CN103457017A - Three-frequency dual polarization cone conformal micro-strip antenna array - Google Patents

Three-frequency dual polarization cone conformal micro-strip antenna array Download PDF

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CN103457017A
CN103457017A CN2013104051046A CN201310405104A CN103457017A CN 103457017 A CN103457017 A CN 103457017A CN 2013104051046 A CN2013104051046 A CN 2013104051046A CN 201310405104 A CN201310405104 A CN 201310405104A CN 103457017 A CN103457017 A CN 103457017A
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microstrip
frequency
microstrip antenna
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antenna array
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王昊
陈康
周静
方鑫
张平平
孙长富
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Nanjing University of Science and Technology
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Abstract

本发明公开了一种三频双极化圆锥共形全向微带天线阵列,通过将单频和双频的微带天线阵列呈上下放置在圆锥体表面来实现三频工作,同时天线阵列均匀围绕在圆锥体表面来实现波束全向性覆盖。每个阵列由四个微带天线单元通过微带线并联馈电构成。单频天线单元由微带天线辐射边馈电、双频天线单元由微带天线非辐射边馈电。在单频天线单元的非辐射边上通过开缝来减小贴片的尺寸,贴片单元为线极化工作;在双频天线单元的辐射边上通过开缝来实现双频,低频为圆极化,高频为线极化。天线加工所用的微带介质为易弯曲的特种介质。本发明可以在有限的载体表面实现三频双极化工作要求,且可以实现波束的全向性覆盖。

Figure 201310405104

The invention discloses a triple-frequency dual-polarization conical conformal omnidirectional microstrip antenna array. The triple-frequency operation is realized by placing the single-frequency and dual-frequency microstrip antenna arrays up and down on the surface of the cone, and the antenna array is uniform. Surround the surface of the cone to achieve omnidirectional coverage of the beam. Each array consists of four microstrip antenna elements fed in parallel through microstrip lines. The single-frequency antenna unit is fed by the radiating side of the microstrip antenna, and the dual-frequency antenna unit is fed by the non-radiating side of the microstrip antenna. Slits are made on the non-radiating side of the single-frequency antenna unit to reduce the size of the patch, and the patch unit works for linear polarization; dual-frequency is achieved by slits on the radiating side of the dual-frequency antenna unit, and the low frequency is circular Polarization, high frequency is linear polarization. The microstrip medium used in antenna processing is a flexible special medium. The invention can realize the working requirement of triple frequency and dual polarization on the limited carrier surface, and can realize the omnidirectional coverage of the beam.

Figure 201310405104

Description

三频双极化圆锥共形微带天线阵列Triple-band dual-polarized conical conformal microstrip antenna array

技术领域 technical field

本发明涉及共形于圆锥载体表面的一种微带天线阵列,特别是一种三频双极化圆锥共形微带天线阵列。 The invention relates to a microstrip antenna array conformal to the surface of a conical carrier, in particular to a triple-frequency dual-polarization conical conformal microstrip antenna array.

背景技术 Background technique

随着现代通信、军事的不断发展,机载、星载及各类通信和遥测遥控系统所需要的电子组件部件向着短、小、轻、薄、高可靠性、高速度的方向快速发展,在性能方面,迫切需要电磁兼容性好、不易受电子干扰、雷达散射截面RCS(Radar Cross Section)小,具有隐身/反隐身特性的高性能阵列天线。共形微带天线具有剖面低、重量轻、体积小、易于实现共形等一系列优点,因此近年来日益受到重视。 With the continuous development of modern communications and military, the electronic components required by airborne, spaceborne and various communication and telemetry remote control systems are developing rapidly in the direction of short, small, light, thin, high reliability and high speed. In terms of performance, there is an urgent need for high-performance array antennas with good electromagnetic compatibility, less susceptible to electronic interference, small RCS (Radar Cross Section), and stealth/anti-stealth characteristics. Conformal microstrip antennas have a series of advantages such as low profile, light weight, small size, and easy to achieve conformality, so they have been paid more and more attention in recent years.

弹体上的共形微带天线,由于其使用环境的特殊性对共形天线的设计也提出了新的要求。弹体上的共形微带天线出于空气动力学的考虑往往需要设计在锥面上,但由于锥面几何形状相对较复杂、因此设计难度较大。另外弹体上的共形天线需要全向性,以保证弹体在飞行旋转状态下接收信号。而全向性天线的设计需要仔细的考虑天线单元的排列,使得天线方向图的全向性覆盖得到满足。随着通信技术的发展,双频和多频的工作模式日益成为技术的主流。弹体上的共形天线也有同样的需求,以保证收发共用的需要。但是如何在弹体有限的尺寸上实现双频或多频工作也是一个技术难点,现有技术中尚无相关描述。 The conformal microstrip antenna on the projectile also puts forward new requirements for the design of the conformal antenna due to the particularity of its use environment. The conformal microstrip antenna on the projectile often needs to be designed on the cone surface due to aerodynamic considerations, but due to the relatively complex geometric shape of the cone surface, the design is difficult. In addition, the conformal antenna on the projectile needs to be omnidirectional to ensure that the projectile receives signals when it is in flight and rotating. The design of the omnidirectional antenna needs to carefully consider the arrangement of the antenna elements so that the omnidirectional coverage of the antenna pattern can be satisfied. With the development of communication technology, dual-frequency and multi-frequency working modes have increasingly become the mainstream of technology. The conformal antenna on the projectile also has the same requirement to ensure the sharing of sending and receiving. However, how to realize dual-frequency or multi-frequency operation on the limited size of the missile body is also a technical difficulty, and there is no related description in the prior art.

发明内容 Contents of the invention

本发明的目的在于提供一种三频双极化圆锥共形微带天线阵列。 The object of the present invention is to provide a triple-frequency dual-polarized conical conformal microstrip antenna array.

实现本发明目的的技术解决方案为:一种三频双极化圆锥共形微带天线阵列,包括圆锥载体、第一微带线、第一微带天线阵列、第二微带线和第二微带天线阵列,所述第一微带天线阵列和第二微带天线阵列均设置在圆锥载体的外表面,并均匀的围绕在圆锥载体表面,其中第一微带天线阵列位于第二微带天线阵列的上方,其中第一微带天线阵列包括四个单频微带天线单元,该四个单频微带天线单元通过第一微带线并联,第二微带天线阵列包括四个双频微带天线单元,该四个双频微带天线单元通过第二微带线并联。  The technical solution to realize the object of the present invention is: a triple-frequency dual-polarized conical conformal microstrip antenna array, including a conical carrier, a first microstrip line, a first microstrip antenna array, a second microstrip line and a second A microstrip antenna array, the first microstrip antenna array and the second microstrip antenna array are both arranged on the outer surface of the conical carrier, and uniformly surround the surface of the conical carrier, wherein the first microstrip antenna array is located on the second microstrip Above the antenna array, wherein the first microstrip antenna array includes four single-frequency microstrip antenna units, the four single-frequency microstrip antenna units are connected in parallel through the first microstrip line, and the second microstrip antenna array includes four dual-frequency A microstrip antenna unit, the four dual-band microstrip antenna units are connected in parallel through a second microstrip line. the

本发明与现有技术相比,其显著优点为:1)在单频天线单元微带贴片上开缝,减小天线的尺寸来满足圆锥载体轴线尺寸的要求;2)在双频天线单元微带贴片上开缝,实现双频工作;3)本发明采用三种不同谐振频率的微带天线阵列上下放置在圆锥载体来满足三频的工作要求,多频的工作方式可以增加信息的通信容量;4)在双频微带天线单元中通过微扰和边馈实现圆极化工作,圆极化的工作方式用于接收GPS信号;5)在圆锥体这一复杂的几何结构上实现了全向性的天线波束覆盖,这样能保证载体在高速旋转的情况下还可以接收信号;6)本发明可以在有限的载体表面实现三频双极化工作要求,且可以实现波束的全向性覆盖。 Compared with the prior art, the present invention has the following significant advantages: 1) Slits are made on the microstrip patch of the single-frequency antenna unit to reduce the size of the antenna to meet the requirements of the axial size of the conical carrier; 2) The dual-frequency antenna unit Slits on the microstrip patch realize dual-frequency operation; 3) The present invention uses three microstrip antenna arrays with different resonant frequencies to be placed up and down on the conical carrier to meet the three-frequency working requirements, and the multi-frequency working method can increase information Communication capacity; 4) In the dual-frequency microstrip antenna unit, circular polarization is realized through perturbation and side feed, and the circular polarization working method is used to receive GPS signals; 5) Realized on the complex geometric structure of the cone Omnidirectional antenna beam coverage is achieved, which can ensure that the carrier can still receive signals under the condition of high-speed rotation; 6) The present invention can realize the three-frequency dual-polarization working requirement on the limited carrier surface, and can realize the omnidirectional beam sexual coverage.

下面结合附图对本发明作进一步详细描述。 The present invention will be described in further detail below in conjunction with the accompanying drawings.

附图说明 Description of drawings

图1为本发明的圆锥体上的三频共形微带天线结构图。 FIG. 1 is a structure diagram of a triple-band conformal microstrip antenna on a cone of the present invention.

图2为本发明的双频微带天线单元的俯视图。 Fig. 2 is a top view of the dual-band microstrip antenna unit of the present invention.

图3为本发明的双频微带天线单元的侧视图。 Fig. 3 is a side view of the dual-band microstrip antenna unit of the present invention.

图4为本发明的单频微带天线单元的俯视图。 Fig. 4 is a top view of the single-frequency microstrip antenna unit of the present invention.

图5为本发明的单频微带天线单元的侧视图。 Fig. 5 is a side view of the single-frequency microstrip antenna unit of the present invention.

图6为本发明的双频微带天线阵列的反射系数结果图。 Fig. 6 is a graph showing reflection coefficient results of the dual-band microstrip antenna array of the present invention.

图7为本发明的双频微带天线阵列低频的全向轴比结果图。 Fig. 7 is a result diagram of the omnidirectional axial ratio of the dual-frequency microstrip antenna array of the present invention at low frequencies.

图8为本发明的单频微带天线阵列的反射系数结果图。 Fig. 8 is a graph showing reflection coefficient results of the single-frequency microstrip antenna array of the present invention.

具体实施方式 Detailed ways

本发明的一种三频双极化圆锥共形微带天线阵列,包括圆锥载体1、第一微带线2、第一微带天线阵列3、第二微带线4和第二微带天线阵列5,所述第一微带天线阵列3和第二微带天线阵列5均设置在圆锥载体1的外表面,并均匀的围绕在圆锥载体表面,其中第一微带天线阵列3位于第二微带天线阵列5的上方,其中第一微带天线阵列3包括四个单频微带天线单元11,该四个单频微带天线单元11通过第一微带线2并联,第二微带天线阵列5包括四个双频微带天线单元6,该四个双频微带天线单元6通过第二微带线4并联。 A triple-frequency dual-polarized conical conformal microstrip antenna array of the present invention includes a conical carrier 1, a first microstrip line 2, a first microstrip antenna array 3, a second microstrip line 4 and a second microstrip antenna Array 5, the first microstrip antenna array 3 and the second microstrip antenna array 5 are all arranged on the outer surface of the conical carrier 1, and uniformly surround the conical carrier surface, wherein the first microstrip antenna array 3 is located on the second Above the microstrip antenna array 5, wherein the first microstrip antenna array 3 includes four single-frequency microstrip antenna units 11, the four single-frequency microstrip antenna units 11 are connected in parallel through the first microstrip line 2, and the second microstrip The antenna array 5 includes four dual-band microstrip antenna units 6 connected in parallel through the second microstrip line 4 .

所述单频微带天线单元11通过第一微带线2在辐射边进行馈电,双频微带天线单元6通过第二微带线4在非辐射边进行馈电。 The single-frequency microstrip antenna unit 11 is fed on the radiation side through the first microstrip line 2 , and the dual-frequency microstrip antenna unit 6 is fed on the non-radiation side through the second microstrip line 4 .

双频微带天线单元6包括第二地板8、第二介质9和第二微带贴片10,所述第二地板8位于第二介质9的下方,第二微带贴片10位于第二介质9的上方,第二微带贴片10的辐射边上各开有一个缝,上述两个缝关于第二微带贴片10的垂直中心线对称;单频微带天线单元11包括第一地板13、第一介质14和第一微带贴片15,所述第一地板13位于第一介质14的下方,第一微带贴片15位于第一介质14的上方,第一微带贴片15的非辐射边上各开有两个缝,所述单频微带天线单元11关于垂直中心线对称。 The dual-band microstrip antenna unit 6 includes a second floor 8, a second medium 9 and a second microstrip patch 10, the second floor 8 is located under the second medium 9, and the second microstrip patch 10 is located on the second Above the medium 9, there is a slit on the radiation side of the second microstrip patch 10, and the two slits are symmetrical about the vertical center line of the second microstrip patch 10; the single-frequency microstrip antenna unit 11 includes a first Floor 13, the first medium 14 and the first microstrip patch 15, the first floor 13 is located below the first medium 14, the first microstrip patch 15 is located above the first medium 14, the first microstrip patch There are two slits on each non-radiating side of the sheet 15, and the single-frequency microstrip antenna unit 11 is symmetrical about the vertical center line.

双频微带天线单元6的长度为b1,宽度为a1,缝隙的长度为b2,缝隙的宽度为a2,左边缝隙与天线左边沿的距离为a5,天线单元的馈线宽度为a3,天线单元的馈线距天线右边沿的距离为a4,具体尺寸为: a1为59.8mm,b1为62.0mm,a2为2.2mm,b2为45.7mm,a3为1.3mm,a4为8.3mm,a5为2.0mm。 The length of the dual-frequency microstrip antenna unit 6 is b1, the width is a1, the length of the slot is b2, the width of the slot is a2, the distance between the left slot and the left edge of the antenna is a5, the feeder line width of the antenna unit is a3, and the The distance between the feeder and the right edge of the antenna is a4, and the specific dimensions are: a1 is 59.8mm, b1 is 62.0mm, a2 is 2.2mm, b2 is 45.7mm, a3 is 1.3mm, a4 is 8.3mm, and a5 is 2.0mm.

单频微带天线单元11宽度为a6,左上缝隙与天线单元上沿的长度为b3,左上缝隙的宽度为b4,长度为a7,左上缝隙与左下缝隙的相邻边的长度b5,左下缝隙的宽度为b6,长度为a7,左下缝隙与天线单元下沿的长度为b7,馈线插入天线单元的深度为b8,馈线两边的缝宽为a8,具体尺寸为:b3为8.5mm, b4为3.0mm, b5为6.0mm, a6为56.2mm, a7为18.7mm,a8为1.1mm ,b6为3.0mm, b7为8.5mm, b8为12.0mm。 The width of the single-frequency microstrip antenna unit 11 is a6, the length of the upper left slit and the upper edge of the antenna unit is b3, the width of the upper left slit is b4, and the length is a7, the length of the adjacent side of the upper left slit and the lower left slit is b5, and the length of the upper left slit is b5. The width is b6, the length is a7, the length between the lower left slit and the bottom edge of the antenna unit is b7, the depth of the feeder inserted into the antenna unit is b8, the width of the slit on both sides of the feeder is a8, and the specific dimensions are: b3 is 8.5mm, b4 is 3.0mm , b5 is 6.0mm, a6 is 56.2mm, a7 is 18.7mm, a8 is 1.1mm, b6 is 3.0mm, b7 is 8.5mm, b8 is 12.0mm.

第二介质9和第一介质14的厚度均为1.143mm,介电常数均为2.17,损耗角均为0.0009。 Both the thickness of the second medium 9 and the first medium 14 are 1.143 mm, the dielectric constant is 2.17, and the loss angle is 0.0009.

下面结合附图对本发明作进一步详细描述。 The present invention will be described in further detail below in conjunction with the accompanying drawings.

本发明的一种L波段和S波段圆锥共形全向三频微带阵列,包括两种微带天线阵列,第一微带天线阵列对应于一个工作频率,第二微带天线阵列对应于两个工作频率,并且呈上下共形放置在圆锥体表面,其中第一微带天线阵列放置在圆锥体周长较短的部分,而相应第二微带天线阵列放置在圆锥体周长较长的部分。第一微带天线阵列和第二微带天线阵列均由四个微带天线单元通过微带线并联馈电构成,第一微带天线阵列和第二微带天线阵列的四个天线单元在圆锥的圆周上均匀分布。其第二微带天线阵列的天线单元由微带线非辐射边馈电,同时天线单元上通过在辐射边开缝来实现双频工作,天线单元低频为圆极化、高频为线极化;第一微带天线阵列的天线单元由微带线辐射边馈电,同时在天线单元的非辐射边上开缝,从而实现小型化,天线单元为线极化工作。第一微带天线阵列对应于一个工作频率、第二微带天线阵列对应于两个工作频率。 An L-band and S-band conical conformal omnidirectional triple-frequency microstrip array of the present invention includes two microstrip antenna arrays, the first microstrip antenna array corresponds to one operating frequency, and the second microstrip antenna array corresponds to two working frequency, and placed on the surface of the cone conformally up and down, where the first microstrip antenna array is placed on the shorter part of the cone circumference, and the corresponding second microstrip antenna array is placed on the longer cone circumference. part. Both the first microstrip antenna array and the second microstrip antenna array are composed of four microstrip antenna units fed in parallel by microstrip lines, and the four antenna units of the first microstrip antenna array and the second microstrip antenna array evenly distributed on the circumference. The antenna unit of the second microstrip antenna array is fed by the non-radiating side of the microstrip line. At the same time, the antenna unit realizes dual-frequency operation by slits on the radiation side. The antenna unit is circularly polarized at low frequencies and linearly polarized at high frequencies. ; The antenna unit of the first microstrip antenna array is fed by the radiating side of the microstrip line, and at the same time, slots are opened on the non-radiating side of the antenna unit, thereby realizing miniaturization, and the antenna unit works for linear polarization. The first microstrip antenna array corresponds to one operating frequency, and the second microstrip antenna array corresponds to two operating frequencies.

结合图1,本发明专利的一种L波段和S波段三频工作的全向共形微带天线阵列,包括圆锥载体1、第一微带天线阵列3、第一微带线2、第二微带天线阵列5、第二微带线4,第一微带线2通过并联馈电连接四个单频微带天线单元11,第二微带线4通过并联馈电连接四个双频微带天线单元6。 In combination with Fig. 1 , an omnidirectional conformal microstrip antenna array for L-band and S-band tri-band work according to the patent of the present invention includes a conical carrier 1, a first microstrip antenna array 3, a first microstrip line 2, a second Microstrip antenna array 5, the second microstrip line 4, the first microstrip line 2 connects four single-frequency microstrip antenna units 11 through parallel feed, and the second microstrip line 4 connects four dual-frequency microstrip antenna units 11 through parallel feed. With antenna unit 6.

结合图2,本发明专利的双频微带天线单元6的俯视图,其特征为通过在辐射边上各开一条缝隙来实现天线双频工作,输入口7为天线单元的馈电口。双频微带天线单元6的长度为b1,宽度为a1,缝隙的长度为b2,缝隙的宽度为a2,左边缝隙与天线左边沿的距离为a5,天线单元的馈线宽度为a3,天线单元的馈线距天线右边沿的距离为a4。 Combined with Fig. 2, the top view of the dual-frequency microstrip antenna unit 6 of the patent of the present invention is characterized in that the dual-frequency operation of the antenna is realized by opening a slot on each radiation side, and the input port 7 is the feed port of the antenna unit. The length of the dual-frequency microstrip antenna unit 6 is b1, the width is a1, the length of the slot is b2, the width of the slot is a2, the distance between the left slot and the left edge of the antenna is a5, the feeder width of the antenna unit is a3, and the The distance between the feeder and the right edge of the antenna is a4.

结合图3,本发明专利的双频天线单元6侧视图,该结构包括第二地板8,第二介质9,第二微带贴片10。 Referring to FIG. 3 , a side view of the patented dual-band antenna unit 6 of the present invention, the structure includes a second floor 8 , a second medium 9 , and a second microstrip patch 10 .

结合图4,本发明专利的单频天线单元11的俯视图,其特征为通过在非辐射边上开了两条缝隙来减小天线的尺寸,输入口12为天线单元的馈电口。单频微带天线单元11宽度为a6,左上缝隙与天线单元上沿的长度为b3,左上缝隙的宽度为b4,长度为a7,左上缝隙与左下缝隙的相邻边的长度b5,左下缝隙的宽度为b6,长度为a7,左下缝隙与天线单元下沿的长度为b7,馈线插入天线单元的深度为b8,馈线两边的缝宽为a8。 Referring to Fig. 4, the top view of the single-frequency antenna unit 11 of the patent of the present invention is characterized in that the size of the antenna is reduced by opening two slits on the non-radiating side, and the input port 12 is the feed port of the antenna unit. The width of the single-frequency microstrip antenna unit 11 is a6, the length of the upper left slit and the upper edge of the antenna unit is b3, the width of the upper left slit is b4, and the length is a7, the length of the adjacent side of the upper left slit and the lower left slit is b5, and the length of the upper left slit is b5. The width is b6, the length is a7, the length between the lower left slot and the bottom edge of the antenna unit is b7, the depth of the feeder inserted into the antenna unit is b8, and the width of the slot on both sides of the feeder is a8.

结合图5,本发明专利的单频天线单元11的侧视图,该结构包括第一地板13,第一介质14,第一微带贴片15。 Referring to FIG. 5 , it is a side view of the single-frequency antenna unit 11 of the patent of the present invention. The structure includes a first floor 13 , a first medium 14 , and a first microstrip patch 15 .

双频微带天线单元6的低频为圆极化、高频为线极化工作;单频微带天线单元11为线极化工作。 The low frequency of the dual-frequency microstrip antenna unit 6 is circularly polarized, and the high frequency is linearly polarized; the single-frequency microstrip antenna unit 11 is linearly polarized.

下面结合实施例对本发明专利做进一步详细的描述。 Below in conjunction with embodiment the patent of the present invention is described in further detail.

在本实施例中所用的三个频点为1.575GHz、1.78GHZ和2.428GHz,所用的介质板的介电常数为2.17,厚度为1.143mm,损耗角为0.0009。 其中圆锥载体的上边沿弧长为321mm,下边沿的弧长为433mm,圆锥的切边长为111.5mm。a1为59.8mm,b1为62.0mm,a2为2.2mm,b2为45.7mm,a3为1.3mm,a4为8.3mm,a5为2.0mm; b3为8.5mm,b4为3.0mm,b5为6.0mm,a6为56.2mm,a7为18.7mm,a8为1.1mm,b6为3.0mm,b7为8.5mm,b8为12.0mm。 The three frequency points used in this embodiment are 1.575 GHz, 1.78 GHz and 2.428 GHz, the dielectric constant of the used dielectric plate is 2.17, the thickness is 1.143 mm, and the loss angle is 0.0009. Among them, the arc length of the upper edge of the conical carrier is 321mm, the arc length of the lower edge is 433mm, and the cutting edge length of the cone is 111.5mm. a1 is 59.8mm, b1 is 62.0mm, a2 is 2.2mm, b2 is 45.7mm, a3 is 1.3mm, a4 is 8.3mm, a5 is 2.0mm; b3 is 8.5mm, b4 is 3.0mm, b5 is 6.0mm, A6 is 56.2mm, a7 is 18.7mm, a8 is 1.1mm, b6 is 3.0mm, b7 is 8.5mm, and b8 is 12.0mm.

其中图6-7分别为双频微带天线阵列对应的反射系数图和全向轴比图。图8为单频微带天线阵列对应的反射系数图。由图6-7可知,双频微带天线阵列满足双频工作要求,且轴比在全向都低于3dB。由图8可知,单频微带天线阵列满足单频工作要求。 Figures 6-7 are reflection coefficient diagrams and omnidirectional axial ratio diagrams corresponding to the dual-band microstrip antenna array, respectively. FIG. 8 is a reflection coefficient diagram corresponding to a single-frequency microstrip antenna array. It can be seen from Figure 6-7 that the dual-band microstrip antenna array meets the requirements of dual-band work, and the axial ratio is lower than 3dB in all directions. It can be seen from Figure 8 that the single-frequency microstrip antenna array meets the single-frequency working requirements.

Claims (6)

1.一种三频双极化圆锥共形微带天线阵列,其特征在于,包括圆锥载体[1]、第一微带线[2]、第一微带天线阵列[3]、第二微带线[4]和第二微带天线阵列[5],所述第一微带天线阵列[3]和第二微带天线阵列[5]均设置在圆锥载体[1]的外表面,并均匀的围绕在圆锥载体表面,其中第一微带天线阵列[3]位于第二微带天线阵列[5]的上方,其中第一微带天线阵列[3]包括四个单频微带天线单元[11],该四个单频微带天线单元[11]通过第一微带线[2]并联,第二微带天线阵列[5]包括四个双频微带天线单元[6],该四个双频微带天线单元[6]通过第二微带线[4]并联。 1. A triple-frequency dual-polarized conical conformal microstrip antenna array, characterized in that it comprises a conical carrier [1], the first microstrip line [2], the first microstrip antenna array [3], the second microstrip Stripline [4] and the second microstrip antenna array [5], the first microstrip antenna array [3] and the second microstrip antenna array [5] are all arranged on the outer surface of the conical carrier [1], and Evenly surround the surface of the conical carrier, wherein the first microstrip antenna array [3] is located above the second microstrip antenna array [5], wherein the first microstrip antenna array [3] includes four single-frequency microstrip antenna elements [11], the four single-frequency microstrip antenna units [11] are connected in parallel through the first microstrip line [2], and the second microstrip antenna array [5] includes four dual-frequency microstrip antenna units [6], the Four dual-frequency microstrip antenna units [6] are connected in parallel through the second microstrip line [4]. 2.根据权利要求1所述的三频双极化圆锥共形微带天线阵列,其特征在于,所述单频微带天线单元[11]通过第一微带线[2]在辐射边进行馈电,双频微带天线单元[6]通过第二微带线[4]在非辐射边进行馈电。 2. triple-frequency dual-polarization conical conformal microstrip antenna array according to claim 1, is characterized in that, described single-frequency microstrip antenna unit [11] is carried out on radiation side by the first microstrip line [2] Feeding, the dual-frequency microstrip antenna unit [6] is fed on the non-radiating side through the second microstrip line [4]. 3.根据权利要求1或2所述的三频双极化圆锥共形微带天线阵列,其特征在于,双频微带天线单元[6]包括第二地板[8]、第二介质[9]和第二微带贴片[10],所述第二地板[8]位于第二介质[9]的下方,第二微带贴片[10]位于第二介质[9]的上方,第二微带贴片[10]的辐射边上各开有一个缝,上述两个缝关于第二微带贴片[10]的垂直中心线对称;单频微带天线单元[11]包括第一地板[13]、第一介质[14]和第一微带贴片[15],所述第一地板[13]位于第一介质[14]的下方,第一微带贴片[15]位于第一介质[14]的上方,第一微带贴片[15]的非辐射边上各开有两个缝,所述单频微带天线单元[11]关于垂直中心线对称。 3. according to claim 1 and 2 described triple-frequency dual-polarized conical conformal microstrip antenna arrays, it is characterized in that the dual-frequency microstrip antenna unit [6] comprises a second floor [8], a second medium [9] ] and the second microstrip patch [10], the second floor [8] is located below the second medium [9], the second microstrip patch [10] is located above the second medium [9], the second A slit is respectively arranged on the radiation side of the two microstrip patches [10], and the above-mentioned two slits are symmetrical about the vertical center line of the second microstrip patch [10]; the single-frequency microstrip antenna unit [11] includes the first The floor [13], the first medium [14] and the first microstrip patch [15], the first floor [13] is located under the first medium [14], the first microstrip patch [15] is located Above the first medium [14], two slits are opened on the non-radiating side of the first microstrip patch [15], and the single-frequency microstrip antenna unit [11] is symmetrical about the vertical center line. 4.根据权利要求3所述的三频双极化圆锥共形微带天线阵列,其特征在于,双频微带天线单元[6]的长度为b1,宽度为a1,缝隙的长度为b2,缝隙的宽度为a2,左边缝隙与天线左边沿的距离为a5,天线单元的馈线宽度为a3,天线单元的馈线距天线右边沿的距离为a4,具体尺寸为: a1为59.8mm,b1为62.0mm,a2为2.2mm,b2为45.7mm,a3为1.3mm,a4为8.3mm,a5为2.0mm。 4. triple-frequency dual-polarization conical conformal microstrip antenna array according to claim 3, is characterized in that, the length of dual-frequency microstrip antenna unit [6] is b1, and width is a1, and the length of slit is b2, The width of the slot is a2, the distance between the left slot and the left edge of the antenna is a5, the feeder width of the antenna unit is a3, the distance between the feeder line of the antenna unit and the right edge of the antenna is a4, and the specific dimensions are: a1 is 59.8mm, b1 is 62.0 mm, a2 is 2.2mm, b2 is 45.7mm, a3 is 1.3mm, a4 is 8.3mm, and a5 is 2.0mm. 5.根据权利要求3所述的三频双极化圆锥共形微带天线阵列,其特征在于,单频微带天线单元[11]宽度为a6,左上缝隙与天线单元上沿的长度为b3,左上缝隙的宽度为b4,长度为a7,左上缝隙与左下缝隙的相邻边的长度b5,左下缝隙的宽度为b6,长度为a7,左下缝隙与天线单元下沿的长度为b7,馈线插入天线单元的深度为b8,馈线两边的缝宽为a8,具体尺寸为:b3为8.5mm, b4为3.0mm, b5为6.0mm, a6为56.2mm, a7为18.7mm,a8为1.1mm,b6为3.0mm, b7为8.5mm,b8为12.0mm。 5. triple-frequency dual-polarization conical conformal microstrip antenna array according to claim 3, is characterized in that, single-frequency microstrip antenna unit [11] width is a6, and the length of upper left slit and antenna unit upper edge is b3 , the width of the upper left slot is b4, the length is a7, the length of the adjacent side of the upper left slot and the lower left slot is b5, the width of the lower left slot is b6, the length is a7, the length of the lower left slot and the lower edge of the antenna unit is b7, and the feeder is inserted The depth of the antenna unit is b8, the slot width on both sides of the feeder is a8, the specific dimensions are: b3 is 8.5mm, b4 is 3.0mm, b5 is 6.0mm, a6 is 56.2mm, a7 is 18.7mm, a8 is 1.1mm, b6 is 3.0mm, b7 is 8.5mm, and b8 is 12.0mm. 6.根据权利要求3所述的三频双极化圆锥共形微带天线阵列,其特征在于,第二介质[9]和第一介质[14]的厚度均为1.143mm,介电常数均为2.17,损耗角均为0.0009。 6. triple-frequency dual-polarization conical conformal microstrip antenna array according to claim 3, is characterized in that the thickness of the second medium [9] and the first medium [14] is 1.143mm, and the dielectric constant is equal to 1.143 mm. is 2.17, and the loss angle is 0.0009.
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Application publication date: 20131218