CN111785244A - An Acoustic Focusing Fractional Vortex Field Emitter - Google Patents

An Acoustic Focusing Fractional Vortex Field Emitter Download PDF

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CN111785244A
CN111785244A CN202010641570.4A CN202010641570A CN111785244A CN 111785244 A CN111785244 A CN 111785244A CN 202010641570 A CN202010641570 A CN 202010641570A CN 111785244 A CN111785244 A CN 111785244A
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helical grooves
grooves
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spiral
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陈帝超
吴大建
贾雨柔
朱兴凤
魏琦
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Nanjing Normal University
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    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
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Abstract

本发明公开了一种声学聚焦分数涡旋场发射器,包括一个结构板,所述结构板上设置有按同中心轴方式设置的第一组螺线槽以及第二组螺线槽,第二组螺线槽位于第一组螺线槽的外围,且在第二组螺线槽距离中心轴最近的螺旋线与第一组螺线槽距离中心轴最远的螺旋线之间设置预设间距。本发明当入射超声波通过该声学聚焦分数涡旋场发射器时,透射声场将聚焦超声波产生分数涡旋场;在空间中对涡旋进行聚焦的同时,通过调整第一组阿基米德螺线槽以及第二组阿基米德螺线槽的数目,可以实现不同拓扑荷数的分数涡旋;本结构也可以依据不同的入射超声波长进行任意调制。本发明是一种被动的无源人工结构,仅依靠本身的结构就能对透射声场进行调制,应用广泛。

Figure 202010641570

The invention discloses an acoustic focusing fractional vortex field transmitter, comprising a structural plate, wherein a first group of helical grooves and a second group of helical grooves arranged in a concentric axis manner are arranged on the structural plate, and a second group of helical grooves is arranged on the structural plate. The set of helical grooves is located on the periphery of the first set of helical grooves, and a preset distance is set between the helical line of the second set of helical grooves closest to the central axis and the helical line of the first set of helical grooves farthest from the central axis . In the present invention, when the incident ultrasonic wave passes through the acoustically focused fractional vortex field transmitter, the transmitted sound field will focus the ultrasonic wave to generate a fractional vortex field; while focusing the vortex in space, by adjusting the first group of Archimedes spirals The number of grooves and the second group of Archimedes spiral grooves can realize fractional vortices with different topological charges; the structure can also be arbitrarily modulated according to different incident ultrasonic wave lengths. The invention is a passive passive artificial structure, which can modulate the transmission sound field only by its own structure, and is widely used.

Figure 202010641570

Description

一种声学聚焦分数涡旋场发射器An Acoustic Focusing Fractional Vortex Field Emitter

技术领域technical field

本发明涉及一种声学聚焦分数涡旋场发射器,属于声学器件领域。The invention relates to an acoustic focusing fractional vortex field transmitter, which belongs to the field of acoustic devices.

背景技术Background technique

分数涡旋场具有径向相位分布不连续性的特点,在过去十年中引起了越来越多的关注。一方面分数涡旋场其不对称中空涡旋光束中具有较强的声强区域,可以在一定方向上产生力,这非常有利于捕获和操纵粒子。另一方面其携带着轨道角动量并且能够将轨道角动量传递给吸收的物体,从而使物体发生旋转。在此基础上,声学聚焦分数涡旋场由于它可以提供更强的捕获力,更大的力矩和更深的渗透深度,使得它在实际应用中具有非常重要的价值。如何设计一种高效、简单、低成本的声学聚焦分数涡旋场发射器一直是相关研究领域的一个热点问题。Fractional vortex fields, characterized by radial phase distribution discontinuities, have attracted increasing attention over the past decade. On the one hand, the fractional vortex field has a strong sound intensity region in its asymmetric hollow vortex beam, which can generate force in a certain direction, which is very beneficial for trapping and manipulating particles. On the other hand, it carries orbital angular momentum and is able to transfer the orbital angular momentum to the absorbing object, thereby causing the object to rotate. On this basis, the acoustically focused fractional vortex field has very important value in practical applications because it can provide stronger trapping force, larger moment and deeper penetration depth. How to design an efficient, simple and low-cost acoustically focused fractional vortex field emitter has always been a hot issue in related research fields.

目前产生声学聚焦涡旋场的方式主要依赖于主动换能器阵列,通过电学手段控制每一个主动换能器的相位偏移,并且通过物理改变主动换能器的排布形状,使得它整体的相位满足分数涡旋场相位的要求同时它的弯曲弧面使得声波满足声波聚焦的要求,从而可以将整个换能器阵列看成一个聚焦分数涡旋场发射器。其所产生的总声场是所有主动换能器声场的叠加。At present, the method of generating the acoustically focused vortex field mainly relies on the active transducer array. The phase shift of each active transducer is controlled by electrical means, and the arrangement shape of the active transducer is physically changed, so that its overall The phase satisfies the phase requirements of the fractional vortex field, and its curved arc surface makes the sound wave meet the requirements of sound wave focusing, so that the entire transducer array can be regarded as a focused fractional vortex field transmitter. The resulting total sound field is the superposition of all active transducer sound fields.

然而,依赖于主动换能器阵列产生的声学聚焦涡旋场也存在着自身的缺陷和不足。首先,为了产生声学聚焦涡旋场通常需要几十个几百个甚至上千个主动换能器,通过复杂的电路系统来控制每一个主动换能器的振幅和相位,巨大的设计成本和繁琐的操作流程极大的限制了它的应用与发展。其次,为了达到声学聚焦分数涡旋场的效果,换能器阵列通常要摆成一个弧面,这也限制了它在某些特殊场景中的应用(例如需要一个平面结构来实现声学聚焦分数涡旋场)。因此通过一个简单的人工结构对换能器发射的入射超声波进行调制从而产生不同拓扑荷数的聚焦声分数涡旋是非常有必要和重要的。However, relying on the acoustically focused vortex field generated by the active transducer array also has its own shortcomings and deficiencies. First, in order to generate the acoustically focused vortex field, dozens, hundreds or even thousands of active transducers are usually required, and the amplitude and phase of each active transducer are controlled by a complex circuit system, resulting in huge design cost and cumbersomeness. Its operation process greatly limits its application and development. Secondly, in order to achieve the effect of the acoustically focused fractional vortex field, the transducer array is usually arranged into a curved surface, which also limits its application in some special scenarios (for example, a planar structure is required to realize the acoustically focused fractional vortex field). swirl field). Therefore, it is very necessary and important to modulate the incident ultrasonic waves emitted by the transducer through a simple artificial structure to generate focused acoustic fractional vortices with different topological charges.

发明内容SUMMARY OF THE INVENTION

本发明提供了一种可以产生声学聚焦分数涡旋场的发射器,声波通过在螺线槽里的特殊衍射和透射声波之间的相互干涉能够在传播方向上产生不同拓扑荷数的聚焦声分数涡旋场。The invention provides a transmitter capable of generating an acoustically focused fractional vortex field. The acoustic waves can generate focused acoustic fractions with different topological charges in the propagation direction through the mutual interference between the special diffraction in the helical groove and the transmitted acoustic waves. vortex field.

为了实现上述的目的,本发明的声学聚焦分数涡旋场发射器,包括了一个结构板,所述结构板上设置有同中心轴设置的第一组螺线槽以及第二组螺线槽,第二组螺线槽位于第一组螺线槽的外围,且第二组螺线槽距离中心轴最近的螺旋线与第一组螺线槽距离中心轴最远的螺旋线之间设置预设间距。In order to achieve the above-mentioned purpose, the acoustically focused fractional vortex field transmitter of the present invention includes a structural plate, and the structural plate is provided with a first group of helical grooves and a second group of helical grooves arranged concentrically, The second group of helical grooves is located on the periphery of the first group of helical grooves, and a preset is set between the helical line of the second group of helical grooves closest to the central axis and the helical line of the first group of helical grooves farthest from the central axis spacing.

优选地,所述结构板的声阻抗与背景媒质的声阻抗至少相差20倍以上。Preferably, the acoustic impedance of the structural plate is at least 20 times different from the acoustic impedance of the background medium.

优选地所述第一组螺线槽以及第二组螺线槽均包括一个螺线槽,第一组螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000021
和rII(θ)=rI(θ)+d,第二组螺线槽的两根螺线rIII和rIV的方程为
Figure BDA0002571670290000022
和rIV(θ)=rIII(θ)+d,其中d设置为第一组螺线槽以及第二组螺线槽的宽度,所述宽度小于入射波长,g设置为入射波长,r0为第一组螺线槽的初始半径,r1为第二组德螺线槽的初始半径,N为第一组螺线槽以及第二组螺线槽中两根螺线的圈数;m为拓扑荷数,在0到1之间任意取值;θ的取值从0到2π/m。Preferably, the first group of spiral grooves and the second group of spiral grooves each include one spiral groove, and the equations of the two spirals r I and r II of the first group of spiral grooves are respectively:
Figure BDA0002571670290000021
and r II (θ)=r I (θ)+d, the equations of the two spirals r III and r IV of the second set of spiral grooves are
Figure BDA0002571670290000022
and r IV (θ) = r III (θ) + d, where d is set to the width of the first set of helical grooves and the second set of helical grooves that is less than the incident wavelength, g is set to the incident wavelength, r 0 is the initial radius of the first group of helical grooves, r 1 is the initial radius of the second group of helical grooves, N is the number of turns of the first group of helical grooves and the two spirals in the second group of helical grooves; m is the topological charge, which can be any value between 0 and 1; the value of θ ranges from 0 to 2π/m.

优选地,所述第一组螺线槽以及第二组螺线槽均包括2个螺线槽,其中,第一组螺线槽的第1个螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000023
和rII(θ)=rI(θ)+d,此时θ的取值从0到2π/m;m为拓扑荷数,在1到2之间任意取值;r0为第一组螺线槽的初始半径,第一组螺线槽的第2个螺线槽的两根螺线rIII和rIV的方程分别为
Figure BDA0002571670290000024
和rIV(θ)=rIII(θ)+d,此时θ的取值从2π/m到2π,Preferably, the first group of spiral grooves and the second group of spiral grooves each include two spiral grooves, wherein the two spiral grooves r I and r of the first spiral groove of the first group of spiral grooves The equations of II are
Figure BDA0002571670290000023
and r II (θ)=r I (θ)+d, at this time, the value of θ ranges from 0 to 2π/m; m is the topological charge, which can be any value between 1 and 2; r 0 is the first group The initial radius of the helical groove, the equations of the two spirals r III and r IV of the second helical groove of the first group of helical grooves are respectively:
Figure BDA0002571670290000024
and r IV (θ)=r III (θ)+d, at this time, the value of θ ranges from 2π/m to 2π,

第二组螺线槽的第1个螺线槽的两根螺线r′I和r′II的方程分别为

Figure BDA0002571670290000025
和r′II(θ)=r′I(θ)+d,此时θ的取值从0到2π/m;r1为第二组螺线槽的初始半径,第二组螺线槽的第2个螺线槽的两根螺线r′III和r′IV的方程分别为
Figure BDA0002571670290000026
和r′IV(θ)=r′III(θ)+d,此时θ的取值从0到2π/m;其中d设置为第一组螺线槽以及第二组螺线槽的宽度,所述宽度小于入射波长,N为第一组螺线槽以及第二组螺线槽的圈数,g设置为入射波长。The equations of the two spirals r' I and r' II of the first spiral slot of the second group of spiral slots are respectively:
Figure BDA0002571670290000025
and r′ II (θ)=r′ I (θ)+d, at this time, the value of θ ranges from 0 to 2π/m; r 1 is the initial radius of the second group of helical grooves. The equations of the two spirals r' III and r' IV of the second spiral slot are respectively
Figure BDA0002571670290000026
and r′ IV (θ)=r′ III (θ)+d, at this time, the value of θ ranges from 0 to 2π/m; where d is set to the width of the first group of helical grooves and the second group of helical grooves, The width is smaller than the incident wavelength, N is the number of turns of the first group of helical grooves and the second group of helical grooves, and g is set to the incident wavelength.

优选地,所述一组螺线槽以及第二组螺线槽均包括3个螺线槽,其中,第一组螺线槽的第M个螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000027
和rII(θ)=rI(θ)+d,此时θ的取值从2(M-1)π/m到2Mπ/m,m为拓扑荷数,在2到3之间任意取值,r0为第一组螺线槽的初始半径,M≤2,M为正整数;第一组螺线槽的第3个螺线槽的两根螺线rIII和rIV的方程分别为
Figure BDA0002571670290000031
和rIV(θ)=rIII(θ)+d,此时θ的取值从4π/m到2π;Preferably, the set of helical grooves and the second set of helical grooves each include three helical grooves, wherein the two helical grooves r I and r II of the Mth helical groove of the first set of helical grooves The equations are
Figure BDA0002571670290000027
and r II (θ)=r I (θ)+d, at this time, the value of θ ranges from 2(M-1)π/m to 2Mπ/m, where m is the topological charge, which can be arbitrarily chosen between 2 and 3 value, r 0 is the initial radius of the first group of helical grooves, M≤2, M is a positive integer; the equations of the two spirals r III and r IV of the third helical groove of the first group of helical grooves are respectively for
Figure BDA0002571670290000031
and r IV (θ)=r III (θ)+d, the value of θ is from 4π/m to 2π at this time;

第二组螺线槽的第M个螺线槽的两根螺线r′I和r′II的方程分别为

Figure BDA0002571670290000032
和r′II(θ)=r′I(θ)+d,r1为第二组螺线槽的初始半径;第二组螺线槽的3个螺线槽的两根螺线r′III和r′IV的方程分别为
Figure BDA0002571670290000033
和r′IV(θ)=r′III(θ)+d,其中d设置为第一组螺线槽以及第二组螺线槽的宽度,所述宽度小于入射波长,N为第一组螺线槽以及第二组螺线槽的圈数,g设置为入射波长。The equations of the two spirals r' I and r' II of the M-th spiral slot of the second group of spiral slots are respectively:
Figure BDA0002571670290000032
and r′ II (θ)=r′ I (θ)+d, r 1 is the initial radius of the second group of helical grooves; the two spirals r′ III of the three helical grooves of the second group of helical grooves and the equations of r′ IV are respectively
Figure BDA0002571670290000033
and r′ IV (θ)=r′ III (θ)+d, where d is set to the width of the first set of helical grooves and the second set of helical grooves, the widths being smaller than the incident wavelength, and N is the first set of helical grooves. The number of turns of the wire groove and the second set of helical grooves, and g is set to the incident wavelength.

优选地,所述一组螺线槽以及第二组螺线槽均包括4个螺线槽,其中,第一组螺线槽的第M个螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000034
和rII(θ)=rI(θ)+d,此时θ的取值从2(M-1)π/m到2Mπ/m,m为拓扑荷数,在3到4之间任意取值,r0为第一组螺线槽的初始半径,M≤3,M为正整数;第一组螺线槽的第4个螺线槽的两根螺线rIII和rIV的方程分别为
Figure BDA0002571670290000035
和rIV(θ)=rIII(θ)+d,此时θ的取值从6π/m到2π;Preferably, the set of helical grooves and the second set of helical grooves each include 4 helical grooves, wherein the two helical grooves r I and r II of the Mth helical groove of the first set of helical grooves The equations are
Figure BDA0002571670290000034
And r II (θ)=r I (θ)+d, the value of θ is from 2(M-1)π/m to 2Mπ/m, m is the topological charge, which can be arbitrarily chosen between 3 and 4 value, r 0 is the initial radius of the first group of helical grooves, M≤3, M is a positive integer; the equations of the two spirals r III and r IV of the fourth helical groove of the first group of helical grooves are respectively for
Figure BDA0002571670290000035
and r IV (θ)=r III (θ)+d, the value of θ is from 6π/m to 2π at this time;

第二组螺线槽的第M个螺线槽的两根螺线r′I和r′II的方程分别为

Figure BDA0002571670290000036
和r′II(θ)=r′I(θ)+d,r1为第二组螺线槽的初始半径,第二组螺线槽的4个螺线槽的两根螺线r′III和r′IV的方程分别为
Figure BDA0002571670290000037
和r′IV(θ)=r′III(θ)+d,其中d设置为第一组螺线槽以及第二组螺线槽的宽度,所述宽度小于入射波长,N为第一组螺线槽以及第二组螺线槽的圈数,g设置为入射波长。The equations of the two spirals r' I and r' II of the M-th spiral slot of the second group of spiral slots are respectively:
Figure BDA0002571670290000036
and r′ II (θ)=r′ I (θ)+d, r 1 is the initial radius of the second group of helical grooves, and the two spirals r′ III of the four helical grooves of the second group of helical grooves and the equations of r′ IV are respectively
Figure BDA0002571670290000037
and r′ IV (θ)=r′ III (θ)+d, where d is set to the width of the first group of helical grooves and the second group of helical grooves, the widths being smaller than the incident wavelength, and N is the first group of helical grooves. The number of turns of the groove and the second set of helical grooves, g is set to the incident wavelength.

优选地,第一组螺线槽为阿基米德螺线槽。Preferably, the first group of spiral grooves are Archimedes spiral grooves.

优选地,第二组螺线槽为阿基米德螺线槽。Preferably, the second group of spiral grooves are Archimedes spiral grooves.

优选地,所述预设间距为半个入射波长。Preferably, the preset distance is half the incident wavelength.

本发明当入射超声波通过该聚焦涡旋场发射器时,透射声场将聚焦声波产生分数涡旋场;在空间中对涡旋进行聚焦的同时,通过调整第一组螺线槽以及第二组螺线槽的数目,可以实现不同拓扑荷数的分数涡旋;本声学聚焦分数涡旋场发射器也可以依据不同的入射超声波长进行任意调制。本发明是一种被动的无源人工结构,仅依靠本身的结构就能对透射声场进行调制,应用广泛。In the present invention, when the incident ultrasonic wave passes through the focused vortex field transmitter, the transmitted sound field will focus the sound wave to generate a fractional vortex field; while focusing the vortex in space, by adjusting the first group of helical grooves and the second group of helical grooves The number of grooves can realize fractional vortex with different topological charges; the acoustically focused fractional vortex field transmitter can also be arbitrarily modulated according to different incident ultrasonic wave lengths. The invention is a passive passive artificial structure, which can modulate the transmission sound field only by its own structure, and is widely used.

附图说明Description of drawings

图1为本发明声学聚焦涡旋场发射器实施例在x-z平面的原理示意图,其中图1(a)为在x-y平面的原理示意图,图1(b)为侧面工作示意图;1 is a schematic diagram of the principle of an embodiment of an acoustic focusing vortex field transmitter of the present invention in the x-z plane, wherein FIG. 1(a) is a schematic diagram of the principle in the x-y plane, and FIG. 1(b) is a schematic diagram of the side operation;

图2为产生拓扑荷数为0.5的声学聚焦分数涡旋场发射器在x-y平面的设计示意图;Figure 2 is a schematic diagram of the design of an acoustically focused fractional vortex field emitter with a topological charge of 0.5 in the x-y plane;

图3为产生拓扑荷数为1.25的声学聚焦分数涡旋场发射器在x-y平面的设计示意图;Figure 3 is a schematic diagram of the design of an acoustically focused fractional vortex field emitter with a topological charge of 1.25 in the x-y plane;

图4为产生拓扑荷数为1.5的声学聚焦分数涡旋场发射器在x-y平面的设计示意图;Figure 4 is a schematic diagram of the design of an acoustically focused fractional vortex field emitter with a topological charge of 1.5 in the x-y plane;

图5为产生拓扑荷数为1.75的声学聚焦分数涡旋场发射器在x-y平面的设计示意图;Figure 5 is a schematic diagram of the design of an acoustically focused fractional vortex field emitter with a topological charge of 1.75 in the x-y plane;

图6为产生拓扑荷数为2.5的声学聚焦分数涡旋场发射器在x-y平面的设计示意图;Figure 6 is a schematic diagram of the design of an acoustically focused fractional vortex field emitter with a topological charge of 2.5 in the x-y plane;

图7为产生拓扑荷数为3.5的声学聚焦分数涡旋场发射器在x-y平面的设计示意图;Figure 7 is a schematic diagram of the design of an acoustically focused fractional vortex field emitter with a topological charge of 3.5 in the x-y plane;

图8为图2所示结构的声学聚焦分数涡旋场发射器在聚焦平面的仿真分布图,其中图8(a)为强度分布图,图8(b)为相位分布图;Fig. 8 is a simulation distribution diagram of the acoustically focused fractional vortex field emitter of the structure shown in Fig. 2 on the focal plane, wherein Fig. 8(a) is an intensity distribution diagram, and Fig. 8(b) is a phase distribution diagram;

图9为图3所示结构的声学聚焦分数涡旋场发射器在聚焦平面的仿真分布图,其中图9(a)为强度分布图,图9(b)为相位分布图;Fig. 9 is a simulation distribution diagram of the acoustically focused fractional vortex field emitter of the structure shown in Fig. 3 on the focal plane, wherein Fig. 9(a) is an intensity distribution diagram, and Fig. 9(b) is a phase distribution diagram;

图10为图4所示结构的声学聚焦分数涡旋场发射器在聚焦平面的仿真分布图,其中图10(a)为强度分布图,图10(b)为相位分布图;Fig. 10 is a simulation distribution diagram of the acoustically focused fractional vortex field emitter of the structure shown in Fig. 4 on the focal plane, wherein Fig. 10(a) is an intensity distribution diagram, and Fig. 10(b) is a phase distribution diagram;

图11为图5所示结构的声学聚焦分数涡旋场发射器在聚焦平面的仿真分布图,其中图11(a)为强度分布图,图11(b)为相位分布图;Fig. 11 is a simulated distribution diagram of the acoustically focused fractional vortex field emitter of the structure shown in Fig. 5 in the focal plane, wherein Fig. 11(a) is an intensity distribution diagram, and Fig. 11(b) is a phase distribution diagram;

图12为图6所示结构的声学聚焦分数涡旋场发射器在聚焦平面的仿真分布图,其中图12(a)为强度分布图,图12(b)为相位分布图;Fig. 12 is a simulation distribution diagram of the acoustically focused fractional vortex field emitter of the structure shown in Fig. 6 in the focal plane, wherein Fig. 12(a) is an intensity distribution diagram, and Fig. 12(b) is a phase distribution diagram;

图13为图7所示结构的声学聚焦分数涡旋场发射器在聚焦平面的仿真分布图,其中图13(a)为强度分布图,图13(b)为相位分布图;以及Fig. 13 is a simulation distribution diagram of the acoustically focused fractional vortex field emitter of the structure shown in Fig. 7 in the focal plane, wherein Fig. 13(a) is an intensity distribution diagram, and Fig. 13(b) is a phase distribution diagram; and

图14(a),图14(b),图14(c),和图14(d)分别为拓扑荷数为0.5,1.5,2.5,3.5的聚焦涡旋场在x-z平面上的强度分布图。Fig. 14(a), Fig. 14(b), Fig. 14(c), and Fig. 14(d) are the intensity distributions of the focused vortex field on the x-z plane with topological charges of 0.5, 1.5, 2.5, and 3.5, respectively .

具体实施方式Detailed ways

下面结合附图对本发明作进一步的说明。The present invention will be further described below in conjunction with the accompanying drawings.

如图1所示,为本发明声学聚焦分数涡旋场发射器实施例的原理示意图,图1(a)中显示了声学聚焦分数涡旋场发射器在x-y平面的截面示意图,本实施例包括一个结构板,所述结构板上设置有同中心轴设置的第一组螺线槽,包括但不限于阿基米德螺线槽(图中用Part I表示)以及第二组阿基米德螺线槽(图中用Part II表示),第二组螺线槽,包括但不限于阿基米德螺线槽位于第一组阿基米德螺线槽的外围,且第二组阿基米德螺线槽距离中心轴最近的螺旋线与第一组阿基米德螺线槽距离中心轴最远的螺旋线间隔为半个入射波长。图1(a)中显示了声学聚焦分数涡旋场发射器侧面工作示意图,当声波沿z轴方向垂直入射到发射器,部分声波透过阿基米德螺线槽而另一部分则被结构板的硬表面所反射,透过每组阿基米德螺线槽的声波都会形成一个分数涡旋。当第二组阿基米德螺线槽位于第一组阿基米德螺线槽的外围,且第二组阿基米德螺线槽距离中心轴最近的螺旋线与第一组阿基米德螺线槽距离中心轴最远的螺旋线之间的距离为预设间距,包括但不限于0.5个波长(图中用0.5g表示)时,两组阿基米德螺线槽之间的相位差应该为π。同时从两组阿基米德螺线槽到聚焦平面的路程差满足半个波长,因此透射声波透过两组阿基米德螺线槽总的相位差为2π。在这种情况下,透过两组阿基米德螺线槽的声分数涡旋将在聚焦面内发生强烈的建设性干涉,从而就实现了聚焦声分数涡旋。其中,当预设间距为半波长的整数倍时,产生的聚焦声分数涡旋最强,当预设间距为波长的整数倍时,不会产生的聚焦声分数涡旋,当预设间距为不为半波长和波长的整数倍时,可以产生聚焦声分数涡旋且聚焦位置会随预设间距的改动而发生移动。As shown in FIG. 1, it is a schematic diagram of the principle of an embodiment of the acoustically focused fractional vortex field transmitter of the present invention. FIG. 1(a) shows a schematic cross-sectional view of the acoustically focused fractional vortex field transmitter in the x-y plane. This embodiment includes A structural plate, the structural plate is provided with a first group of spiral grooves arranged concentrically, including but not limited to Archimedes spiral grooves (represented by Part I in the figure) and a second group of Archimedes The spiral groove (represented by Part II in the figure), the second group of spiral grooves, including but not limited to the Archimedes spiral grooves are located on the periphery of the first group of Archimedes spiral grooves, and the second group of Archimedes spiral grooves The distance between the helix of the Meadian helical groove closest to the central axis and the helix of the first group of Archimedes helical grooves farthest from the central axis is half the incident wavelength. Figure 1(a) shows a schematic diagram of the side operation of the acoustically focused fractional vortex field transmitter. When the acoustic wave is perpendicularly incident on the transmitter along the z-axis direction, part of the acoustic wave passes through the Archimedes spiral groove and the other part is absorbed by the structural plate. A fractional vortex is formed by the sound waves that pass through each set of Archimedes' spiral grooves, reflected off of the hard surface. When the second group of Archimedes spiral grooves is located on the periphery of the first group of Archimedes spiral grooves, and the helix closest to the central axis of the second group of Archimedes spiral grooves is the same as the first group of Archimedes spiral grooves The distance between the spiral grooves farthest from the central axis is a preset distance, including but not limited to 0.5 wavelengths (represented by 0.5g in the figure), the distance between the two groups of Archimedes spiral grooves. The phase difference should be π. At the same time, the path difference from the two groups of Archimedes spiral grooves to the focusing plane satisfies half a wavelength, so the total phase difference of the transmitted acoustic waves through the two groups of Archimedes spiral grooves is 2π. In this case, the acoustic fractional vortices passing through the two sets of Archimedes spiral grooves will have strong constructive interference in the focusing plane, thus realizing the focused acoustic fractional vortices. Among them, when the preset spacing is an integer multiple of the half wavelength, the generated focused sound fractional vortex is the strongest. When the preset spacing is an integer multiple of the wavelength, the focused sound fractional vortex will not be generated. When the preset spacing is When it is not the half wavelength and the integer multiple of the wavelength, the focused acoustic fractional vortex can be generated and the focus position will move with the change of the preset distance.

如图2所示,在结构板上开设两组阿基米德螺线槽,每组阿基米德螺线槽上有一个螺线槽,其中第一组阿基米德螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000051
和rII(θ)=rI(θ)+d,第二组阿基米德螺线槽的两根螺线rIII和rIV的方程为
Figure BDA0002571670290000052
和rIV(θ)=rIII(θ)+d。具体实现时,可以但不限于固定d=0.5mm,N=4,g=1.5mm,r0=12mm,r1=18.75mm,θ的取值从0到2π/0.5。其中,内、外两根螺线和以与中心轴的距离远近来定义,内螺线相对于外螺线与中心轴的距离近(以下各实施例同)。As shown in Figure 2, two sets of Archimedes spiral grooves are opened on the structural board, each group of Archimedes spiral grooves has a spiral groove, and two sets of Archimedes spiral grooves in the first group The equations of the root spirals r I and r II are respectively
Figure BDA0002571670290000051
and r II (θ)=r I (θ)+d, the equations of the two spirals r III and r IV of the second set of Archimedes' spiral grooves are
Figure BDA0002571670290000052
and r IV (θ)=r III (θ)+d. In specific implementation, d=0.5 mm, N=4, g=1.5 mm, r 0 =12 mm, r 1 =18.75 mm may be fixed but not limited to, and the value of θ ranges from 0 to 2π/0.5. The sum of the inner and outer spirals is defined by the distance from the central axis, and the inner spiral is closer to the central axis than the outer spiral (the same in the following embodiments).

如图3所示,在结构板上开设两组阿基米德螺线槽,每组阿基米德螺线槽有两个螺线槽,第一组阿基米德螺线槽的第1个螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000061
和rII(θ)=rI(θ)+d,此时θ的取值从0到2π/1.25。第一组阿基米德螺线槽的第2个螺线槽的两根螺线rIII和rIV的方程分别为
Figure BDA0002571670290000062
和rIV(θ)=rIII(θ)+d,此时θ的取值从2π/1.25到2π。第二组阿基米德螺线槽除了初始半径r1与第一组阿基米德螺线槽r0不同,其它与第一组阿基米德螺线槽有相同的形式。具体实现时,可以但不限于固定d=0.5mm,N=4,g=1.5mm,r0=12mm,r1=18.75mm。其中,内、外两根螺线和以与中心轴的距离远近来定义,内螺线相对于外螺线与中心轴的距离近(以下各实施例同)。As shown in Figure 3, two sets of Archimedes spiral grooves are opened on the structural board, each group of Archimedes spiral grooves has two spiral grooves, and the first group of Archimedes spiral grooves has two spiral grooves. The equations of the two spirals r I and r II of each spiral slot are
Figure BDA0002571670290000061
And r II (θ)=r I (θ)+d, the value of θ is from 0 to 2π/1.25 at this time. The equations of the two spirals r III and r IV of the second spiral groove of the first group of Archimedes spiral grooves are respectively
Figure BDA0002571670290000062
and r IV (θ)=r III (θ)+d, where the value of θ ranges from 2π/1.25 to 2π. The second group of Archimedes spiral grooves has the same form as the first group of Archimedes spiral grooves except that the initial radius r 1 is different from that of the first group of Archimedes spiral grooves r 0 . In specific implementation, d=0.5 mm, N=4, g=1.5 mm, r 0 =12 mm, and r 1 =18.75 mm may be fixed, but not limited to. The sum of the inner and outer spirals is defined by the distance from the central axis, and the inner spiral is closer to the central axis than the outer spiral (the same in the following embodiments).

如图4所示,在结构板上开设两组阿基米德螺线槽,每组阿基米德螺线槽有两个螺线槽,第一组阿基米德螺线槽的第1个螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000063
和rII(θ)=rI(θ)+d,此时θ的取值从0到2π/1.5。第一组阿基米德螺线槽的第2个螺线槽的两根螺线rIII和rIV的方程分别为
Figure BDA0002571670290000064
和rIV(θ)=rIII(θ)+d,此时θ的取值从2π/1.5到2π。第二组阿基米德螺线槽除了初始半径r1与第一组阿基米德螺线槽r0不同,其它与第一组阿基米德螺线槽有相同的形式。具体实现时,可以但不限于固定d=0.5mm,N=4,g=1.5mm,r0=12mm,r1=18.75mm。其中,内、外两根螺线和以与中心轴的距离远近来定义,内螺线相对于外螺线与中心轴的距离近(以下各实施例同)。As shown in Figure 4, two sets of Archimedes spiral grooves are opened on the structural plate, each group of Archimedes spiral grooves has two spiral grooves, and the first group of Archimedes spiral grooves has two spiral grooves. The equations of the two spirals r I and r II of each spiral slot are
Figure BDA0002571670290000063
And r II (θ)=r I (θ)+d, the value of θ is from 0 to 2π/1.5 at this time. The equations of the two spirals r III and r IV of the second spiral groove of the first group of Archimedes spiral grooves are respectively
Figure BDA0002571670290000064
and r IV (θ)=r III (θ)+d, where the value of θ ranges from 2π/1.5 to 2π. The second group of Archimedes spiral grooves has the same form as the first group of Archimedes spiral grooves except that the initial radius r 1 is different from that of the first group of Archimedes spiral grooves r 0 . In specific implementation, d=0.5 mm, N=4, g=1.5 mm, r 0 =12 mm, and r 1 =18.75 mm may be fixed, but not limited to. The sum of the inner and outer spirals is defined by the distance from the central axis, and the inner spiral is closer to the central axis than the outer spiral (the same in the following embodiments).

如图5所示,在结构板上开设两组阿基米德螺线槽,每组阿基米德螺线槽有两个螺线槽,第一组阿基米德螺线槽的第1个螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000065
和rII(θ)=rI(θ)+d,此时θ的取值从0到2π/1.75。第一组阿基米德螺线槽的第2个螺线槽的两根螺线rIII和rIV的方程分别为
Figure BDA0002571670290000071
和rIV(θ)=rIII(θ)+d,此时θ的取值从2π/1.75到2π。第二组阿基米德螺线槽除了初始半径r1与第一组阿基米德螺线槽r0不同,其它与第一组阿基米德螺线槽有相同的形式。具体实现时,可以但不限于固定d=0.5mm,N=4,g=1.5mm,r0=12mm,r1=18.75mm。其中,内、外两根螺线和以与中心轴的距离远近来定义,内螺线相对于外螺线与中心轴的距离近(以下各实施例同)。As shown in Figure 5, two sets of Archimedes spiral grooves are set on the structural board, each group of Archimedes spiral grooves has two spiral grooves, and the first group of Archimedes spiral grooves is the first The equations of the two spirals r I and r II of each spiral slot are
Figure BDA0002571670290000065
And r II (θ)=r I (θ)+d, the value of θ is from 0 to 2π/1.75 at this time. The equations of the two spirals r III and r IV of the second spiral groove of the first group of Archimedes spiral grooves are respectively
Figure BDA0002571670290000071
and r IV (θ)=r III (θ)+d, where the value of θ ranges from 2π/1.75 to 2π. The second group of Archimedes spiral grooves has the same form as the first group of Archimedes spiral grooves except that the initial radius r 1 is different from that of the first group of Archimedes spiral grooves r 0 . In specific implementation, d=0.5 mm, N=4, g=1.5 mm, r 0 =12 mm, and r 1 =18.75 mm may be fixed, but not limited to. The sum of the inner and outer spirals is defined by the distance from the central axis, and the inner spiral is closer to the central axis than the outer spiral (the same in the following embodiments).

如图6所示,在结构板上开设两组阿基米德螺线槽,每组阿基米德螺线槽有三个螺线槽,第一组阿基米德螺线槽的第M个螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000072
和rII(θ)=rI(θ)+d,此时θ的取值从2(M-1)π/2.5到2Mπ/2.5,M≤2,M为正整数。第一组阿基米德螺线槽的第3个螺线槽的两根螺线rIII和rIV的方程分别为
Figure BDA0002571670290000073
和rIV(θ)=rIII(θ)+d,此时θ的取值从4π/2.5到2π。第二组阿基米德螺线槽除了初始半径r1与第一组阿基米德螺线槽r0不同,其它与第一组阿基米德螺线槽有相同的形式。具体实现时,可以但不限于固定d=0.5mm,N=4,g=1.5mm,r0=12mm,r1=18.75mm。其中,内、外两根螺线和以与中心轴的距离远近来定义,内螺线相对于外螺线与中心轴的距离近(以下各实施例同)。As shown in Figure 6, two sets of Archimedes spiral grooves are opened on the structural board, each group of Archimedes spiral grooves has three spiral grooves, and the Mth of the first group of Archimedes spiral grooves The equations of the two spirals r I and r II of the spiral groove are respectively
Figure BDA0002571670290000072
and r II (θ)=r I (θ)+d, at this time, the value of θ ranges from 2(M-1)π/2.5 to 2Mπ/2.5, M≤2, and M is a positive integer. The equations of the two spirals r III and r IV of the third spiral slot of the first group of Archimedes spiral slots are respectively
Figure BDA0002571670290000073
and r IV (θ)=r III (θ)+d, where the value of θ ranges from 4π/2.5 to 2π. The second group of Archimedes spiral grooves has the same form as the first group of Archimedes spiral grooves except that the initial radius r 1 is different from that of the first group of Archimedes spiral grooves r 0 . In specific implementation, d=0.5 mm, N=4, g=1.5 mm, r 0 =12 mm, and r 1 =18.75 mm may be fixed, but not limited to. The sum of the inner and outer spirals is defined by the distance from the central axis, and the inner spiral is closer to the central axis than the outer spiral (the same in the following embodiments).

如图7所示,在结构板上开设两组阿基米德螺线槽,每组阿基米德螺线槽有四个螺线槽,第一组阿基米德螺线槽的第M个螺线槽的两根螺线rI和rII的方程分别为

Figure BDA0002571670290000074
和rII(θ)=rI(θ)+d,此时θ的取值从2(M-1)π/3.5到2Mπ/3.5,M≤3,M为正整数。第一组螺线槽的第4个螺线槽的两根螺线rIII和rIV的方程分别为
Figure BDA0002571670290000075
和rIV(θ)=rIII(θ)+d,此时θ的取值从6π/3.5到2π。第二组阿基米德螺线槽除了初始半径r1与第一组阿基米德螺线槽r0不同,其它与第一组阿基米德螺线槽有相同的形式。具体实现时,可以但不限于固定d=0.5mm,N=4,g=1.5mm,r0=12mm,r1=18.75mm。其中,内、外两根螺线和以与中心轴的距离远近来定义,内螺线相对于外螺线与中心轴的距离近(以下各实施例同)。As shown in Figure 7, two sets of Archimedes spiral grooves are set on the structural board, each group of Archimedes spiral grooves has four spiral grooves, and the Mth of the first group of Archimedes spiral grooves is The equations of the two spirals r I and r II of each spiral slot are
Figure BDA0002571670290000074
and r II (θ)=r I (θ)+d, at this time, the value of θ ranges from 2(M-1)π/3.5 to 2Mπ/3.5, M≤3, and M is a positive integer. The equations of the two spirals r III and r IV of the fourth spiral slot of the first group of spiral slots are respectively
Figure BDA0002571670290000075
and r IV (θ)=r III (θ)+d, where the value of θ ranges from 6π/3.5 to 2π. The second group of Archimedes spiral grooves has the same form as the first group of Archimedes spiral grooves except that the initial radius r 1 is different from that of the first group of Archimedes spiral grooves r 0 . In specific implementation, d=0.5mm, N=4, g=1.5mm, r 0 =12mm, and r 1 =18.75mm may be fixed, but not limited to. The sum of the inner and outer spirals is defined by the distance from the central axis, and the inner spiral is closer to the central axis than the outer spiral (the same in the following embodiments).

对图2至图7的四种发射器进行仿真,背景介质设定为水,入射超声波的频率固定为1MHz,结构板的材料系数设为不锈钢。如图8至图13所示,分别为相应的结构板在1MHz、在聚焦平面(比如但不限定距离出射面5.4个入射波长(λ)的平面)内,产生的具有拓扑荷数为0.5,1.25,1.5,1.75,2.5,3.5的聚焦声分数涡旋的强度分布图和相位分布图。高强度的声能量集中分布在一个不对称的圆环上并随着拓扑荷数的增大不对称圆环周长逐步增大。同时,相应的相位分布在一个圆周内出现的相位奇点偏移和变多的相位变化,这些声学的特征与相应的拓扑荷数的声学分数涡旋场的性质相吻合,说明图2-图7所示六种结构的声学聚焦分数涡旋场发射器能够很好地在聚焦平面内调制入射超声波从而产生聚焦分数涡旋场。The four transmitters shown in Figures 2 to 7 are simulated, the background medium is set to water, the frequency of incident ultrasonic waves is fixed to 1MHz, and the material coefficient of the structural plate is set to stainless steel. As shown in Fig. 8 to Fig. 13 , the corresponding structural plates have a topological charge of 0.5 at 1 MHz and in a focal plane (such as but not limited to a plane 5.4 incident wavelengths (λ) away from the exit plane). Intensity profile and phase profile of the focused acoustic fractional vortex at 1.25, 1.5, 1.75, 2.5, 3.5. The high-intensity acoustic energy is concentrated on an asymmetrical ring and the circumference of the asymmetrical ring gradually increases with the increase of the topological charge. At the same time, the phase singularity shift and more and more phase changes appear in the corresponding phase distribution within a circle, and these acoustic characteristics are consistent with the properties of the acoustic fractional vortex field of the corresponding topological charge, illustrating Fig. 2-Fig. The acoustically focused fractional vortex field transmitters of the six structures shown in 7 can well modulate the incident ultrasonic waves in the focal plane to generate a focused fractional vortex field.

如图10所示,分别为相应的结构板在1MHz、在x-z平面内,产生的具有拓扑荷数为0.5,1.5,2.5,3.5的聚焦声分数涡旋的强度分布图。背景介质设定为水,入射声波的频率固定为1MHz,结构板的材料系数设为不锈钢。大部分的声能量集中在z方向有限长度的区域内并随着拓扑荷数的增大两个有限长度的区域会分裂成两个并且两个区域之间的距离会逐渐增大。这些声学的特征与相应的拓扑荷数的声学聚焦分数涡旋场的性质相吻合。这说明我们所设计的发射器能够在传播方向上调制入射超声波从而产生所要求的聚焦超声分数涡旋场。As shown in Figure 10, the intensity distributions of the focused acoustic fractional vortices with topological charges of 0.5, 1.5, 2.5, and 3.5 generated by the corresponding structural plates at 1 MHz and in the x-z plane, respectively. The background medium was set as water, the frequency of the incident acoustic wave was fixed at 1 MHz, and the material coefficient of the structural plate was set as stainless steel. Most of the acoustic energy is concentrated in a region of finite length in the z direction and with the increase of the topological charge, the two regions of finite length will split into two and the distance between the two regions will gradually increase. These acoustic features are consistent with the properties of the acoustically focused fractional vortex fields of the corresponding topological charges. This shows that our designed transmitter can modulate the incident ultrasonic wave in the propagation direction to generate the required focused ultrasonic fractional vortex field.

本发明各实施例的声学聚焦涡旋场发射器是一种平面形结构,它在传播方向上的厚度对结果几乎没有影响,可应根据实际需求改变发射器的厚度,当换能器发射的入射超声波通过该声学分数涡旋场发射器时,透射声场将产生超声聚焦分数涡旋;在空间中对分数涡旋进行聚焦的同时,通过调整每组的阿基米德螺线槽的数目,可以实现不同拓扑荷数的聚焦声分数涡旋。本声学涡旋场发射器各实施例也可以依据不同的入射超声波长进行任意调制。本发明是一种被动的无源人工结构,仅依靠本身的结构就能对透射声场进行调制,进而通过在螺线槽里的特殊衍射和透射声波之间的相互干涉能够在传播方向上产生不同拓扑荷数的声分数涡旋场,应用范围广。The acoustically focused vortex field transmitter of each embodiment of the present invention is a planar structure, and its thickness in the propagation direction has little effect on the results. The thickness of the transmitter can be changed according to actual needs. When the incident ultrasonic wave passes through the acoustic fractional vortex field transmitter, the transmitted sound field will generate an ultrasonic focused fractional vortex; while focusing the fractional vortex in space, by adjusting the number of Archimedes spiral grooves in each group, Focused acoustic fractional vortices with different topological charges can be realized. Each embodiment of the acoustic vortex field transmitter can also be arbitrarily modulated according to different incident ultrasonic wave lengths. The invention is a passive passive artificial structure, which can modulate the transmission sound field only by its own structure, and then can produce different propagation directions through the special diffraction in the spiral groove and the mutual interference between the transmission sound waves. Acoustic fractional vortex field of topological charge, which has a wide range of applications.

以上所述仅是本发明的优选实施方案,应当指出:对于技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进何润饰,这些改进和润饰也应视为本发明的保护范围。The above is only the preferred embodiment of the present invention, it should be pointed out: for those of ordinary skill in the technical field, on the premise of not departing from the principle of the present invention, several improvements and modifications can also be made, and these improvements and modifications should also be It is regarded as the protection scope of the present invention.

Claims (9)

1.一种声学聚焦分数涡旋场发射器,其特征在于:包括一个结构板,所述结构板上设置有按同中心轴方式设置的第一组螺线槽以及第二组螺线槽,第二组螺线槽位于第一组螺线槽的外围,且在第二组螺线槽距离中心轴最近的螺旋线与第一组螺线槽距离中心轴最远的螺旋线之间设置预设间距。1. an acoustic focusing fractional vortex field transmitter, characterized in that: comprising a structural plate, the structural plate is provided with a first group of helical grooves and a second group of helical grooves that are arranged in a concentric axis mode, The second group of helical grooves is located on the periphery of the first group of helical grooves, and a pre-set is set between the helical line of the second group of helical grooves closest to the central axis and the helical line of the first group of helical grooves farthest from the central axis Set the spacing. 2.根据权利要求1所述的声学聚焦分数涡旋场发射器,其特征在于:所述结构板的声阻抗与背景媒质的声阻抗至少相差20倍。2 . The acoustically focused fractional vortex field transmitter according to claim 1 , wherein the acoustic impedance of the structural plate is at least 20 times different from the acoustic impedance of the background medium. 3 . 3.根据权利要求2所述的声学聚焦分数涡旋场发射器,其特征在于:所述第一组螺线槽以及第二组螺线槽均包括一个螺线槽,第一组螺线槽的两根螺线rI和rII的方程分别为
Figure FDA0002571670280000011
和rII(θ)=rI(θ)+d,第二组螺线槽的两根螺线rIII和rIV的方程为
Figure FDA0002571670280000012
和rIV(θ)=rIII(θ)+d,其中d为第一组螺线槽以及第二组螺线槽的宽度,所述宽度小于入射波长,g为入射波长,r0为第一组螺线槽的初始半径,r1为第二组德螺线槽的初始半径,N为第一组螺线槽以及第二组螺线槽中两根螺线的圈数,m为拓扑荷数,在0到1之间任意取值;θ的取值0从到2π/m。
3. The acoustically focused fractional vortex field transmitter according to claim 2, wherein the first group of helical grooves and the second group of helical grooves each comprise one helical groove, and the first group of helical grooves The equations of the two spirals r I and r II are respectively
Figure FDA0002571670280000011
and r II (θ)=r I (θ)+d, the equations of the two spirals r III and r IV of the second set of spiral grooves are
Figure FDA0002571670280000012
and r IV (θ)=r III (θ)+d, where d is the width of the first set of helical grooves and the second set of helical grooves, and the width is smaller than the incident wavelength, g is the incident wavelength, and r 0 is the first The initial radius of a group of spiral grooves, r 1 is the initial radius of the second group of spiral grooves, N is the number of turns of the first group of spiral grooves and the two spiral grooves in the second group of spiral grooves, m is the topology The number of charges, which can be any value between 0 and 1; the value of θ ranges from 0 to 2π/m.
4.根据权利要求2所述的声学聚焦分数涡旋场发射器,其特征在于:所述第一组螺线槽以及第二组螺线槽均包括2个螺线槽,其中,4. The acoustically focused fractional vortex field transmitter according to claim 2, wherein the first group of helical grooves and the second group of helical grooves each comprise two helical grooves, wherein, 第一组螺线槽的第1个螺线槽的两根螺线rI和rII的方程分别为
Figure FDA0002571670280000013
和rII(θ)=rI(θ)+d,此时θ的取值从0到2π/m;m为拓扑荷数,在1到2之间任意取值;r0为第一组螺线槽的初始半径;第一组螺线槽的第2个螺线槽的两根螺线rIII和rIV的方程分别为
Figure FDA0002571670280000014
和rIV(θ)=rIII(θ)+d,此时θ的取值从2π/m到2π;
The equations of the two spirals r I and r II of the first spiral slot of the first group of spiral slots are respectively
Figure FDA0002571670280000013
and r II (θ)=r I (θ)+d, at this time, the value of θ ranges from 0 to 2π/m; m is the topological charge, which can be any value between 1 and 2; r 0 is the first group The initial radius of the helical groove; the equations of the two spirals r III and r IV of the second helical groove of the first group of helical grooves are respectively
Figure FDA0002571670280000014
and r IV (θ)=r III (θ)+d, the value of θ is from 2π/m to 2π at this time;
第二组螺线槽的第1个螺线槽的两根螺线r′I和r′II的方程分别为
Figure FDA0002571670280000015
和r′II(θ)=r′I(θ)+d,此时θ的取值从0到2π/m;r1为第二组螺线槽的初始半径,第二组螺线槽的第2个螺线槽的两根螺线r′III和r′IV的方程分别为
Figure FDA0002571670280000021
和r′IV(θ)=r′III(θ)+d,此时θ的取值从0到2π/m;其中d为第一组螺线槽以及第二组螺线槽的宽度,所述宽度小于入射波长,N为第一组螺线槽以及第二组螺线槽的圈数,g设置为入射波长。
The equations of the two spirals r' I and r' II of the first spiral slot of the second group of spiral slots are respectively:
Figure FDA0002571670280000015
and r′ II (θ)=r′ I (θ)+d, at this time, the value of θ ranges from 0 to 2π/m; r 1 is the initial radius of the second group of helical grooves. The equations of the two spirals r' III and r' IV of the second spiral slot are respectively
Figure FDA0002571670280000021
and r′ IV (θ)=r′ III (θ)+d, at this time, the value of θ ranges from 0 to 2π/m; where d is the width of the first group of spiral grooves and the second group of spiral grooves, so The width is smaller than the incident wavelength, N is the number of turns of the first group of helical grooves and the second group of helical grooves, and g is set to the incident wavelength.
5.根据权利要求2所述的声学聚焦分数涡旋场发射器,其特征在于:所述一组螺线槽以及第二组螺线槽均包括3个螺线槽,其中,5 . The acoustically focused fractional vortex field transmitter according to claim 2 , wherein the set of helical grooves and the second set of helical grooves each comprise 3 helical grooves, wherein, 6 . 第一组螺线槽的第M个螺线槽的两根螺线rI和rII的方程分别为
Figure FDA0002571670280000022
和rII(θ)=rI(θ)+d,此时θ的取值从2(M-1)π/m到2Mπ/m;m为拓扑荷数,在2到3之间任意取值;r0为第一组螺线槽的初始半径,M≤2,M为正整数;第一组螺线槽的3个螺线槽的两根螺线rIII和rIV的方程分别为
Figure FDA0002571670280000023
和rIV(θ)=rIII(θ)+d,此时θ的取值从4π/m到2π;
The equations of the two spirals r I and r II of the M-th spiral groove of the first group of spiral grooves are respectively:
Figure FDA0002571670280000022
and r II (θ)=r I (θ)+d, at this time, the value of θ ranges from 2(M-1)π/m to 2Mπ/m; m is the topological charge, which can be arbitrarily chosen between 2 and 3 value; r 0 is the initial radius of the first group of helical grooves, M≤2, M is a positive integer; the equations of the two spirals r III and r IV of the three helical grooves of the first group of helical grooves are respectively
Figure FDA0002571670280000023
and r IV (θ)=r III (θ)+d, the value of θ is from 4π/m to 2π at this time;
第二组螺线槽的第M个螺线槽的两根螺线r′I和r′II的方程分别为
Figure FDA0002571670280000024
和r′II(θ)=r′I(θ)+d,r1为第二组螺线槽的初始半径;第二组螺线槽的3个螺线槽的两根螺线r′III和r′IV的方程分别为
Figure FDA0002571670280000025
和r′IV(θ)=r′III(θ)+d;其中d设置为第一组螺线槽以及第二组螺线槽的宽度,所述宽度小于入射波长,N为第一组螺线槽以及第二组螺线槽的圈数,g设置为入射波长。
The equations of the two spirals r' I and r' II of the M-th spiral slot of the second group of spiral slots are respectively:
Figure FDA0002571670280000024
and r′ II (θ)=r′ I (θ)+d, r 1 is the initial radius of the second group of helical grooves; the two spirals r′ III of the three helical grooves of the second group of helical grooves and the equations of r′ IV are respectively
Figure FDA0002571670280000025
and r′ IV (θ)=r′ III (θ)+d; where d is set to the width of the first group of helical grooves and the second group of helical grooves, the width is less than the incident wavelength, and N is the first group of helical grooves. The number of turns of the wire groove and the second set of helical grooves, and g is set to the incident wavelength.
6.根据权利要求2所述的声学聚焦分数涡旋场发射器,其特征在于:所述一组螺线槽以及第二组螺线槽均包括4个螺线槽,其中,6. The acoustically focused fractional vortex field transmitter according to claim 2, wherein the set of helical grooves and the second set of helical grooves each comprise 4 helical grooves, wherein, 第一组螺线槽的第M个螺线槽的两根螺线rI和rII的方程分别为
Figure FDA0002571670280000026
和rII(θ)=rI(θ)+d,此时θ的取值从2(M-1)π/m到2Mπ/m;m为拓扑荷数,在3到4之间任意取值;r0为第一组螺线槽的初始半径,M≤3,M为正整数;第一组螺线槽的4个螺线槽的两根螺线rIII和rIV的方程分别为
Figure FDA0002571670280000031
和rIV(θ)=rIII(θ)+d,此时θ的取值从6π/m到2π;
The equations of the two spirals r I and r II of the M-th spiral groove of the first group of spiral grooves are respectively:
Figure FDA0002571670280000026
and r II (θ)=r I (θ)+d, at this time, the value of θ ranges from 2(M-1)π/m to 2Mπ/m; m is the topological charge, which can be arbitrarily selected between 3 and 4 value; r 0 is the initial radius of the first group of helical grooves, M≤3, M is a positive integer; the equations of the two spirals r III and r IV of the four helical grooves of the first group of helical grooves are respectively
Figure FDA0002571670280000031
and r IV (θ)=r III (θ)+d, the value of θ is from 6π/m to 2π at this time;
第二组螺线槽的第M个螺线槽的两根螺线r′I和r′II的方程分别为
Figure FDA0002571670280000032
和r′II(θ)=r′I(θ)+d,r1为第二组螺线槽的初始半径,第二组螺线槽的4个螺线槽的两根螺线r′III和r′IV的方程分别为
Figure FDA0002571670280000033
和r′IV(θ)=r′III(θ)+d,其中d设置为第一组螺线槽以及第二组螺线槽的宽度,所述宽度小于入射波长,N为第一组螺线槽以及第二组螺线槽的圈数,g设置为入射波长。
The equations of the two spirals r' I and r' II of the M-th spiral slot of the second group of spiral slots are respectively:
Figure FDA0002571670280000032
and r′ II (θ)=r′ I (θ)+d, r 1 is the initial radius of the second group of helical grooves, and the two spirals r′ III of the four helical grooves of the second group of helical grooves and the equations of r′ IV are respectively
Figure FDA0002571670280000033
and r′ IV (θ)=r′ III (θ)+d, where d is set to the width of the first set of helical grooves and the second set of helical grooves, the widths being smaller than the incident wavelength, and N is the first set of helical grooves. The number of turns of the wire groove and the second set of helical grooves, and g is set to the incident wavelength.
7.根据权利要求1所述的声学聚焦分数涡旋场发射器,其特征在于:第一组螺线槽为阿基米德螺线槽。7 . The acoustically focused fractional vortex field transmitter according to claim 1 , wherein the first group of helical grooves is an Archimedes helical groove. 8 . 8.根据权利要求1所述的声学聚焦分数涡旋场发射器,其特征在于:第二组螺线槽为阿基米德螺线槽。8 . The acoustically focused fractional vortex field transmitter of claim 1 , wherein the second group of helical grooves is an Archimedes helical groove. 9 . 9.根据权利要求1所述的声学聚焦分数涡旋场发射器,其特征在于:所述预设间距为半个入射波长。9 . The acoustically focused fractional vortex field transmitter according to claim 1 , wherein the preset distance is half an incident wavelength. 10 .
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