CN108736154A - A kind of circular polarisation orbital angular momentum antenna - Google Patents

A kind of circular polarisation orbital angular momentum antenna Download PDF

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CN108736154A
CN108736154A CN201810385633.7A CN201810385633A CN108736154A CN 108736154 A CN108736154 A CN 108736154A CN 201810385633 A CN201810385633 A CN 201810385633A CN 108736154 A CN108736154 A CN 108736154A
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antenna
angular momentum
orbital angular
dielectric material
radiation patch
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CN108736154B (en
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李文涛
孙顺莱
崔灿
魏萌
史小卫
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Xidian University
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/48Earthing means; Earth screens; Counterpoises
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/50Structural association of antennas with earthing switches, lead-in devices or lightning protectors
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/52Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure
    • H01Q1/521Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure reducing the coupling between adjacent antennas
    • H01Q1/523Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure reducing the coupling between adjacent antennas between antennas of an array
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/20Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a curvilinear path

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  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Waveguide Aerials (AREA)

Abstract

本发明提出了一种圆极化轨道角动量天线,用于提高天线的抗干扰能力,包括N个天线单元,N≥3,该天线单元包括介质材料板,以及印制在介质材料板一个侧面的辐射贴片和另一个侧面的辐射地板,其中辐射贴片的形状为任意对角上带有切角的正方形,其与辐射地板通过同轴线连接;所述N个天线单元排列成空心柱状结构,且各天线单元印制有辐射贴片的一侧位于空心柱状结构的外侧,形成共形阵列,各天线单元的激励信号幅度相等,相邻天线单元具有连续的相位延迟其中l代表携带轨道角动量的模式数,满足‑N/2<l<N/2。本发明能够产生多种模态的具有圆极化和轨道角动量双重特性的涡旋电磁波,有效提高了天线的抗干扰能力。

The invention proposes a circularly polarized orbital angular momentum antenna, which is used to improve the anti-interference ability of the antenna, including N antenna units, N≥3, the antenna unit includes a dielectric material plate, and is printed on one side of the dielectric material plate The radiation patch and the radiation floor on the other side, wherein the shape of the radiation patch is a square with cut corners on any diagonal, which is connected to the radiation floor through a coaxial line; the N antenna elements are arranged in a hollow column structure, and the side of each antenna unit printed with a radiation patch is located outside the hollow cylindrical structure, forming a conformal array, the excitation signal amplitude of each antenna unit is equal, and adjacent antenna units have continuous phase delay Where l represents the number of modes carrying orbital angular momentum, satisfying -N/2<l<N/2. The invention can generate multiple modal vortex electromagnetic waves with dual characteristics of circular polarization and orbital angular momentum, and effectively improves the anti-interference ability of the antenna.

Description

一种圆极化轨道角动量天线A Circularly Polarized Orbital Angular Momentum Antenna

技术领域technical field

本发明属于天线技术领域,尤其涉及一种圆极化轨道角动量天线,可用于无线通信技术领域。The invention belongs to the technical field of antennas, in particular to a circularly polarized orbital angular momentum antenna, which can be used in the technical field of wireless communication.

背景技术Background technique

根据经典电动力学理论,电磁辐射不仅能够携带能量还可携带角动量,描述极化状态的自旋角动量SAM与描述螺旋相位结构的轨道角动量OAM,共同组成了角动量,携带轨道角动量的电磁波称为涡旋电磁波。OAM复用是一种频率公用方式的共享频谱资源技术,在相同载频上,调制不同的轨道角动量和传输信息,大大提高频谱利用效率,可以解决无线通信领域频谱资源短缺的问题。According to the classical electrodynamic theory, electromagnetic radiation can carry not only energy but also angular momentum. The spin angular momentum SAM describing the polarization state and the orbital angular momentum OAM describing the helical phase structure together constitute the angular momentum. The orbital angular momentum Electromagnetic waves are called vortex electromagnetic waves. OAM multiplexing is a shared frequency spectrum resource technology in a common way. On the same carrier frequency, different orbital angular momentums are modulated and information is transmitted, which greatly improves the spectrum utilization efficiency and can solve the problem of spectrum resource shortage in the wireless communication field.

由于天线应用的环境复杂,传统的线极化天线有时无法满足通讯的要求,与之相比,圆极化天线可以接收任意极化方向的线极化波,同时它发射的信号也可以由任意极化方向的线极化天线接收,并且具有旋向正交性。在OAM复用技术的基础上进一步研究电磁波的圆极化特性,可以有效提高系统抗干扰能力,能更好的解决由于不同发射和接收天线角度不同带来的能量损耗,最大限度的增加频谱资源利用率。Due to the complex environment in which the antenna is applied, the traditional linearly polarized antenna sometimes cannot meet the requirements of communication. In contrast, the circularly polarized antenna can receive linearly polarized waves in any The linearly polarized antenna of the polarization direction receives, and has the orthogonality of rotation. Further research on the circular polarization characteristics of electromagnetic waves on the basis of OAM multiplexing technology can effectively improve the system's anti-interference ability, better solve the energy loss caused by different transmitting and receiving antenna angles, and maximize spectrum resources utilization rate.

目前,结合轨道角动量在相关领域中的研究进展,轨道角动量涡旋电磁波的产生与发射方式主要有两种,分别是螺旋抛物面天线和阵列天线,前者通过调整抛物面开口两端的间距产生任意模式的轨道角动量无线电波束;后者通过控制阵元辐射场的相位差产生想要的轨道角动量涡旋电磁波。然而,轨道角动量螺旋抛物面天线造价高,制作困难,不适用于连续相位控制;阵列天线中一般偶极子天线阵列半径高达几米到几十米,在进行阵列布置时祈要极小的误差才能产生预期的模态值,适用场所条件要求较为苛刻,在实际通信系统中应用价值并不高,而微带天线阵列由于其平面结构,剖物面低,小尺寸,并且馈电方式简单,方便控制输入相位,在轨道角动量天线中应用有重要意义。At present, combined with the research progress of orbital angular momentum in related fields, there are mainly two ways to generate and emit orbital angular momentum vortex electromagnetic waves, namely the helical parabolic antenna and the array antenna. The former generates arbitrary patterns by adjusting the distance between the two ends of the parabolic opening. The orbital angular momentum radio beam; the latter generates the desired orbital angular momentum vortex electromagnetic wave by controlling the phase difference of the radiation field of the array element. However, the orbital angular momentum helical parabolic antenna is expensive and difficult to manufacture, and is not suitable for continuous phase control; in the array antenna, the radius of the dipole antenna array is as high as several meters to tens of meters, and a very small error is required when the array is arranged. To generate the expected modal value, the applicable site conditions are relatively harsh, and the application value in the actual communication system is not high. However, due to its planar structure, the microstrip antenna array has a low profile, small size, and the feeding method is simple and convenient. Controlling the input phase is of great significance in the application of orbital angular momentum antennas.

实现圆极化波的关键是产生两个方向正交、幅度相等、相位相差90°的线极化波。微带天线中存在何种模式完全取决于贴片的形状和激励模型,在对角线上单点馈电的正方形贴片、正方形对角切角贴片、四周切有缝隙的方向贴片,以及相互正交的两个偶极子均可产生圆极化辐射波束,然而对如何将圆极化辐射贴片作为轨道角动量天线的辐射贴片,产生性能良好的圆极化涡旋电磁波缺乏相应研究。The key to realizing circularly polarized waves is to generate two linearly polarized waves with orthogonal directions, equal amplitude, and 90° phase difference. Which modes exist in a microstrip antenna depends entirely on the shape of the patch and the excitation model, a square patch fed from a single point on the diagonal, a square patch with diagonally cut corners, a directional patch with slots cut all around, and Two dipoles that are orthogonal to each other can generate circularly polarized radiation beams, but there is no response to how to use the circularly polarized radiation patch as the radiation patch of the orbital angular momentum antenna to generate circularly polarized vortex electromagnetic waves with good performance. Research.

传统的轨道角动量天线,是由多个辐射贴片组成的圆环阵列,通过给每个辐射贴片输入幅度相等的激励信号,且相邻辐射贴片具有连续的相位延迟从而产携带轨道角动量的涡旋电磁波。例如申请公布号为CN 107134659A,名称为“基于多层介质板的高增益轨道角动量阵列”的专利申请,公开了一种基于多层介质板的高增益轨道角动量阵列,在介质材料板上方设置有由沿Z轴一维排布的P个辐射贴片,p为大于2的正整数,且各个辐射贴片之间的间距相等,天线阵元通过馈电金属柱与金属地板上的输入端口相连。该发明通过控制输入相位实现了多种模态的轨道角动量涡旋电磁波之间的切换,但是由于辐射贴片的结构简单,仅能实现线极化的轨道角动量涡旋电磁波,抗干扰能力低。The traditional orbital angular momentum antenna is a circular array composed of multiple radiating patches, by inputting an excitation signal with equal amplitude to each radiating patch, and adjacent radiating patches have a continuous phase delay Thus, vortex electromagnetic waves carrying orbital angular momentum are produced. For example, the application publication number is CN 107134659A, and the patent application titled "High-gain Orbital Angular Momentum Array Based on Multilayer Dielectric Plate" discloses a high-gain orbital angular momentum array based on a multilayer dielectric plate. There are P radiating patches arranged one-dimensionally along the Z axis, p is a positive integer greater than 2, and the spacing between each radiating patch is equal, and the antenna element passes through the feeding metal column and the input on the metal floor The ports are connected. The invention realizes the switching between various modes of orbital angular momentum vortex electromagnetic waves by controlling the input phase, but due to the simple structure of the radiation patch, only linearly polarized orbital angular momentum vortex electromagnetic waves can be realized, and the anti-interference ability Low.

发明内容Contents of the invention

本发明的目的在于克服上述现有技术存在的缺陷,提出了一种圆极化轨道角动量天线,用于产生具有圆极化和轨道角动量双重特性的涡旋电磁波,提高天线的抗干扰能力。The purpose of the present invention is to overcome the defects in the above-mentioned prior art, and propose a circularly polarized orbital angular momentum antenna, which is used to generate vortex electromagnetic waves with dual characteristics of circular polarization and orbital angular momentum, and improve the anti-interference ability of the antenna .

一种圆极化轨道角动量天线,包括N个天线单元1,N≥3,所述天线单元1包括介质材料板12,以及印制在介质材料板12一个侧面的辐射贴片11和另一个侧面的辐射地板14,所述辐射贴片11的形状为任意对角上带有切角的正方形,其与辐射地板14通过同轴线13连接;所述N个天线单元1排列成空心柱状结构,且各天线单元1印制有辐射贴片11的一侧位于空心柱状结构的外侧,形成共形阵列,各天线单元1的激励信号幅度相等,相邻天线单元1具有连续的相位延迟其中l代表携带轨道角动量的模式数,满足-N/2<l<N/2。A circularly polarized orbital angular momentum antenna, comprising N antenna units 1, N≥3, said antenna unit 1 comprising a dielectric material plate 12, and a radiation patch 11 printed on one side of the dielectric material plate 12 and another The radiation floor 14 on the side, the shape of the radiation patch 11 is a square with cut corners on any diagonal, which is connected to the radiation floor 14 through the coaxial line 13; the N antenna units 1 are arranged in a hollow columnar structure , and the side of each antenna unit 1 printed with the radiation patch 11 is located outside the hollow columnar structure, forming a conformal array, the amplitude of the excitation signal of each antenna unit 1 is equal, and the adjacent antenna units 1 have a continuous phase delay Where l represents the number of modes carrying orbital angular momentum, and satisfies -N/2<l<N/2.

上述一种圆极化轨道角动量天线,所述介质材料板12,采用偏离中心位置设置有同轴线13过孔的正方形板材,该介质材料板12的几何中心与辐射贴片11的几何中心共轴。The above-mentioned circularly polarized orbital angular momentum antenna, the dielectric material plate 12, adopts a square plate with a coaxial 13 via hole at an off-center position, and the geometric center of the dielectric material plate 12 is the same as the geometric center of the radiation patch 11 coaxial.

上述一种圆极化轨道角动量天线,所述辐射贴片11,其切去的切角为等腰直角三角形,该辐射贴片11的中心位置蚀刻有U型缝隙111,且该U型缝隙111的开口面向介质材料板12上所设置的过孔一侧。In the above-mentioned circularly polarized orbital angular momentum antenna, the radiating patch 11 has a cut angle of an isosceles right triangle, and a U-shaped slit 111 is etched in the center of the radiating patch 11, and the U-shaped slit 111 The opening of 111 faces the side of the via hole provided on the dielectric material board 12 .

本发明与现有技术相比,具有如下优点:Compared with the prior art, the present invention has the following advantages:

1.本发明采用由多个天线单元排列成的空心柱状结构,且各天线单元印制有辐射贴片的一侧位于空心柱状结构的外侧,形成共形阵列,其中辐射贴片采用正方形结构,并在任意对角位置设置切角,通过给各天线单元输入幅度相等,且相邻天线单元具有连续的相位延迟的激励信号,产生了具有良好性能的圆极化和轨道角动量双重特性的涡旋电磁波,最大限度的提高了频谱资源利用率和系统容量,有效提高了天线的抗干扰能力。1. The present invention adopts a hollow columnar structure arranged by multiple antenna units, and the side of each antenna unit printed with a radiation patch is located outside the hollow columnar structure, forming a conformal array, wherein the radiation patch adopts a square structure, And set the cut angle at any diagonal position, by giving each antenna unit an equal input amplitude, and adjacent antenna units have a continuous phase delay The excitation signal generates a vortex electromagnetic wave with dual characteristics of circular polarization and orbital angular momentum with good performance, which maximizes the utilization of spectrum resources and system capacity, and effectively improves the anti-interference ability of the antenna.

2.本发明通过在辐射贴片的中心位置添加U型缝隙,且该U型缝隙开口面向介质材料板上所设置的过孔一侧,从而改变辐射贴片表面电流的传导路径,增加多个谐振点,有效扩宽了天线的阻抗带宽和轴比带宽。2. The present invention adds a U-shaped slit at the center of the radiation patch, and the opening of the U-shaped slit faces the side of the via hole provided on the dielectric material plate, thereby changing the conduction path of the surface current of the radiation patch and increasing multiple The resonance point effectively widens the impedance bandwidth and axial ratio bandwidth of the antenna.

附图说明Description of drawings

图1是本发明实施例1的整体结构示意图;Fig. 1 is the overall structure schematic diagram of embodiment 1 of the present invention;

图2是本发明的天线单元的结构示意图图;Fig. 2 is a structural schematic view of the antenna unit of the present invention;

图3是本发明的辐射贴片结构示意图;Fig. 3 is a schematic structural diagram of the radiation patch of the present invention;

图4是本发明实施例1的S11仿真结果图;Fig. 4 is the S11 simulation result figure of embodiment 1 of the present invention;

图5是本发明实施例1的轴比仿真结果图;Fig. 5 is the axial ratio simulation result figure of embodiment 1 of the present invention;

图6是本发明实施例1的辐射方向图;Fig. 6 is the radiation pattern of embodiment 1 of the present invention;

图7是本发明实施例1的电场相位分布图。Fig. 7 is a diagram of electric field phase distribution in Embodiment 1 of the present invention.

具体实施方式Detailed ways

下面结合附图和具体实施例,对本发明作进一步详细描述:Below in conjunction with accompanying drawing and specific embodiment, the present invention is described in further detail:

实施例1Example 1

参考图1,本发明提出的一种圆极化轨道角动量天线,包括八个天线单元1,该天线单元1包括介质材料板12,以及印制在介质材料板12一个侧面的辐射贴片11和另一个侧面的辐射地板14,其中辐射贴片11和辐射地板14通过同轴线13连接。该天线单元1排列成的空心柱状结构,且各天线单元1印制有辐射贴片11的一侧位于空心柱状结构的外侧,形成共形阵列,该结构可以有效抑制单元之间的互耦,保持天线单元1的特性,提升天线性能。With reference to Fig. 1, a kind of circular polarization orbital angular momentum antenna that the present invention proposes comprises eight antenna elements 1, and this antenna element 1 comprises a dielectric material plate 12, and a radiation patch 11 printed on one side of the dielectric material plate 12 and the radiant floor 14 on the other side, wherein the radiant patch 11 and the radiant floor 14 are connected by a coaxial line 13 . The antenna units 1 are arranged in a hollow columnar structure, and the side of each antenna unit 1 printed with a radiation patch 11 is located outside the hollow columnar structure, forming a conformal array. This structure can effectively suppress the mutual coupling between the units. The characteristics of the antenna unit 1 are maintained, and the performance of the antenna is improved.

参考图2,辐射贴片11的几何中心与介质材料板12的几何中心共轴,且介质材料板12采用偏离中心位置设置有同轴线13过孔的正方形板材,选择介电常数为10.2的介质材料板,整体尺寸为80mm×80mm×9mm,且辐射地板14与介质材料板12同尺寸,同轴线13偏离距离为20mm,其半径为0.5mm。根据微带天线公式可知,微带天线的谐振频率f0与εr-1/2成正比,因此对于一个固定的频率,采用高介电常数的介质基片可以有效的降低天线的尺寸。Referring to Fig. 2, the geometric center of the radiation patch 11 is coaxial with the geometric center of the dielectric material plate 12, and the dielectric material plate 12 adopts a square plate with a coaxial 13 via hole located off the center, and a dielectric constant of 10.2 is selected. The overall size of the dielectric material plate is 80mm×80mm×9mm, and the radiant floor 14 is the same size as the dielectric material plate 12, the deviation distance of the coaxial line 13 is 20mm, and its radius is 0.5mm. According to the microstrip antenna formula, the resonant frequency f 0 of the microstrip antenna is proportional to ε r - 1/2 , so for a fixed frequency, the use of a dielectric substrate with a high dielectric constant can effectively reduce the size of the antenna.

参考图3,辐射贴片11为正方形结构,其边长为60mm,为了激励起两个正交极化,幅度相等且相位相差90°的电磁波,在辐射贴片11的左上角和右下角分别切去两个等腰直角三角形,且三角形的直角边边长为7.2mm,并通过调节同轴线13的位置,产生性能良好的圆极化辐射波束。在辐射贴片11上添加U型缝隙111,该U型缝隙111的长边e=11mm,短边c=6.5mm,宽度w1=1mm,其开口面向介质材料板上所设置的过孔一侧,该U型缝隙111可以改变电流的传导路径,增加多个谐振点,有效扩宽了天线的阻抗带宽和轴比带宽。Referring to Fig. 3, the radiation patch 11 is a square structure with a side length of 60mm. In order to excite two orthogonally polarized electromagnetic waves with equal amplitude and a phase difference of 90°, the radiation patch 11 is placed in the upper left corner and the lower right corner respectively. Two isosceles right triangles are cut off, and the length of the sides of the triangles is 7.2mm, and the position of the coaxial line 13 is adjusted to generate a circularly polarized radiation beam with good performance. Add a U-shaped slit 111 on the radiation patch 11, the long side e=11mm of the U-shaped slit 111, the short side c=6.5mm, the width w1=1mm, and its opening faces the side of the via hole set on the dielectric material plate , the U-shaped slot 111 can change the conduction path of the current, increase multiple resonance points, and effectively widen the impedance bandwidth and axial ratio bandwidth of the antenna.

产生携带轨道角动量的涡旋电磁波的必要条件,需要给各天线单元1输入幅度相等的激励信号,且相邻天线单元1具有连续的相位延迟从而在正常的电磁波中添加一个相位旋转因子其中l代表携带轨道角动量的模式数,满足-N/2<l<N/2,N代表天线单元1的数量,天线单元1的数目决定了能产生轨道角动量模态的的最大值。The necessary condition for generating vortex electromagnetic waves carrying orbital angular momentum is to input excitation signals with equal amplitudes to each antenna unit 1, and adjacent antenna units 1 have a continuous phase delay thus adding a phase rotation factor to normal electromagnetic waves Where l represents the number of modes carrying orbital angular momentum, satisfying -N/2<l<N/2, N represents the number of antenna units 1, and the number of antenna units 1 determines the maximum value of the modes that can generate orbital angular momentum.

本发明的天线单元1的数目N=8,且模式数l=1,根据产生携带轨道角动量的涡旋电磁波的必要条件,可以得出相邻单元的相位延迟假设有第一个天线单元1的初始相位φ=0,则各个单元依次输入相位为0°、45°、90°、135°、180°、225°、270°、315°的激励信号,且幅度相等,由于带切角的辐射贴片11以及采用共形阵列的形式,有效避免的单元之间的耦合,保持天线单元1的圆极化特性,可以产生轨道角动量模式数为1的圆极化涡旋电磁波,由于相位旋转因子的存在,此时的电磁波不再是平面结构,而是绕着传播方向旋转,呈现一种螺旋的电场相位分布,且涡旋电磁波本身的发散特性,轨道角动量模式数l=1的电磁波不再是全向的辐射方向图,而是存在一定的中空现象。The number N=8 of the antenna unit 1 of the present invention, and the pattern number l=1, according to the necessary condition of producing the vortex electromagnetic wave carrying the orbital angular momentum, the phase delay of the adjacent unit can be obtained Assuming that the initial phase φ=0 of the first antenna unit 1, each unit sequentially inputs excitation signals with phases of 0°, 45°, 90°, 135°, 180°, 225°, 270°, 315°, and The amplitudes are equal, and due to the radiation patch 11 with a cut angle and the form of a conformal array, the coupling between the units is effectively avoided, and the circular polarization characteristics of the antenna unit 1 are maintained, and a circle with an orbital angular momentum mode number of 1 can be generated. Polarized vortex electromagnetic waves, due to the phase rotation factor At this time, the electromagnetic wave is no longer a planar structure, but rotates around the propagation direction, presenting a spiral electric field phase distribution, and the divergence characteristics of the vortex electromagnetic wave itself, the electromagnetic wave with the orbital angular momentum mode number l=1 does not It is an omnidirectional radiation pattern, but there is a certain hollow phenomenon.

实施例2中天线的结构与实施例1的结构相同,如下参数作了调整:The structure of the antenna in embodiment 2 is the same as that of embodiment 1, and the following parameters have been adjusted:

天线单元1的数目为N=4,将模式数设为l=1/2,根据产生携带轨道角动量的涡旋电磁波的必要条件,可以得出相邻单元的相位延迟为假设有第一个天线单元1的初始相位φ=0,则各个单元依次输入相位为0°、45°、90°、135°的激励信号,且幅度相等,产生轨道角动量模式数为2的圆极化涡旋电磁波。The number of antenna elements 1 is N=4, and the number of modes is set to l=1/2. According to the necessary conditions for generating vortex electromagnetic waves carrying orbital angular momentum, the phase delay of adjacent elements can be obtained as Assuming that there is an initial phase φ=0 of the first antenna unit 1, each unit sequentially inputs excitation signals with phases of 0°, 45°, 90°, and 135°, and the amplitudes are equal, and the orbital angular momentum mode number is 2. Circularly polarized vortex electromagnetic waves.

本发明的效果可结合仿真结果作进一步说明:Effect of the present invention can be further explained in conjunction with simulation result:

1、仿真内容1. Simulation content

1.1利用商业仿真软件HFSS_13.0对上述实施例1的S11参数进行仿真计算,结果如图4所示。1.1 Using the commercial simulation software HFSS_13.0 to simulate and calculate the S11 parameter of the above-mentioned embodiment 1, the result is shown in FIG. 4 .

1.2利用商业仿真软件HFSS_13.0对上述实施例1的轴比参数进行仿真计算,结果如图5所示。1.2 Use the commercial simulation software HFSS_13.0 to simulate and calculate the axial ratio parameters of the above-mentioned embodiment 1, and the results are shown in FIG. 5 .

1.3利用商业仿真软件HFSS_13.0对上述实施例1的辐射方向图进行仿真计算,结果如图6所示。1.3 Using the commercial simulation software HFSS_13.0 to simulate the radiation pattern of the above-mentioned embodiment 1, the result is shown in FIG. 6 .

1.4利用商业仿真软件HFSS_13.0对上述实施例1的电场相位分布进行仿真计算,结果如图7所示。1.4 Using the commercial simulation software HFSS_13.0 to simulate and calculate the phase distribution of the electric field in the above-mentioned embodiment 1, the result is shown in FIG. 7 .

2、仿真结果2. Simulation results

参照图4,以S11<-10dB为标准,实施例1中天线的阻抗带宽为1.46GHz~1.65GHz,相对带宽为12%。Referring to FIG. 4 , taking S11<-10dB as the standard, the impedance bandwidth of the antenna in Embodiment 1 is 1.46GHz-1.65GHz, and the relative bandwidth is 12%.

参照图5,以轴比AR<3为标准,实施例1中天线的轴比带宽为1.46GHz~1.65GHz,在阻抗带宽内满足圆极化要求。Referring to FIG. 5 , taking the axial ratio AR<3 as the standard, the axial ratio bandwidth of the antenna in Embodiment 1 is 1.46 GHz-1.65 GHz, which meets the requirement of circular polarization within the impedance bandwidth.

参照图6,实施例1中天线的最大辐射方向始终垂直于辐射单元表面,并且有一定的中空现象,最大增益为3.1dB。Referring to Fig. 6, the maximum radiation direction of the antenna in Embodiment 1 is always perpendicular to the surface of the radiation unit, and there is a certain hollow phenomenon, and the maximum gain is 3.1dB.

参照图7,实施例1中天线的电场相位呈螺旋状分布。Referring to FIG. 7 , the electric field phase of the antenna in Embodiment 1 is distributed in a spiral shape.

以上仿真结果说明,本发明天线具有理想的阻抗带宽和轴比带宽,并满足轨道角动量天线的要求。The above simulation results show that the antenna of the present invention has ideal impedance bandwidth and axial ratio bandwidth, and meets the requirements of the orbital angular momentum antenna.

Claims (3)

1.一种圆极化轨道角动量天线,其特征在于,包括N个天线单元(1),N≥3,所述天线单元(1)包括介质材料板(12),以及印制在介质材料板(12)一个侧面的辐射贴片(11)和另一个侧面的辐射地板(14),所述辐射贴片(11)的形状为任意对角上带有切角的正方形,其与辐射地板(14)通过同轴线(13)连接;所述N个天线单元(1)排列成空心柱状结构,且各天线单元(1)印制有辐射贴片(11)的一侧位于空心柱状结构的外侧,形成共形阵列,各天线单元(1)的激励信号幅度相等,相邻天线单元(1)具有连续的相位延迟其中l代表携带轨道角动量的模式数,满足-N/2<l<N/2。1. A circularly polarized orbital angular momentum antenna is characterized in that, comprises N antenna units (1), N≥3, and said antenna unit (1) comprises a dielectric material plate (12), and is printed on a dielectric material The radiant patch (11) on one side of the board (12) and the radiant floor (14) on the other side, the shape of the radiant patch (11) is a square with chamfered corners on any diagonal, which is consistent with the radiant floor (14) Connected by a coaxial line (13); the N antenna units (1) are arranged in a hollow columnar structure, and the side of each antenna unit (1) printed with a radiation patch (11) is located in the hollow columnar structure , forming a conformal array, the excitation signal amplitude of each antenna element (1) is equal, and the adjacent antenna elements (1) have continuous phase delay Where l represents the number of modes carrying orbital angular momentum, and satisfies -N/2<l<N/2. 2.根据权利要求1所述的一种圆极化轨道角动量天线,其特征在于,所述介质材料板(12),采用偏离中心位置设置有同轴线(13)过孔的正方形板材,该介质材料板(12)的几何中心与辐射贴片(11)的几何中心共轴。2. a kind of circularly polarized orbital angular momentum antenna according to claim 1, is characterized in that, described dielectric material plate (12), adopts the square sheet material that off-centre position is provided with coaxial line (13) via hole, The geometric center of the dielectric material plate (12) is coaxial with the geometric center of the radiation patch (11). 3.根据权利要求2所述的一种圆极化轨道角动量天线,其特征在于,所述辐射贴片(11),其切去的切角为等腰直角三角形,该辐射贴片(11)的中心位置蚀刻有U型缝隙(111),且该U型缝隙(111)的开口面向介质材料板(12)上所设置的过孔一侧。3. a kind of circularly polarized orbital angular momentum antenna according to claim 2, is characterized in that, described radiation patch (11), the cut angle that it cuts off is an isosceles right triangle, and this radiation patch (11 ) is etched with a U-shaped slit (111), and the opening of the U-shaped slit (111) faces the side of the via hole provided on the dielectric material plate (12).
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110212313A (en) * 2019-06-10 2019-09-06 南京航空航天大学 A kind of adjustable road angular momentum wave mode reconfigurable antenna of electricity
CN110444903A (en) * 2019-07-18 2019-11-12 西安电子科技大学 Sidelobe vortex wave beam production method based on multi-ring array
CN111613874A (en) * 2020-04-30 2020-09-01 南京理工大学 A Tri-Mode OAM Antenna Based on Triangular Half-Mode
CN112909579A (en) * 2021-01-21 2021-06-04 伊犁师范大学 Multi-mode orbital angular momentum antenna
CN116632526A (en) * 2023-07-24 2023-08-22 上海英内物联网科技股份有限公司 Circularly polarized microstrip patch antenna with miniaturized ground plane

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103022731A (en) * 2012-11-28 2013-04-03 北京中欧美经济技术发展中心 Multi-frequency circularly polarized stacked micro-strip antenna
US20150357710A1 (en) * 2014-06-04 2015-12-10 Fujitsu Limited Antenna apparatus and antenna direction control method

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103022731A (en) * 2012-11-28 2013-04-03 北京中欧美经济技术发展中心 Multi-frequency circularly polarized stacked micro-strip antenna
US20150357710A1 (en) * 2014-06-04 2015-12-10 Fujitsu Limited Antenna apparatus and antenna direction control method

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
范玉堂: ""基于电磁涡旋波的新型多模态OAM阵列天线研究与设计"", 《中国优秀硕士学位论文全文数据库》 *
马留涛: ""锥体与柱体载体平台共形天线阵列设计"", 《中国优秀硕士学位论文全文数据库》 *

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110212313A (en) * 2019-06-10 2019-09-06 南京航空航天大学 A kind of adjustable road angular momentum wave mode reconfigurable antenna of electricity
CN110212313B (en) * 2019-06-10 2024-04-12 南京航空航天大学 An electrically tunable orbital angular momentum wave mode reconfigurable antenna
CN110444903A (en) * 2019-07-18 2019-11-12 西安电子科技大学 Sidelobe vortex wave beam production method based on multi-ring array
CN111613874A (en) * 2020-04-30 2020-09-01 南京理工大学 A Tri-Mode OAM Antenna Based on Triangular Half-Mode
CN111613874B (en) * 2020-04-30 2022-11-04 南京理工大学 A Tri-Mode OAM Antenna Based on Triangular Half-Mode
CN112909579A (en) * 2021-01-21 2021-06-04 伊犁师范大学 Multi-mode orbital angular momentum antenna
CN116632526A (en) * 2023-07-24 2023-08-22 上海英内物联网科技股份有限公司 Circularly polarized microstrip patch antenna with miniaturized ground plane
CN116632526B (en) * 2023-07-24 2023-10-31 上海英内物联网科技股份有限公司 Circularly polarized microstrip patch antenna with miniaturized ground plane

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