CN114543980B - Acoustic wave phase modulation and acoustic field reconstruction method based on near-field orbital angular momentum conversion - Google Patents
Acoustic wave phase modulation and acoustic field reconstruction method based on near-field orbital angular momentum conversion Download PDFInfo
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Abstract
Description
技术领域technical field
本发明涉及声波传输相位调制和自由空间声场重构,属于声学信号处理和声场调控领域。The invention relates to sound wave transmission phase modulation and free space sound field reconstruction, and belongs to the field of acoustic signal processing and sound field control.
背景技术Background technique
声场重构与复杂三维声场调控在粒子操控、超声成像、医疗诊断和虚拟现实等领域中具有广泛的应用。目前,在实验室以及商业上获得复杂三维空间声场的成熟技术手段主要有两种:一种是利用集成扬声器阵列,通过电子线路设计和计算机编程实现不同像素点位置处扬声器驱动电压的幅值和相位的逐点调控,进而调节扬声器所辐射的声场的振幅和相位,重构出目标声场,属于主动式声场调控技术;另一种是基于计算机制全息图,采用合适的物理模型和算法,求解得到目标声场所对应的声学全息干板的透反射系数空间分布函数,随后通过设计合适的像素结构并结合成熟的三维快速成型技术制备得到符合要求的声学全息干板,最终在平面声波照射下重构出目标声场,属于被动式声场调控技术。但是,基于大面积集成扬声器阵列的主动式声场调控技术,所需要控制的信号通道众多,系统组成复杂,成本高昂,并且所获得的声场声压大小有限,限制其在虚拟显示和粒子操控领域的应用;另一方面,基于声学全息干板的被动式声场重构技术,受结构组成材料和加工尺寸限制,可以利用的工作波段较为有限。Acoustic field reconstruction and complex three-dimensional acoustic field regulation have a wide range of applications in the fields of particle manipulation, ultrasound imaging, medical diagnosis and virtual reality. At present, there are mainly two mature technical means to obtain complex three-dimensional sound fields in the laboratory and commercially: one is to use the integrated speaker array, and realize the amplitude and the driving voltage of the speaker at different pixel positions through electronic circuit design and computer programming. The point-by-point control of the phase, and then adjust the amplitude and phase of the sound field radiated by the speaker, and reconstruct the target sound field, which belongs to the active sound field control technology; the other is based on computer-made holograms, using appropriate physical models and algorithms to solve The spatial distribution function of the transmission and reflection coefficient of the acoustic holographic dry plate corresponding to the target acoustic field is obtained, and then the acoustic holographic dry plate that meets the requirements is prepared by designing a suitable pixel structure and combining mature 3D rapid prototyping technology, and finally reproduced under the irradiation of plane acoustic waves. Constructing the target sound field is a passive sound field control technology. However, the active sound field control technology based on a large-area integrated speaker array requires many signal channels to be controlled, the system composition is complex, the cost is high, and the sound pressure of the sound field obtained is limited, which limits its application in the fields of virtual display and particle manipulation. On the other hand, the passive sound field reconstruction technology based on the acoustic holographic dry plate is limited by the structural material and processing size, and the available working band is relatively limited.
近些年来,以超构材料和超构表面为代表,基于声学人造结构的声场重构和声场调控方案得到了学术界和工业界的广泛关注。声学人造结构具有极高的设计灵活度和可控性,作为超构材料和超构表面的一个重要研究分支,基于声学超构表面的声场调控的核心任务是设计具有特定空间透射振幅和相位调制分布的声学全息干板。目前,声学全息干板组成像素单元的设计实施方案主要有两个:一个是采用结构共振特性设计的共振型人造结构,例如经典的亥姆霍兹共振腔结构(Helmholtz resonator);另一个是基于等效介质理论的声波传播相位调控设计,例如空间折叠的细弯曲声学波导结构(coiling-up spacestructure)。上述方案在实际实施过程中表现出如下三个缺陷:第一、人造声学结构的几何参数一经确定,其声学响应特性便无法改变,难以应用到动态可编程的声场重构场景;第二、基于人造声学结构设计的声场散射特性调控,其透反射声场的相位和振幅往往相互关联,无法独立调节,会对重构声场的质量造成一定的影响;第三、大部分基于几何结构参数优化的像素单元声学结构设计方法,其工作机制和原理往往并不明晰,通常需要消耗巨大的计算资源来确定合适的结构参数。因此,如何提出一种新的技术方案,仅通过一些简单可控的方式让人造声学结构实现可调节的声波相移调控,对基于声学人造结构的声场重构及声场调控技术的实际应用和推广至关重要。In recent years, represented by metamaterials and metasurfaces, sound field reconstruction and sound field regulation schemes based on acoustic artificial structures have attracted extensive attention from academia and industry. Acoustic artificial structures have extremely high design flexibility and controllability. As an important research branch of metamaterials and metasurfaces, the core task of acoustic field regulation based on acoustic metasurfaces is to design Distributed acoustic holographic dry plate. At present, there are two main design schemes for the design of pixel units composed of acoustic holographic dry plates: one is a resonant artificial structure designed using structural resonance characteristics, such as the classic Helmholtz resonator structure (Helmholtz resonator); the other is based on Design of acoustic wave propagation phase control based on equivalent medium theory, such as space-folded thin curved acoustic waveguide structure (coiling-up spacestructure). The above scheme shows the following three defects in the actual implementation process: first, once the geometric parameters of the artificial acoustic structure are determined, its acoustic response characteristics cannot be changed, and it is difficult to apply to the scene of dynamically programmable sound field reconstruction; second, based on In the control of sound field scattering characteristics in the design of artificial acoustic structures, the phase and amplitude of the transflective sound field are often interrelated and cannot be adjusted independently, which will have a certain impact on the quality of the reconstructed sound field; third, most pixels based on geometric structure parameter optimization The working mechanism and principle of unit acoustic structure design methods are often not clear, and it usually needs to consume huge computing resources to determine the appropriate structural parameters. Therefore, how to propose a new technical solution to allow the artificial acoustic structure to achieve adjustable acoustic phase shift control through some simple and controllable methods, and the practical application and promotion of the sound field reconstruction and sound field control technology based on the acoustic artificial structure very important.
发明内容Contents of the invention
本发明的目的之一是提供一种基于近场轨道角动量转换的可调声波相位调制方法。声学轨道角动量作为一个独立于声压场振幅和相位的全新自由度,在通过人造声学结构实现不同轨道角动量之间的转换过程中,仅需转动人造声学结构便能够获得精准可控且可调节的声波传输相位调制,即声学几何相位(acoustic geometric phase)。声学几何相位的产生和调节过程与人造声学结构的具体形式无关,仅依赖于人造声学结构所能支持的轨道角动量转换过程和旋转操作。因此,基于轨道角动量转换的声波相位调制方法的实施简单便捷,人造结构的设计方案灵活多样,并且对于不同的工作波段能够针对性地选取合适的结构形式,能够提高声波传输相位调节的灵活度和提升声场调控的自由度。One of the objectives of the present invention is to provide an adjustable acoustic wave phase modulation method based on near-field orbital angular momentum conversion. Acoustic orbital angular momentum is a new degree of freedom independent of the amplitude and phase of the acoustic pressure field. In the process of converting between different orbital angular momentums through artificial acoustic structures, it is only necessary to rotate the artificial acoustic structures to obtain precise controllable and The modulated acoustic transmission is phase modulated, ie the acoustic geometric phase. The generation and adjustment process of the acoustic geometric phase has nothing to do with the specific form of the artificial acoustic structure, but only depends on the orbital angular momentum conversion process and rotation operation that the artificial acoustic structure can support. Therefore, the implementation of the acoustic wave phase modulation method based on orbital angular momentum conversion is simple and convenient, the design scheme of artificial structures is flexible and diverse, and the appropriate structural form can be selected for different working bands, which can improve the flexibility of acoustic wave transmission phase adjustment And improve the freedom of sound field control.
在此基础上,本发明的目的之一是提供一种基于近场轨道角动量转换的声场重构方法。基于微型扬声器阵列产生的倏逝声学涡旋声源与声学涡旋超构表面的近场耦合相互作用实现声学轨道角动量转换,能够突破波导管自身截止频率对管道最小内径的限制,显著降低声学几何相位声场重构功能器件像素点的横向尺寸至亚波长大小,提升器件的信息存储密度,有效抑制高阶衍射的不利影响,提供了一种亚波长像素、大视场角、大信息容量的声场重构方法。此外,基于像素点相位的可重构特性能够显著拓展声场重构方式,拓展不同声场重构应用场景,如动态可编程的声场重构和声学信号加密。On this basis, one of the objectives of the present invention is to provide a sound field reconstruction method based on near-field orbital angular momentum conversion. Acoustic orbital angular momentum conversion is realized based on the near-field coupling interaction between the evanescent acoustic vortex sound source generated by the microspeaker array and the acoustic vortex metasurface, which can break through the limit of the waveguide's own cut-off frequency on the minimum inner diameter of the pipe, and significantly reduce the acoustic The geometric phase sound field reconstructs the lateral size of the pixel of the functional device to the sub-wavelength size, improves the information storage density of the device, effectively suppresses the adverse effects of high-order diffraction, and provides a sub-wavelength pixel, large viewing angle, and large information capacity. Sound field reconstruction method. In addition, the reconfigurable feature based on the pixel phase can significantly expand the sound field reconstruction method and expand different sound field reconstruction application scenarios, such as dynamically programmable sound field reconstruction and acoustic signal encryption.
本发明的目的是通过下述技术方案实现的:The purpose of the present invention is achieved through the following technical solutions:
本发明公开的基于近场轨道角动量转换的可调声波相位调制方法,包括以下步骤:The adjustable acoustic wave phase modulation method based on near-field orbital angular momentum conversion disclosed by the present invention comprises the following steps:
步骤一:将扬声器阵列放置到刚性圆柱形波导管中产生高质量的倏逝声学涡旋。Step 1: Place the loudspeaker array into a rigid cylindrical waveguide to generate high-quality evanescent acoustic vortices.
所述的倏逝声学涡旋(evanescent acoustic vortex)是半径为R的刚性圆柱形波导管中声学涡旋本征模式的一种特殊形式。通常,刚性圆柱形波导管中的声场可以写成一系列不同加权系数声学涡旋本征波导模式的和,如式(1)所示:The evanescent acoustic vortex is a special form of the eigenmode of the acoustic vortex in a rigid cylindrical waveguide with a radius R. Typically, the acoustic field in a rigid cylindrical waveguide It can be written as the sum of a series of acoustic vortex eigenwaveguide modes with different weighting coefficients, as shown in formula (1):
式中r,z为圆柱波导内的空间坐标;Pm,n为第(m,n)阶本征波导模式的加权系数(即振幅),j为虚数单位;Jm(km,nr)为第m阶柱贝塞尔函数;αm,n是方程dJm(km,nr)/d(km,nr)|r=R=Jm′(αm,n)=0第n阶根,故km,n=αm,n/R;是轴向波矢大小,k0为自由空间声波波矢量大小;描述声学涡旋所携带的轨道角动量,其中m为拓扑荷数,又称TC(topological charge)。where r, z is the spatial coordinate in the cylindrical waveguide; P m,n is the (m,n)th order eigenwaveguide mode The weighting coefficient (i.e. amplitude) of , j is the imaginary unit; J m (k m,n r) is the m-th order column Bessel function; α m,n is the equation dJ m (k m,n r)/d( k m,n r)| r=R =J m ′(α m,n )=0th order root, so k m,n =α m,n /R; is the axial wave vector size, k 0 is the free space acoustic wave vector size; Describe the orbital angular momentum carried by the acoustic vortex, where m is the topological charge, also known as TC (topological charge).
当km,n>k0时,轴向波矢量kz是一个纯虚数,涡旋声场沿+z轴方向场呈指数衰减,是典型的倏逝场(evanescent field)。此时,声学涡旋本征模式无法在波导管中传播,即倏逝声学涡旋。When k m,n >k 0 , the axial wave vector k z is a pure imaginary number, and the vortex sound field decays exponentially along the +z axis, which is a typical evanescent field. At this time, the eigenmode of the acoustic vortex cannot propagate in the waveguide, that is, the evanescent acoustic vortex.
为了获得倏逝声学涡旋,作为优选,刚性圆柱形波导管半径满足R<αm,n/k0,n=0。In order to obtain the evanescent acoustic vortex, preferably, the radius of the rigid cylindrical waveguide satisfies R<α m,n /k 0 , n=0.
为了获得高质量的倏逝声学涡旋,作为优选,使用M×N个微型扬声器组成扬声器阵列,其中M=|m|为倏逝声学涡旋的拓扑荷数(TC)大小,N为扬声器驱动电压的相位离散级次,相邻扬声器驱动电压的相位差为扬声器阵列不同微型扬声器的驱动电压大小相等。In order to obtain high-quality evanescent acoustic vortex, it is preferred to use M×N micro-speakers to form a speaker array, where M=|m| is the topological charge (TC) of the evanescent acoustic vortex, and N is the speaker drive The phase discrete order of the voltage, the phase difference of the adjacent loudspeaker driving voltage is The drive voltages for different microspeakers in the speaker array are equal.
为了优化和提升扬声器阵列的集成度,作为优选,倏逝声学涡旋的拓扑荷数大小M可以为1,2和3,对应的微型扬声器驱动电压相位离散级次N为4,3和3,相邻扬声器驱动电压的相位差分别为90°,120°和120°。In order to optimize and enhance the integration of the loudspeaker array, preferably, the topological charge size M of the evanescent acoustic vortex can be 1, 2 and 3, and the corresponding micro-speaker driving voltage phase discrete order N is 4, 3 and 3, The phase differences of the driving voltages of adjacent loudspeakers are 90°, 120° and 120° respectively.
为了方便扬声器阵列的安装,作为优选,扬声器阵列中的微型扬声器沿角向方向等间隔排布,相邻扬声器之间的角度间隔为 In order to facilitate the installation of the speaker array, preferably, the micro-speakers in the speaker array are arranged at equal intervals along the angular direction, and the angular interval between adjacent speakers is
作为优选,后续步骤中倏逝声涡旋只具有唯一的拓扑荷数,扬声器阵列产生的倏逝声涡旋如式(2)所示:Preferably, in the subsequent steps, the evanescent vortex only has a unique topological charge, and the evanescent vortex produced by the loudspeaker array As shown in formula (2):
步骤二:设计具有特定拓扑荷数的声学涡旋超构表面。Step 2: Design an acoustic vortex metasurface with specific topological charges.
声学涡旋超构表面具有可设定的拓扑荷数,针对入射声涡旋可以通过引入额外的轨道角动量增量,改变透射声涡旋的拓扑荷数,实现声学轨道角动量转换。The acoustic vortex metasurface has a settable topological charge. For the incident acoustic vortex, an additional orbital angular momentum increment can be introduced to change the topological charge of the transmitted acoustic vortex to realize the conversion of acoustic orbital angular momentum.
声学涡旋超构表面的设计方法:半径为R的圆柱形声学涡旋超构表面由K×L个扇形圆柱子单元组成,其中K为声学涡旋超构表面的拓扑荷数大小,L为子单元透射声场相位的离散级次。通过选取合适的声学结构并进行几何参数优化,每个扇形圆柱具有特定的透射声场相位和振幅调制系数,理想的子单元透射振幅为1,并且相邻两个子单元间的透射相位差为将上述扇形圆柱子单元按照透射声场相位大小,沿逆时针方向递增(拓扑荷数为K)或递减(拓扑荷数为-K)的方式周期排列,组成声学涡旋超构表面。The design method of the acoustic vortex metasurface: the cylindrical acoustic vortex metasurface with radius R is composed of K×L fan-shaped cylindrical subunits, where K is the topological charge of the acoustic vortex metasurface, and L is Subunits transmit discrete orders of phase in the sound field. By selecting a suitable acoustic structure and optimizing the geometric parameters, each fan-shaped cylinder has a specific phase and amplitude modulation coefficient of the transmitted acoustic field. The ideal subunit transmission amplitude is 1, and the transmission phase difference between two adjacent subunits is According to the phase size of the transmitted sound field, the fan-shaped cylindrical subunits are arranged periodically in the counterclockwise direction in a manner of increasing (topological charge is K) or decreasing (topological charge is -K) to form an acoustic vortex metasurface.
作为优选,扇形圆柱子单元个数L≥4。Preferably, the number of fan-shaped cylindrical subunits is L≥4.
作为优选,扇形圆柱子单元透射声场的相位和振幅尽可能接近理想值。Preferably, the phase and amplitude of the sound field transmitted by the fan-shaped cylindrical subunit are as close to ideal values as possible.
作为优选,声学涡旋超构表面的拓扑荷数大小K等于倏逝声学涡旋的拓扑荷数大小M。Preferably, the magnitude K of the topological charge of the acoustic vortex metasurface is equal to the magnitude M of the topological charge of the evanescent acoustic vortex.
步骤三:使用步骤二的声学涡旋超构表面与步骤一的倏逝声学涡旋通过近场耦合相互作用实现轨道角动量转换过程,旋转声学涡旋超构表面获得声波传输相位-180°到180°的连续调控。Step 3: Use the acoustic vortex metasurface of
在微纳光学领域,利用光子自旋角动量的转换可获得与微纳结构单元面内空间取向相关的几何相位(geometric phase),通过设计各个微纳结构单元在二维平面内旋转取向能够实现复杂光场整形的功能。已知声学涡旋可携带特定的轨道角动量,因此,基于动量守恒原理,将微纳光学中利用自旋角动量转换获得几何相位的思路推广到声学,将声学轨道角动量作为独立于声压场振幅和相位的自由度,利用轨道角动量转换过程得到声波传输相位的调控。该相位又被称为声学几何相位。In the field of micro-nano optics, the conversion of photon spin angular momentum can be used to obtain the geometric phase related to the in-plane spatial orientation of micro-nano structural units, which can be realized by designing each micro-nano structural unit to rotate in a two-dimensional plane. Functions for complex light field shaping. It is known that the acoustic vortex can carry a specific orbital angular momentum. Therefore, based on the principle of momentum conservation, the idea of using spin angular momentum conversion in micro-nano optics to obtain geometric phase is extended to acoustics, and the acoustic orbital angular momentum is independent of the sound pressure. The degree of freedom of the field amplitude and phase is used to control the phase of the acoustic wave transmission by using the orbital angular momentum conversion process. This phase is also called the acoustic geometric phase.
为了简化分析,将式(2)所述的倏逝声学涡旋记为|m>。步骤二中声学涡旋超构表面将倏逝声学涡旋声场能量耦合成平面声波|0>的过程可以表示成式(3):In order to simplify the analysis, the evanescent acoustic vortex described in formula (2) is denoted as |m>. In
式(3)中,为声学涡旋超构表面的透射算符,θi为声学涡旋超构表面的初始角度。沿+z轴方向,将产生倏逝声学涡旋的扬声器阵列沿逆时针方向旋转得到新的声场分布此时旋转前后的坐标系之间满足r′=r,z′=z。因此,旋转前后的涡旋声场满足式(4):In formula (3), is the transmission operator of the acoustic vortex metasurface, θ i is the initial angle of the acoustic vortex metasurface. Along the +z axis, the loudspeaker array that creates the evanescent acoustic vortex is rotated counterclockwise Get new sound field distribution At this time, r′=r is satisfied between the coordinate systems before and after rotation, z'=z. Therefore, the vortex sound field before and after rotation satisfies formula (4):
同时沿逆时针方向旋转倏逝声学涡旋和声学涡旋超构表面,旋转角度大小为则式(3)变为:Simultaneously rotate the evanescent acoustic vortex and the acoustic vortex metasurface counterclockwise, the rotation angle is Then formula (3) becomes:
结合式(3)和式(5),得到:Combining formula (3) and formula (5), we get:
因此,旋转声学涡旋超构表面,其透射系数将得到一个额外的相位即声学几何相位。根据运动的相对性,固定声学涡旋超构表面,沿逆时针方向将倏逝声学涡旋旋转等价于固定倏逝声学涡旋超构表面,沿顺时针方向将声学涡旋超构表面则此时透射平面声波所携带的相位调制为由于透射平面声波信号的相移大小与扬声器阵列或编码超构表面旋转角度大小具有线性关系,因此能够显著提升声波相位调控的精度。Therefore, the transmission coefficient of the rotating acoustic vortex metasurface will get an additional phase That is, the acoustic geometric phase. According to the relativity of motion, the acoustic vortex metasurface is fixed, and the evanescent acoustic vortex is rotated counterclockwise Equivalent to a fixed evanescent acoustic vortex metasurface, moving the acoustic vortex metasurface clockwise Then the phase modulation carried by the transmitted plane acoustic wave is Since the phase shift of the transmitted plane acoustic wave signal has a linear relationship with the rotation angle of the loudspeaker array or the encoding metasurface, the accuracy of the acoustic wave phase regulation can be significantly improved.
定义产生倏逝声学涡旋的扬声器阵列与声学涡旋超构表面之间的距离为d,由式(2)可知,此时入射并耦合到声学涡旋超构表面的声场幅值的表达式为:Define the distance between the loudspeaker array that produces the evanescent acoustic vortex and the acoustic vortex metasurface as d, from formula (2), we can see that the expression of the amplitude of the sound field incident and coupled to the acoustic vortex metasurface at this time for:
当间隔d越大,则耦合进声学涡旋超构表面的声场能量平均强度就越低,进而出射的平面声波信号的振幅也就越小。When the interval d is larger, the average intensity of the acoustic field energy coupled into the acoustic vortex metasurface is lower, and the amplitude of the outgoing plane acoustic wave signal is also smaller.
为了保证基于轨道角动量转换产生的平面声波信号振幅大小,作为优选,扬声器与声学涡旋超构表面的距离在一个工作波长以下。In order to ensure the amplitude of the plane acoustic wave signal generated based on orbital angular momentum conversion, preferably, the distance between the loudspeaker and the acoustic vortex metasurface is below one working wavelength.
步骤四:本发明还公开一种基于轨道角动量转换的声场重构方法,基于所述一种基于近场耦合声学轨道角动量转换的可调声波传输相位调制方法实现。Step 4: The present invention also discloses a sound field reconstruction method based on orbital angular momentum conversion, which is realized based on the adjustable sound wave transmission phase modulation method based on near-field coupling acoustic orbital angular momentum conversion.
声学轨道角动量作为独立于声压场振幅和相位的自由度,基于轨道角动量转换的可调声波传输相位调控方法提升声场调控的维度,只需一次性设计,不需要重新调整声学人造结构的几何参数,通过旋转产生倏逝声学涡旋的扬声器阵列或声学涡旋超构表面实现对声场重构功能器件像素点相位的编码,简化和降低声场重构功能器件实现的复杂度和难度。Acoustic orbital angular momentum is a degree of freedom independent of the amplitude and phase of the acoustic pressure field. The adjustable acoustic wave transmission phase regulation method based on orbital angular momentum conversion improves the dimension of sound field regulation. It only needs one-time design and does not need to readjust the acoustic artificial structure. Geometric parameters, by rotating the loudspeaker array or the metasurface of the acoustic vortex to generate the evanescent acoustic vortex, the pixel phase encoding of the sound field reconstruction function device is realized, which simplifies and reduces the complexity and difficulty of the realization of the sound field reconstruction function device.
为了减小声场重构功能器件像素点的几何尺寸,提升像素点密度和信息存储容量,本发明采用基于微型扬声器阵列产生的倏逝声学涡旋声源与声学涡旋超构表面通过近场耦合相互作用实现声学轨道角动量转换。该方法中,倏逝声学涡旋可以突破波导管自身截止频率对管道最小内径的限制,可显著降低声学几何相位声场重构功能器件像素点的横向尺寸至亚波长大小,提升器件的信息存储密度,有效抑制高阶衍射的不利影响,提升重构声场的声场质量和分辨率。In order to reduce the geometric size of the pixels of the sound field reconstruction function device and improve the pixel density and information storage capacity, the present invention uses the evanescent acoustic vortex sound source generated based on the micro-speaker array and the acoustic vortex metasurface through near-field coupling. The interaction achieves an acoustic orbital angular momentum transfer. In this method, the evanescent acoustic vortex can break through the limit of the waveguide's own cut-off frequency on the minimum inner diameter of the pipe, which can significantly reduce the lateral size of the pixel of the acoustic geometric phase sound field reconstruction function device to the sub-wavelength size, and improve the information storage density of the device. , effectively suppress the adverse effects of high-order diffraction, and improve the sound field quality and resolution of the reconstructed sound field.
基于近场声学轨道角动量转换的声波相位调控方法能够进行像素点级别的相位独立和可重构调控,此时波导管透射端等价于一个声学点源,根据目标空间声场形式,结合点源算法反解出声学全息图的空间相位和振幅分布,对应调整不同空间位置处编码超构表面的旋转角度,重构出目标声场。The acoustic wave phase control method based on near-field acoustic orbital angular momentum conversion can perform phase independent and reconfigurable control at the pixel level. At this time, the transmission end of the waveguide is equivalent to an acoustic point source. According to the form of the sound field in the target space, combined with the point source The algorithm inversely solves the spatial phase and amplitude distribution of the acoustic hologram, adjusts the rotation angle of the encoded metasurface at different spatial positions correspondingly, and reconstructs the target sound field.
所述点源算法获得目标声场全息图并重构出目标声场的步骤如下:The steps of obtaining the target sound field hologram and reconstructing the target sound field by the point source algorithm are as follows:
1)已知目标声学图像平面位于z=Zd,包含M′×N′个像素点,每个像素点等效处理成一个声学点源,(m′,n′)像素点P(Xm′,Yn′,Zd)的振幅和相位分别为Am′,n′和假设声学全息平面位于z=0,包含K′×L′个像素点,则声学全息平面上(k′,l′)像素点的声场为目标声学图像上所有点源沿-z方向辐射出的球面声波的叠加:1) It is known that the target acoustic image plane is located at z=Z d , contains M′×N′ pixels, and each pixel is equivalently treated as an acoustic point source, (m′,n′) pixel P(X m ′ , Y n′ , Z d ), the amplitude and phase of A m′, n′ and Assuming that the acoustic holographic plane is located at z=0 and contains K'×L' pixels, the sound field of the (k',l') pixel on the acoustic holographic plane is the radiation from all point sources on the target acoustic image along the -z direction Superposition of spherical acoustic waves:
式(8)中为目标声学图像像素点(m′,n′)与目标声学全息图像素点(k′,l′)之间的距离。则目标全息图(k′,l′)像素点的振幅和相位分别为Ak′,l′=abs[p(xk′,yl′,0)]和abs和arg分别对应取幅值和取幅角数学算符。In formula (8) is the distance between the target acoustic image pixel point (m′, n′) and the target acoustic hologram pixel point (k′, l′). Then the amplitude and phase of the target hologram (k′,l′) pixel point are A k′,l′ =abs[p(x k′ ,y l′ ,0)] and abs and arg correspond to the magnitude and argument mathematical operators, respectively.
全息图的具体实施有两种方案:一种是复振幅型全息图(像素点振幅和相位同时调制);另一种是相位型全息图(仅调制像素点的相位值),即忽略所有振幅编码的信息(Ak′,l′为一个常数),只保留相位编码信息。上述两种全息图实施方案均可重构出目标声场,但是,复振幅型较相位型全息图通常能够获得更好的声场重构质量。There are two schemes for the specific implementation of the hologram: one is the complex amplitude hologram (the amplitude and phase of the pixel are modulated at the same time); the other is the phase hologram (only the phase value of the pixel is modulated), that is, all amplitudes are ignored. The encoded information (A k', l' is a constant), only retains the phase encoding information. The above two hologram implementations can reconstruct the target sound field, but the complex amplitude type hologram can usually obtain better sound field reconstruction quality than the phase type hologram.
2)已知声波传播满足时间反演对称性(time-reversal symmetry),由式(8)得到的点源沿+z方向辐射出的球面声波叠加将可以重构出目标声学图像,即:2) It is known that the sound wave propagation satisfies time-reversal symmetry, and the superposition of spherical sound waves radiated from the point source along the +z direction obtained by formula (8) can reconstruct the target acoustic image, namely:
式(9)中为目标声学全息图像素点(k′,l′)与目标声学图像之间任意像素点的距离。Ak′,l′和为全息图像素点的振幅大小和相位,并且:In formula (9) is the distance between any pixel point between the target acoustic hologram pixel point (k′, l′) and the target acoustic image. A k′,l′ and is the amplitude and phase of the hologram pixel, and:
其中,m为倏逝声学涡旋的拓扑荷数,θk′,l′为全息图第(k′,l′)像素点中扬声器阵列或声学涡旋超构表面的旋转角度。对于振幅调制Ak′,l′,由式(7)可知,全息图像素点的声场振幅大小可通过改变扬声器阵列与声学涡旋超构表面之间的距离实现。除此以外,还能够通过调节扬声器阵列中微型扬声器的驱动电压振幅实现。Among them, m is the topological charge of the evanescent acoustic vortex, θ k′,l′ is the rotation angle of the loudspeaker array or the metasurface of the acoustic vortex in the (k′,l′)th pixel of the hologram. For the amplitude modulation A k′,l′ , it can be seen from formula (7) that the amplitude of the sound field of the hologram pixel can be realized by changing the distance between the loudspeaker array and the acoustic vortex metasurface. In addition, it can also be realized by adjusting the driving voltage amplitude of the micro-speakers in the speaker array.
此外,像素点相位的可重构特性能够显著拓展声场重构方式,拓展不同声场重构应用场景,如动态可编程的声场重构,即将微型扬声器阵列固定到步进电机等传动装置,通过计算机主机中的上位机程序,根据式(10)得到的不同像素点位置处扬声器阵列的旋转角度对运动控制器发出指令,控制对应像素点位置处步进电机,实现动态编程的声场重构功能。In addition, the reconfigurable feature of the pixel point phase can significantly expand the sound field reconstruction method and expand different sound field reconstruction application scenarios, such as dynamic programmable sound field reconstruction, that is, the micro speaker array is fixed to the stepping motor and other transmission devices, and through the computer The host computer program in the host sends commands to the motion controller to control the stepping motors at the corresponding pixel positions according to the rotation angles of the speaker arrays at different pixel positions obtained by formula (10), realizing the sound field reconstruction function of dynamic programming.
由式(9)可知,当倏逝声学涡旋的拓扑荷数由m变为-m,全息图像素点相位也从变为此时重构目标声场P′(X,Y,Zd)的表达式为:From formula (9), when the topological charge of the evanescent acoustic vortex changes from m to -m, the phase of the hologram pixel also changes from becomes At this time, the expression for reconstructing the target sound field P′(X, Y, Z d ) is:
其中conj为取共轭(conjugate)。式(11)所述声场分布是由振幅分布为Ak′,l′(xk′,yl′)和相位分布为的点源沿-z方向辐射出的球面声波叠加得到的声场的共轭(强度分布与原目标声学图像相同),此时重构出的目标声学图像位于z=-Zd,是一个虚像。因此,倏逝声学涡旋拓扑荷数的符号也可以对目标重构声场的特性进行操控。Where conj is to take the conjugate (conjugate). The sound field distribution described in formula (11) is composed of the amplitude distribution A k′, l′ (x k′ , y l′ ) and the phase distribution The conjugate of the sound field obtained by the superposition of the spherical acoustic waves radiated from the point source along the -z direction (the intensity distribution is the same as the original target acoustic image), and the reconstructed target acoustic image is located at z=-Z d , which is a virtual image. Therefore, the sign of the topological charge of the evanescent acoustic vortex can also manipulate the characteristics of the target reconstructed sound field.
考虑位于z=Z1,d和z=-Z2,d的两幅声学图像P1(X,Y,Z1,d)(实像)和P2(X,Y,-Z2,d)(虚像),二者在z=0平面上的声场叠加得到:Consider two acoustic images P 1 (X,Y,Z 1,d ) (real image) and P 2 (X,Y,-Z 2,d ) located at z=Z 1,d and z=-Z 2,d (virtual image), the sound fields of the two on the z=0 plane are superimposed to obtain:
p(xk′,yl′,0)=p1(xk′,yl′,0)+p2(xk′,yl′,0) (12)p(x k′ ,y l′ ,0)=p 1 (x k′ ,y l′ ,0)+p 2 (x k′ ,y l′ ,0) (12)
其中:in:
并且A1,m′,n′和分别为声学图像P1(X,Y,Z1,d)的(m′,n′)像素点P1(Xm′,Yn′,Z1,d)的振幅和相位,A2,m′,n′和分别为声学图像P2(X,Y,Z2,d)的(m′,n′)像素点P2(Xm′,Yn′,Z2,d)的振幅和相位。由式(11)知,当倏逝声学涡旋由m变为-m,则分别在z=-Z1,d和z=Z2,d获得共轭的目标声学图像conj[P1(X,Y,Z1,d)]和conj[P2(X,Y,-Z2,d)]。原先的实像P1变成虚像conj(P1),而原来的虚像P2则变成实像conj(P2)。因此,通过上述方法设计得到的声学全息图,能够通过改变倏逝声学涡旋的拓扑荷数的符号实现全息图同侧不同声场的重现,提升声学全息图的信息存储容量,并在声学信号加密方面具有应用价值。and A 1,m′,n′ and are respectively the amplitude and phase of the (m′,n′) pixel point P 1 (X m′ ,Y n′ ,Z 1,d ) of the acoustic image P 1 (X,Y,Z 1,d ), A 2, m',n' and are the amplitude and phase of the (m′,n′) pixel point P 2 (X m′ , Y n′ , Z 2,d ) of the acoustic image P 2 (X, Y, Z 2,d ), respectively. From formula (11) , when the evanescent acoustic vortex changes from m to -m, the conjugate target acoustic image conj[P 1 (X ,Y,Z 1,d )] and conj[P 2 (X,Y,-Z 2,d )]. The original real image P 1 becomes the virtual image conj(P 1 ), and the original virtual image P 2 becomes the real image conj(P 2 ). Therefore, the acoustic hologram designed by the above method can realize the reproduction of different sound fields on the same side of the hologram by changing the sign of the topological charge of the evanescent acoustic vortex, and improve the information storage capacity of the acoustic hologram. The encryption aspect has application value.
为了获得最佳的声场重构效果,作为优选,本发明采用复振幅型全息图进行声场重构。In order to obtain the best sound field reconstruction effect, preferably, the present invention uses complex amplitude holograms for sound field reconstruction.
为了最大限度减小像素点横向尺寸和增加器件像素点密度,作为优选,使用1×4个微型扬声器组成的扬声器阵列产生倏逝声学涡旋作为信号源。In order to minimize the lateral size of the pixels and increase the pixel density of the device, preferably, a speaker array composed of 1×4 micro-speakers is used to generate an evanescent acoustic vortex as a signal source.
为了简便动态可编程声场重构功能的实现,作为优选,本发明通过改变微型扬声器驱动电压振幅实现像素点振幅大小的调制。In order to facilitate the realization of the dynamic programmable sound field reconstruction function, preferably, the present invention realizes the modulation of the amplitude of the pixel point by changing the driving voltage amplitude of the micro-speaker.
为了实现声学全息图像加密和大容量声学信息存储,作为优选,倏逝声学涡旋的拓扑荷数符号可以在保持电压幅值不变的条件下,通过切换微型扬声器驱动电压相位的符号实现。In order to realize acoustic holographic image encryption and large-capacity acoustic information storage, preferably, the topological charge sign of the evanescent acoustic vortex can be realized by switching the sign of the driving voltage phase of the micro-speaker under the condition of keeping the voltage amplitude constant.
有益效果:Beneficial effect:
1、本发明公开的一种基于近场轨道角动量转换的声波相位调制及声场重构方法,利用轨道角动量转换过程获得声学传输相位的调制,相比于改变人造声学结构几何参数的方法,通过旋转人造声学结构实现声学传输相位调制的方法简单直观且调控精度高。1. The present invention discloses a sound wave phase modulation and sound field reconstruction method based on near-field orbital angular momentum conversion, which uses the orbital angular momentum conversion process to obtain the modulation of the acoustic transmission phase. Compared with the method of changing the geometric parameters of artificial acoustic structures, The method of realizing the phase modulation of acoustic transmission by rotating the artificial acoustic structure is simple and intuitive with high control precision.
2、本发明公开的一种基于近场轨道角动量转换的声波相位调制及声场重构方法,利用微型扬声器阵列产生的倏逝声学涡旋声源与声学涡旋超构表面通过近场耦合相互作用实现声学轨道角动量转换,显著减小像素点的几何尺寸至亚波长大小,提升像素点密度和信息存储容量。2. A sound wave phase modulation and sound field reconstruction method based on near-field orbital angular momentum conversion disclosed in the present invention uses the evanescent acoustic vortex sound source generated by the micro-speaker array and the acoustic vortex metasurface to interact with each other through near-field coupling The function realizes the conversion of acoustic orbital angular momentum, significantly reduces the geometric size of pixels to sub-wavelength size, and improves pixel density and information storage capacity.
3、本发明公开的一种基于近场轨道角动量转换的声波相位调制及声场重构方法,采用点源算法获得不同目标声学图像复振幅型全息图,通过调整扬声器驱动电压的幅值和扬声器阵列或声学涡旋超构表面的旋转角度,获得目标声学图像的高质量重构。3. A sound wave phase modulation and sound field reconstruction method based on near-field orbital angular momentum conversion disclosed in the present invention uses a point source algorithm to obtain complex-amplitude holograms of different target acoustic images, and adjusts the amplitude of the speaker drive voltage and the loudspeaker The angle of rotation of the array or the acoustic vortex metasurface to obtain a high-quality reconstruction of the acoustic image of the target.
4、本发明公开的一种基于近场轨道角动量转换的声波相位调制及声场重构方法,通过声学全息图设计和改变倏逝声学涡旋拓扑荷数的符号,重构得到不同的声学图像,相比于传统的声学全息声场重构技术,能够实现声学信号的加密和提升信息存储容量。4. An acoustic wave phase modulation and acoustic field reconstruction method based on near-field orbital angular momentum conversion disclosed in the present invention, through acoustic hologram design and changing the sign of the evanescent acoustic vortex topological charge, reconstructing different acoustic images , compared with the traditional acoustic holographic sound field reconstruction technology, it can realize the encryption of the acoustic signal and improve the information storage capacity.
附图说明Description of drawings
图1为本发明公开的基于近场轨道角动量转换的声波相位调制及声场重构方法的装置原理示意图;Fig. 1 is a schematic diagram of the device principle of the acoustic wave phase modulation and acoustic field reconstruction method based on near-field orbital angular momentum conversion disclosed by the present invention;
图2为本发明公开的基于近场轨道角动量转换的声波相位调制及声场重构方法的流程图;Fig. 2 is the flowchart of the sound wave phase modulation and sound field reconstruction method based on near-field orbital angular momentum conversion disclosed by the present invention;
图3为声学涡旋超构表面示意图,其中:图3(a)为声学涡旋超构表面的结构示意图,图3(b)为扇形圆柱子单元的结构示意图;Fig. 3 is a schematic diagram of an acoustic vortex metasurface, wherein: Fig. 3 (a) is a structural schematic diagram of an acoustic vortex metasurface, and Fig. 3 (b) is a structural schematic diagram of a fan-shaped cylindrical subunit;
图4为声学涡旋超构表面扇形圆柱的声学响应,其中:图4(a)为不同扇形圆柱的透射相位曲线图,图4(b)为不同扇形圆柱的透射振幅曲线图;Fig. 4 is the acoustic response of the fan-shaped cylinder on the acoustic vortex metasurface, wherein: Fig. 4 (a) is the transmission phase curve of different fan-shaped cylinders, and Fig. 4 (b) is the transmission amplitude curve of different fan-shaped cylinders;
图5为本发明公开的基于近场轨道角动量转换的声波相位调制及声场重构方法基本像素单元的结构示意图;5 is a schematic structural diagram of the basic pixel unit of the acoustic wave phase modulation and acoustic field reconstruction method based on near-field orbital angular momentum conversion disclosed by the present invention;
其中:1─扬声器阵列、2─声学涡旋超构表面、3─波导管;Among them: 1─speaker array, 2─acoustic vortex metasurface, 3─waveguide;
图6为透射声波传输相位随涡旋超构表面旋转角度改变的变化图;Fig. 6 is a change diagram of the transmission phase of the transmitted acoustic wave as the rotation angle of the vortex metasurface changes;
图7为本发明实例中声学全息声场结果,其中:图7(a)为声学全息图重构出目标声学图像的示意图,图7(b)为声学全息图的归一化振幅,图7(c)为声学全息图的相位,图7(d)为重构出的目标声学图像声场能量分布。Fig. 7 is the acoustic field result of the acoustic hologram in the example of the present invention, wherein: Fig. 7 (a) is the schematic diagram of the target acoustic image reconstructed by the acoustic hologram, Fig. 7 (b) is the normalized amplitude of the acoustic hologram, Fig. 7 ( c) is the phase of the acoustic hologram, and Fig. 7(d) is the energy distribution of the sound field of the reconstructed target acoustic image.
图8为本发明实例中基于拓扑荷数切换的两幅不同声学全息声场结果。其中:图8(a)为倏逝声学涡旋的拓扑荷数为1时重构出“心”型声场的示意图,图8(b)为倏逝声学涡旋的拓扑荷数为-1时重构出“星”型声场的示意图,图8(c)为声学全息图的归一化振幅,相位和重构出的声场强度分布。Fig. 8 is the result of two different acoustic holographic sound fields based on topological charge switching in the example of the present invention. Among them: Figure 8(a) is a schematic diagram of reconstructing the "heart" sound field when the topological charge of the evanescent acoustic vortex is 1, and Figure 8(b) is when the topological charge of the evanescent acoustic vortex is -1 The schematic diagram of reconstructing the "star" sound field, Fig. 8(c) is the normalized amplitude, phase and intensity distribution of the reconstructed sound field of the acoustic hologram.
具体实施方式detailed description
为了更好的说明本发明的目的和优点,下面结合附图和实例对本发明作更进一步的说明。In order to better illustrate the purpose and advantages of the present invention, the present invention will be further described below in conjunction with the accompanying drawings and examples.
实施例1Example 1
如图1所示,本实施例公开的一种基于近场轨道角动量转换的声波相位调制及声场重构方法,利用刚性圆柱波导管中扬声器阵列所产生的倏逝声学涡旋与声学涡旋超构表面的近场耦合相互作用实现轨道角动量转换,通过旋转扬声器阵列或者声学涡旋超构表面得到透射声波传输相位的调制。再利用点源算法,得到目标声学图像的全息图复振幅分布,对应调节不同像素点处扬声器阵列的驱动电压幅值和扬声器阵列/声学涡旋超构表面的旋转角度重构出目标声学图像。As shown in Figure 1, this embodiment discloses a sound wave phase modulation and sound field reconstruction method based on near-field orbital angular momentum conversion, using the evanescent acoustic vortex and acoustic vortex generated by the speaker array in the rigid cylindrical waveguide The near-field coupling interaction of the metasurface realizes the conversion of the orbital angular momentum, and the modulation of the transmission phase of the transmitted acoustic wave is obtained through the rotating speaker array or the acoustic vortex metasurface. Using the point source algorithm, the complex amplitude distribution of the hologram of the target acoustic image is obtained, and the driving voltage amplitude of the speaker array at different pixel points and the rotation angle of the speaker array/acoustic vortex metasurface are correspondingly adjusted to reconstruct the target acoustic image.
如图2所示,本实施例公开的一种基于近场轨道角动量转换的声波相位调制及声场重构方法,具体的实现步骤如下:As shown in Figure 2, a method for acoustic phase modulation and acoustic field reconstruction based on near-field orbital angular momentum conversion disclosed in this embodiment, the specific implementation steps are as follows:
步骤1:将扬声器阵列放置到刚性圆柱形波导管中产生高质量的倏逝声学涡旋。Step 1: Place the loudspeaker array into a rigid cylindrical waveguide to generate high-quality evanescent acoustic vortices.
使用4个直径为10mm的微型扬声器,按2×2正方形格点阵列排布安装并固定到直径为40mm的吸声海绵上,扬声器间隔设置为15mm,利用函数信号发生器产生4路幅值大小相同但是各自独立的正弦电压信号对微型扬声器阵列进行同步驱动,正弦电压信号的频率为2858Hz,并且沿逆时针方向,与4个微型扬声器相对应驱动电信号依次具有0°,90°,180°和270°相移。
将所述扬声器阵列放置到内径为40mm长为120mm的刚性亚克力圆柱波导管内,产生拓扑荷数为1的倏逝声学涡旋声源。The loudspeaker array is placed in a rigid acrylic cylindrical waveguide with an inner diameter of 40 mm and a length of 120 mm to generate an evanescent acoustic vortex sound source with a topological charge of 1.
步骤2:设计具有拓扑荷数大小等于倏逝声学涡旋声源拓扑荷数大小的声学涡旋超构表面。Step 2: Design an acoustic vortex metasurface with a topological charge equal to the topological charge of the evanescent acoustic vortex source.
声学涡旋超构表面工作环境的介质为空气,其密度和声速度大小分别为1.21kg/m3和343m/s,入射声波的频率f0为2858Hz,对应波长λ0约为12cm。声学涡旋超构表面的组成材料为光敏树脂,也可选取其他与空气声阻抗差别较大的材料,如尼龙,ABS塑料,金属等。The medium of the working environment of the acoustic vortex metasurface is air, its density and sound velocity are 1.21kg/m 3 and 343m/s respectively, the frequency f 0 of the incident sound wave is 2858Hz, and the corresponding wavelength λ 0 is about 12cm. The material of the acoustic vortex metasurface is photosensitive resin, and other materials with a large difference in acoustic impedance from air can also be selected, such as nylon, ABS plastic, metal, etc.
如图3(a)所示,作为优选,声学涡旋超构表面由十二个扇形圆柱子单元组成。As shown in Fig. 3(a), preferably, the acoustic vortex metasurface is composed of twelve fan-shaped cylindrical subunits.
如图3(b)所示,作为优选,扇形圆柱子单元由同轴的一层厚度dR为15mm圆柱面和中心位置处半径r为3mm的实心圆柱组成,扇形柱高H为75mm,不同扇形柱由厚度为1.5mm的连接板分隔开并连接到超构表面中心半径r为3mm的实心圆柱,故编码超构表面的直径为40mm,与传输管道内径吻合。每个扇形柱沿轴向包含四个相同的圆环型共振腔,圆环型共振腔的壁厚为1.5mm,宽度为通过设计圆环型共振腔的深度及腔的开口大小,可以实现透射声波相位的调节。As shown in Figure 3(b), as a preference, the fan-shaped cylindrical subunit is composed of a coaxial cylindrical surface with a thickness dR of 15mm and a solid cylinder with a radius r of 3mm at the center, and the height H of the fan-shaped column is 75mm. The columns are separated by connecting plates with a thickness of 1.5 mm and connected to a solid cylinder with a central radius r of the metasurface of 3 mm, so the diameter of the coded metasurface is 40 mm, which coincides with the inner diameter of the transmission pipeline. Each fan-shaped column contains four identical circular resonant cavities along the axial direction. The wall thickness of the circular resonant cavity is 1.5mm, and the width is Adjustment of the sound wave phase.
组成涡旋超构表面的十二个扇形圆柱子单元具有近1的透射振幅(如图4(a)所示)和-180°到150°离散步长为30°的透射相位大小(如图4(b)所示)。因此,按照透射相位大小逆时针或顺时针方向排列扇形柱子单元即可获得拓扑荷数为1或-1的涡旋超构表面。The twelve fan-shaped cylindrical subunits that make up the vortex metasurface have a transmission amplitude of nearly 1 (as shown in Figure 4(a)) and a transmission phase magnitude of -180° to 150° with a discrete step of 30° (Figure 4(b)). Therefore, a vortex metasurface with a topological charge of 1 or -1 can be obtained by arranging the fan-shaped pillar units counterclockwise or clockwise according to the magnitude of the transmission phase.
步骤3:声学涡旋超构表面与紧邻的倏逝声学涡旋通过近场耦合相互作用实现轨道角动量转换过程,旋转声学涡旋超构表面获得声波传输相位-180°到180°的连续调控。Step 3: The acoustic vortex metasurface and the adjacent evanescent acoustic vortex realize the orbital angular momentum conversion process through the near-field coupling interaction, and the rotating acoustic vortex metasurface obtains continuous control of the acoustic wave transmission phase from -180° to 180° .
步骤1产生倏逝声学涡旋声源的扬声器阵列和步骤2中的声学涡旋超构表面相邻放置在刚性亚克力圆柱波导管中构成像素单元,如图5所示。倏逝声学涡旋与声学涡旋超构表面通过耦合相互作用在透射端产生拓扑荷数为0的平面声波并在波导管中继续向前传播。The loudspeaker array that generates the evanescent acoustic vortex sound source in
以圆柱波导管长轴方向的中心对称轴为旋转轴,沿声波传播方向顺时针旋转声学涡旋超构表面或逆时针旋转扬声器阵列。此时,透射平面声波的相位变化量等于旋转角度与倏逝声学涡旋拓扑荷数的乘积。Taking the central symmetry axis in the long axis direction of the cylindrical waveguide as the rotation axis, the acoustic vortex metasurface is rotated clockwise along the sound wave propagation direction or the loudspeaker array is rotated counterclockwise. At this time, the phase change of the transmitted plane acoustic wave is equal to the product of the rotation angle and the topological charge of the evanescent acoustic vortex.
所述采用拓扑荷数为1的倏逝声学涡旋声源与拓扑荷数为1的声学涡旋超构表面相互作用得到声学传输相位调制,声波传输相位变化量等于声学涡旋超构表面的旋转角度,如图6所示。The interaction between the evanescent acoustic vortex sound source with a topological charge of 1 and the acoustic vortex metasurface with a topological charge of 1 is used to obtain phase modulation of acoustic transmission, and the amount of change in the acoustic wave transmission phase is equal to that of the acoustic vortex metasurface Rotation angle, as shown in Figure 6.
步骤4:使用点源算法,求解出复振幅型全息图像素点的归一化振幅和相位的空间分布。Step 4: Using the point source algorithm, the spatial distribution of the normalized amplitude and phase of the pixels of the complex amplitude hologram is obtained.
选取目标声学图像“柠檬”,假设其位于声学全息图平面前10λ0的位置,并且该声学图像空间几何尺寸为15λ0×15λ0,像素点个数为100×100,每个像素点的大小为0.15λ0,其中λ0为所述声学涡旋超构表面的中心工作波长。声学全息图的像素大小设为0.5λ0,像素点个数为50×50,故声学全息图的空间尺寸为25λ0×25λ0。Select the target acoustic image "lemon", assuming it is located at a position 10λ 0 in front of the plane of the acoustic hologram, and the spatial geometric size of the acoustic image is 15λ 0 × 15λ 0 , the number of pixels is 100×100, and the size of each pixel is is 0.15λ 0 , where λ 0 is the central working wavelength of the acoustic vortex metasurface. The pixel size of the acoustic hologram is set to 0.5λ 0 , and the number of pixels is 50×50, so the spatial size of the acoustic hologram is 25λ 0 ×25λ 0 .
目标图像上第(m′,n′)像素点作为独立的声学点源辐射出球面声波,沿-z方向传播到位于原点处的声学全息图平面,其中Am′,n′和分别为目标图像像素点的振幅和相位。由于目标声学图像设定为仅具有空间强度分布的二维图像,因此为0或随机噪声。The (m′,n′)th pixel on the target image Spherical acoustic waves are radiated as independent acoustic point sources, and propagate along the -z direction to the plane of the acoustic hologram at the origin, where A m′,n′ and are the amplitude and phase of the target image pixel, respectively. Since the target acoustic image is set to be a two-dimensional image with only spatial intensity distribution, so is 0 or random noise.
目标图像像素点的相位 The phase of the target image pixel
目标图像的所有像素点在声学全息平面上第(k′,l′)像素点上叠加得到的总声场为:The total sound field obtained by superimposing all pixels of the target image on the (k′,l′)th pixel on the acoustic holographic plane is:
式(8)中为目标声学图像像素点(m′,n′)与目标声学全息图像素点(k′,l′)之间的距离,像素点个数M′=N′=100,目标声学图像和声学全息平面的距离Zd=10λ0。In formula (8) is the distance between the target acoustic image pixel (m′, n′) and the target acoustic hologram pixel (k′, l′), the number of pixels M′=N′=100, the target acoustic image and the acoustic hologram The distance Z d =10λ 0 of the plane.
由声波传播满足时间反演对称性(time-reversal symmetry),式(8)所得到的声学全息平面处的声场应与声学全息图辐射的声场相同。因此,目标全息图(k′,l′)像素点的振幅和相位分别为Ak′,l′=abs[p(xk′,yl′,0)]和abs和arg分别对应取幅值和取幅角数学算符。Since sound wave propagation satisfies time-reversal symmetry, the sound field at the acoustic holographic plane obtained by Eq. (8) should be the same as the sound field radiated by the acoustic hologram. Therefore, the amplitude and phase of the target hologram (k′,l′) pixel are respectively A k′,l′ = abs[p(x k′ ,y l′ ,0)] and abs and arg correspond to the magnitude and argument mathematical operators, respectively.
步骤5:调节扬声器阵列驱动电压幅值并旋转扬声器阵列或声学涡旋超构表面,将像素点归一化振幅和相位与步骤4得到的复振幅型全息图一一对应,重构出目标声场。Step 5: Adjust the driving voltage amplitude of the speaker array and rotate the speaker array or the acoustic vortex metasurface, correspond the normalized amplitude and phase of the pixels with the complex amplitude hologram obtained in
图7(a)为声学全息图重构出目标声学图像的示意图,虚线框为声学全息图的局部放大图,作为展示,这里不同像素点处通过针对性地旋转声学涡旋超构表面改变其空间取向实现像素点相位调制,像素点的声学涡旋超构表面旋转角度为如果选择固定声学涡旋超构表面不动而旋转扬声器阵列,则扬声器阵列的旋转角度为 Figure 7(a) is a schematic diagram of reconstructing the target acoustic image from the acoustic hologram, and the dotted line box is a partially enlarged image of the acoustic hologram. The spatial orientation realizes the phase modulation of the pixel point, and the rotation angle of the acoustic vortex metasurface of the pixel point is If you choose to fix the acoustic vortex metasurface and rotate the speaker array, the rotation angle of the speaker array is
基于步骤4所得到的复振幅全息图的振幅(图7(b))和相位(图7(c))信息,设置好声学全息图不同像素点的归一化振幅和相位,最终重构出的声学全息声场的能量分布如图7(d)所示,可以清晰地辨认出目标声学图像“柠檬”。Based on the amplitude (Fig. 7(b)) and phase (Fig. 7(c)) information of the complex amplitude hologram obtained in
综上所述,本实例提供了一种基于近场轨道角动量转换的声波相位调制及声场重构方法,利用倏逝声学涡旋与声学涡旋超构表面的近场耦合相互作用所实现的轨道角动量转换过程,获得声波传输相位的连续可控调制。再利用点源算法,得到目标声学图像的全息图复振幅分布,对应调节不同像素点处扬声器阵列的驱动电压幅值和扬声器阵列/声学涡旋超构表面的旋转角度重构出目标声学图像。In summary, this example provides an acoustic wave phase modulation and acoustic field reconstruction method based on near-field orbital angular momentum conversion, which is realized by the near-field coupling interaction between the evanescent acoustic vortex and the acoustic vortex metasurface The orbital angular momentum conversion process obtains a continuous controllable modulation of the acoustic transmission phase. Using the point source algorithm, the complex amplitude distribution of the hologram of the target acoustic image is obtained, and the driving voltage amplitude of the speaker array at different pixel points and the rotation angle of the speaker array/acoustic vortex metasurface are correspondingly adjusted to reconstruct the target acoustic image.
实施例2Example 2
设计声学全息图,通过倏逝声学涡旋拓扑荷数符号的切换实现不同目标声学图像的重构。The acoustic hologram is designed, and the reconstruction of different target acoustic images is realized by switching the sign of the topological charge of the evanescent acoustic vortex.
如图2所示,本施例包括以下步骤:As shown in Figure 2, this embodiment includes the following steps:
步骤1:将扬声器阵列放置到刚性圆柱形波导管中产生高质量的倏逝声学涡旋。Step 1: Place the loudspeaker array into a rigid cylindrical waveguide to generate high-quality evanescent acoustic vortices.
使用4个直径为10mm的微型扬声器,按2×2正方形格点阵列排布安装并固定到直径为40mm的吸声海绵上,扬声器间隔设置为15mm,利用函数信号发生器产生4路幅值大小相同但是各自独立的正弦电压信号对微型扬声器阵列进行同步驱动,正弦电压信号的频率为2858Hz,并且沿逆时针方向,与4个微型扬声器相对应驱动电信号依次具有0°,90°,180°和270°相移。
将所述扬声器阵列放置到内径为40mm长为120mm的刚性亚克力圆柱波导管内,产生拓扑荷数为1的倏逝声学涡旋声源。The loudspeaker array is placed in a rigid acrylic cylindrical waveguide with an inner diameter of 40 mm and a length of 120 mm to generate an evanescent acoustic vortex sound source with a topological charge of 1.
将四个微型扬声器驱动电压的初始相移由0°,90°,180°和270°变为0°,-90°,-180°和-270°或者是270°,180°,90°和0°,可以实现倏逝声学涡旋的拓扑荷数由1到-1的切换。Change the initial phase shift of four microspeaker drive voltages from 0°, 90°, 180° and 270° to 0°, -90°, -180° and -270° or 270°, 180°, 90° and 0°, the topological charge of the evanescent acoustic vortex can be switched from 1 to -1.
步骤2:设计具有拓扑荷数大小等于倏逝声学涡旋声源拓扑荷数大小的声学涡旋超构表面。Step 2: Design an acoustic vortex metasurface with a topological charge equal to the topological charge of the evanescent acoustic vortex source.
声学涡旋超构表面工作环境的介质为空气,其密度和声速度大小分别为1.21kg/m3和343m/s,入射声波的频率f0为2858Hz,对应波长λ0约为12cm。声学涡旋超构表面的组成材料为光敏树脂,也可选取其他与空气声阻抗差别较大的材料,如尼龙,ABS塑料,金属等。The medium of the working environment of the acoustic vortex metasurface is air, its density and sound velocity are 1.21kg/m 3 and 343m/s respectively, the frequency f 0 of the incident sound wave is 2858Hz, and the corresponding wavelength λ 0 is about 12cm. The material of the acoustic vortex metasurface is photosensitive resin, and other materials with a large difference in acoustic impedance from air can also be selected, such as nylon, ABS plastic, metal, etc.
如图3(a)所示,作为优选,声学涡旋超构表面由十二个扇形圆柱子单元组成。As shown in Fig. 3(a), preferably, the acoustic vortex metasurface is composed of twelve fan-shaped cylindrical subunits.
如图3(b)所示,作为优选,扇形圆柱子单元由同轴的一层厚度dR为15mm圆柱面和中心位置处半径r为3mm的实心圆柱组成,扇形柱高H为75mm,不同扇形柱由厚度为1.5mm的连接板分隔开并连接到超构表面中心半径r为3mm的实心圆柱。每个扇形柱沿轴向包含四个相同的圆环型共振腔,圆环型共振腔的壁厚为1.5mm,宽度为通过设计圆环型共振腔的深度及腔的开口大小,可以实现透射声波相位的调节。As shown in Figure 3(b), as a preference, the fan-shaped cylindrical subunit is composed of a coaxial cylindrical surface with a thickness dR of 15mm and a solid cylinder with a radius r of 3mm at the center, and the height H of the fan-shaped column is 75mm. The columns are separated by connecting plates with a thickness of 1.5 mm and connected to a solid cylinder with a central radius r of 3 mm on the metasurface. Each fan-shaped column contains four identical circular resonant cavities along the axial direction. The wall thickness of the circular resonant cavity is 1.5mm, and the width is Adjustment of the sound wave phase.
组成涡旋超构表面的十二个扇形圆柱子单元具有近1的透射振幅(如图4(a)所示)和-180°到150°离散步长为30°的透射相位大小(如图4(b)所示)。因此,按照透射相位大小依次排列扇形柱子单元即可获得拓扑荷数大小为1的涡旋超构表面。The twelve fan-shaped cylindrical subunits that make up the vortex metasurface have a transmission amplitude of nearly 1 (as shown in Figure 4(a)) and a transmission phase magnitude of -180° to 150° with a discrete step of 30° (Figure 4(b)). Therefore, a vortex metasurface with a topological charge of 1 can be obtained by arranging the fan-shaped pillar units in sequence according to the size of the transmission phase.
步骤3:声学涡旋超构表面与紧邻的倏逝声学涡旋通过近场耦合相互作用实现轨道角动量转换过程,旋转声学涡旋超构表面获得声波传输相位-180°到180°的连续调控。Step 3: The acoustic vortex metasurface and the adjacent evanescent acoustic vortex realize the orbital angular momentum conversion process through the near-field coupling interaction, and the rotating acoustic vortex metasurface obtains continuous control of the acoustic wave transmission phase from -180° to 180° .
步骤1产生倏逝声学涡旋声源的扬声器阵列和步骤2中的声学涡旋超构表面相邻放置在刚性亚克力圆柱波导管中构成像素单元,如图5所示。倏逝声学涡旋与声学涡旋超构表面通过耦合相互作用在透射端产生拓扑荷为0的平面声波并在波导管中继续向前传播。The loudspeaker array that generates the evanescent acoustic vortex sound source in
以圆柱波导管长轴方向的中心对称轴为旋转轴,沿声波传播方向顺时针旋转声学涡旋超构表面或逆时针旋转扬声器阵列。此时,透射平面声波的相位变化量等于旋转角度与倏逝声学涡旋拓扑荷数的乘积。Taking the central symmetry axis in the long axis direction of the cylindrical waveguide as the rotation axis, the acoustic vortex metasurface is rotated clockwise along the sound wave propagation direction or the loudspeaker array is rotated counterclockwise. At this time, the phase change of the transmitted plane acoustic wave is equal to the product of the rotation angle and the topological charge of the evanescent acoustic vortex.
所述采用拓扑荷数为1的倏逝声学涡旋声源与拓扑荷数为1的声学涡旋超构表面相互作用得到声学传输相位调制,声波传输相位变化量等于声学涡旋超构表面的旋转角度,如图6所示。The interaction between the evanescent acoustic vortex sound source with a topological charge of 1 and the acoustic vortex metasurface with a topological charge of 1 is used to obtain phase modulation of acoustic transmission, and the amount of change in the acoustic wave transmission phase is equal to that of the acoustic vortex metasurface Rotation angle, as shown in Figure 6.
步骤4:使用点源算法,求解出复振幅型全息图像素点的归一化振幅和相位的空间分布。Step 4: Using the point source algorithm, the spatial distribution of the normalized amplitude and phase of the pixels of the complex amplitude hologram is obtained.
选取“心”型和“星”型图案作为目标图像,假设声学全息图平面位于原点,“心”型图案位于声学全息图平面前10λ0的位置,“星”型图案位于声学全息图平面后10λ0的位置,并且所述两个声学图像的空间几何尺寸均为15λ0×15λ0,像素点个数为100×100,每个像素点的大小为0.15λ0,其中λ0为所述声学涡旋超构表面的中心工作波长。声学全息图的空间尺寸为25λ0×25λ0,像素点个数为50×50,像素大小设为0.5λ0。Select the "heart" and "star" patterns as the target image, assuming that the plane of the acoustic hologram is located at the origin, the "heart" pattern is located at the position 10λ0 in front of the plane of the acoustic hologram, and the "star" pattern is located behind the plane of the acoustic hologram 10λ 0 , and the spatial geometric dimensions of the two acoustic images are both 15λ 0 ×15λ 0 , the number of pixels is 100×100, and the size of each pixel is 0.15λ 0 , where λ 0 is the The central operating wavelength of the acoustic vortex metasurface. The spatial size of the acoustic hologram is 25λ 0 ×25λ 0 , the number of pixels is 50×50, and the pixel size is set to 0.5λ 0 .
所述“心”型目标声学图像的像素点沿-z方向辐射并传播的球面波和“星”型目标声学图像的像素点沿+z方向辐射并传播的球面波在z=0平面上的声场叠加得到:Pixels of the acoustic image of the "heart" target Spherical waves radiating and propagating in the -z direction and pixel points of the acoustic image of the "star" target The sound field superposition of the spherical wave radiating and propagating along the +z direction on the z=0 plane is obtained:
p(xk′,yl′,0)=p1(xk′,yl′,0)+p2(xk′,yl′,0) (12)p(x k′ ,y l′ ,0)=p 1 (x k′ ,y l′ ,0)+p 2 (x k′ ,y l′ ,0) (12)
其中:in:
并且i=1,2。A1,m′,n′和分别为声学图像P1(X,Y,Z1,d)的(m′,n′)像素点P1(Xm′,Yn′,Z1,d)的振幅和相位,A2,m′,n′和分别为声学图像P2(X,Y,Z2,d)的(m′,n′)像素点P2(Xm′,Yn′,Z2,d)的振幅和相位。and i=1,2. A 1,m′,n′ and are respectively the amplitude and phase of the (m′,n′) pixel point P 1 (X m′ ,Y n′ ,Z 1,d ) of the acoustic image P 1 (X,Y,Z 1,d ), A 2, m',n' and are the amplitude and phase of the (m′,n′) pixel point P 2 (X m′ , Y n′ , Z 2,d ) of the acoustic image P 2 (X, Y, Z 2,d ), respectively.
目标全息图(k′,l′)像素点的振幅和相位分别为Ak′,l′=abs[p(xk′,yl′,0)]和abs和arg分别对应取幅值和取幅角数学算符。The amplitude and phase of the target hologram (k′,l′) pixel point are respectively A k′,l′ = abs[p(x k′ ,y l′ ,0)] and abs and arg correspond to the magnitude and argument mathematical operators, respectively.
步骤5:调节扬声器阵列驱动电压幅值并旋转声学涡旋超构表面,将像素点归一化振幅和相位与步骤4得到的复振幅型全息图一一对应。通过改变倏逝声学涡旋声源拓扑荷数,重构出不同的目标声场。Step 5: Adjust the driving voltage amplitude of the loudspeaker array and rotate the acoustic vortex metasurface, and correspond the normalized amplitude and phase of the pixel to the complex amplitude hologram obtained in
图8(a)为声学全息图重构出“心”型目标声学图像的示意图,虚线框为声学全息图的局部放大图,作为展示,这里不同像素点处通过针对性地旋转声学涡旋超构表面改变其空间取向实现像素点相位调制,像素点的声学涡旋超构表面旋转角度为基于步骤4所得到的复振幅全息图的振幅(见图8(c)(左图)),当倏逝声学涡旋的拓扑荷数为1时(扬声器阵列的4个微型扬声器相对应驱动电信号依次具有0°,90°,180°和270°相移),全息图像素点的相位如图8(c)(中上)所示。设置好声学全息图不同像素点的归一化振幅和相位,最终重构出的声学全息声场的能量分布如图8(c)(右上)所示,可以清晰地辨认出“心”型目标声学图像。Figure 8(a) is a schematic diagram of reconstructing the acoustic image of a "heart"-shaped target from an acoustic hologram. The dashed box is a partially enlarged image of the acoustic hologram. The textured surface changes its spatial orientation to realize the phase modulation of the pixel point, and the rotation angle of the acoustic vortex metasurface of the pixel point is Based on the amplitude of the complex amplitude hologram obtained in step 4 (see Fig. 8(c) (left figure)), when the topological charge of the evanescent acoustic vortex is 1 (the four micro-speakers of the speaker array correspond to the driving voltage The signals have phase shifts of 0°, 90°, 180° and 270° in turn), and the phases of the hologram pixels are shown in Fig. 8(c) (top middle). After setting the normalized amplitude and phase of different pixels of the acoustic hologram, the energy distribution of the finally reconstructed acoustic holographic sound field is shown in Figure 8(c) (upper right). image.
图8(b)为声学全息图重构出“星”型目标声学图像的示意图,虚线框为声学全息图局部放大图,作为展示,这里不同像素点处通过针对性地旋转声学涡旋超构表面改变其空间取向实现像素点相位调制,像素点的声学涡旋超构表面旋转角度与图8(a)相同,仍为基于步骤4所得到的复振幅全息图的振幅(见图8(c)(左图)),当倏逝声学涡旋的拓扑荷数为-1时(扬声器阵列的4个微型扬声器相对应驱动电信号依次具有0°,-90°,-180°和-270°相移),全息图像素点的相位如图8(c)(中下)所示,该相位分布为图8(c)(中上)的共轭。设置好声学全息图不同像素点的归一化振幅和相位,最终重构出的声学全息声场的能量分布如图8(c)(右下)所示,可以清晰地辨认出“星”型目标声学图像。Figure 8(b) is a schematic diagram of reconstructing the acoustic image of a "star"-shaped target from an acoustic hologram. The dotted box is a partially enlarged image of the acoustic hologram. The surface changes its spatial orientation to realize pixel phase modulation, and the rotation angle of the acoustic vortex metasurface of the pixel is the same as that in Fig. 8(a), which is still Based on the amplitude of the complex amplitude hologram obtained in step 4 (see Figure 8(c) (left figure)), when the topological charge of the evanescent acoustic vortex is -1 (the four micro-speakers of the speaker array correspond to drive The electrical signal has 0°, -90°, -180° and -270° phase shift in turn), the phase of the hologram pixel point is shown in Fig. 8(c) (middle bottom), and the phase distribution is Fig. 8(c) (middle upper) conjugate. After setting the normalized amplitude and phase of different pixels of the acoustic hologram, the energy distribution of the finally reconstructed acoustic holographic sound field is shown in Figure 8(c) (lower right), and the "star" target can be clearly identified Acoustic image.
综上所述,本实例提供了一种基于近场轨道角动量转换的声波相位调制及声场重构方法,利用倏逝声学涡旋与声学涡旋超构表面的近场耦合相互作用所实现的轨道角动量转换过程,获得声波传输相位的连续可控调制。再利用点源算法,得到两幅目标声学图像叠加下的全息图复振幅分布,对应调节不同像素点处扬声器阵列的驱动电压幅值和声学涡旋超构表面的旋转角度,最终通过调整倏逝声学涡旋拓扑荷数(1或-1)重构出不同的目标声学图像。In summary, this example provides an acoustic wave phase modulation and acoustic field reconstruction method based on near-field orbital angular momentum conversion, which is realized by the near-field coupling interaction between the evanescent acoustic vortex and the acoustic vortex metasurface The orbital angular momentum conversion process obtains a continuous controllable modulation of the acoustic transmission phase. Then use the point source algorithm to obtain the complex amplitude distribution of the hologram under the superimposition of two target acoustic images, correspondingly adjust the driving voltage amplitude of the loudspeaker array at different pixel points and the rotation angle of the acoustic vortex metasurface, and finally adjust the evanescent The acoustic vortex topological charge (1 or -1) reconstructs different target acoustic images.
以上所述的具体描述,对发明的目的、技术方案和有益效果进行了进一步详细说明,所应理解的是,以上所述仅为本发明的具体实施例而已,并不用于限定本发明的保护范围,凡在本发明的精神和原则之内,所做的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The specific description above further elaborates the purpose, technical solution and beneficial effect of the invention. It should be understood that the above description is only a specific embodiment of the present invention and is not used to limit the protection of the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.
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