CN102904064A - an antenna - Google Patents

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CN102904064A
CN102904064A CN2012103754853A CN201210375485A CN102904064A CN 102904064 A CN102904064 A CN 102904064A CN 2012103754853 A CN2012103754853 A CN 2012103754853A CN 201210375485 A CN201210375485 A CN 201210375485A CN 102904064 A CN102904064 A CN 102904064A
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cavity
antenna
cone
patch
antenna according
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CN102904064B (en
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张艳君
杨慧杰
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China Academy of Space Technology CAST
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Abstract

本发明涉及一种天线,包括微带激励器(1)和腔体(2);腔体(2)的顶部直径比底部直径大;所述腔体(2)包括从下到上依次分布的多个锥形腔体,从下到上分布的多个锥形腔体的斜率逐渐变大;所述微带激励器位于腔体(2)内。本发明的天线具有高增益、小型化、结构简单、易加工的特点。

The invention relates to an antenna, comprising a microstrip exciter (1) and a cavity (2); the top diameter of the cavity (2) is larger than the bottom diameter; the cavity (2) includes sequentially distributed from bottom to top A plurality of conical cavities, the slope of the plurality of conical cavities distributed from bottom to top gradually increases; the microstrip actuator is located in the cavities (2). The antenna of the invention has the characteristics of high gain, miniaturization, simple structure and easy processing.

Description

一种天线an antenna

技术领域 technical field

本发明涉及一种天线。The invention relates to an antenna.

背景技术 Background technique

微波通信领域中,某卫星S频段相控阵天线(工作在S频段的接收天线)为高增益大范围扫描的相控阵天线,工作方式为双圆极化,同时为提高侦察截获信号的能力,并且减少天线单元和通道数目,对天线阵元提出了高增益和小型化的要求。常见的用来提高天线单元增益的方法为带辐射腔体的天线,例如在微带贴片辐射方向增加喇叭结构来提高增益,但该类结构天线效率比较低,天线方向图主瓣对称性和滚降较差,并且天线外型尺寸和质量比较大。目前国内外已有的高增益增强型天线大多具有的缺点在于:a.尺寸大,体积大,口径效率低;b.结构复杂,不易加工。In the field of microwave communication, a satellite S-band phased array antenna (receiving antenna working in the S-band) is a phased array antenna with high gain and large-scale scanning, and the working mode is dual circular polarization. , and reduce the number of antenna elements and channels, and put forward the requirements of high gain and miniaturization for the antenna elements. A common method to increase the gain of the antenna unit is an antenna with a radiating cavity, such as adding a horn structure in the radiation direction of the microstrip patch to increase the gain, but the efficiency of this type of structural antenna is relatively low, and the main lobe of the antenna pattern is symmetric and The roll-off is poor, and the antenna size and quality are relatively large. At present, most of the existing high-gain enhanced antennas at home and abroad have the following disadvantages: a. large size, large volume, and low aperture efficiency; b. complex structure and difficult to process.

发明内容 Contents of the invention

本发明的目的在于克服现有技术的不足,提供一种高增益、小型化、结构简单、易加工的天线。The purpose of the present invention is to overcome the deficiencies of the prior art and provide an antenna with high gain, miniaturization, simple structure and easy processing.

本发明的上述目的是通过如下技术方案予以实现的:Above-mentioned purpose of the present invention is achieved by following technical scheme:

一种天线,包括微带激励器和腔体;腔体的顶部直径比底部直径大;所述腔体包括从下到上依次分布的多个锥形腔体,从下到上分布的多个锥形腔体的斜率逐渐变大;所述微带激励器位于腔体内。An antenna, including a microstrip exciter and a cavity; the top diameter of the cavity is larger than the bottom diameter; the cavity includes a plurality of tapered cavities distributed sequentially from bottom to top, and a plurality of tapered cavities distributed from bottom to top The slope of the tapered cavity gradually becomes larger; the microstrip actuator is located in the cavity.

所述多个锥形腔体为3个。There are three tapered cavities.

每个锥形腔体的高度均等于1/4工作波长。The height of each tapered cavity is equal to 1/4 of the working wavelength.

所述微带激励器包括上层寄生贴片、下层辐射贴片和介质支撑棒;所述介质支撑棒将上层寄生贴片和下层辐射贴片悬于空气中。The microstrip exciter includes an upper parasitic patch, a lower radiation patch and a dielectric support rod; the dielectric support rod suspends the upper parasitic patch and the lower radiation patch in the air.

所述上层寄生贴片和下层辐射贴片均为圆形。Both the upper parasitic patch and the lower radiation patch are circular.

所述介质支撑棒为四根聚酰亚胺介质棒。The medium support rods are four polyimide medium rods.

所述腔体的底部作为微带激励器的接地板。The bottom of the cavity serves as a ground plate for the microstrip driver.

所述天线还包括馈电部分,所述馈电部分包括多个同轴馈电探针,在腔体的底部形成多个用于容纳所述馈电探针的通孔,所述多个同轴馈电探针与下层辐射贴片接触。The antenna also includes a feeding part, the feeding part includes a plurality of coaxial feeding probes, and a plurality of through holes for accommodating the feeding probes are formed at the bottom of the cavity, and the plurality of coaxial feeding probes are formed at the bottom of the cavity. The shaft-fed probe is in contact with the underlying radiating patch.

所述多个同轴馈电探针为4个方形同轴馈电探针。The plurality of coaxial feeding probes are four square coaxial feeding probes.

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、通过采用多级渐变锥形腔体结构,可有效降低腔体剖面,使之具有紧凑结构;采用这种突变不连续结构,加强了腔体内局部场强的显著集中,使后向辐射电磁波发生反射,并与前向辐射波同相叠加,最终最大限度增强天线的正向辐射,从而使天线获得高增益和良好的主瓣特性,天线口径效率达94.8%;天线结构紧凑便于组阵,可以实现阵列的小型化和轻量化;1. By adopting a multi-stage tapered cavity structure, the section of the cavity can be effectively reduced, so that it has a compact structure; the adoption of this abruptly discontinuous structure strengthens the significant concentration of the local field strength in the cavity, and makes the electromagnetic wave radiate backward Reflection occurs and is superimposed in phase with the forward radiation wave, and finally the forward radiation of the antenna is enhanced to the maximum, so that the antenna obtains high gain and good main lobe characteristics, and the antenna aperture efficiency reaches 94.8%; the antenna structure is compact and easy to form an array, and can Realize the miniaturization and light weight of the array;

2、本发明的天线结构克服了传统波纹喇叭和螺旋天线的诸多缺点,具有强度高、剖面低、结构简单、易加工和易安装的优点,电性能优良,实现了高增益和高效率。2. The antenna structure of the present invention overcomes many shortcomings of traditional corrugated horns and helical antennas, and has the advantages of high strength, low profile, simple structure, easy processing and easy installation, excellent electrical performance, and high gain and high efficiency.

3、采用该天线作为阵元便于实现天线阵列的小型化和轻量化,因此在相控阵天线系统中,尤其是高轨电子侦察卫星接收天线系统中具有广泛的应用前景。3. Using the antenna as an array element facilitates miniaturization and light weight of the antenna array, so it has broad application prospects in phased array antenna systems, especially in high-orbit electronic reconnaissance satellite receiving antenna systems.

附图说明Description of drawings

图1为本发明高增益多级渐变锥形腔体天线结构示意图;Fig. 1 is a schematic diagram of the structure of the high-gain multi-stage tapered cavity antenna of the present invention;

图2为本发明高增益多级渐变锥形腔体天线结构剖面图;2 is a cross-sectional view of the structure of the high-gain multi-stage tapered cavity antenna of the present invention;

图3为本发明微带激励器结构示意图;Fig. 3 is the structure schematic diagram of microstrip exciter of the present invention;

图4为本发明多级锥形辐射腔体结构示意图;Fig. 4 is a schematic diagram of the structure of the multi-stage conical radiation cavity of the present invention;

图5为本发明方形同轴馈电部分结构示意图。Fig. 5 is a schematic diagram of the structure of the square coaxial feeding part 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内容作进一步的详细说明:Below in conjunction with accompanying drawing and specific embodiment content of the present invention is described in further detail:

如图1所示为本发明的天线结构示意图,如图2所示为本发明的天线结构剖面图,由图可以看出本发明的天线包括微带激励器1、多级渐变锥形辐射腔体2、和馈电部分3。多级渐变锥形辐射腔体2的顶部开口,底部封闭。顶部的直径比底部的直径大。多级渐变锥形辐射腔体2的斜率依次变大。微带激励器1位于腔体2内,并安装在腔体2的底部中心位置;通过馈电部分3给微带激励器1馈电。采用多级渐变锥形腔体可提高天线效率和增益,同时降低天线剖面高度。本实施方式中的天线最大口径在250mm~265mm范围内,天线剖面高度最大在95mm~105mm范围内。根据天线增益要求、天线口径和剖面高度要求确定锥形腔体的级数;级数越少,天线剖面高度越低,但若要达到15dBi增益,则会使得天线方向图主瓣对称性和滚降较差,同时天线口径效率变低;级数越高,天线方形图主瓣对称性和滚降越好,但天线剖面高度越高,不利于实现天线的小型化和轻量化,级数过多也会导致天线口径利用效率降低,同时也由于互耦的增加将不利于天线组阵。锥体斜率由每级锥形腔体高度和锥形腔体底面、顶面直径决定,每级锥形腔体高度均等于1/4工作波长,根据天线增益要求和最大限度提高天线口径效率目标,加强腔体内局部场强的集中,优化设计出每级锥形腔体底面和顶面直径。As shown in Figure 1, it is a schematic diagram of the antenna structure of the present invention, and as shown in Figure 2, it is a sectional view of the antenna structure of the present invention, as can be seen from the figure that the antenna of the present invention includes a microstrip exciter 1, a multi-stage tapered radiation cavity Body 2, and feeder part 3. The top of the multi-stage tapered radiation cavity 2 is open and the bottom is closed. The diameter of the top is larger than the diameter of the bottom. The slope of the multi-stage tapered radiation cavity 2 becomes larger successively. The microstrip exciter 1 is located in the cavity 2 and installed at the center of the bottom of the cavity 2 ; the microstrip exciter 1 is fed through the feeding part 3 . The use of a multi-stage tapered cavity can improve antenna efficiency and gain while reducing the height of the antenna profile. The maximum diameter of the antenna in this embodiment is in the range of 250 mm to 265 mm, and the maximum cross-sectional height of the antenna is in the range of 95 mm to 105 mm. Determine the series of tapered cavity according to the antenna gain requirements, antenna aperture and section height requirements; the fewer the series, the lower the antenna section height, but to achieve 15dBi gain, it will make the main lobe symmetry and roll of the antenna pattern At the same time, the antenna aperture efficiency becomes lower; the higher the number of series, the better the symmetry and roll-off of the main lobe of the antenna square diagram, but the higher the height of the antenna profile, it is not conducive to the miniaturization and light weight of the antenna. Too many will also lead to a decrease in the utilization efficiency of the antenna aperture, and at the same time, the increase in mutual coupling will not be conducive to the antenna array. The slope of the cone is determined by the height of each conical cavity and the diameter of the bottom and top surfaces of the conical cavity. The height of each conical cavity is equal to 1/4 of the working wavelength. According to the antenna gain requirements and the goal of maximizing the antenna aperture efficiency , strengthen the concentration of the local field strength in the cavity, and optimize the design of the bottom and top diameters of each conical cavity.

如图3所示,微带激励器1由上层寄生贴片4、下层辐射贴片5和起支撑作用的四根聚酰亚胺材料介质支撑棒6组成。四根聚酰亚胺材料介质支撑棒6均匀分布在同一圆周上,用于将上层寄生贴片4、下层辐射贴片5悬于空气中。介质支撑棒6一端与上层寄生贴片4固定,另一端穿过下层辐射贴片5与腔体2的底部接触(如图2所示)。寄生贴片4和辐射贴片5均采用圆形结构。上层寄生贴片4的半径比下层辐射贴片5的半径小,上层寄生贴片4主要是用来展宽带宽,下层辐射贴片5主要用于调节增益。其中上层寄生贴片4的直径d4=52mm,相对于多级渐变锥形辐射腔体底部的高度h4=17mm,厚度m4=1mm,辐射贴片5的直径d5=75mm,相对于多级渐变锥形辐射腔体底部的高度h5=5.8mm,厚度m5=1mm。微带激励器采用双层结构,寄生贴片和辐射贴片采用悬空结构,并用四根聚酰亚胺介质棒进行支撑,采用上述结构有效展宽了天线阻抗带宽,并降低了损耗。As shown in FIG. 3 , the microstrip driver 1 is composed of an upper parasitic patch 4 , a lower radiation patch 5 and four polyimide dielectric support rods 6 for support. Four dielectric support rods 6 made of polyimide material are evenly distributed on the same circumference, and are used to suspend the upper layer parasitic patch 4 and the lower layer radiation patch 5 in the air. One end of the dielectric support rod 6 is fixed to the upper parasitic patch 4 , and the other end passes through the lower radiation patch 5 and contacts the bottom of the cavity 2 (as shown in FIG. 2 ). Both the parasitic patch 4 and the radiation patch 5 adopt a circular structure. The radius of the upper parasitic patch 4 is smaller than that of the lower radiation patch 5 , the upper parasitic patch 4 is mainly used to widen the bandwidth, and the lower radiation patch 5 is mainly used to adjust the gain. The diameter d4=52mm of the upper parasitic patch 4, the height h4=17mm relative to the bottom of the multi-stage tapered radiation cavity, the thickness m4=1mm, the diameter d5=75mm of the radiation patch 5, relative to the multi-stage tapered radiation cavity The height of the bottom of the shaped radiation cavity h5=5.8mm, and the thickness m5=1mm. The microstrip exciter adopts a double-layer structure. The parasitic patch and the radiation patch adopt a suspended structure and are supported by four polyimide dielectric rods. The above structure effectively widens the antenna impedance bandwidth and reduces loss.

如图2,4所示;多级渐变锥形腔体2优选为三级,由第一级锥形腔体7、第二级锥形腔体8和第三级锥形腔体9组成,第一级锥形腔体7顶面直径与第二级锥形腔体8底面直径相等,第二级锥形腔体8顶面直径与第三级锥形腔体9底面直径相等。三级锥形腔体的斜率依次变大。多级渐变锥形腔体2底面作为接地板,并设置4个用于容纳馈电探针的方形孔10。如图2所示剖面图,以锥形腔体底面线为基准线,对每级腔体母线与基准线之间的夹角取正切值即为每级腔体的锥体斜率。其中第一级锥形腔体7底面直径d7=190mm,锥体斜率为k1=1.6,第二级锥形腔体8底面直径为d8=233.4mm,锥体斜率为k2=3.8,第三级锥形腔体9底面直径为d9=251.8mm,锥体斜率为k3=8.5,顶面直径(最大口面直径)260mm,每级锥形腔体高度均等于1/4工作波长,多级渐变锥形腔体2最大口径直径为1.86工作波长。高增益多级渐变锥形腔体天线采用3级不同斜率渐变锥形腔体,可使腔体内局部场强显著集中,在达到15dB i高增益的同时最大限度的提高了天线口径效率,天线方向图主瓣接近线性滚降,同时天线整体剖面高度比较低,便于实现天线的小型化和轻量化。As shown in Figures 2 and 4; the multi-stage tapered cavity 2 is preferably three-stage, consisting of a first-stage tapered cavity 7, a second-stage tapered cavity 8 and a third-stage tapered cavity 9, The diameter of the top surface of the first-stage conical cavity 7 is equal to the diameter of the bottom surface of the second-stage conical cavity 8 , and the diameter of the top surface of the second-stage conical cavity 8 is equal to the diameter of the bottom surface of the third-stage conical cavity 9 . The slope of the three-stage conical cavity becomes larger in turn. The bottom surface of the multi-stage tapered cavity 2 is used as a grounding plate, and four square holes 10 for accommodating feeding probes are provided. As shown in the sectional view in Figure 2, taking the bottom line of the conical cavity as the reference line, taking the tangent value of the angle between the busbar of each cavity and the reference line is the slope of the cone of each cavity. Wherein the diameter of the bottom surface of the first-stage conical cavity 7 is d7=190mm, and the slope of the cone is k1=1.6; the diameter of the bottom surface of the second-stage conical cavity 8 is d8=233.4mm, and the slope of the cone is k2=3.8; The diameter of the bottom surface of the conical cavity 9 is d9=251.8mm, the slope of the cone is k3=8.5, the diameter of the top surface (the maximum diameter of the mouth surface) is 260mm, and the height of each conical cavity is equal to 1/4 of the working wavelength, multi-level gradient The maximum diameter of the tapered cavity 2 is 1.86 working wavelength. The high-gain multi-level tapered cavity antenna adopts 3 levels of tapered cavity with different slopes, which can significantly concentrate the local field strength in the cavity, and maximize the antenna aperture efficiency and antenna direction while achieving a high gain of 15dB i. The main lobe in the figure is close to linear roll-off, and the overall section height of the antenna is relatively low, which facilitates the miniaturization and weight reduction of the antenna.

如图5所示,馈电部分3包括多个同轴馈电结构,所述多个同轴馈电结构优选为4个方形同轴馈电结构,方形同轴馈电结构由方形同轴馈电探针11和方形同轴介质12和方形同轴外导体13组成,4个方形同轴馈电探针11穿过腔体2底部的通孔10后与下层辐射贴片5接触。4个方形同轴馈电探针11以腔体2的底部圆心为中心,分布在同一圆周上;其幅度相同,相位依次相差90°。馈电部分采用相位依次相差90°的4个方形同轴馈电探针11对下层辐射贴片5进行平衡馈电,可方便获得双圆极化性能,显著改善了轴比带宽和圆极化性能。As shown in Figure 5, the feeding part 3 includes a plurality of coaxial feeding structures, and the plurality of coaxial feeding structures are preferably 4 square coaxial feeding structures, and the square coaxial feeding structure is formed by a square coaxial feeding structure. The electrical probe 11 is composed of a square coaxial medium 12 and a square coaxial outer conductor 13. Four square coaxial feeding probes 11 pass through the through hole 10 at the bottom of the cavity 2 and then contact the lower radiation patch 5. The four square coaxial feeding probes 11 are centered on the center of the bottom of the cavity 2 and distributed on the same circumference; their amplitudes are the same, and their phases are sequentially different by 90°. The feeding part uses four square coaxial feeding probes 11 with a phase difference of 90° in sequence to feed the lower radiation patch 5 in a balanced manner, which can conveniently obtain dual circular polarization performance and significantly improve the axial ratio bandwidth and circular polarization performance.

本发明的天线的工作原理如下:The working principle of the antenna of the present invention is as follows:

天线由微带激励器和多级渐变锥形腔体组成,微带激励器采用双层结构,由上下两个不同直径和高度、悬空放置的贴片组成,用于展宽阻抗带宽,并降低损耗,其中下层辐射贴片由4个幅度相同,相位依次相差90°的方同轴馈电探针进行平衡馈电;多级渐变锥形腔体采用了不同斜率的渐变3级腔体结构,由于微带激励器仅辐射单一的TE11模式的电磁波,抑制了高次模的产生,同时这些突变不连续结构又加强了腔体内局部场强的显著集中;通过综合优化每级锥体斜率和锥体高度,使后向辐射电磁波反射后与前向辐射波同相叠加,直到满足所需高增益的同时方向图主瓣接近线性滚降,并且使辐射腔体最大口径和剖面最小化,最终设计出具有良好电性能的高增益天线。The antenna consists of a microstrip exciter and a multi-stage tapered cavity. The microstrip exciter adopts a double-layer structure, consisting of two patches with different diameters and heights suspended in the air, which are used to widen the impedance bandwidth and reduce loss. , in which the lower radiation patch is fed by four square coaxial feeding probes with the same amplitude and 90° phase difference in turn; the multi-stage tapered cavity adopts a gradual three-level cavity structure with different slopes. The microstrip exciter only radiates a single TE11 mode electromagnetic wave, which suppresses the generation of high-order modes. At the same time, these abruptly discontinuous structures strengthen the significant concentration of the local field strength in the cavity; by comprehensively optimizing the slope of each cone and cone Height, so that the backward radiation electromagnetic wave is reflected and superimposed in phase with the forward radiation wave until the required high gain is met, while the main lobe of the pattern is close to linear roll-off, and the maximum diameter and section of the radiation cavity are minimized, and finally a design with High gain antenna with good electrical performance.

通过以上设计,本发明高增益多级渐变锥形腔体天线的电性能可以达到:Through the above design, the electrical performance of the high-gain multi-stage tapered cavity antenna of the present invention can reach:

极化方式:左右旋圆极化;Polarization mode: left and right circular polarization;

增益:15.1dBi;天线中心频率处最大增益为15.1dBi,在7.2%的相对带宽内大于15dBi,方向图主瓣对称性比较好,方向图主瓣锥削和滚降较快,天线口径效率为94.8%。Gain: 15.1dBi; the maximum gain at the center frequency of the antenna is 15.1dBi, which is greater than 15dBi within the relative bandwidth of 7.2%, the symmetry of the main lobe of the pattern is relatively good, the main lobe of the pattern is tapered and rolled off quickly, and the aperture efficiency of the antenna is 94.8%.

驻波:<1.4(在带宽范围内);该天线在14%的相对带宽内可以获得VSWR<1.4的性能。Standing wave: <1.4 (within the bandwidth); the antenna can obtain the performance of VSWR<1.4 within 14% of the relative bandwidth.

轴比:<1.2dB(在带宽范围内);在±25°波束范围内小于1.2dB,圆极化特性良好。Axial ratio: <1.2dB (in the bandwidth range); less than 1.2dB in the ±25° beam range, good circular polarization characteristics.

由于本发明的高增益多级渐变锥形腔体天线具有高增益、高效率、低剖面、天线方向图主瓣对称性和滚降好的优点,因此由本发明的高增益多级渐变锥形腔体天线可以组成32元稀疏天线阵,在天线阵的直径小于2m,扫描角度±13°情况下增益大于28.1dBi,阵列旁瓣抑制到小于-16dB。Since the high-gain multistage tapered cavity antenna of the present invention has the advantages of high gain, high efficiency, low profile, antenna pattern main lobe symmetry and good roll-off, the high-gain multistage tapered cavity antenna of the present invention The body antenna can form a 32-element sparse antenna array. When the diameter of the antenna array is less than 2m and the scanning angle is ±13°, the gain is greater than 28.1dBi, and the sidelobe of the array is suppressed to less than -16dB.

以上所述,仅为本发明最佳的具体实施方式,但本发明的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,可轻易想到的变化或替换,都应涵盖在本发明的保护范围之内。The above description is only the best specific implementation mode of the present invention, but the scope of protection of the present invention is not limited thereto. Any person skilled in the art can easily conceive of changes or modifications within the technical scope disclosed in the present invention. Replacement should be covered within the protection scope of the present invention.

本发明说明书中未作详细描述的内容属于本领域专业技术人员的公知技术。The content that is not described in detail in the specification of the present invention belongs to the well-known technology of those skilled in the art.

Claims (9)

1. an antenna comprises micro-strip excitation device (1) and cavity (2); Cavity (2) top diameter larger than base diameter; It is characterized in that: described cavity (2) comprises a plurality of cone-shaped cavities that distribute successively from top to bottom, and the slope of a plurality of cone-shaped cavities that distribute from top to bottom becomes large gradually; Described micro-strip excitation device is positioned at cavity (2).
2. multistage gradual change cone-shaped cavity antenna according to claim 1, it is characterized in that: described a plurality of cone-shaped cavities are 3.
3. multistage gradual change cone-shaped cavity antenna according to claim 1 and 2, it is characterized in that: the height of each cone-shaped cavity is equal to 1/4 operation wavelength.
4. antenna according to claim 1 is characterized in that: described micro-strip excitation device (1) comprises upper strata parasitic patch (4), lower floor's radiation patch (5) and dielectric support rod (6); Described dielectric support rod (6) is suspended from upper strata parasitic patch (4) and lower floor's radiation patch (5) in the air.
5. antenna according to claim 4, it is characterized in that: described upper strata parasitic patch (4) and lower floor's radiation patch (5) are circle.
6. it is characterized in that according to claim 4 or 5 described antennas: described dielectric support rod (6) is four polyimides dielectric rods (6).
7. according to claim 1 or 4 described antennas, it is characterized in that: the bottom of described cavity (2) is as the ground plate of micro-strip excitation device (1).
8. multistage gradual change cone-shaped cavity antenna according to claim 7, it is characterized in that: described antenna also comprises feed part (3), described feed part (3) comprises a plurality of coaxial feed probe, form a plurality of through holes be used to holding described feed probes in the bottom of cavity (2), described a plurality of coaxial feed probe contact with lower floor's radiation patch (5).
9. multistage gradual change cone-shaped cavity antenna according to claim 8, it is characterized in that: described a plurality of coaxial feed probe are 4 square coaxial feed probe.
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CN107181050A (en) * 2017-04-06 2017-09-19 上海交通大学 The high-gain circular polarised array antenna of bowl-type high impedance reflector
CN110828983A (en) * 2019-10-18 2020-02-21 江苏三和欣创通信科技有限公司 Dual-frequency microstrip antenna device
CN111525275A (en) * 2020-05-06 2020-08-11 合肥若森智能科技有限公司 Variable polarization luneberg lens antenna
CN111740214A (en) * 2020-06-20 2020-10-02 北京华龙通科技有限公司 Measuring antenna adopting wave dish-shaped director
CN111786121A (en) * 2020-07-10 2020-10-16 深圳迈睿智能科技有限公司 Microwave detector and its side lobe suppression method
CN113644447A (en) * 2020-05-11 2021-11-12 诺基亚通信公司 Antenna device

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CN101170220A (en) * 2007-10-30 2008-04-30 北京卫星信息工程研究所 Dual-frequency band and dual round polarization rear radiation spiral antenna
CN101436715A (en) * 2008-12-05 2009-05-20 邢红兵 Dual polarization back cavity type radiating antenna
CN201601227U (en) * 2009-12-15 2010-10-06 西安科技大学 An Indoor MIMO Antenna

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CN101170220A (en) * 2007-10-30 2008-04-30 北京卫星信息工程研究所 Dual-frequency band and dual round polarization rear radiation spiral antenna
CN101436715A (en) * 2008-12-05 2009-05-20 邢红兵 Dual polarization back cavity type radiating antenna
CN201601227U (en) * 2009-12-15 2010-10-06 西安科技大学 An Indoor MIMO Antenna

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107181050A (en) * 2017-04-06 2017-09-19 上海交通大学 The high-gain circular polarised array antenna of bowl-type high impedance reflector
CN110828983A (en) * 2019-10-18 2020-02-21 江苏三和欣创通信科技有限公司 Dual-frequency microstrip antenna device
CN111525275A (en) * 2020-05-06 2020-08-11 合肥若森智能科技有限公司 Variable polarization luneberg lens antenna
CN113644447A (en) * 2020-05-11 2021-11-12 诺基亚通信公司 Antenna device
CN111740214A (en) * 2020-06-20 2020-10-02 北京华龙通科技有限公司 Measuring antenna adopting wave dish-shaped director
CN111740214B (en) * 2020-06-20 2022-08-05 北京华龙通科技有限公司 Measuring antenna adopting wave dish-shaped director
CN111786121A (en) * 2020-07-10 2020-10-16 深圳迈睿智能科技有限公司 Microwave detector and its side lobe suppression method

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