, and the airflow for generating the vortex is directly derived from air or other fluid medium, but is not limited thereto, and those skilled in the art will appreciate that other devices capable of generating the vortex array are also suitable for the present invention.

Depending on the nature of the noise, the vortex array of the present invention includes at least one of the following arrays: the noise reduction array comprises a high-frequency noise reduction array, a medium-frequency noise reduction array and a low-frequency noise reduction array. It will be understood by those skilled in the art that the array described in this embodiment refers to an array having two or more vortices arranged according to a certain rule. For example, 2 vortices form an array, or 3 vortices form an array, or 4 vortices form an array, or more vortices form an array, and the high-frequency noise reduction array, the medium-frequency noise reduction array and the low-frequency noise reduction array are arranged in a staggered manner, which can all have a certain noise reduction effect.

Preferably, an array formed by 3 vortices has a good noise reduction effect, as shown in fig. 1:

the high-frequency noise reduction array comprises three vortices A1, A2 and A3, and is arranged in an equilateral triangle, A1 rotates anticlockwise, A3 rotates clockwise, and A2 rotates clockwise;

the medium-frequency noise reduction array comprises three vortices B1, B2 and B3, the vortices are arranged in an equilateral triangle, B1 rotates anticlockwise, B3 rotates clockwise, and B2 rotates clockwise;

the low-frequency noise reduction array comprises three vortices C1, C2 and C3, and is arranged in an equilateral triangle, C1 rotates anticlockwise, C3 rotates clockwise, and C2 rotates clockwise;

the coordinates of each vortex are respectively，，，，，，，，(ii) a WhereinR1 is the vortex core radius of each vortex in the high-frequency noise reduction array;R2 is the vortex core radius of each vortex in the medium frequency noise reduction array;Rand 3 is the vortex core radius of each vortex in the low-frequency noise reduction array.

Example 2

A noise reduction method based on vortex arrays comprises the following steps:

s10, obtaining noise parameters and analyzing noise attributes

Specifically, in this embodiment, a time domain signal of noise is obtained, and a spectral characteristic of the noise is analyzed. And a microphone is placed on a propagation path of the noise to collect a noise signal, wherein the collection time is 60s, and the sampling frequency is 102.4 kHz. The collected noise signal is subjected to frequency characteristic analysis, in this embodiment, the analysis is performedA segmented average windowed fast Fourier transform method is adopted, the length of each data block is 8192, time domain data is divided into 750 segments, and a window function is a Hanning (Hanning) window. The signal in the time domain is converted into a signal in the frequency domain. The signal is further analyzed by one third octave to obtain a low frequency band (f<200 Hz), middle frequency range (less than or equal to 200 Hz)fLess than or equal to 2000 Hz) and a high frequency range (f>2000 Hz) of the frequency band that prevails, in turn notedf _l 、f _m Andf _h corresponding wavelengths are respectivelyλ _l 、λ _m Andλ _h the spectral density of acoustic energy at the corresponding frequency band isE _l 、E _m AndE _h (ii) a The noise can also be one or more of low-frequency noise, intermediate-frequency noise and high-frequency noise; the analysis noise is broadband noise or single-frequency noise, wherein the broadband noise is noise containing any two or three of low, medium and high frequencies, and the single-frequency noise only contains any one of the low, medium and high frequencies.

S20, selecting a corresponding vortex array according to the noise attribute and/or the noise reduction target;

according to the noise attribute, if the noise contains low-frequency noise, the selected noise reduction array contains a low-frequency noise reduction array; if the noise contains intermediate frequency noise, the selected noise reduction array contains an intermediate frequency noise reduction array; if the noise contains high-frequency noise, the selected noise reduction array contains a high-frequency noise reduction array;

for example, if the noise is broadband noise and there are low, medium and high frequency noise, it is necessary to select a high frequency noise reduction array, a medium frequency noise reduction array and a low frequency noise reduction array at the same time; if the noise is any two kinds of noise, selecting a corresponding noise reduction array; similarly, if the noise is a single-frequency noise, i.e. only one of low, medium and high-frequency noise is included, only one kind of noise reduction array corresponding to the noise reduction array needs to be selected. The skilled person knows that, in general, low, medium and high frequency noises in broadband noise are all present, and the latter two cases belong to extreme cases and rarely occur; more generally, how to select the denoising array is determined according to the denoising target.

The noise reduction target comprises at least one of low frequency noise reduction, medium frequency noise reduction or high frequency noise reduction; that is, when only one of low, medium and high frequency noise needs to be reduced, only one corresponding noise reduction array is needed; when two kinds of noises need to be reduced, two corresponding noise reduction arrays are set; when low, medium and high frequency noise needs to be removed simultaneously, three noise reduction arrays are arranged.

The vortex array may also be optionally set in conjunction with noise and noise reduction targets:

when the noise is broadband noise, namely low, medium and high frequency noise, and the noise reduction target is to reduce the low frequency noise, a low frequency noise reduction array is selected to be arranged; if the noise reduction target is to reduce the intermediate frequency noise, selecting to set an intermediate frequency noise reduction array; if the noise reduction target is to reduce high-frequency noise, selecting to set a high-frequency noise reduction array; similarly, if the noise reduction target is to reduce one or two of the noise reduction targets, the corresponding one or two of the noise reduction arrays may be correspondingly set.

When the noise is single-frequency noise and the noise reduction target is to reduce all the low, medium and high-frequency noise, only a noise reduction array with the frequency corresponding to the noise needs to be set; if the noise reduction target is to reduce one of low, medium and high frequencies and is the same as the dominant frequency of the noise, the noise reduction array of the corresponding frequency is set, and if the noise reduction target is different from the dominant frequency of the noise, the vortex array is not required to be generated for noise reduction.

Wherein the distribution of each vortex is:

，

wherein the content of the first and second substances,u，ρ，pvelocity, density and intensity of the vortex, respectively;rthe distance from any point in space to the center of the vortex;Ris the radius of the vortex core of the vortex,M _v in order to be the strength of the vortex,γis gas adiabatic index, in airThe concentration of the organic solvent is generally 1.4,αconstant, V and P are polynomial distribution functions.

The high frequency noise reduction array comprises three vortices，，A1, A3 counterclockwise rotation, a2 clockwise rotation; a1, a2, A3 are distributed in an equilateral triangle, a1, a2, A3 are located at the vertices of the equilateral triangle, and:

， ；

in the present embodiment, the first and second electrodes are,

in the present embodiment, the first and second electrodes are,a ₁constants in formula for vorticity distribution of high frequency noise reduction arrayaTaking the value of (A); V ₁andP ₁is a polynomial distribution function formula in a vortex distribution formula of the high-frequency noise reduction array, ；R ₁for the radius of the vortex core of the vortex in the high frequency noise reduction array,M _v1 the strength of vortices in the array is denoised for high frequency noise.

The medium-frequency noise reduction array comprises three vortexes，，B1, B3 counterclockwise rotation, B2 clockwise rotation, B1, B2, B3 are distributed in an equilateral triangle, B1, B2, B3 are located at the vertices of the equilateral triangle, and:

， ；

in the present embodiment, the first and second electrodes are,

in the present embodiment, the first and second electrodes are,a ₂constants in formula for vortex distribution of medium frequency noise reduction arrayaTaking the value of (A);V ₂andP ₂is a polynomial distribution function formula in a vortex distribution formula of the medium-frequency noise reduction array,；R ₂the radius of the vortex core of the vortex in the medium-frequency noise reduction array,M _v2 and the strength of the vortex in the medium-frequency noise reduction array is obtained.

The low frequency noise reduction array includes three vortices，，C1, C3 counterclockwise rotation, C2 clockwise rotation, C1, C2, C3 are distributed in an equilateral triangle, C1, C2, C3 are located at the vertices of the equilateral triangle, and:

， ；

in the present embodiment, the first and second electrodes are,

in the present embodiment, the first and second electrodes are,a ₃constants in formula for vorticity distribution of low frequency noise reduction arrayaTaking the value of (A); v₃AndP ₃is a polynomial distribution function in the vortex distribution formula of the low-frequency noise reduction array,；R ₃for the radius of the vortex core of the vortices in the low frequency noise reduction array,M _v3 the strength of vortices in the low frequency noise reduction array.

It should be noted that the present embodiment relates toaThe value of (a) is selected,PandVthe selected specific polynomial expression is only an example, and is not the only implementation way, and the values can be derived by a person skilled in the art according to the compressible unsteady vortex motion theory to obtain different values and expression forms, which cannot be exhausted in the invention.

S30, starting the vortex generator to generate a corresponding vortex array.

Vortex arrays are produced by adopting vortex generators according to corresponding requirements, and are arranged on a sound propagation path, preferably, the sound propagation direction and the sound propagation directionxThe positive directions of the axes are consistent, and the noise can be effectively reduced.

Fig. 1 is a diagram of a vortex array arrangement according to an embodiment of the present invention, where the diagram includes high-frequency noise reduction arrays a1, a2, A3, intermediate-frequency noise reduction arrays B1, B2, B3, and low-frequency noise reduction arrays C1, C2, and C3, and the vortex array can achieve a noise reduction effect of 7.5 dB; of course, according to the noise attribute and the noise reduction target, the single-frequency noise is reduced, and the noise reduction effect of 10dB can be obtained.

The airflow vortex array is adopted for noise reduction, so that a good noise reduction effect can be obtained, a solid noise reduction device adopted in the prior art can be replaced for noise reduction, and the airflow vortex array has a very high practical value.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.