CN116632536A - A kind of circularly polarized antenna array and its preparation method - Google Patents
A kind of circularly polarized antenna array and its preparation method Download PDFInfo
- Publication number
- CN116632536A CN116632536A CN202310632830.5A CN202310632830A CN116632536A CN 116632536 A CN116632536 A CN 116632536A CN 202310632830 A CN202310632830 A CN 202310632830A CN 116632536 A CN116632536 A CN 116632536A
- Authority
- CN
- China
- Prior art keywords
- layer
- circularly polarized
- antenna array
- polarized antenna
- metal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/52—Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure
- H01Q1/521—Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure reducing the coupling between adjacent antennas
- H01Q1/523—Means 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/36—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
- H01Q1/38—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/50—Structural association of antennas with earthing switches, lead-in devices or lightning protectors
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/10—Resonant slot antennas
- H01Q13/103—Resonant slot antennas with variable reactance for tuning the antenna
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/0006—Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices
- H01Q15/0013—Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices said selective devices working as frequency-selective reflecting surfaces, e.g. FSS, dichroic plates, surfaces being partly transmissive and reflective
- H01Q15/002—Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices said selective devices working as frequency-selective reflecting surfaces, e.g. FSS, dichroic plates, surfaces being partly transmissive and reflective said selective devices being reconfigurable or tunable, e.g. using switches or diodes
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/0006—Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices
- H01Q15/0013—Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices said selective devices working as frequency-selective reflecting surfaces, e.g. FSS, dichroic plates, surfaces being partly transmissive and reflective
- H01Q15/004—Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices said selective devices working as frequency-selective reflecting surfaces, e.g. FSS, dichroic plates, surfaces being partly transmissive and reflective using superconducting materials or magnetised substrates
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/0006—Particular feeding systems
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/0087—Apparatus or processes specially adapted for manufacturing antenna arrays
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/24—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
- H01Q9/04—Resonant antennas
- H01Q9/0407—Substantially flat resonant element parallel to ground plane, e.g. patch antenna
- H01Q9/0414—Substantially flat resonant element parallel to ground plane, e.g. patch antenna in a stacked or folded configuration
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
- H01Q9/04—Resonant antennas
- H01Q9/0407—Substantially flat resonant element parallel to ground plane, e.g. patch antenna
- H01Q9/0428—Substantially flat resonant element parallel to ground plane, e.g. patch antenna radiating a circular polarised wave
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
- H01Q9/04—Resonant antennas
- H01Q9/0407—Substantially flat resonant element parallel to ground plane, e.g. patch antenna
- H01Q9/0442—Substantially flat resonant element parallel to ground plane, e.g. patch antenna with particular tuning means
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Waveguide Aerials (AREA)
Abstract
Description
技术领域technical field
本发明涉及天线去耦领域,尤其涉及一种圆极化天线阵列及其制备方法。The invention relates to the field of antenna decoupling, in particular to a circularly polarized antenna array and a preparation method thereof.
背景技术Background technique
当前,无线通信技术正在向6G通信发展。大信道容量和高速率传输等需求推动多输入多输出(Multiple-Input-Multiple-Output,MIMO)技术的发展。在MIMO平台中,由于载体的小型化和天线数量的大规模集成,使得天线间的电磁耦合作用无法忽略,降低天线性能。降低天线间互耦是无线通信发展的关键。Currently, wireless communication technology is developing towards 6G communication. Demands such as large channel capacity and high-speed transmission promote the development of Multiple-Input-Multiple-Output (MIMO) technology. In the MIMO platform, due to the miniaturization of the carrier and the large-scale integration of the number of antennas, the electromagnetic coupling between the antennas cannot be ignored and the performance of the antennas will be reduced. Reducing the mutual coupling between antennas is the key to the development of wireless communication.
圆极化天线一方面可以接收任意线极化方向的电磁波,另一方面当圆极化波入射到一对称目标(如空气中的球形水滴),反射的电磁波旋向相反。圆极化在实际通信中既能抑制雨雾干扰,又能减小多路径干扰被广泛应用在车载和卫星通信中。On the one hand, the circularly polarized antenna can receive electromagnetic waves in any linear polarization direction. On the other hand, when the circularly polarized wave is incident on a symmetrical target (such as a spherical water droplet in the air), the reflected electromagnetic wave has the opposite direction of rotation. In actual communication, circular polarization can not only suppress rain and fog interference, but also reduce multipath interference, and is widely used in vehicle and satellite communications.
当前去耦技术多用于线极化天线阵列,其中的去耦方法不适用于圆极化天线阵列。圆极化天线阵列解耦相较于线极化天线阵列而言解耦更具挑战。在工作频段需要同时考虑阻抗匹配,耦合水平和圆极化轴比特性。The current decoupling technology is mostly used in linearly polarized antenna arrays, and the decoupling method is not suitable for circularly polarized antenna arrays. The decoupling of circularly polarized antenna arrays is more challenging than that of linearly polarized antenna arrays. In the working frequency band, impedance matching, coupling level and circular polarization axial ratio characteristics need to be considered at the same time.
发明内容Contents of the invention
为提高现有天线间的隔离度和改善单元辐射性能,本发明提供一种圆极化天线阵列及其制备方法。所述圆极化天线阵列利用超表面覆层调控电磁场,实现场相消,以提高天线间的隔离度和改善单元辐射性能。In order to improve the isolation between existing antennas and improve the radiation performance of units, the invention provides a circularly polarized antenna array and a preparation method thereof. The circularly polarized antenna array utilizes the metasurface coating to regulate the electromagnetic field to realize field cancellation, so as to improve the isolation between antennas and improve the unit radiation performance.
本发明是通过以下技术方案实现:一种圆极化天线阵列,所述圆极化天线阵列上方安装有一个超表面覆盖结构,所述超表面覆盖结构与所述圆极化天线阵列之间设计为空气层,所述空气层的高度为6.5mm;所述超表面覆盖结构包括绝缘介质层一以及分别固定在绝缘介质层一相对两侧上的上层金属阵列、下层金属阵列,且所述下层金属阵列面向所述圆极化天线阵列;The present invention is achieved through the following technical solutions: a circularly polarized antenna array, a metasurface covering structure is installed above the circularly polarized antenna array, and a design is made between the metasurface covering structure and the circularly polarized antenna array It is an air layer, and the height of the air layer is 6.5mm; the supersurface covering structure includes an insulating dielectric layer one and an upper metal array and a lower metal array respectively fixed on the opposite sides of the insulating dielectric layer one, and the lower layer a metal array facing the circularly polarized antenna array;
其中,所述上层金属阵列包括层阵列式分布的多个上层金属,每个上层金属上开设有均贯穿相应上层金属横向上的相对两端的两条横向缝隙、均贯穿相应上层金属纵向上的相对两端的两条纵向缝隙、在两条纵向缝隙之间且与两条纵向缝隙平行的中间缝隙;中间缝隙的两端均穿过两条横向缝隙但中间缝隙的长度小于两条纵向缝隙的长度;Wherein, the upper-layer metal array includes a plurality of upper-layer metals distributed in a layer array, and each upper-layer metal is provided with two transverse slits that run through the opposite ends of the corresponding upper-layer metal in the transverse direction, and both penetrate the corresponding upper-layer metal in the longitudinal direction. Two longitudinal slits at both ends, a central slit between and parallel to the two longitudinal slits; both ends of the central slit pass through the two transverse slits but the length of the central slit is less than the length of the two longitudinal slits;
所述下层金属阵列包括层阵列式分布的多个下层金属,多个下层金属与多个上层金属在绝缘介质层一上的位置上、下一一对应;每个下层金属呈倾斜的十字架状。The lower layer metal array includes a plurality of lower layer metals distributed in a layer array, and the plurality of lower layer metals correspond to the positions of the plurality of upper layer metals on the first insulating medium layer one by one; each lower layer metal is in the shape of an inclined cross.
作为上述方案的进一步改进,所述超表面覆盖结构通过多个尼龙支柱固定在所述圆极化天线阵列上方。As a further improvement of the above solution, the metasurface covering structure is fixed above the circularly polarized antenna array through a plurality of nylon pillars.
作为上述方案的进一步改进,相邻两个上层金属之间的间隔为10mm。As a further improvement of the above solution, the interval between two adjacent upper metal layers is 10 mm.
作为上述方案的进一步改进,每个上层金属呈正方形,两条横向缝隙的宽度相同,两条纵向缝隙的宽度也相同;As a further improvement of the above scheme, each upper layer of metal is in a square shape, the width of the two transverse slits is the same, and the width of the two longitudinal slits is also the same;
两条横向缝隙的宽度、两条横向缝隙离相应上层金属的中心间距、两条纵向缝隙的宽度、两条纵向缝隙离相应上层金属的中心间距、中间缝隙的长度、中间缝隙的宽度、相应上层金属的边长比为0.4mm∶1.6mm∶0.2mm∶2.3mm∶6.4mm∶0.4mm∶8.4mm。The width of two transverse slits, the center distance between two transverse slits and the corresponding upper metal layer, the width of two longitudinal slits, the center distance between two longitudinal slits and the corresponding upper metal layer, the length of the middle slit, the width of the middle slit, the corresponding upper layer The side length ratio of the metal is 0.4mm: 1.6mm: 0.2mm: 2.3mm: 6.4mm: 0.4mm: 8.4mm.
进一步地,每个下层金属的长轴是由边长为A mm的正方向贴片,蚀刻掉对角两个边长为Bmm的等边直角三角形剩余而成;每个下层金属的短轴是由边长为Cmm的正方向贴片,蚀刻掉对角两个边长为Dmm的等边直角三角形剩余而成;A∶B∶C∶D为5.6∶4.4∶3.6∶2.8。Furthermore, the long axis of each underlying metal is formed by etching away two equilateral right-angled triangles whose sides are Bmm at the opposite corners of the patch in the positive direction with a side length of A mm; the short axis of each underlying metal is It is formed by etching away two equilateral right-angled triangles with a side length of Dmm from a positive direction patch with a side length of Cmm; A:B:C:D is 5.6:4.4:3.6:2.8.
作为上述方案的进一步改进,所述圆极化天线阵列包括:As a further improvement of the above scheme, the circularly polarized antenna array includes:
绝缘介质层二,其位于绝缘介质层一的下方;The second insulating medium layer is located below the first insulating medium layer;
两个金属贴片,固定在绝缘介质层二面向绝缘介质层一的一侧上;Two metal patches are fixed on the side of the insulating medium layer 2 facing the insulating medium layer 1;
金属地层,其平铺固定在绝缘介质层二背向绝缘介质层一的相对另一侧上。The metal ground layer is tiled and fixed on the opposite side of the insulating medium layer 2 facing away from the insulating medium layer 1.
进一步地,绝缘介质层一、绝缘介质层二的介电常数均为4.4,均采用FR4制成,厚度均为1.5mm,两个绝缘介质层的长度、宽度均与所述圆极化天线阵列的长度、宽度相同。Further, the dielectric constants of the insulating dielectric layer 1 and the insulating dielectric layer 2 are both 4.4, both are made of FR4, and the thickness is 1.5mm. The length and width of the two insulating dielectric layers are the same as that of the circularly polarized antenna array. same length and width.
进一步地,两个金属贴片关于绝缘介质层二中心对称,分别设置同轴馈电结构;每个金属贴片是在边长为E mm的正方向贴片对角蚀刻F mm的等边直角三角形,金属贴片边与边之间的距离为G mm;E∶F∶G为14∶4∶3。Further, the two metal patches are symmetrical about the two centers of the insulating medium layer, and coaxial feed structures are respectively provided; each metal patch is an equilateral right angle of F mm in the positive direction with a side length of E mm. Triangle, the distance between the sides of the metal patch is G mm; E:F:G is 14:4:3.
本发明还提供上述任意圆极化天线阵列的制备方法,其包括以下步骤:The present invention also provides a method for preparing the above-mentioned arbitrary circularly polarized antenna array, which includes the following steps:
首先设计圆极化天线阵列,在所述圆极化天线阵列的天线阵层设计同轴馈电结构,并在所述天线阵层的四角对称打4个M3通孔,通孔之间相距长55mm,宽35mm;First design the circularly polarized antenna array, design the coaxial feed structure at the antenna array layer of the circularly polarized antenna array, and punch four M3 through holes symmetrically at the four corners of the antenna array layer, and the distance between the through holes is long 55mm, width 35mm;
在绝缘介质层一的相对两侧上分别刻印多个上层金属和多个下层金属;在绝缘介质层一的四周对称打通孔,其位置与绝缘介质层二上的通孔位置一致;A plurality of upper-layer metals and a plurality of lower-layer metals are respectively engraved on opposite sides of the insulating dielectric layer 1; through holes are symmetrically drilled around the insulating dielectric layer 1, and the positions thereof are consistent with the positions of the through holes on the insulating dielectric layer 2;
将每一对通孔位置安装一个绝缘支撑结构,留下厚度在6.5mm的空气层。Install an insulating support structure for each pair of through-hole positions, leaving an air layer with a thickness of 6.5mm.
作为上述方案的进一步改进,在设计圆极化天线阵列时,在绝缘介质层二的相对两侧上分别刻印金属贴片层和金属地层,构成所述天线阵层。As a further improvement of the above solution, when designing a circularly polarized antenna array, a metal patch layer and a metal ground layer are respectively printed on opposite sides of the insulating medium layer 2 to form the antenna array layer.
本发明利用超表面覆盖结构以提高圆极化天线阵列间的隔离度,超表面覆盖结构主要由上下金属层和介质层组成;超表面覆盖结构与圆极化天线阵列的天线层之间设计为空气层,可利用尼龙支柱来固定结构。本发明设计的超表面覆盖结构可以适用在阵元间距非常近的微带圆极化天线阵列中,解耦后的圆极化天线阵列可以降低天线间的耦合,同时改善单元的辐射性能。The present invention utilizes the metasurface covering structure to improve the isolation between circularly polarized antenna arrays, the metasurface covering structure is mainly composed of upper and lower metal layers and dielectric layers; the design between the metasurface covering structure and the antenna layer of the circularly polarized antenna array is The air layer can utilize nylon struts to fix the structure. The metasurface covering structure designed by the present invention can be applied in a microstrip circularly polarized antenna array with very close spacing between array elements, and the decoupled circularly polarized antenna array can reduce the coupling between antennas and improve the radiation performance of the units at the same time.
因此,本发明设计的超表面可以对小边距的微带圆极化天线阵列进行解耦,具备以下优势:Therefore, the metasurface designed in the present invention can decouple the microstrip circularly polarized antenna array with small margins, and has the following advantages:
1、引入新的谐振点,拓宽了阻抗匹配带宽,S11低于10dB范围提高了300%以上。1. The introduction of a new resonance point broadens the impedance matching bandwidth, and the range of S11 below 10dB has been increased by more than 300%.
2、耦合水平大幅度下降,在中心频带处隔离度提升了30dB以上。2. The coupling level is greatly reduced, and the isolation at the center frequency band is increased by more than 30dB.
3、圆极化轴比带宽进行拓宽,且修正了初始圆极化阵列轴比和阻抗匹配频带偏移不匹配。3. The bandwidth of the circular polarization axis ratio is widened, and the mismatch between the axis ratio of the initial circular polarization array and the offset of the impedance matching frequency band is corrected.
4、圆极化天线阵列的包络相关系数大幅度下降,整体趋于0,辐射方向图不相关。4. The envelope correlation coefficient of the circularly polarized antenna array drops sharply, tends to 0 as a whole, and the radiation pattern is irrelevant.
5、加载超表面后天线的辐射效率得到提升。5. The radiation efficiency of the antenna is improved after loading the metasurface.
附图说明Description of drawings
图1为本发明实例提供的具有超表面覆盖结构的微带圆极化天线阵的结构示意图。Fig. 1 is a schematic structural diagram of a microstrip circularly polarized antenna array with a metasurface covering structure provided by an example of the present invention.
图2为图1中超表面覆盖结构的上层金属结构示意图。FIG. 2 is a schematic diagram of the upper metal structure of the metasurface covering structure in FIG. 1 .
图3为图1中超表面覆盖结构的下层金属结构示意图。FIG. 3 is a schematic diagram of the underlying metal structure of the metasurface covering structure in FIG. 1 .
图4为图1中圆极化天线阵的金属贴片层结构示意图。FIG. 4 is a schematic diagram of the metal patch layer structure of the circularly polarized antenna array in FIG. 1 .
图5为图1中圆极化天线阵的参数对照图,其中图5a、图5b分别为本发明实例提供的微带圆极化天线阵列未加载和加载超表面的仿真S参数示意图。Fig. 5 is a parameter comparison diagram of the circularly polarized antenna array in Fig. 1, wherein Fig. 5a and Fig. 5b are schematic diagrams of simulated S parameters of the unloaded and loaded metasurfaces of the microstrip circularly polarized antenna array provided by the example of the present invention, respectively.
图6为本发明实例提供的微带圆极化天线阵列加载超表面覆盖结构前后的仿真轴比示意图。Fig. 6 is a schematic diagram of the simulated axial ratio before and after the microstrip circularly polarized antenna array is loaded with the metasurface covering structure provided by the example of the present invention.
图7为本发明实例提供的微带圆极化天线阵列加载超表面覆盖结构前后的包络相关系数示意图。Fig. 7 is a schematic diagram of the envelope correlation coefficient before and after the microstrip circularly polarized antenna array is loaded with the metasurface covering structure provided by the example of the present invention.
图8为本发明实例提供的微带圆极化天线阵列加载超表面覆盖结构前后的辐射效率示意图。Fig. 8 is a schematic diagram of the radiation efficiency of the microstrip circularly polarized antenna array before and after loading the metasurface covering structure provided by the example of the present invention.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
需要说明的是,当组件被称为“安装于”另一个组件,它可以直接在另一个组件上或者也可以存在居中的组件。当一个组件被认为是“设置于”另一个组件,它可以是直接设置在另一个组件上或者可能同时存在居中组件。当一个组件被认为是“固定于”另一个组件,它可以是直接固定在另一个组件上或者可能同时存在居中组件。It should be noted that when a component is said to be "mounted on" another component, it can be directly on the other component or there can also be an intervening component. When a component is said to be "set on" another component, it may be set directly on the other component or there may be an intervening component at the same time. When a component is said to be "fixed" to another component, it may be directly fixed to the other component or there may be an intervening component at the same time.
除非另有定义,本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本文中在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的,不是旨在于限制本发明。本文所使用的术语“或/及”包括一个或多个相关的所列项目的任意的和所有的组合。Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the technical field of the invention. The terms used herein in the description of the present invention are for the purpose of describing specific embodiments only, and are not intended to limit the present invention. As used herein, the term "or/and" includes any and all combinations of one or more of the associated listed items.
本发明的微带圆极化天线阵具有超表面覆盖结构如图1所示,所述圆极化天线阵列上方安装有一个超表面覆盖结构,也就是说将超表面覆层正放置在微带圆极化天线阵列上方。所述超表面覆盖结构与所述圆极化天线阵列之间设计为空气层,所述空气层的高度为6.5mm。本发明的基本原理是在相邻天线间引入间接耦合场,与原耦合场进行场合并相消,达到解耦作用。所述超表面覆盖结构可通过多个支撑结构7如尼龙支柱固定在所述圆极化天线阵列上方。The microstrip circularly polarized antenna array of the present invention has a metasurface covering structure as shown in Figure 1, and a metasurface covering structure is installed above the circularly polarized antenna array, that is to say, the metasurface coating is placed on the microstrip Above the circularly polarized antenna array. An air layer is designed between the metasurface covering structure and the circularly polarized antenna array, and the height of the air layer is 6.5mm. The basic principle of the invention is to introduce an indirect coupling field between adjacent antennas, and perform field merge and cancellation with the original coupling field to achieve decoupling. The metasurface covering structure can be fixed above the circularly polarized antenna array through a plurality of supporting structures 7 such as nylon pillars.
所述超表面覆盖结构包括绝缘介质层一2以及分别固定在绝缘介质层一2相对两侧上的上层金属阵列、下层金属阵列,且所述下层金属阵列面向所述圆极化天线阵列。上层金属阵列、下层金属阵列两者元素不仅数量相对应,而且在绝缘介质层一2的上、下相对两侧上的位置也是上下一一对应。The metasurface covering structure includes an insulating dielectric layer 2 and an upper metal array and a lower metal array respectively fixed on opposite sides of the insulating dielectric layer 2, and the lower metal array faces the circularly polarized antenna array. The elements of the upper metal array and the lower metal array are not only corresponding in number, but also corresponding in position on the upper and lower opposite sides of the insulating medium layer-2.
请结合图2,所述上层金属阵列包括层阵列式分布的多个上层金属1,相邻两个上层金属1之间的间隔为10mm。在本实施例中,多个上层金属1为3行5列周期排列的15个基本单元,单元周期间隔为10mm。Please refer to FIG. 2 , the upper metal array includes a plurality of upper metals 1 distributed in a layered array, and the interval between two adjacent upper metals 1 is 10mm. In this embodiment, the plurality of upper metal layers 1 are 15 basic units arranged periodically in 3 rows and 5 columns, and the unit period interval is 10 mm.
每个上层金属1上开设有两条横向缝隙11、两条纵向缝隙12、一条中间缝隙13。两条横向缝隙11均贯穿相应上层金属1横向上的相对两端,两条纵向缝隙12均贯穿相应上层金属1纵向上的相对两端,中间缝隙13在两条纵向缝隙12之间且与两条纵向缝隙12平行,中间缝隙13的两端均穿过两条横向缝隙11但中间缝隙13的长度小于两条纵向缝隙12的长度。每个上层金属1呈正方形,两条横向缝隙11的宽度相同,两条纵向缝隙12的宽度也相同。两条横向缝隙11的宽度、两条横向缝隙11离相应上层金属1的中心间距、两条纵向缝隙12的宽度、两条纵向缝隙12离相应上层金属1的中心间距、中间缝隙13的长度、中间缝隙13的宽度、相应上层金属1的边长比为0.4mm∶1.6mm∶0.2mm∶2.3mm∶6.4mm∶0.4mm∶8.4mm。Each upper layer of metal 1 is provided with two transverse slits 11 , two longitudinal slits 12 and one middle slit 13 . Two transverse slits 11 run through the opposite ends of the corresponding upper layer metal 1 in the transverse direction, two longitudinal slits 12 run through the opposite ends of the corresponding upper layer metal 1 in the longitudinal direction, and the middle slit 13 is between the two longitudinal slits 12 and connected to the two longitudinal slits 12. The longitudinal slits 12 are parallel, the two ends of the middle slit 13 pass through the two transverse slits 11 but the length of the middle slit 13 is shorter than the length of the two longitudinal slits 12 . Each upper layer of metal 1 is in the shape of a square, the width of the two transverse slits 11 is the same, and the width of the two longitudinal slits 12 is also the same. The width of the two transverse slits 11, the center distance between the two transverse slits 11 and the corresponding upper metal 1, the width of the two longitudinal slits 12, the center distance between the two longitudinal slits 12 and the corresponding upper metal 1, the length of the middle slit 13, The ratio of the width of the middle gap 13 to the side length of the corresponding upper layer metal 1 is 0.4mm: 1.6mm: 0.2mm: 2.3mm: 6.4mm: 0.4mm: 8.4mm.
在本实施例中,上层金属1是在边长为8.4mm的方形贴片蚀刻横向缝隙和纵向缝隙。两条横向缝隙11相同,宽度为0.4mm,离中心间距1.6mm。左右两条纵向缝隙12相同,宽度为0.2mm,离中心间距2.3mm。中间的纵向缝隙即中间缝隙13长度为6.4mm,宽度为0.4mm。In this embodiment, the upper metal layer 1 is a square patch with a side length of 8.4mm and etched horizontal and vertical slits. The two transverse slits 11 are the same, with a width of 0.4 mm and a distance of 1.6 mm from the center. The left and right longitudinal slits 12 are the same, with a width of 0.2 mm and a distance of 2.3 mm from the center. The middle longitudinal slit, namely the middle slit 13, has a length of 6.4 mm and a width of 0.4 mm.
下层金属阵列包括层阵列式分布的多个下层金属3,多个下层金属3与多个上层金属1在绝缘介质层一2上的位置上、下一一对应。也就是说在本实施例中,多个下层金属3为3行5列周期排列的15个基本单元,单元周期间隔也为10mm。The lower layer metal array includes a plurality of lower layer metals 3 distributed in a layer array, and the plurality of lower layer metals 3 correspond to the positions of the plurality of upper layer metals 1 on the first insulating medium layer 2 one by one. That is to say, in this embodiment, the multiple underlying metals 3 are 15 basic units arranged periodically in 3 rows and 5 columns, and the unit period interval is also 10mm.
请结合图3,每个下层金属3呈倾斜的十字架状。每个下层金属3的长轴是由边长为A mm的正方向贴片,蚀刻掉对角两个边长为Bmm的等边直角三角形剩余而成;每个下层金属3的短轴是由边长为Cmm的正方向贴片,蚀刻掉对角两个边长为Dmm的等边直角三角形剩余而成;A∶B∶C∶D为5.6∶4.4∶3.6∶2.8。Please refer to FIG. 3 , each lower layer metal 3 is in the shape of an inclined cross. The major axis of each underlying metal 3 is formed by etching away two equilateral right-angled triangles whose sides are Bmm in the opposite corner with a positive patch with a side length of A mm; the minor axis of each underlying metal 3 is formed by The patch in the positive direction with a side length of Cmm is formed by etching away two equilateral right-angled triangles with a side length of Dmm at the diagonal; A:B:C:D is 5.6:4.4:3.6:2.8.
在本实施例中,每个下层金属3的长轴是由边长为5.6mm的正方向贴片,蚀刻掉对角两个边长为4.4mm的等边直角三角形剩余而成。每个下层金属3的短轴是由边长为3.6mm的正方向贴片,蚀刻掉对角两个边长为2.8mm的等边直角三角形剩余而成。In this embodiment, the long axis of each underlying metal 3 is formed by etching away two equilateral right-angled triangles with a side length of 4.4 mm from a positive patch with a side length of 5.6 mm. The minor axis of each underlying metal 3 is formed by etching away two equilateral right-angled triangles with a side length of 2.8 mm from a positive patch with a side length of 3.6 mm.
超表面介质层即绝缘介质层一2的介电常数为4.4,厚度为1.5mm,长度为60mm,宽度为40mm,采用FR4制成。The dielectric constant of the metasurface dielectric layer, that is, the insulating dielectric layer-2, is 4.4, the thickness is 1.5 mm, the length is 60 mm, and the width is 40 mm, and it is made of FR4.
请结合图4,圆极化天线阵列包括绝缘介质层二5、两个金属贴片4、金属地层6。绝缘介质层二5位于绝缘介质层一2的下方;两个金属贴片4固定在绝缘介质层二5面向绝缘介质层一2的一侧上;金属地层6平铺固定在绝缘介质层二5背向绝缘介质层一2的相对另一侧上。绝缘介质层二5的介电常数为4.4,厚度为1.5mm,长度为60mm,宽度为40mm,采用FR4制成。Please refer to FIG. 4 , the circularly polarized antenna array includes an insulating dielectric layer 2 5 , two metal patches 4 , and a metal ground layer 6 . The insulating medium layer 2 5 is located below the insulating medium layer 1 2; two metal patches 4 are fixed on the side of the insulating medium layer 2 5 facing the insulating medium layer 1 2; the metal ground layer 6 is tiled and fixed on the insulating medium layer 2 5 On the other side opposite to the insulating dielectric layer one 2 . The insulating dielectric layer 2 5 has a dielectric constant of 4.4, a thickness of 1.5 mm, a length of 60 mm, and a width of 40 mm, and is made of FR4.
两个金属贴片4关于绝缘介质层二5中心对称,分别设置同轴馈电结构;每个金属贴片4是在边长为E mm的正方向贴片对角蚀刻F mm的等边直角三角形,金属贴片边与边之间的距离为G mm;E∶F∶G为14∶4∶3。The two metal patches 4 are symmetrical about the center of the insulating medium layer 25, and coaxial feed structures are respectively provided; each metal patch 4 is an equilateral right angle of F mm in the positive direction with a side length of E mm. Triangle, the distance between the sides of the metal patch is G mm; E:F:G is 14:4:3.
在本实施例中,微带圆极化阵列的金属贴片包括两个金属贴片,设计的贴片位置关于基板中心对称,分别设置同轴馈电结构。金属贴片是在边长为14mm的正方向贴片对角蚀刻4mm的等边直角三角形(对比去耦前的金属贴片是在边长为13.4mm的正方向贴片对角蚀刻2.8mm的等边直角三角形)。金属贴片边与边之间的距离为3mm。In this embodiment, the metal patch of the microstrip circularly polarized array includes two metal patches, the designed patch positions are symmetrical with respect to the center of the substrate, and coaxial feeding structures are provided respectively. The metal patch is an equilateral right-angled triangle with a side length of 14mm and a 4mm diagonal etching in the positive direction (compared with the metal patch before decoupling, which is 2.8mm in the positive direction with a side length of 13.4mm) equilateral right triangle). The distance between the edges of the metal patch is 3mm.
在超表面覆层和天线阵层的四角(即绝缘介质层一2和绝缘介质层二5的四角)分别设计M3的通孔,上下相对应。支撑结构设计成尼龙支柱。将尼龙支柱安装在通孔位置,分离超表面覆层和天线阵层。Through holes of M3 are respectively designed at the four corners of the metasurface cladding layer and the antenna array layer (that is, the four corners of the first insulating dielectric layer 2 and the second insulating dielectric layer 5), corresponding up and down. The support structure is designed as nylon struts. Install nylon struts at the through-hole locations to separate the metasurface cladding and antenna array layers.
本发明的圆极化天线阵列在制备时,其制备方法包括以下步骤。When the circularly polarized antenna array of the present invention is prepared, its preparation method includes the following steps.
首先设计圆极化天线阵列,在所述圆极化天线阵列的天线阵层设计同轴馈电结构,并在所述天线阵层的四角对称打4个M3通孔,通孔之间相距长55mm,宽35mm。其中,在设计圆极化天线阵列时,在绝缘介质层二5的相对两侧上分别刻印金属贴片层4和金属地层6,构成所述天线阵层。First design the circularly polarized antenna array, design the coaxial feed structure at the antenna array layer of the circularly polarized antenna array, and punch four M3 through holes symmetrically at the four corners of the antenna array layer, and the distance between the through holes is long 55mm, 35mm wide. Wherein, when designing a circularly polarized antenna array, the metal patch layer 4 and the metal ground layer 6 are respectively printed on opposite sides of the insulating medium layer 2 5 to form the antenna array layer.
其次,在绝缘介质层一2的相对两侧上分别刻印多个上层金属1和多个下层金属3。Secondly, a plurality of upper-layer metals 1 and a plurality of lower-layer metals 3 are respectively imprinted on opposite sides of the insulating dielectric layer one 2 .
然后,在绝缘介质层一2的四周对称打通孔,其位置与绝缘介质层二5上的通孔位置一致。Then, through holes are symmetrically drilled around the first insulating medium layer 2 , and the positions thereof are consistent with the positions of the through holes on the second insulating medium layer 5 .
最后,将每一对通孔位置安装一个绝缘支撑结构7,留下厚度在6.5mm的空气层8。Finally, install an insulating support structure 7 for each pair of through-hole positions, leaving an air layer 8 with a thickness of 6.5 mm.
在本实施例中,圆极化天线阵列的具体的制备方法可以为如下具体介绍。首先设计天线阵层,在厚度为1.5mm,长度为60mm,宽度为40mm的天线介质层5上下刻印金属贴片层4和金属地层6,构成天线阵层。天线介质层5采用介电常数为4.4的FR4。在天线阵层设计同轴馈电结构,并在四角对称打4个M3通孔,通孔之间相距长55mm,宽35mm。超表面覆层是在厚度为1.5mm,长度为60mm,宽度为40mm的超表面介质层2上下刻印上金属层1和下金属层2。超表面介质层2采用介电常数为4.4的FR4。在超表面覆盖层的四周对称打通孔,其位置与天线阵层的通孔位置一致。最后将尼龙柱支撑结构7安装在通孔位置,留下空气层8。空气层厚度在6.5mm。In this embodiment, the specific preparation method of the circularly polarized antenna array may be specifically introduced as follows. First, the antenna array layer is designed, and the metal patch layer 4 and the metal ground layer 6 are engraved on the top and bottom of the antenna dielectric layer 5 with a thickness of 1.5mm, a length of 60mm, and a width of 40mm to form the antenna array layer. The antenna dielectric layer 5 adopts FR4 with a dielectric constant of 4.4. Design a coaxial feed structure on the antenna array layer, and drill four M3 through holes symmetrically at the four corners. The distance between the through holes is 55mm long and 35mm wide. The super-surface coating is to engrave the upper metal layer 1 and the lower metal layer 2 on the upper and lower sides of the meta-surface dielectric layer 2 with a thickness of 1.5 mm, a length of 60 mm, and a width of 40 mm. The metasurface dielectric layer 2 adopts FR4 with a dielectric constant of 4.4. Holes are symmetrically punched around the metasurface covering layer, and the positions thereof are consistent with the positions of the through holes of the antenna array layer. Finally, the nylon column support structure 7 is installed at the position of the through hole, leaving the air layer 8 . The thickness of the air layer is 6.5mm.
本发明的基本原理是在相邻天线间引入间接耦合场,与原耦合场进行场合并相消,达到解耦作用。如图5a、图5b的S参数对比可以看出,本发明的去耦方法即可以拓宽阻抗匹配频率,又能降低耦合值,在中心频带处隔离度提升了30dB以上。如图6的轴比参数对比可以看出设计方法可以拓宽圆极化轴比带宽。除了端口性能隔离度的提高,超表面覆层好可以改善天线辐射性能。如图7所示,在加载超表面后,圆极化天线阵列的包络相关系数趋于0,辐射方向图不相关。如图8所示,加载超表面后天线的辐射效率得到提升。The basic principle of the invention is to introduce an indirect coupling field between adjacent antennas, and perform field merge and cancellation with the original coupling field to achieve decoupling. It can be seen from the comparison of S parameters in Fig. 5a and Fig. 5b that the decoupling method of the present invention can not only broaden the impedance matching frequency, but also reduce the coupling value, and the isolation at the central frequency band is increased by more than 30dB. The comparison of axial ratio parameters in Figure 6 shows that the design method can widen the axial ratio bandwidth of circular polarization. In addition to the improvement of port performance isolation, metasurface cladding can improve antenna radiation performance. As shown in Fig. 7, after loading the metasurface, the envelope correlation coefficient of the circularly polarized antenna array tends to 0, and the radiation pattern is not correlated. As shown in Figure 8, the radiation efficiency of the antenna is improved after loading the metasurface.
本发明可以对边距较近的微带圆极化天线阵列实现较好的解耦效果。综上所述,本发明是将超表面覆层正放置在微带圆极化天线阵列上方。超表面覆盖层由上下金属层和介质层组成;所介绍的微带圆极化天线包括对角蚀刻三角形的金属贴片层、天线电介质层和金属地层。超表面覆盖层与天线层之间设计为空气层,利用尼龙支柱来固定结构。The invention can realize a better decoupling effect for the microstrip circularly polarized antenna array with a relatively close side distance. In summary, the present invention places a metasurface coating just above a microstrip circularly polarized antenna array. The metasurface covering layer consists of upper and lower metal layers and dielectric layers; the introduced microstrip circularly polarized antenna includes a diagonally etched triangular metal patch layer, an antenna dielectric layer and a metal formation layer. An air layer is designed between the metasurface covering layer and the antenna layer, and nylon pillars are used to fix the structure.
以上所述实施例仅表达了本发明的几种实施方式,其描述较为具体和详细,但并不能因此而理解为对发明专利范围的限制。应当指出的是,对于本领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干变形和改进,这些都属于本发明的保护范围。因此,本发明专利的保护范围应以所附权利要求为准。The above-mentioned embodiments only express several implementation modes of the present invention, and the descriptions thereof are relatively specific and detailed, but should not be construed as limiting the patent scope of the invention. It should be noted that, for those skilled in the art, several modifications and improvements can be made without departing from the concept of the present invention, and these all belong to the protection scope of the present invention. Therefore, the protection scope of the patent for the present invention should be based on the appended claims.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310632830.5A CN116632536A (en) | 2023-05-31 | 2023-05-31 | A kind of circularly polarized antenna array and its preparation method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310632830.5A CN116632536A (en) | 2023-05-31 | 2023-05-31 | A kind of circularly polarized antenna array and its preparation method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN116632536A true CN116632536A (en) | 2023-08-22 |
Family
ID=87621008
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310632830.5A Pending CN116632536A (en) | 2023-05-31 | 2023-05-31 | A kind of circularly polarized antenna array and its preparation method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116632536A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080258981A1 (en) * | 2006-04-27 | 2008-10-23 | Rayspan Corporation | Antennas, Devices and Systems Based on Metamaterial Structures |
| US8451189B1 (en) * | 2009-04-15 | 2013-05-28 | Herbert U. Fluhler | Ultra-wide band (UWB) artificial magnetic conductor (AMC) metamaterials for electrically thin antennas and arrays |
| CN104466359A (en) * | 2014-11-25 | 2015-03-25 | 骆柳春 | Coated antenna |
| CN115036687A (en) * | 2022-06-22 | 2022-09-09 | 航天特种材料及工艺技术研究所 | An Antenna with High Radiation Characteristics Based on Butterfly Metasurface |
| CN115064877A (en) * | 2022-06-10 | 2022-09-16 | 西安电子科技大学 | Decoupling super surface applied to dual-polarization compact base station antenna array |
-
2023
- 2023-05-31 CN CN202310632830.5A patent/CN116632536A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080258981A1 (en) * | 2006-04-27 | 2008-10-23 | Rayspan Corporation | Antennas, Devices and Systems Based on Metamaterial Structures |
| US8451189B1 (en) * | 2009-04-15 | 2013-05-28 | Herbert U. Fluhler | Ultra-wide band (UWB) artificial magnetic conductor (AMC) metamaterials for electrically thin antennas and arrays |
| CN104466359A (en) * | 2014-11-25 | 2015-03-25 | 骆柳春 | Coated antenna |
| CN115064877A (en) * | 2022-06-10 | 2022-09-16 | 西安电子科技大学 | Decoupling super surface applied to dual-polarization compact base station antenna array |
| CN115036687A (en) * | 2022-06-22 | 2022-09-09 | 航天特种材料及工艺技术研究所 | An Antenna with High Radiation Characteristics Based on Butterfly Metasurface |
Non-Patent Citations (1)
| Title |
|---|
| 邓莎莎: "宽带与多频MIMO平面天线阵列的去耦技术研究", 中国优秀硕士学位论文全文数据库 (信息科技辑), vol. 136, no. 2023, 15 February 2023 (2023-02-15), pages 136 - 82 * |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9323877B2 (en) | Beam-steered wide bandwidth electromagnetic band gap antenna | |
| US20200287277A1 (en) | Low-profile broadband circularly-polarized array antenna using stacked traveling wave antenna elements | |
| Li et al. | Wideband perforated dense dielectric patch antenna array for millimeter-wave applications | |
| US10424847B2 (en) | Wideband dual-polarized current loop antenna element | |
| US20100007572A1 (en) | Dual-polarized phased array antenna with vertical features to eliminate scan blindness | |
| CN208208987U (en) | A kind of high isolation low-cross polarization Double-polarization micro-strip array antenna | |
| KR20210077808A (en) | Microstrip antenna, antenna array and method of manufacturing microstrip antenna | |
| CN209515999U (en) | A kind of circular polarization microstrip antenna | |
| CN114583457A (en) | Four-patch broadband microstrip antenna unit based on coupling feed and antenna array | |
| CN113690595A (en) | Wide-beam antenna unit and phased array | |
| CN113506976B (en) | High-gain circularly polarized antenna and wireless communication device | |
| CN109950693B (en) | Integrated substrate gap waveguide circular polarization gap traveling wave array antenna | |
| CN115347359B (en) | A Broadband High Gain Circularly Polarized Magnetoelectric Dipole Antenna Array | |
| CN110504527B (en) | L and X wave band common-caliber antenna with novel structure | |
| CN115173068B (en) | Broadband circularly polarized substrate integrated waveguide horn antenna array and wireless communication equipment | |
| CN115832706B (en) | A Miniaturized Broadband Circularly Polarized Magnetoelectric Dipole Antenna | |
| US11581656B2 (en) | Wide frequency range dual polarized radiating element with integrated radome | |
| CN113036438A (en) | Broadband low-profile dielectric resonator antenna for beamforming application | |
| CN117317578A (en) | SIW broadband circularly polarized high-gain low-profile magneto-electric dipole antenna array | |
| CN115764331A (en) | High-polarization-isolation dual-polarization tightly-coupled ultra-wideband phased array antenna | |
| CN106997986A (en) | A kind of circular polarized antenna array of X-band | |
| Ginting et al. | Proximity-coupled L-band patch array antenna fed by binomial power distribution | |
| CN115799819A (en) | Millimeter wave wide beam circular polarization double-layer microstrip patch antenna | |
| CN114843772A (en) | A dual frequency, dual circular polarization, high isolation Fabry-Perot cavity MIMO antenna and its processing method | |
| US10170829B2 (en) | Self-complementary multilayer array antenna |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |