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CN112993560A - Antenna structure and phased array antenna - Google Patents

Antenna structure and phased array antenna Download PDF

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Publication number
CN112993560A
CN112993560A CN202110421891.8A CN202110421891A CN112993560A CN 112993560 A CN112993560 A CN 112993560A CN 202110421891 A CN202110421891 A CN 202110421891A CN 112993560 A CN112993560 A CN 112993560A
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dielectric layer
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probe
antenna
feeding
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CN112993560B (en
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郭凡玉
陈智慧
王新辉
许峰凯
朱蕾
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Chengdu Tianrui Xingtong Technology Co ltd
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Chengdu T Ray Technology Co Ltd
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/50Structural association of antennas with earthing switches, lead-in devices or lightning protectors
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems

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Abstract

The application provides an antenna structure and phased array antenna relates to phased array antenna technical field. The antenna structure comprises a feed structure, a radiation patch, a first feed probe, a second feed probe, a third feed probe and a power divider, wherein the first feed probe, the second feed probe, the third feed probe and the power divider are all connected with the radiation patch, the first feed probe, the second feed probe and the third feed probe are respectively connected with a branch of the power divider, and the feed structure is connected with a junction of the power divider, wherein the first feed probe, the second feed probe and the third feed probe are arranged in an equilateral triangle manner, so that the feed phase difference of the first feed probe, the second feed probe and the third feed probe is sequentially increased by 120 degrees. The antenna structure and the phased array antenna have the advantages that phase center offset is improved, and grating lobes caused by periodic changes of the phase centers when the array is rotated are avoided.

Description

一种天线结构与相控阵天线An antenna structure and phased array antenna

技术领域technical field

本申请涉及相控阵天线技术领域,具体而言,涉及一种天线结构与相控阵天线。The present application relates to the technical field of phased array antennas, and in particular, to an antenna structure and a phased array antenna.

背景技术Background technique

目前,圆极化天线广泛应用于我们的日常生活中。At present, circularly polarized antennas are widely used in our daily life.

然而,目前的圆极化天线普遍采用单馈和双馈形式的天线馈电结构,由于单馈和双馈形式的馈电结构不对称,因此可能出现天线方向图不圆以及相位中心偏离天线几何中心,相位中心偏移在旋转组阵时阵面扫描会出现栅瓣的情况。However, the current circularly polarized antennas generally use single-fed and double-fed antenna feed structures. Due to the asymmetry of the single-fed and double-fed feed structures, the antenna pattern may be out of circle and the phase center may deviate from the antenna geometry. Center, phase center offset When the array is rotated, grating lobes will appear in the array scan.

综上,现有的圆极化天线存在天线相位中心出现偏移,存在栅瓣的问题。To sum up, the existing circularly polarized antenna has the problem that the phase center of the antenna is shifted, and there is a problem of grating lobes.

发明内容SUMMARY OF THE INVENTION

本申请的目的在于提供一种天线结构与相控阵天线,以解决现有技术中圆极化天线存在天线相位中心出现偏移,存在栅瓣的问题。The purpose of the present application is to provide an antenna structure and a phased array antenna, so as to solve the problem that the phase center of the antenna is shifted and grating lobes exist in the circularly polarized antenna in the prior art.

为了实现上述目的,本申请实施例采用的技术方案如下:In order to achieve the above purpose, the technical solutions adopted in the embodiments of the present application are as follows:

一方面,本申请提供了一种天线结构,所述天线结构包括馈电结构、辐射贴片、第一馈电探针、第二馈电探针、第三馈电探针以及功分器,所述第一馈电探针、所述第二馈电探针、所述第三馈电探针以及所述功分器均与所述辐射贴片连接,所述第一馈电探针、所述第二馈电探针、所述第三馈电探针均分别与所述功分器的支路连接,所述馈电结构与所述功分器的合口连接,其中,In one aspect, the present application provides an antenna structure, the antenna structure includes a feed structure, a radiation patch, a first feed probe, a second feed probe, a third feed probe, and a power divider, The first feeding probe, the second feeding probe, the third feeding probe and the power divider are all connected to the radiation patch, and the first feeding probe, The second feeding probe and the third feeding probe are respectively connected to the branches of the power divider, and the feeding structure is connected to the joint of the power divider, wherein,

所述第一馈电探针、所述第二馈电探针以及所述第三馈电探针呈等边三角形排布,以使所述第一馈电探针、所述第二馈电探针以及所述第三馈电探针的馈电相位差依次增加120°。The first feeding probe, the second feeding probe and the third feeding probe are arranged in an equilateral triangle, so that the first feeding probe, the second feeding probe The feeding phase difference between the probe and the third feeding probe is sequentially increased by 120°.

可选地,所述馈电结构包括馈电线、类同轴内导体、类同轴外导体以及耦合缝隙,所述类同轴内导体分别与所述类同轴外导体、所述馈电线连接,所述馈电线与所述功分器的合口通过所述耦合缝隙实现耦合,并进行射频信号的传输。Optionally, the feeding structure includes a feeding line, a coaxial-like inner conductor, a coaxial-like outer conductor, and a coupling slot, and the coaxial-like inner conductor is respectively connected to the coaxial-like outer conductor and the feeding line. , the joint of the feed line and the power divider is coupled through the coupling slot, and transmits radio frequency signals.

可选地,所述天线结构还包括第一介质层、第二介质层以及第三介质层,所述第一介质层、所述第二介质层以及所述第三介质层逐层连接;Optionally, the antenna structure further includes a first dielectric layer, a second dielectric layer, and a third dielectric layer, and the first dielectric layer, the second dielectric layer, and the third dielectric layer are connected layer by layer;

所述第一馈电探针、所述第二馈电探针以及所述第三馈电探针均穿过所述第一介质层,所述类同轴内导体穿过所述第三介质层。The first feeding probe, the second feeding probe and the third feeding probe all pass through the first dielectric layer, and the coaxial-like inner conductor passes through the third dielectric Floor.

可选地,所述第三介质层包括第一子介质层、第二子介质层、第三子介质层、第四子介质层以及第五子介质层,所述第一子介质层、所述第二子介质层、所述第三子介质层、所述第四子介质层以及所述第五子介质层逐层连接;Optionally, the third dielectric layer includes a first sub-dielectric layer, a second sub-dielectric layer, a third sub-dielectric layer, a fourth sub-dielectric layer, and a fifth sub-dielectric layer, and the first sub-dielectric layer, all the the second sub-dielectric layer, the third sub-dielectric layer, the fourth sub-dielectric layer and the fifth sub-dielectric layer are connected layer by layer;

所述类同轴外导体穿过所述第一子介质层、所述第二子介质层、所述第三子介质层以及所述第四子介质层;所述类同轴内导体穿过所述第一子介质层、所述第二子介质层、所述第三子介质层、所述第四子介质层以及所述第五子介质层。The coaxial-like outer conductor passes through the first sub-dielectric layer, the second sub-dielectric layer, the third sub-dielectric layer and the fourth sub-dielectric layer; the coaxial-like inner conductor passes through the first sub-dielectric layer, the second sub-dielectric layer, the third sub-dielectric layer, the fourth sub-dielectric layer, and the fifth sub-dielectric layer.

可选地,所述第二介质层包括金属层,在每个所述子介质层上设置通孔后压合形成所述第三介质层。Optionally, the second dielectric layer includes a metal layer, and the third dielectric layer is formed by pressing through holes on each of the sub-dielectric layers.

可选地,所述第一介质层包括第六子介质层与第七子介质层,在所述第六子介质层与所述第七子介质层上设置通孔后压合形成所述第一介质层。Optionally, the first dielectric layer includes a sixth sub-dielectric layer and a seventh sub-dielectric layer, and the sixth sub-dielectric layer and the seventh sub-dielectric layer are provided with through holes and then pressed together to form the sixth sub-dielectric layer. a dielectric layer.

可选地,所述功分器包括三合一功分器。Optionally, the power divider includes a three-in-one power divider.

另一方面,本申请还提供了一种所述相控阵天线,包括多个上述的天线结构,多个所述天线结构旋转拼接组成所述相控阵天线。On the other hand, the present application also provides the phased array antenna, which includes a plurality of the above-mentioned antenna structures, and the plurality of the antenna structures are rotated and spliced to form the phased array antenna.

可选地,每个所述天线结构的旋转角度与馈电相位满足公式:Optionally, the rotation angle and feed phase of each of the antenna structures satisfy the formula:

Figure P_210415140105001
Figure P_210415140105001

其中,

Figure P_210415140105002
表示天线结构的旋转角度,
Figure P_210415140105003
表示天线结构的馈电相位,m=1、2…M,P≠M/2,P=2n,n表示1~M的随机数,M表示天线结构的数量。in,
Figure P_210415140105002
represents the rotation angle of the antenna structure,
Figure P_210415140105003
Represents the feed phase of the antenna structure, m=1, 2...M, P≠M/2, P=2n, n represents a random number from 1 to M, and M represents the number of antenna structures.

可选地,M=8,P=2。Optionally, M=8 and P=2.

相对于现有技术,本申请具有以下有益效果:Compared with the prior art, the present application has the following beneficial effects:

本申请提供了一种天线结构与相控阵天线,该天线结构包括馈电结构、辐射贴片、第一馈电探针、第二馈电探针、第三馈电探针以及功分器,第一馈电探针、第二馈电探针、第三馈电探针以及功分器均与辐射贴片连接,第一馈电探针、第二馈电探针、第三馈电探针均分别与功分器的支路连接,馈电结构与功分器的合口连接,其中,第一馈电探针、第二馈电探针以及第三馈电探针呈等边三角形排布,以使第一馈电探针、第二馈电探针以及第三馈电探针的馈电相位差依次增加120°。由于本申请采用三个馈电探针的方式,且三个馈电探针的馈电相位差依次增加120°,因此可以达到改善相位中心偏移,避免了旋转组阵时相位中心周期性变化引起的栅瓣。The present application provides an antenna structure and a phased array antenna. The antenna structure includes a feed structure, a radiation patch, a first feed probe, a second feed probe, a third feed probe, and a power divider , the first feed probe, the second feed probe, the third feed probe and the power divider are all connected to the radiation patch, the first feed probe, the second feed probe, the third feed probe The probes are respectively connected to the branches of the power divider, and the feed structure is connected to the joint of the power divider, wherein the first feed probe, the second feed probe and the third feed probe are equilateral triangles Arranged so that the feeding phase difference of the first feeding probe, the second feeding probe and the third feeding probe is sequentially increased by 120°. Since the present application adopts the method of three feeding probes, and the feeding phase difference of the three feeding probes increases by 120° in turn, the phase center offset can be improved, and the periodic change of the phase center when the array is rotated can be avoided. caused grating lobes.

为使本申请的上述目的、特征和优点能更明显易懂,下文特举较佳实施例,并配合所附附图,作详细说明如下。In order to make the above-mentioned objects, features and advantages of the present application more obvious and easy to understand, the preferred embodiments are exemplified below, and are described in detail as follows in conjunction with the accompanying drawings.

附图说明Description of drawings

为了更清楚地说明本申请实施例的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,应当理解,以下附图仅示出了本申请的某些实施例,因此不应被看作是对范围的限定,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其它相关的附图。In order to illustrate the technical solutions of the embodiments of the present application more clearly, the following drawings will briefly introduce the drawings that need to be used in the embodiments. It should be understood that the following drawings only show some embodiments of the present application, and therefore do not It should be regarded as a limitation of the scope. For those skilled in the art, other related drawings can also be obtained according to these drawings without any creative effort.

图1为本申请实施例提供的天线结构的一种结构示意图。FIG. 1 is a schematic structural diagram of an antenna structure provided by an embodiment of the present application.

图2为本申请实施例提供的馈电结构的一种结构示意图。FIG. 2 is a schematic structural diagram of a feeding structure provided by an embodiment of the present application.

图3为本申请实施例提供的天线结构的介质层的排列示意图。FIG. 3 is a schematic diagram of the arrangement of the dielectric layers of the antenna structure provided by the embodiment of the present application.

图4为现有技术中一种相控阵天线的拼接示意图。FIG. 4 is a schematic diagram of splicing of a phased array antenna in the prior art.

图5为本申请实施例提供的一种相控阵天线的拼接示意图。FIG. 5 is a schematic diagram of splicing of a phased array antenna according to an embodiment of the present application.

图中:100-天线结构;110-馈电结构;120-辐射贴片;130-功分器;140-第一馈电探针;150-第二馈电探针;160-第三馈电探针; 111-馈电线;112-类同轴内导体;113-类同轴外导体;114-耦合缝隙;190-第一介质层;180-第二介质层;170-第三介质层;171-第一子介质层;172-第二子介质层;173-第三子介质层;174-第四子介质层;175-第五子介质层;191-第六子介质层;192-第七子介质层;181-第八子介质层;182-第九子介质层。 In the figure: 100-antenna structure; 110-feeding structure; 120-radiating patch; 130-power splitter; 140-first feeding probe; 150-second feeding probe; 160-third feeding Probe; 111-feed line; 112-type coaxial inner conductor; 113-type coaxial outer conductor; 114-coupling slot; 190-first dielectric layer; 180-second dielectric layer; 170-third dielectric layer; 171- the first sub-dielectric layer; 172- the second sub-dielectric layer; 173- the third sub-dielectric layer; 174- the fourth sub-dielectric layer; 175- the fifth sub-dielectric layer; 191- the sixth sub-dielectric layer; 192- The seventh sub-dielectric layer; 181-the eighth sub-dielectric layer; 182-the ninth sub-dielectric layer.

具体实施方式Detailed ways

为使本申请实施例的目的、技术方案和优点更加清楚,下面将结合本申请实施例中的附图,对本申请实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例是本申请一部分实施例,而不是全部的实施例。通常在此处附图中描述和示出的本申请实施例的组件可以以各种不同的配置来布置和设计。In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments It is a part of the embodiments of the present application, but not all of the embodiments. The components of the embodiments of the present application generally described and illustrated in the drawings herein may be arranged and designed in a variety of different configurations.

因此,以下对在附图中提供的本申请的实施例的详细描述并非旨在限制要求保护的本申请的范围,而是仅仅表示本申请的选定实施例。基于本申请中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本申请保护的范围。Thus, the following detailed description of the embodiments of the application provided in the accompanying drawings is not intended to limit the scope of the application as claimed, but is merely representative of selected embodiments of the application. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of the present application.

应注意到:相似的标号和字母在下面的附图中表示类似项,因此,一旦某一项在一个附图中被定义,则在随后的附图中不需要对其进行进一步定义和解释。同时,在本申请的描述中,术语“第一”、“第二”等仅用于区分描述,而不能理解为指示或暗示相对重要性。It should be noted that like numerals and letters refer to like items in the following figures, so once an item is defined in one figure, it does not require further definition and explanation in subsequent figures. Meanwhile, in the description of the present application, the terms "first", "second", etc. are only used to distinguish the description, and cannot be understood as indicating or implying relative importance.

下面结合附图,对本申请的一些实施方式作详细说明。在不冲突的情况下,下述的实施例及实施例中的特征可以相互组合。Some embodiments of the present application will be described in detail below with reference to the accompanying drawings. The embodiments described below and features in the embodiments may be combined with each other without conflict.

正如背景技术中所述,目前的圆极化相控阵常采用将圆极化单元天线依次旋转的方式来组阵,然而,现有的单元天线多为单馈或双馈形式,其存在馈电结构不对称,天线方向图不圆以及相位中心偏离天线几何中心,相位中心偏移在旋转组阵时阵面扫描会出现栅瓣的问题。As mentioned in the background art, the current circularly polarized phased arrays are often formed by rotating the circularly polarized element antennas in sequence. The electrical structure is asymmetric, the antenna pattern is out of circle, and the phase center deviates from the geometric center of the antenna. When the phase center is offset, the grating lobe problem will occur when the array is rotated.

有鉴于此,为了解决上述问题,本申请提供了一种天线结构,通过设置三个馈电探针的方式,改善了相位中心偏移,避免了旋转组阵时相位中心周期性变化引起的栅瓣的问题。In view of this, in order to solve the above problems, the present application provides an antenna structure, which improves the offset of the phase center by setting three feeding probes, and avoids the grid caused by the periodic change of the phase center when the array is rotated. flap problem.

下面对本申请提供的天线结构进行示例性说明:The following is an exemplary description of the antenna structure provided by the present application:

作为一种可选的实现方式,请参阅图1,该天线结构100包括馈电结构110、辐射贴片120、第一馈电探针140、第二馈电探针150、第三馈电探针160以及功分器130,第一馈电探针140、第二馈电探针150、第三馈电探针160以及功分器130均与辐射贴片120连接,第一馈电探针140、第二馈电探针150、第三馈电探针160均分别与功分器130的支路连接,馈电结构110与功分器130的合口连接。As an optional implementation, please refer to FIG. 1 , the antenna structure 100 includes a feed structure 110 , a radiation patch 120 , a first feed probe 140 , a second feed probe 150 , and a third feed probe The needle 160 and the power divider 130, the first feed probe 140, the second feed probe 150, the third feed probe 160 and the power divider 130 are all connected to the radiation patch 120, and the first feed probe 140 , the second feeding probe 150 , and the third feeding probe 160 are respectively connected to the branches of the power divider 130 , and the feeding structure 110 is connected to the joint of the power divider 130 .

其中,第一馈电探针140、第二馈电探针150以及第三馈电探针160呈等边三角形排布,以使第一馈电探针140、第二馈电探针150以及第三馈电探针160的馈电相位差依次增加120°。换言之,第一馈电探针140、第二馈电探针150以及第三馈电探针160的馈电相位可以依次为0°、120°、240°。需要说明的是,馈电探针之间的相位差由功分器130的每个支路线长实现,即通过调节功分器130的线长,可以实现将三个馈电探针按等边三角形进行排布。The first feeding probe 140 , the second feeding probe 150 and the third feeding probe 160 are arranged in an equilateral triangle, so that the first feeding probe 140 , the second feeding probe 150 and the third feeding probe 160 are arranged in an equilateral triangle. The feeding phase difference of the third feeding probe 160 is sequentially increased by 120°. In other words, the feeding phases of the first feeding probe 140 , the second feeding probe 150 and the third feeding probe 160 may be 0°, 120°, and 240° in sequence. It should be noted that the phase difference between the feeding probes is realized by the line length of each branch of the power divider 130 , that is, by adjusting the line length of the power divider 130 , the three feeding probes can be equilaterally arranged. Arranged in triangles.

通过设置三个馈电探针的方式,可以实现扩展单元天线带宽,降低天线轴比以及高次模的影响提升天线性能。并且,相比于传统的单馈和双馈形式的天线馈电结构,本申请提供的天线结构改善了天线相位中心偏移问题,同时避免了旋转组阵由于相位中心偏移引起的栅瓣。By arranging three feeding probes, the bandwidth of the unit antenna can be expanded, the influence of the antenna axial ratio and the high-order mode can be reduced, and the antenna performance can be improved. Moreover, compared with the traditional single-fed and double-fed antenna feeding structures, the antenna structure provided by the present application improves the problem of antenna phase center offset, and simultaneously avoids the grating lobes caused by the phase center offset of the rotating array.

作为一种实现方式,本申请提供的功分器130采用三合一功分器,三合一功分器指设置有三个支路与一个合路的功分器,进而使得功分器的每个支路的端部均与一馈电探针连接。As an implementation manner, the power divider 130 provided by the present application adopts a three-in-one power divider, and a three-in-one power divider refers to a power divider provided with three branches and one combining circuit, so that each power divider of the power divider is The ends of each branch are connected with a feeding probe.

可选的,请参阅图2,馈电结构包括馈电线111、类同轴内导体112、类同轴外导体113以及耦合缝隙114,类同轴内导体112分别与类同轴外导体113、馈电线111连接,馈电线111与功分器130的合口通过耦合缝隙114实现耦合,并进行射频信号的传输。Optionally, please refer to FIG. 2 , the feeding structure includes a feeding line 111 , a coaxial-like inner conductor 112 , a coaxial-like outer conductor 113 and a coupling slot 114 . The feed line 111 is connected, and the joint of the feed line 111 and the power divider 130 is coupled through the coupling slot 114, and transmits radio frequency signals.

现有技术中,天线结构的类同轴内导体112通过馈电线111直接与功分器130的合口连接,然而,该连接方式不仅带宽窄,且其加工工艺相对复杂。其中,若采用二者直接连接的方式,则需要对整个介质层进行钻通孔处理,然而,由于介质层中包含有金属层,因此为了穿孔,需要使用背钻、控深孔的工艺,加工工艺相对复杂。In the prior art, the coaxial-like inner conductor 112 of the antenna structure is directly connected to the joint of the power divider 130 through the feed line 111 . However, this connection method not only has a narrow bandwidth, but also has a relatively complicated processing technology. Among them, if the direct connection between the two is adopted, the entire dielectric layer needs to be drilled through holes. However, since the dielectric layer contains a metal layer, in order to perforate, it is necessary to use the process of back drilling and deep hole control. The process is relatively complicated.

有鉴于此,为了简化加工工艺,同时拓展天线带宽,本申请将类同轴内导体112与功分器130的之间,采用耦合的方式进行射频信号的传输。In view of this, in order to simplify the processing technology and expand the bandwidth of the antenna, the present application uses coupling between the coaxial-like inner conductor 112 and the power divider 130 to transmit radio frequency signals.

作为一种实现方式,请参阅图3,本申请提供的天线结构还包括第一介质层190、第二介质层180以及第三介质层170,第一介质层190、第二介质层180以及第三介质层170逐层连接;As an implementation, please refer to FIG. 3 , the antenna structure provided by the present application further includes a first dielectric layer 190 , a second dielectric layer 180 and a third dielectric layer 170 , the first dielectric layer 190 , the second dielectric layer 180 and the third dielectric layer 170 The three dielectric layers 170 are connected layer by layer;

第一馈电探针140、第二馈电探针150以及第三馈电探针160均穿过第一介质层190,类同轴内导体112穿过第三介质层170。需要说明的是,第二介质层180中包含金属层,由于在加工本申请提供的天线结构时,馈电探针、类同轴内导体112均不会穿过第二介质层180,因此,无需对金属层进行处理,减少了使用背钻、控深孔等工艺的步骤,加工工艺更加简单。The first feeding probe 140 , the second feeding probe 150 and the third feeding probe 160 all pass through the first dielectric layer 190 , and the coaxial-like inner conductor 112 passes through the third dielectric layer 170 . It should be noted that the second dielectric layer 180 includes a metal layer, since neither the feeding probe nor the coaxial-like inner conductor 112 will pass through the second dielectric layer 180 when processing the antenna structure provided by the present application, therefore, There is no need to process the metal layer, the steps of using back drilling, deep hole control and other processes are reduced, and the processing technology is simpler.

可选地,第三介质层170包括第一子介质层171、第二子介质层172、第三子介质层173、第四子介质层174以及第五子介质层175,第一子介质层171、第二子介质层172、第三子介质层173、第四子介质层174以及第五子介质层175逐层连接;Optionally, the third dielectric layer 170 includes a first sub-dielectric layer 171, a second sub-dielectric layer 172, a third sub-dielectric layer 173, a fourth sub-dielectric layer 174, and a fifth sub-dielectric layer 175. The first sub-dielectric layer 175 171, the second sub-dielectric layer 172, the third sub-dielectric layer 173, the fourth sub-dielectric layer 174 and the fifth sub-dielectric layer 175 are connected layer by layer;

类同轴外导体113穿过第一子介质层171、第二子介质层172、第三子介质层173以及第四子介质层174;类同轴内导体112穿过第一子介质层171、第二子介质层172、第三子介质层173、第四子介质层174以及第五子介质层175。需要说明的是,在加工过程中,实际采用在每个子介质上钻通孔,然后压合的方式加工出本申请的天线结构。The coaxial-like outer conductor 113 passes through the first sub-dielectric layer 171 , the second sub-dielectric layer 172 , the third sub-dielectric layer 173 and the fourth sub-dielectric layer 174 ; the coaxial-like inner conductor 112 passes through the first sub-dielectric layer 171 , the second sub-dielectric layer 172 , the third sub-dielectric layer 173 , the fourth sub-dielectric layer 174 and the fifth sub-dielectric layer 175 . It should be noted that, during the processing, through holes are actually drilled on each sub-medium, and then the antenna structure of the present application is processed by pressing.

换言之,首先在第一子介质层171、第二子介质层172、第三子介质层173以及第四子介质层174上制作与类同轴外导体113相应通孔,然后将第一子介质层171、第二子介质层172、第三子介质层173、第四子介质层174以及第五子介质层175进行压合,进而继续在第一子介质层171、第二子介质层172、第三子介质层173、第四子介质层174以及第五子介质层175上制作与类同轴内导体112对应的通孔,得到第三介质层170。可以理解地,由于对于每一子介质层而言,其均可以由通孔方式实现,因此其加工方式更加简单。In other words, firstly, through holes corresponding to the coaxial-like outer conductor 113 are formed on the first sub-dielectric layer 171, the second sub-dielectric layer 172, the third sub-dielectric layer 173 and the fourth sub-dielectric layer 174, and then the first sub-dielectric layer is The layer 171, the second sub-dielectric layer 172, the third sub-dielectric layer 173, the fourth sub-dielectric layer 174 and the fifth sub-dielectric layer 175 are pressed together, and then continue on the first sub-dielectric layer 171 and the second sub-dielectric layer 172. Through holes corresponding to the quasi-coaxial inner conductors 112 are formed on the third sub-dielectric layer 173 , the fourth sub-dielectric layer 174 and the fifth sub-dielectric layer 175 to obtain the third dielectric layer 170 . It can be understood that, since each sub-dielectric layer can be realized by means of through holes, the processing method is simpler.

此外,第一介质层190包括第六子介质层191与第七子介质层192,在第六子介质层191与第七子介质层192上设置通孔后压合形成第一介质层190。其中,第六子介质层191与第七子介质层192上也设置通孔,以使馈电探针穿过该通孔。In addition, the first dielectric layer 190 includes a sixth sub-dielectric layer 191 and a seventh sub-dielectric layer 192. Through holes are provided on the sixth sub-dielectric layer 191 and the seventh sub-dielectric layer 192, and the first dielectric layer 190 is formed by pressing. Wherein, the sixth sub-dielectric layer 191 and the seventh sub-dielectric layer 192 are also provided with through holes, so that the feeding probes pass through the through holes.

可选地,第二介质层180包括第八子介质层181与第九子介质层182,第八子介质层181与第九子介质层182连接,且第八子介质层181与第九子介质层182之间包括金属层。Optionally, the second dielectric layer 180 includes an eighth sub-dielectric layer 181 and a ninth sub-dielectric layer 182, the eighth sub-dielectric layer 181 and the ninth sub-dielectric layer 182 are connected, and the eighth sub-dielectric layer 181 and the ninth sub-dielectric layer 182 are connected. A metal layer is included between the dielectric layers 182 .

因此,本申请在进行天线结构的加工时,首先第三介质层170上进行打孔,并且对第二介质层180并不处理,直接堆叠于第三介质层170上,然后对第一介质层190进行转打孔,并将第一介质层190堆叠于第二介质层180上,最后进行统一的压合,形成本申请提供的天线结。通过上述实现方式,能够有效的简化加工工艺。Therefore, when processing the antenna structure in the present application, firstly, the third dielectric layer 170 is punched, and the second dielectric layer 180 is not processed, but is directly stacked on the third dielectric layer 170, and then the first dielectric layer 170 is directly stacked. 190 is re-drilled, and the first dielectric layer 190 is stacked on the second dielectric layer 180, and finally unified pressing is performed to form the antenna junction provided by the present application. Through the above implementation manner, the processing technology can be effectively simplified.

基于上述实现方式,本申请还提供了一种相控阵天线,该相控阵天线包括多个上述的天线结构,多个天线结构旋转拼接组成相控阵天线。可以理解地,每一个天线结构可以作为一个天线单元。Based on the above implementation manner, the present application further provides a phased array antenna, the phased array antenna includes a plurality of the above-mentioned antenna structures, and the plurality of antenna structures are rotated and spliced to form a phased array antenna. It can be understood that each antenna structure can be used as an antenna unit.

现有的圆极化相控阵常采用将圆极化单元天线依次旋转的方式来组阵,通常采用四个天线单元为一组,依次旋转90度。请参阅图4,图4示出了现有技术中一种相控阵天线的拼接示意图。然而,此种旋转组阵方式相控阵大扫描角度轴比恶化严重,增益下降剧烈,尤其高频部分,使相控阵带宽变窄。The existing circularly polarized phased arrays are often formed by rotating the circularly polarized element antennas in sequence, and usually four antenna elements are used as a group, which are rotated 90 degrees in sequence. Please refer to FIG. 4 , which is a schematic diagram of splicing of a phased array antenna in the prior art. However, the large-scanning angle-to-axis ratio of the phased array in this rotating array method deteriorates seriously, and the gain decreases sharply, especially in the high-frequency part, which narrows the bandwidth of the phased array.

根据旋转组阵理论,每个天线结构的旋转角度与馈电相位满足公式:According to the theory of rotating arrays, the rotation angle and feed phase of each antenna structure satisfy the formula:

Figure P_210415140105004
Figure P_210415140105004

其中,

Figure P_210415140105005
表示天线结构的旋转角度,
Figure P_210415140105006
表示天线结构的馈电相位,m=1、2…M,P≠M/2,P=2n,n表示1~M的随机数,M表示天线结构的数量。in,
Figure P_210415140105005
represents the rotation angle of the antenna structure,
Figure P_210415140105006
Represents the feed phase of the antenna structure, m=1, 2...M, P≠M/2, P=2n, n represents a random number from 1 to M, and M represents the number of antenna structures.

其中,P与M的值会对馈相误差产生影响,且M越大,P越小,馈相误差越小。同时,多次反射情况要求P≠M/2且P=2n时可抵消高次模影响。Among them, the values of P and M will affect the feed-phase error, and the larger M is, the smaller the P is, and the smaller the feed-phase error is. At the same time, the multiple reflections require that P≠M/2 and P=2n to cancel the effects of higher-order modes.

因此,通过验证得知,本申请采用M=8,P=2的方式实现天线结构的旋转组阵。即如图5所示,本申请提供的天线结构依次旋转45°,并且,按照每四个天线结构旋转形成一个小阵列,再将两个小阵列拼接为一个大阵列,进而得到本申请提供的相控阵天线。并且,其中一个小阵列的天线结构的旋转角度由逆时针排列分别为“0°、45°、90°、135°”,另一个小阵列的天线结构的旋转角度由逆时=排列分别为“180°、225°、270°、315°”。Therefore, through verification, it is known that the present application adopts the manner of M=8 and P=2 to realize the rotating array of the antenna structure. That is, as shown in FIG. 5 , the antenna structure provided by the present application is rotated by 45° in turn, and a small array is formed by rotating every four antenna structures, and then the two small arrays are spliced into a large array, thereby obtaining the antenna structure provided by the present application. Phased Array Antenna. Moreover, the rotation angles of the antenna structures of one of the small arrays are arranged counterclockwise as "0°, 45°, 90°, 135°", respectively, and the rotation angles of the antenna structures of the other small array are arranged counterclockwise as "0°, 45°, 90°, 135°" respectively 180°, 225°, 270°, 315°”.

通过该设置方式,不仅能够改善通道馈相误差、信号多次反射、高次模等因素引起的阵面扫描轴比恶化剧烈、增益扫描下降快等影响,同时还能够增加轴比带宽和驻波带宽。This setting method can not only improve the effects of the channel feed phase error, multiple reflections of the signal, high-order modes and other factors, such as the severe deterioration of the front scan axis ratio and the rapid decrease of the gain scan, etc., but also can increase the axis ratio bandwidth and standing wave. bandwidth.

综上所述,本申请提供了一种天线结构与相控阵天线,该天线结构包括馈电结构、辐射贴片、第一馈电探针、第二馈电探针、第三馈电探针以及功分器,第一馈电探针、第二馈电探针、第三馈电探针以及功分器均与辐射贴片连接,第一馈电探针、第二馈电探针、第三馈电探针均分别与功分器的支路连接,馈电结构与功分器的合口连接,其中,第一馈电探针、第二馈电探针以及第三馈电探针呈等边三角形排布,以使第一馈电探针、第二馈电探针以及第三馈电探针的馈电相位差依次增加120°。由于本申请采用三个馈电探针的方式,且三个馈电探针的馈电相位差依次增加120°,因此可以达到改善相位中心偏移,避免了旋转组阵时相位中心周期性变化引起的栅瓣。To sum up, the present application provides an antenna structure and a phased array antenna, the antenna structure includes a feed structure, a radiation patch, a first feed probe, a second feed probe, and a third feed probe Needle and power divider, the first feed probe, the second feed probe, the third feed probe and the power divider are all connected to the radiation patch, the first feed probe, the second feed probe and the third feeding probes are respectively connected with the branches of the power divider, and the feeding structure is connected with the joint of the power divider, wherein the first feeding probe, the second feeding probe and the third feeding probe are The needles are arranged in an equilateral triangle, so that the feeding phase difference of the first feeding probe, the second feeding probe and the third feeding probe is sequentially increased by 120°. Since the present application adopts the method of three feeding probes, and the feeding phase difference of the three feeding probes increases by 120° in turn, the phase center offset can be improved, and the periodic change of the phase center when the array is rotated can be avoided. caused grating lobes.

以上所述仅为本申请的优选实施例而已,并不用于限制本申请,对于本领域的技术人员来说,本申请可以有各种更改和变化。凡在本申请的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本申请的保护范围之内。The above descriptions are only preferred embodiments of the present application, and are not intended to limit the present application. For those skilled in the art, the present application may have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of this application shall be included within the protection scope of this application.

对于本领域技术人员而言,显然本申请不限于上述示范性实施例的细节,而且在不背离本申请的精神或基本特征的情况下,能够以其它的具体形式实现本申请。因此,无论从哪一点来看,均应将实施例看作是示范性的,而且是非限制性的,本申请的范围由所附权利要求而不是上述说明限定,因此旨在将落在权利要求的等同要件的含义和范围内的所有变化囊括在本申请内。不应将权利要求中的任何附图标记视为限制所涉及的权利要求。It will be apparent to those skilled in the art that the present application is not limited to the details of the above-described exemplary embodiments, but that the present application can be implemented in other specific forms without departing from the spirit or essential characteristics of the present application. Accordingly, the embodiments are to be regarded in all respects as illustrative and not restrictive, and the scope of the application is to be defined by the appended claims rather than the foregoing description, which is therefore intended to fall within the scope of the claims. All changes that come within the meaning and scope of equivalents to are included in this application. Any reference signs in the claims shall not be construed as limiting the involved claim.

Claims (10)

1.一种天线结构,其特征在于,所述天线结构包括馈电结构、辐射贴片、第一馈电探针、第二馈电探针、第三馈电探针以及功分器,所述第一馈电探针、所述第二馈电探针、所述第三馈电探针以及所述功分器均与所述辐射贴片连接,所述第一馈电探针、所述第二馈电探针、所述第三馈电探针均分别与所述功分器的支路连接,所述馈电结构与所述功分器的合口连接,其中,1. An antenna structure, characterized in that the antenna structure comprises a feed structure, a radiation patch, a first feed probe, a second feed probe, a third feed probe and a power divider, so The first feeding probe, the second feeding probe, the third feeding probe and the power divider are all connected to the radiation patch, and the first feeding probe, the The second feeding probe and the third feeding probe are respectively connected to the branches of the power divider, and the feeding structure is connected to the joint of the power divider, wherein, 所述第一馈电探针、所述第二馈电探针以及所述第三馈电探针呈等边三角形排布,以使所述第一馈电探针、所述第二馈电探针以及所述第三馈电探针的馈电相位差依次增加120°。The first feeding probe, the second feeding probe and the third feeding probe are arranged in an equilateral triangle, so that the first feeding probe, the second feeding probe The feeding phase difference between the probe and the third feeding probe is sequentially increased by 120°. 2.如权利要求1所述的天线结构,其特征在于,所述馈电结构包括馈电线、类同轴内导体、类同轴外导体以及耦合缝隙,所述类同轴内导体分别与所述类同轴外导体、所述馈电线连接,所述馈电线与所述功分器的合口通过所述耦合缝隙实现耦合,并进行射频信号的传输。2. The antenna structure according to claim 1, wherein the feeding structure comprises a feeding line, a coaxial-like inner conductor, a coaxial-like outer conductor, and a coupling slot, and the coaxial-like inner conductor is respectively connected with the coaxial-like inner conductor. The quasi-coaxial outer conductor is connected with the feed line, and the coupling between the feed line and the power divider is coupled through the coupling slot, and transmits radio frequency signals. 3.如权利要求2所述的天线结构,其特征在于,所述天线结构还包括第一介质层、第二介质层以及第三介质层,所述第一介质层、所述第二介质层以及所述第三介质层逐层连接;3. The antenna structure according to claim 2, wherein the antenna structure further comprises a first dielectric layer, a second dielectric layer and a third dielectric layer, the first dielectric layer and the second dielectric layer and the third dielectric layer is connected layer by layer; 所述第一馈电探针、所述第二馈电探针以及所述第三馈电探针均穿过所述第一介质层,所述类同轴内导体穿过所述第三介质层。The first feeding probe, the second feeding probe and the third feeding probe all pass through the first dielectric layer, and the coaxial-like inner conductor passes through the third dielectric Floor. 4.如权利要求3所述的天线结构,其特征在于,所述第三介质层包括第一子介质层、第二子介质层、第三子介质层、第四子介质层以及第五子介质层,所述第一子介质层、所述第二子介质层、所述第三子介质层、所述第四子介质层以及所述第五子介质层逐层连接;4. The antenna structure according to claim 3, wherein the third dielectric layer comprises a first sub-dielectric layer, a second sub-dielectric layer, a third sub-dielectric layer, a fourth sub-dielectric layer and a fifth sub-dielectric layer a dielectric layer, the first sub-dielectric layer, the second sub-dielectric layer, the third sub-dielectric layer, the fourth sub-dielectric layer and the fifth sub-dielectric layer are connected layer by layer; 所述类同轴外导体穿过所述第一子介质层、所述第二子介质层、所述第三子介质层以及所述第四子介质层;所述类同轴内导体穿过所述第一子介质层、所述第二子介质层、所述第三子介质层、所述第四子介质层以及所述第五子介质层。The coaxial-like outer conductor passes through the first sub-dielectric layer, the second sub-dielectric layer, the third sub-dielectric layer and the fourth sub-dielectric layer; the coaxial-like inner conductor passes through the first sub-dielectric layer, the second sub-dielectric layer, the third sub-dielectric layer, the fourth sub-dielectric layer, and the fifth sub-dielectric layer. 5.如权利要求4所述的天线结构,其特征在于,所述第二介质层包括金属层,在每个所述子介质层上设置通孔后压合形成所述第三介质层。5 . The antenna structure according to claim 4 , wherein the second dielectric layer comprises a metal layer, and a through hole is provided on each of the sub-dielectric layers to form the third dielectric layer by pressing. 6 . 6.如权利要求4所述的天线结构,其特征在于,所述第一介质层包括第六子介质层与第七子介质层,在所述第六子介质层与所述第七子介质层上设置通孔后压合形成所述第一介质层。6. The antenna structure according to claim 4, wherein the first dielectric layer comprises a sixth sub-dielectric layer and a seventh sub-dielectric layer, and the sixth sub-dielectric layer and the seventh sub-dielectric layer The first dielectric layer is formed by pressing through holes on the layer. 7.如权利要求1所述的天线结构,其特征在于,所述功分器包括三合一功分器。7. The antenna structure of claim 1, wherein the power divider comprises a three-in-one power divider. 8.一种相控阵天线,其特征在于,所述相控阵天线包括多个如权利要求1至7任一项所述的天线结构,多个所述天线结构旋转拼接组成所述相控阵天线。8. A phased array antenna, characterized in that, the phased array antenna comprises a plurality of antenna structures according to any one of claims 1 to 7, and a plurality of the antenna structures are rotated and spliced to form the phased array antenna. array antenna. 9.如权利要求8所述的相控阵天线,其特征在于,每个所述天线结构的旋转角度与馈电相位满足公式:9. The phased array antenna of claim 8, wherein the rotation angle of each of the antenna structures and the feed phase satisfy the formula:
Figure P_210415140104001
Figure P_210415140104001
其中,
Figure P_210415140104002
表示天线结构的旋转角度,
Figure P_210415140104003
表示天线结构的馈电相位,m=1、2…M,P≠M/2,P=2n,n表示1~M的随机数,M表示天线结构的数量。
in,
Figure P_210415140104002
represents the rotation angle of the antenna structure,
Figure P_210415140104003
Represents the feed phase of the antenna structure, m=1, 2...M, P≠M/2, P=2n, n represents a random number from 1 to M, and M represents the number of antenna structures.
10.如权利要求9所述的相控阵天线,其特征在于,M=8,P=2。10 . The phased array antenna of claim 9 , wherein M=8 and P=2. 11 .
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