CN106384872A - High frequency absorption antenna for reducing back lobe influence - Google Patents
High frequency absorption antenna for reducing back lobe influence Download PDFInfo
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- 238000010521 absorption reaction Methods 0.000 title claims abstract 3
- 239000002184 metal Substances 0.000 claims abstract description 48
- 229910052751 metal Inorganic materials 0.000 claims abstract description 48
- 239000000758 substrate Substances 0.000 claims abstract description 37
- 239000004020 conductor Substances 0.000 claims abstract description 24
- 238000013461 design Methods 0.000 claims description 12
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- 239000006096 absorbing agent Substances 0.000 description 2
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- 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
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- 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
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
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- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/48—Earthing means; Earth screens; Counterpoises
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- H—ELECTRICITY
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Abstract
Description
技术领域technical field
本发明属于电磁能量接收天线技术领域,具体涉及一种用于接收环境中射频能量的减弱后瓣影响的高频吸收天线。The invention belongs to the technical field of electromagnetic energy receiving antennas, and in particular relates to a high-frequency absorbing antenna used for receiving radio frequency energy in an environment and weakening the influence of back lobe.
背景技术Background technique
在国内,关于射频无线能量有限空间内的传输技术研究起步较晚,在科技迅猛发展的今天,随着经济的进步和科研水平的提高,越来越多的公司和科研机构开始关注并开展这方面的研究,在有限空间内进行无线射频能量的收集。In China, the research on the transmission technology of radio frequency wireless energy in a limited space started relatively late. Today, with the rapid development of science and technology, with the progress of economy and the improvement of scientific research level, more and more companies and scientific research institutions have begun to pay attention to and develop this technology. Research on the field of radio frequency energy collection in a limited space.
发明内容Contents of the invention
本发明解决的技术问题是提供了一种结构简单且设计合理的减弱后瓣影响的高频吸收天线,该天线较其它天线而言拥有的更小的尺寸、相对较低的回拨损耗、良好的阻抗匹配和较高的增益。The technical problem solved by the present invention is to provide a high-frequency absorbing antenna with simple structure and reasonable design to weaken the influence of the back lobe. Compared with other antennas, the antenna has smaller size, relatively lower callback loss, good Impedance matching and higher gain.
本发明为解决上述技术问题采用如下技术方案,减弱后瓣影响的高频吸收天线,其特征在于包括由上到下尺寸一致且相互贴合的介质覆盖层、介质基板和接地板,其中与介质覆盖层贴合一侧的介质基板上贴附有金属天线贴片,介质基板的中部设有垂直贯穿介质基板的圆柱形金属导体和四个圆柱形孔洞,接地板上设有与圆柱形金属导体底面同心的圆孔;所述介质覆盖层的材料为Rogers RO6002,介电常数εr=2.94,厚度d=0.51mm,长度和宽度均为30mm;所述金属天线贴片的圆形覆盖面的半径为0.11312λ,其中λ=122mm,λ为2.45GHz射频的波长,厚度为0.02mm,材料为铜,所述介质基板的材料为Rogers RO6010,介电常数εr=10.2,厚度d=2.54mm,长度和宽度均为30mm,金属天线贴片的中心点与介质基板上表面的中心点位置一致;所述金属天线贴片的设计形状及尺寸满足如下要求,建立平面直角坐标系,将(0mm,-2.5mm)作为起点,(13.75mm,-2.5mm)为另一端点沿x轴正方向做出一条长为13.75mm的线段一,以点(13.75mm,-2.5mm)为旋转点,将线段一沿逆时针方向旋转105°,与曲线方程的交点为H(14.72057mm,-6.1222mm),以直线y=-x为对称轴作镜面对称得到点L(6.1222mm,-14.72057mm),将线段一以直线y=-x为对称轴作镜面对称得到线段二,线段一和线段二的交点为分别连接点H(14.72057mm,-6.1222mm)、和L(6.1222mm,-14.72057mm)、得到线段HW和线段LW,再次将原点(0mm,0mm)作为起点,沿x轴正方向作出一条长为2.5mm的线段,以(2.5mm,-1.25mm)为第一个曲线的圆心,以(2.5mm,0mm)为一端点,以(3.75mm,-1.25mm)为另一端点,半径r1=1.25mm,作出圆周角为90°,方向为向x轴及y轴正方向凸出的圆弧,以(5mm,-1.25mm)为第二个曲线的圆心,以(3.75mm,-1.25mm)为一端点,以(6.25mm,-1.25mm)为另一端点,半径r2=1.25mm,作出圆周角为180°,方向为向y轴负方向凸出的圆弧,然后以(7.5mm,-1.25mm)为第三个曲线的圆心,以(6.25mm,-1.25mm)为一端点,以(7.5mm,0mm)为另一端点,半径r3=1.25mm,作出圆周角为90°,方向为向x轴负方向及y轴正方向凸出的圆弧,以(7.5mm,-2.5mm)为第四个曲线的圆心,以(7.5mm,0mm)为一端点,以(10mm,-2.5mm)为另一端点,半径r4=2.5mm,作出圆周角为90°,方向为向x轴及y轴正方向凸出的圆弧;以(13.75mm,-2.5mm)为第五个曲线的圆心,以(10mm,-2.5mm)为一端点,以H(14.72057mm,-6.1222mm)为另一端点,半径r5=3.75mm,作出圆周角为105°,方向为向x轴及y轴负方向凸出的圆弧得到初始图形一,以直线y=-x为对称轴,将初始图形一进行镜面对称,得到初始图形二,线段HW、线段LW、初始图形一和初始图形二合并得到旋转图形一,将旋转图形一以点为旋转点,顺时针依次旋转60°、120°、180°、240°和300°,分别得到旋转图形二、旋转图形三、旋转图形四、旋转图形五和旋转图形六,旋转图形一、旋转图形二、旋转图形三、旋转图形四、旋转图形五和旋转图形六合并得到封闭图形,将封闭图形的圆形覆盖面半径缩小为原来的0.77234倍得到所需金属天线贴片的设计形状及尺寸,按照设计形状及尺寸裁剪得到金属天线贴片;所述介质基板上四个圆柱形孔洞的半径均为0.5mm,四个圆柱形孔洞的圆心连线构成边长为22mm的正方形,该正方形上下边与介质基板上下侧边的垂直距离分别为2.8mm和5.2mm,正方形左右侧边与介质基板左右两侧的垂直距离分别为2mm和6mm;所述圆柱形金属导体的一端与金属天线贴片连接,圆柱形金属导体的材料为铜,其底面半径r=0.5mm,厚度d=2.54mm,圆柱形金属导体与金属天线贴片的连接处圆心与介质基板四条侧边的垂直距离分别为16.48mm、16.48mm、13.52mm和13.52mm,与圆柱形金属导体相对的接地板上圆孔的孔径R=1.9mm,所述圆柱形金属导体另一端的输出接口与能量管理电路相连,该能量管理电路用于将吸收到的能量进行储存。In order to solve the above technical problems, the present invention adopts the following technical scheme, the high-frequency absorbing antenna that weakens the influence of the back lobe, is characterized in that it includes a dielectric covering layer, a dielectric substrate and a ground plate that are consistent in size from top to bottom and are attached to each other. A metal antenna patch is attached to the dielectric substrate on the bonding side of the cover layer. A cylindrical metal conductor and four cylindrical holes are provided in the middle of the dielectric substrate, and a cylindrical metal conductor is provided on the ground plate. Concentric circular holes on the bottom surface; the material of the dielectric covering layer is Rogers RO6002, the dielectric constant ε r =2.94, the thickness d=0.51mm, and the length and width are 30mm; the radius of the circular covering surface of the metal antenna patch is 0.11312λ, wherein λ=122mm, λ is the wavelength of 2.45GHz radio frequency, the thickness is 0.02mm, and the material is copper, the material of the dielectric substrate is Rogers RO6010, the dielectric constant ε r =10.2, and the thickness d=2.54mm, Both length and width are 30mm, and the center point of the metal antenna patch is consistent with the center point position of the upper surface of the dielectric substrate; the design shape and size of the metal antenna patch meet the following requirements, and a plane Cartesian coordinate system is established, with (0mm, -2.5mm) as the starting point, (13.75mm, -2.5mm) as the other end point, make a line segment 1 with a length of 13.75mm along the positive direction of the x-axis, and take the point (13.75mm, -2.5mm) as the rotation point, and place Line segment 1 is rotated 105° counterclockwise, and the curve equation The point of intersection is H (14.72057mm, -6.1222mm), and the point L (6.1222mm, -14.72057mm) is obtained by taking the straight line y=-x as the axis of symmetry for mirror symmetry, and the line segment one is made as the axis of symmetry of the line y=-x Mirror symmetry to get line segment 2, the intersection point of line segment 1 and line segment 2 is Respectively connecting point H (14.72057mm, -6.1222mm), and L(6.1222mm, -14.72057mm), Get the line segment HW and line segment LW, take the origin (0mm, 0mm) as the starting point again, make a line segment with a length of 2.5mm along the positive direction of the x-axis, take (2.5mm, -1.25mm) as the center of the first curve, and (2.5mm, 0mm) as one end point, (3.75mm, -1.25mm) as the other end point, radius r 1 = 1.25mm, make a circular angle of 90°, and the direction is convex to the positive direction of x-axis and y-axis The arc, with (5mm, -1.25mm) as the center of the second curve, with (3.75mm, -1.25mm) as one end point, with (6.25mm, -1.25mm) as the other end point, radius r 2 =1.25mm, make a circular arc with a circumference angle of 180° and a direction protruding toward the negative direction of the y-axis, then take (7.5mm, -1.25mm) as the center of the third curve, and take (6.25mm, -1.25mm) ) as one end point, (7.5mm, 0mm) as the other end point, radius r 3 =1.25mm, make a circular arc with a circular angle of 90° and a direction protruding toward the negative direction of the x-axis and the positive direction of the y-axis, with (7.5mm, -2.5mm) is the center of the fourth curve, with (7.5mm, 0mm) as one end point, (10mm, -2.5mm) as the other end point, radius r 4 =2.5mm, and make a circle angle is 90°, and the direction is a circular arc protruding toward the positive direction of x-axis and y-axis; with (13.75mm, -2.5mm) as the center of the fifth curve, with (10mm, -2.5mm) as one end point, and H(14.72057mm, -6.1222mm) is the other end point, the radius r 5 =3.75mm, make a circular arc with a circular angle of 105°, and the direction is to protrude toward the negative direction of the x-axis and y-axis to obtain the initial figure 1, and use a straight line y=-x is the symmetry axis, the initial figure 1 is mirror-symmetrical to obtain the initial figure 2, the line segment HW, the line segment LW, the initial figure 1 and the initial figure 2 are combined to obtain the rotation figure 1, and the rotation figure 1 is represented by a point is the rotation point, rotate 60°, 120°, 180°, 240° and 300° clockwise, respectively, to obtain the rotation figure 2, the rotation figure 3, the rotation figure 4, the rotation figure 5 and the rotation figure 6, the rotation figure 1, the rotation Figure 2, Rotation Figure 3, Rotation Figure 4, Rotation Figure 5 and Rotation Figure 6 are combined to obtain a closed figure, and the circular coverage radius of the closed figure is reduced to 0.77234 times of the original to obtain the design shape and size of the required metal antenna patch, The metal antenna patch is cut according to the design shape and size; the radius of the four cylindrical holes on the dielectric substrate is 0.5mm, and the connecting lines of the centers of the four cylindrical holes form a square with a side length of 22mm, and the upper and lower sides of the square The vertical distances from the upper and lower sides of the dielectric substrate are 2.8mm and 5.2mm respectively, and the vertical distances between the left and right sides of the square and the left and right sides of the dielectric substrate are 2mm and 6mm respectively; one end of the cylindrical metal conductor is connected to the metal antenna patch , the material of the cylindrical metal conductor is copper, the radius of the bottom surface r=0.5mm, the thickness d=2.54mm, the vertical distance between the center of the connection between the cylindrical metal conductor and the metal antenna patch and the four sides of the dielectric substrate is 16.48mm respectively , 16.48mm, 13.52mm and 13.52mm, the aperture R=1.9mm of the circular hole on the ground plate opposite to the cylindrical metal conductor, the output interface at the other end of the cylindrical metal conductor is connected to the energy management circuit, the energy management circuit Used to store the absorbed energy.
本发明的技术效果为:减弱后瓣影响的高频吸收天线具有更低的回波损耗、良好的阻抗匹配和驻波比以及较高的增益,从而能够高效接收环境中的射频能量。The technical effect of the invention is that the high-frequency absorbing antenna with weakened back lobe has lower return loss, good impedance matching, standing wave ratio and high gain, thereby being able to efficiently receive radio frequency energy in the environment.
附图说明Description of drawings
图1是金属天线贴片的结构示意图;Fig. 1 is a structural schematic diagram of a metal antenna patch;
图2是减弱后瓣影响的高频吸收天线结构示意图;Figure 2 is a schematic diagram of the structure of a high-frequency absorbing antenna that weakens the influence of the back lobe;
图3是利用HFSS天线模拟仿真软件模拟的减弱后瓣影响的高频吸收天线的回波损耗图;Fig. 3 is the return loss diagram of the high-frequency absorbing antenna with weakened back lobe effect simulated by HFSS antenna simulation software;
图4是利用HFSS天线模拟仿真软件模拟的减弱后瓣影响的高频吸收天线输入阻抗图。Fig. 4 is the input impedance diagram of the high-frequency absorbing antenna simulated by HFSS antenna simulation software to weaken the effect of the back lobe.
图中:1、介质覆盖层,2、介质基板,3、接地板,4、金属天线贴片,5、圆柱形金属导体,6、圆柱形孔洞,7、圆孔。In the figure: 1. Dielectric covering layer, 2. Dielectric substrate, 3. Grounding plate, 4. Metal antenna patch, 5. Cylindrical metal conductor, 6. Cylindrical hole, 7. Round hole.
具体实施方式detailed description
下面将结合本发明中的附图,对本发明具体实施过程中的技术方案进行清楚、完整、具体的描述。The technical solutions in the specific implementation process of the present invention will be clearly, completely and specifically described below in conjunction with the accompanying drawings in the present invention.
此发明的核心部分是减弱后瓣影响的高频吸收天线设计,在微带天线设计时需要对减弱后瓣影响的高频吸收天线的金属天线贴片的尺寸,介质基板的尺寸、厚度进行理论上的估算,才能在模拟实验的时候更加快速精确的找到适合特定频率的减弱后瓣影响的高频吸收天线。所以下面以矩形微带天线为例,讲解微带天线各个数据参数的理论计算方法。The core part of this invention is the design of the high-frequency absorbing antenna that weakens the influence of the back lobe. In the design of the microstrip antenna, the size of the metal antenna patch of the high-frequency absorbing antenna that weakens the influence of the back lobe, and the size and thickness of the dielectric substrate need to be theoretically In order to find the high-frequency absorbing antenna suitable for a specific frequency and weaken the influence of the back lobe more quickly and accurately during the simulation experiment. So the following takes the rectangular microstrip antenna as an example to explain the theoretical calculation method of each data parameter of the microstrip antenna.
贴片尺寸L×W,贴片宽度W为:The patch size is L×W, and the patch width W is:
在(1)式中,c为光速,f0为禁带中心频率,εr为相对介电常数。In (1), c is the speed of light, f 0 is the center frequency of the forbidden band, and ε r is the relative permittivity.
微带天线介质基板的相对有效介电常数εre为:The relative effective permittivity ε re of the dielectric substrate of the microstrip antenna is:
h表示介质层厚度,为了降低表面波辐射对天线性能的影响,介质基片的厚度应该满足一下的理论计算公式:h represents the thickness of the dielectric layer. In order to reduce the influence of surface wave radiation on the performance of the antenna, the thickness of the dielectric substrate should satisfy the following theoretical calculation formula:
其中fu为微带天线的工作的最高频率。Among them f u is the highest working frequency of the microstrip antenna.
微带天线的等效辐射缝隙长度ΔL为:The equivalent radiation slot length ΔL of the microstrip antenna is:
则微带天线贴片的长度L为:Then the length L of the microstrip antenna patch is:
接地板的尺寸Lg×Wg满足下列理论公式The size of the ground plate L g × W g satisfies the following theoretical formula
Lg≥L+6h (6) Lg≥L +6h (6)
Wg≥W+6h (7) Wg≥W +6h (7)
矩形微带天线用的是同轴线进行馈电,当确定了矩形贴片的长度和宽度后,一般在微带天线中加入50Ω的标准阻抗。The rectangular microstrip antenna uses a coaxial line for feeding. After the length and width of the rectangular patch are determined, a standard impedance of 50Ω is generally added to the microstrip antenna.
如图1-2所示,减弱后瓣影响的高频吸收天线,包括由上到下尺寸一致且相互贴合的介质覆盖层1、介质基板2和接地板3,其中与介质覆盖层1贴合一侧的介质基板2上贴附有金属天线贴片4,介质基板2的中部设有垂直贯穿介质基板2的圆柱形金属导体5和四个圆柱形孔洞6,接地板3上设有与圆柱形金属导体5底面同心的圆孔7;所述介质覆盖层1的材料为Rogers RO6002,介电常数εr=2.94,厚度d=0.51mm,长度和宽度均为30mm;所述金属天线贴片4的圆形覆盖面的半径为0.11312λ,其中λ=122mm,λ为2.45GHz射频的波长,厚度为0.02mm,材料为铜,所述介质基板2的材料为Rogers RO6010,介电常数εr=10.2,厚度d=2.54mm,长度和宽度均为30mm,金属天线贴片4的中心点与介质基板2上表面的中心点位置一致;所述金属天线贴片4的设计形状及尺寸满足如下要求,建立平面直角坐标系,将(0mm,-2.5mm)作为起点,(13.75mm,-2.5mm)为另一端点沿x轴正方向做出一条长为13.75mm的线段一,以点(13.75mm,-2.5mm)为旋转点,将线段一沿逆时针方向旋转105°,与曲线方程的交点为H(14.72057mm,-6.1222mm),以直线y=-x为对称轴作镜面对称得到点L(6.1222mm,-14.72057mm),将线段一以直线y=-x为对称轴作镜面对称得到线段二,线段一和线段二的交点为分别连接点H(14.72057mm,-6.1222mm)、和L(6.1222mm,-14.72057mm)、得到线段HW和线段LW,再次将原点(0mm,0mm)作为起点,沿x轴正方向作出一条长为2.5mm的线段,以(2.5mm,-1.25mm)为第一个曲线的圆心,以(2.5mm,0mm)为一端点,以(3.75mm,-1.25mm)为另一端点,半径r1=1.25mm,作出圆周角为90°,方向为向x轴及y轴正方向凸出的圆弧,以(5mm,-1.25mm)为第二个曲线的圆心,以(3.75mm,-1.25mm)为一端点,以(6.25mm,-1.25mm)为另一端点,半径r2=1.25mm,作出圆周角为180°,方向为向y轴负方向凸出的圆弧,然后以(7.5mm,-1.25mm)为第三个曲线的圆心,以(6.25mm,-1.25mm)为一端点,以(7.5mm,0mm)为另一端点,半径r3=1.25mm,作出圆周角为90°,方向为向x轴负方向及y轴正方向凸出的圆弧,以(7.5mm,-2.5mm)为第四个曲线的圆心,以(7.5mm,0mm)为一端点,以(10mm,-2.5mm)为另一端点,半径r4=2.5mm,作出圆周角为90°,方向为向x轴及y轴正方向凸出的圆弧;以(13.75mm,-2.5mm)为第五个曲线的圆心,以(10mm,-2.5mm)为一端点,以H(14.72057mm,-6.1222mm)为另一端点,半径r5=3.75mm,作出圆周角为105°,方向为向x轴及y轴负方向凸出的圆弧得到初始图形一,以直线y=-x为对称轴,将初始图形一进行镜面对称,得到初始图形二,线段HW、线段LW、初始图形一和初始图形二合并得到旋转图形一,将旋转图形一以点为旋转点,顺时针依次旋转60°、120°、180°、240°和300°,分别得到旋转图形二、旋转图形三、旋转图形四、旋转图形五和旋转图形六,旋转图形一、旋转图形二、旋转图形三、旋转图形四、旋转图形五和旋转图形六合并得到封闭图形,将封闭图形的圆形覆盖面半径缩小为原来的0.77234倍得到所需金属天线贴片4的设计形状及尺寸,按照设计形状及尺寸裁剪得到金属天线贴片4;所述介质基板2上四个圆柱形孔洞6的半径均为0.5mm,四个圆柱形孔洞6的圆心连线构成边长为22mm的正方形,该正方形上下边与介质基板2上下侧边的垂直距离分别为2.8mm和5.2mm,正方形左右侧边与介质基板2左右两侧的垂直距离分别为2mm和6mm;所述圆柱形金属导体5的一端与金属天线贴片4连接,圆柱形金属导体5的材料为铜,其底面半径r=0.5mm,厚度d=2.54mm,圆柱形金属导体5与金属天线贴片4的连接处圆心与介质基板2四条侧边的垂直距离分别为16.48mm、16.48mm、13.52mm和13.52mm,与圆柱形金属导体5相对的接地板3上圆孔7的孔径R=1.9mm,所述圆柱形金属导体5另一端的输出接口与能量管理电路相连,该能量管理电路用于将吸收到的能量进行储存。As shown in Figure 1-2, the high-frequency absorbing antenna that weakens the influence of the back lobe includes a dielectric covering layer 1, a dielectric substrate 2, and a ground plate 3 that are consistent in size from top to bottom and are attached to each other. A metal antenna patch 4 is attached to the dielectric substrate 2 on one side, a cylindrical metal conductor 5 and four cylindrical holes 6 vertically penetrating the dielectric substrate 2 are provided in the middle of the dielectric substrate 2, and a ground plate 3 is provided with a The concentric circular hole 7 on the bottom surface of the cylindrical metal conductor 5; the material of the dielectric covering layer 1 is Rogers RO6002, the dielectric constant ε r =2.94, the thickness d=0.51mm, and the length and width are 30mm; the metal antenna paste The radius of the circular covering surface of sheet 4 is 0.11312λ, where λ=122mm, λ is the wavelength of 2.45GHz radio frequency, the thickness is 0.02mm, and the material is copper. The material of the dielectric substrate 2 is Rogers RO6010, and the dielectric constant ε r =10.2, thickness d=2.54mm, length and width are 30mm, the center point of the metal antenna patch 4 is consistent with the center point of the upper surface of the dielectric substrate 2; the design shape and size of the metal antenna patch 4 satisfy the following It is required to establish a plane Cartesian coordinate system, take (0mm, -2.5mm) as the starting point, and (13.75mm, -2.5mm) as the other end point to make a line segment 1 with a length of 13.75mm along the positive direction of the x-axis, and take the point ( 13.75mm, -2.5mm) is the rotation point, rotate the line segment 105° counterclockwise, and the curve equation The point of intersection is H (14.72057mm, -6.1222mm), and the point L (6.1222mm, -14.72057mm) is obtained by taking the straight line y=-x as the axis of symmetry for mirror symmetry, and the line segment one is made as the axis of symmetry of the line y=-x Mirror symmetry to get line segment 2, the intersection point of line segment 1 and line segment 2 is Respectively connecting point H (14.72057mm, -6.1222mm), and L(6.1222mm, -14.72057mm), Get the line segment HW and line segment LW, take the origin (0mm, 0mm) as the starting point again, make a line segment with a length of 2.5mm along the positive direction of the x-axis, take (2.5mm, -1.25mm) as the center of the first curve, and (2.5mm, 0mm) as one end point, (3.75mm, -1.25mm) as the other end point, radius r 1 = 1.25mm, make a circular angle of 90°, and the direction is convex to the positive direction of x-axis and y-axis The arc, with (5mm, -1.25mm) as the center of the second curve, with (3.75mm, -1.25mm) as one end point, with (6.25mm, -1.25mm) as the other end point, radius r 2 =1.25mm, make a circular arc with a circumference angle of 180° and a direction protruding toward the negative direction of the y-axis, then take (7.5mm, -1.25mm) as the center of the third curve, and take (6.25mm, -1.25mm) ) as one end point, (7.5mm, 0mm) as the other end point, radius r 3 =1.25mm, make a circular arc with a circular angle of 90° and a direction protruding toward the negative direction of the x-axis and the positive direction of the y-axis, with (7.5mm, -2.5mm) is the center of the fourth curve, with (7.5mm, 0mm) as one end point, (10mm, -2.5mm) as the other end point, radius r 4 =2.5mm, and make a circle angle is 90°, and the direction is a circular arc protruding toward the positive direction of x-axis and y-axis; with (13.75mm, -2.5mm) as the center of the fifth curve, with (10mm, -2.5mm) as one end point, and H(14.72057mm, -6.1222mm) is the other end point, the radius r 5 =3.75mm, make a circular arc with a circular angle of 105°, and the direction is to protrude toward the negative direction of the x-axis and y-axis to obtain the initial figure 1, and use a straight line y=-x is the symmetry axis, the initial figure 1 is mirror-symmetrical to obtain the initial figure 2, the line segment HW, the line segment LW, the initial figure 1 and the initial figure 2 are combined to obtain the rotation figure 1, and the rotation figure 1 is represented by a point is the rotation point, rotate 60°, 120°, 180°, 240° and 300° clockwise, respectively, to obtain the rotation figure 2, the rotation figure 3, the rotation figure 4, the rotation figure 5 and the rotation figure 6, the rotation figure 1, the rotation Figure 2, Rotation Figure 3, Rotation Figure 4, Rotation Figure 5 and Rotation Figure 6 are combined to obtain a closed figure, and the radius of the circular coverage of the closed figure is reduced to 0.77234 times of the original to obtain the design shape and size of the required metal antenna patch 4 , cutting according to the design shape and size to obtain the metal antenna patch 4; the radius of the four cylindrical holes 6 on the dielectric substrate 2 is 0.5mm, and the connecting lines of the centers of the four cylindrical holes 6 form a square with a side length of 22mm , the vertical distances between the upper and lower sides of the square and the upper and lower sides of the dielectric substrate 2 are 2.8mm and 5.2mm respectively, and the vertical distances between the left and right sides of the square and the left and right sides of the dielectric substrate 2 are 2mm and 6mm respectively; the cylindrical metal conductor 5 One end of one end is connected with metal antenna patch 4, and the material of cylindrical metal conductor 5 is copper, and its bottom surface radius r=0.5mm, thickness d=2.54mm, and the center of circle of the junction of cylindrical metal conductor 5 and metal antenna patch 4 and The vertical distances of the four sides of the dielectric substrate 2 are 16.48mm, 16.48mm, 13.52mm and 13.52mm respectively, and the diameter of the round hole 7 on the ground plate 3 opposite to the cylindrical metal conductor 5 is R=1.9mm. The output interface at the other end of the conductor 5 is connected to the energy management circuit, and the energy management circuit is used for storing the absorbed energy.
图3是利用HFSS天线模拟仿真软件模拟的减弱后瓣影响的高频吸收天线的回波损耗图,由图可知,该减弱后瓣影响的高频吸收天线的回波损耗为-37dB,比其它相同体积天线的回波损耗还要小,性能非常好。Figure 3 is the return loss diagram of the high-frequency absorbing antenna with weakened back-lobe effect simulated by HFSS antenna simulation software. It can be seen from the figure that the return loss of the high-frequency absorber antenna with reduced back-lobe effect is -37dB, which is higher than other The return loss of the antenna with the same volume is even smaller, and the performance is very good.
图4是利用HFSS天线模拟仿真软件模拟的减弱后瓣影响的高频吸收天线输入阻抗图,由图可知,该减弱后瓣影响的高频吸收天线在2.45GHz的输入阻抗为47.88Ω,非常接近标准阻抗50Ω。Figure 4 is the input impedance diagram of the high-frequency absorbing antenna with reduced back-lobe effect simulated by HFSS antenna simulation software. It can be seen from the figure that the input impedance of the high-frequency absorber antenna with reduced back-lobe effect at 2.45GHz is 47.88Ω, which is very close to Standard impedance 50Ω.
以上实施例描述了本发明的基本原理、主要特征及优点,本行业的技术人员应该了解,本发明不受上述实施例的限制,上述实施例和说明书中描述的只是说明本发明的原理,在不脱离本发明原理的范围下,本发明还会有各种变化和改进,这些变化和改进均落入本发明保护的范围内。The above embodiments have described the basic principles, main features and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited by the above embodiments. What are described in the above embodiments and description are only to illustrate the principles of the present invention. Without departing from the scope of the principle of the present invention, there will be various changes and improvements in the present invention, and these changes and improvements all fall within the protection scope of the present invention.
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