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CN203103496U - High Directivity Antenna Module - Google Patents

High Directivity Antenna Module Download PDF

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Publication number
CN203103496U
CN203103496U CN 201220726501 CN201220726501U CN203103496U CN 203103496 U CN203103496 U CN 203103496U CN 201220726501 CN201220726501 CN 201220726501 CN 201220726501 U CN201220726501 U CN 201220726501U CN 203103496 U CN203103496 U CN 203103496U
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carrier
little band
band feed
radiator
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廖文照
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Changze Technology Co ltd
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Changze Technology Co ltd
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Abstract

The utility model relates to an antenna module of high directive property, include: the electromagnetic energy gap structure comprises a carrier, a first radiator, a second radiator, an electromagnetic energy gap, an electrode part, an electric connection part and a pattern layer; the first radiator and the second radiator are arranged in the carrier, the electromagnetic energy gap is arranged in the carrier and is positioned below the second radiator, the electrode part is arranged on the top surface and the bottom surface of the carrier, and the electric connection part is arranged on the two side surfaces of the carrier and is electrically connected with the electrode part, the first radiator and the second radiator. The utility model provides an antenna module, its electric connection is on the base plate of no headroom to with the coupling relation cooperation modulation that the part parallel of this first irradiator and this second irradiator overlapped, reach predetermined target impedance, resonant frequency, bandwidth and radiation effect, can effectively reduce antenna size and reduce the injury of SAR value to the human body.

Description

高指向性的天线模组High Directivity Antenna Module

技术领域 technical field

 本实用新型有关一种天线,尤指一种不须要净空区的高指向性的天线模组。 The utility model relates to an antenna, especially an antenna module with high directivity that does not require a clear space.

背景技术 Background technique

GPS(全球定位系统)的定位方式,则是利用基本的三角定位原理,以测量无线电信号传输时间来测量距离,再以三颗以上的卫星交叉比对,同时换算信号接收速度与时间所得的卫星距离,搭配GPS接受器中内建的电子地图来进行方位辨识。 The positioning method of GPS (Global Positioning System) is to use the basic triangulation positioning principle to measure the distance by measuring the transmission time of radio signals, and then use more than three satellites for cross-comparison, and simultaneously convert the satellites obtained by the signal receiving speed and time Distance, with the built-in electronic map in the GPS receiver for azimuth identification.

目前车用卫星导航系统除了和车内影音系统结合的车载式之外,也发展出可携带式的PDA(掌上电脑)、Notebook(笔记本)、手机型等多种GPS产品,其中与消费者息息相关的莫过于可携式车用GPS。对于车辆并无配备原厂GPS的车主来说,选择可携式车用GPS的确是个不错的选择,因为除了价格较具亲和力外,其可携式特性除了让使用者可以带下车使用,就算日后换车也同样可以使用。 At present, in addition to the vehicle-mounted GPS system combined with the in-car audio-visual system, the satellite navigation system for vehicles has also developed a variety of GPS products such as portable PDA (handheld computer), Notebook (notebook), and mobile phones, among which are closely related to consumers. There is nothing better than portable car GPS. For car owners whose vehicles are not equipped with original GPS, it is indeed a good choice to choose a portable car GPS, because in addition to being more affordable, its portable feature allows users to take it out of the car and use it, even if It can also be used for changing cars in the future.

传统的携带式GPS系统都内建一接收GPS信号的接收天线结构,此GPS系统的接收天线结构为一种插针式平板天线,如图1A、图1B所示。该天线100上具有一陶瓷材料的基体101,该基体101表面具有一辐射金属片102,该基体101的底面具有一接地金属片103,该基体101、辐射金属片102及接地金属片103上开设有一穿孔104,该穿孔104以提供一T形状的信号馈入体105穿过,以形成可组装于主机板200上的平板天线结构。但是,此种的插针天线体积较大,无法安装在新一代轻薄短小的携带式的电子装置上。 Traditional portable GPS systems all have a built-in receiving antenna structure for receiving GPS signals. The receiving antenna structure of this GPS system is a pin type flat antenna, as shown in FIG. 1A and FIG. 1B . The antenna 100 has a substrate 101 of ceramic material, the surface of the substrate 101 has a radiating metal sheet 102, the bottom surface of the substrate 101 has a grounding metal sheet 103, the substrate 101, the radiating metal sheet 102 and the grounding metal sheet 103 are provided with A through hole 104 passes through the through hole 104 to provide a T-shaped signal feeding body 105 to form a planar antenna structure that can be assembled on the motherboard 200 . However, this kind of pin antenna has a large volume and cannot be installed on a new generation of light, thin and small portable electronic devices.

实用新型内容 Utility model content

有鉴于此,本实用新型的目的在于提供一种高指向性的天线模组。 In view of this, the purpose of the present invention is to provide a highly directivity antenna module.

为了达到上述目的,本实用新型提供一种高指向性的天线模组,包括: In order to achieve the above purpose, the utility model provides a high directivity antenna module, including:

一载体,其上至少具有一顶面、一底面及二侧面; A carrier having at least one top surface, one bottom surface and two side surfaces;

一第一辐射体,其设于该载体内部近邻顶面,该第一辐射体上具有一第一端部及第二端部; A first radiator, which is arranged inside the carrier and adjacent to the top surface, and has a first end and a second end on the first radiator;

一第二辐射体,其设于该载体内部并位于该第一辐射体下方且近邻该载体的顶面,该第二辐射体上具有一第三端部及一第四端部; A second radiator, which is disposed inside the carrier, below the first radiator and adjacent to the top surface of the carrier, and has a third end and a fourth end on the second radiator;

一电磁能隙,其设于该载体内部并位于该第二辐射体下方且近邻顶面; an electromagnetic energy gap, which is set inside the carrier and is located below the second radiator and adjacent to the top surface;

一电极部,其设于该顶面及底面; an electrode portion disposed on the top surface and the bottom surface;

一电连接部,其设于该载体的二侧面上,并电性连结电极部、第一辐射体的第二端部及第二辐射体的第四端部; an electrical connection part, which is arranged on two side surfaces of the carrier, and electrically connects the electrode part, the second end part of the first radiator and the fourth end part of the second radiator;

其中,该第一辐射体与该第二辐射体的部分平行重叠,且该第一辐射体的第一端部与该第二辐射体的第三端部呈反方向设立在该载体内部,并以该部分辐射体平行重叠的耦合关系来调整频率高低。 Wherein, part of the first radiator and the second radiator overlap in parallel, and the first end of the first radiator and the third end of the second radiator are set inside the carrier in opposite directions, and The frequency is adjusted according to the coupling relationship of the parallel overlapping of the radiators.

优选地,其中该载体为多层的陶瓷基板或玻璃纤维板组成的长方形半导体芯片天线。 Preferably, the carrier is a rectangular semiconductor chip antenna composed of multi-layer ceramic substrate or glass fiber board.

优选地,其中该第一辐射体为由金属材质制成的片状体。 Preferably, the first radiator is a sheet made of metal.

优选地,其中该第二辐射体为由金属材质制成的片状体。 Preferably, the second radiator is a flake made of metal.

优选地,其中该电磁能隙为由金属材质制成的片状体。 Preferably, the electromagnetic energy gap is a flake made of metal material.

优选地,其中该电极部为由金属材质制成的构件,由一上电极部及一下电极部组成,该上电极部设于该顶面,该下电极部设于该底面上。 Preferably, the electrode part is a member made of metal material, and is composed of an upper electrode part and a lower electrode part, the upper electrode part is arranged on the top surface, and the lower electrode part is arranged on the bottom surface.

优选地,其中该电连接部为由金属材质制成的构件,由一第一电连接部及一第二电连接部组成,该第一电连接部电性连结该顶面及该底面一侧的该上电极部及该下电极部,该第二电连接部电性连结该顶面及该底面另一侧的该上电极部及该下电极部。 Preferably, the electrical connection part is a member made of metal material, consisting of a first electrical connection part and a second electrical connection part, the first electrical connection part electrically connects the top surface and the bottom surface The upper electrode portion and the lower electrode portion, the second electrical connection portion electrically connects the upper electrode portion and the lower electrode portion on the other side of the top surface and the bottom surface.

优选地,其中该第一辐射体及该第二辐射体的部分为平行重叠的耦合关系,以耦合面积及耦合距离,可控制或调整频率高低。 Preferably, parts of the first radiator and the second radiator are in a parallel overlapping coupling relationship, and the frequency can be controlled or adjusted by the coupling area and coupling distance.

优选地,其中更包含有一图案层,该图案层设于该载体的顶面上,该图案层为型号、公司商标图案。 Preferably, it further includes a pattern layer, the pattern layer is arranged on the top surface of the carrier, and the pattern layer is a pattern of a model number and a company logo.

优选地,其中更包含有一基板,该基板至少一表面上具有一第一金属层及一第一镂空部,该第一镂空部两侧的第一金属层上具有一第一接点及一第二接点,该第一接点的一侧电性连结有一微带馈入线,该微带馈入线由第一微带馈入线及第二微带馈入线组成,该微带馈入线的两侧上各具有一与该第一金属层分隔的第二镂空部。 Preferably, it further includes a substrate, at least one surface of the substrate has a first metal layer and a first hollow part, and the first metal layer on both sides of the first hollow part has a first contact and a second A contact, one side of the first contact is electrically connected with a microstrip feed-in line, the microstrip feed-in line is composed of a first microstrip feed-in line and a second microstrip feed-in line, the microstrip feed-in line Each of the two sides has a second hollow part separated from the first metal layer.

优选地,其中该载体底面的下电极部电性连结在该第一金属层的第一接点及第二接点上,该第一微带馈入线与该第二微带馈入线之间电性连结有一耦合元件,且该第二微带馈入线上电性连结有一铜轴电缆线。 Preferably, the lower electrode portion on the bottom surface of the carrier is electrically connected to the first contact point and the second contact point of the first metal layer, and the electrical connection between the first microstrip feed-in line and the second microstrip feed-in line A coupling element is electrically connected to the second microstrip feed-in line, and a copper axis cable is electrically connected to the second microstrip feed-in line.

优选地,其中更包含有一基板,该基板正面上具有一第一金属层及一第一镂空部,该第一镂空部两侧的第一金属层上具有一第一接点及一第二接点,该第一接点的一侧电性连结有一微带馈入线,该微带馈入线由第一微带馈入线及第二微带馈入线组成,该微带馈入线的两侧上各具有一与该第一金属层分隔的第二镂空部;而该基板背面具有一第二金属层。 Preferably, it further includes a substrate, the front surface of the substrate has a first metal layer and a first hollow part, and the first metal layer on both sides of the first hollow part has a first contact and a second contact, One side of the first contact point is electrically connected to a microstrip feed-in line, the microstrip feed-in line is composed of a first microstrip feed-in line and a second microstrip feed-in line, the two sides of the microstrip feed-in line each has a second hollow part separated from the first metal layer; and the back of the substrate has a second metal layer.

优选地,其中该载体底面的下电极部电性连结在该第一金属层的第一接点及第二接点上,并对应该基板背面的第三镂空部,该第一微带馈入线与该第二微带馈入线之间电性连结一耦合元件,且该第二微带馈入线上电性连结有一铜轴电缆线。 Preferably, the lower electrode part on the bottom surface of the carrier is electrically connected to the first contact and the second contact of the first metal layer, and corresponds to the third hollow part on the back of the substrate, and the first microstrip feed-in line and A coupling element is electrically connected between the second microstrip feed-in lines, and a copper-axis cable is electrically connected to the second microstrip feed-in lines.

本实用新型所提供的高指向性的天线模组,其利用二天线的辐射体平行重叠进行耦合关系及反射接收信号波的结构设计,可增加天线指向性,增加天线辐射效率及缩小天线尺寸,相对可以降低SAR值,降低天线辐射对人体的伤害,且不需要净空区,在天线模组靠近金属物或接近金属物时,可以避免受金属物干扰。 The antenna module with high directivity provided by the utility model utilizes the parallel overlapping of the radiators of the two antennas to carry out the coupling relationship and the structural design of reflecting and receiving signal waves, which can increase the directivity of the antenna, increase the radiation efficiency of the antenna and reduce the size of the antenna. It can relatively reduce the SAR value, reduce the damage of antenna radiation to the human body, and does not require a clear space. When the antenna module is close to metal objects or close to metal objects, it can avoid being interfered by metal objects.

附图说明 Description of drawings

图1A为传统GPS所使用的平板天线结构外观立体示意图; FIG. 1A is a three-dimensional schematic diagram of the appearance of a flat panel antenna structure used in a traditional GPS;

图1B为传统GPS所使用的平板天线结构侧视示意图; FIG. 1B is a schematic side view of a flat panel antenna structure used in a traditional GPS;

图2为本实用新型高指向性的天线模组外观立体示意图; Figure 2 is a three-dimensional schematic diagram of the appearance of the high directivity antenna module of the present invention;

图3为本实用新型高指向性的天线模组侧剖示意图; Fig. 3 is a schematic side sectional view of the antenna module with high directivity of the present invention;

图4为本实用新型的基板示意图; Fig. 4 is the schematic diagram of the substrate of the present utility model;

图5为本实用新型的天线模组与基板组合示意图; 5 is a schematic diagram of the combination of the antenna module and the substrate of the present invention;

图6为本实用新型天线模组在1.575GHZ时的XZ平面的辐射场型示意图; Fig. 6 is a schematic diagram of the radiation field pattern of the XZ plane of the antenna module of the present invention at 1.575GHZ;

图7为本实用新型天线模组在1.575GHZ时的YZ平面的辐射场型示意图; Fig. 7 is a schematic diagram of the radiation field pattern of the YZ plane when the antenna module of the present invention is at 1.575GHZ;

图8为本实用新型天线模组在1.575GHZ时的XY平面的辐射场型示意图; Fig. 8 is a schematic diagram of the radiation field pattern of the XY plane when the antenna module of the present invention is at 1.575GHZ;

图9为本实用新型的天线模组的反射系数比较示意图; Fig. 9 is a comparative schematic diagram of the reflection coefficient of the antenna module of the present invention;

图10为本实用新型天线模组在2.48时的XZ平面的辐射场型示意图; Fig. 10 is a schematic diagram of the radiation field pattern of the XZ plane of the antenna module of the present invention at 2.48;

图11为本实用新型天线模组在2.48GHZ时的YZ平面的辐射场型示意图; Fig. 11 is a schematic diagram of the radiation field pattern of the YZ plane of the antenna module of the present invention at 2.48GHZ;

图12为本实用新型天线模组在2.48GHZ时的XY平面的辐射场型示意图; Fig. 12 is a schematic diagram of the radiation field pattern of the XY plane of the antenna module of the present invention at 2.48GHZ;

图13为本实用新型天线模组运用在具有净空区的基板正面示意图; Fig. 13 is a schematic front view of the application of the antenna module of the present invention on a substrate with a clearance area;

图14为本实用新型天线模组运用在具有净空区的基板背面示意图; Figure 14 is a schematic diagram of the application of the antenna module of the present invention on the back of the substrate with a clearance area;

图15为本实用新型天线模组运用在有净空区及无净空区的反射系数比较示意图。 FIG. 15 is a schematic diagram showing the comparison of reflection coefficients of the antenna module of the present invention used in areas with clearance and areas without clearance.

【主要元件符号说明】 [Description of main component symbols]

载体-1;天线模组-10;天线-100;基体-101;辐射金属片-102;接地金属片-103;穿孔-104;信号馈入体-105;顶面-11;底面-12;侧面-13; Carrier-1; Antenna Module-10; Antenna-100; Substrate-101; Radiating Metal Sheet-102; Grounding Metal Sheet-103; side - 13;

第一辐射体-2;主机板-200;第一端部-21;第二端部-22; The first radiator-2; the motherboard-200; the first end-21; the second end-22;

第二辐射体-3;第三端部-31;第四端部-32; The second radiator-3; the third end-31; the fourth end-32;

电磁能隙-4; Electromagnetic gap-4;

电极部-5;上电极部-51;下电极部-52; Electrode part-5; Upper electrode part-51; Lower electrode part-52;

电连接部-6;第一电连接部-61;第二电连接部-62; Electrical connection part-6; first electrical connection part-61; second electrical connection part-62;

图案层-7; pattern_layer-7;

基板-8;第一金属层-81;第一接点-811;第二接点-812;第一镂空部-82;微带馈入线-83;第一微带馈入线-831;第二微带馈入线-832;第二镂空部-84;第二金属层-85;第三镂空部-86。 Substrate-8; first metal layer-81; first contact-811; second contact-812; first hollow-82; microstrip feed-in line-83; first microstrip feed-in-line-831; Microstrip feed-in line-832; second hollow part-84; second metal layer-85; third hollow part-86.

具体实施方式 Detailed ways

有关本实用新型的技术内容及详细说明,现配合附图说明如下。 Relevant technical contents and detailed description of the utility model are described as follows now in conjunction with the accompanying drawings.

请参阅图2、图3,为本实用新型的高指向性的天线模组外观立体、侧剖示意图。如图所示:本实用新型的高指向性的天线模组10,包括:一载体1、一第一辐射体2、一第二辐射体3、一电磁能隙4、一电极部5、一电连接部6及一图案层7。 Please refer to FIG. 2 and FIG. 3 , which are three-dimensional and side-sectional diagrams of the high directivity antenna module of the present invention. As shown in the figure: the high directivity antenna module 10 of the present utility model includes: a carrier 1, a first radiator 2, a second radiator 3, an electromagnetic energy gap 4, an electrode part 5, a The electrical connection part 6 and a pattern layer 7 .

该载体1,为由多层的陶瓷基板或玻璃纤维板所组成的长方形半导体芯片天线,其上至少具有一顶面11、一底面12及二侧面13。 The carrier 1 is a rectangular semiconductor chip antenna composed of multilayer ceramic substrates or glass fiber boards, and has at least a top surface 11 , a bottom surface 12 and two side surfaces 13 .

该第一辐射体2,为由金属材质制成的片状体,其设于该载体1内部近邻顶面11,且该第一辐射体2上具有一第一端部21及一第二端部22。 The first radiator 2 is a sheet-shaped body made of metal material, which is arranged inside the carrier 1 adjacent to the top surface 11, and the first radiator 2 has a first end 21 and a second end. Section 22.

该第二辐射体3,为由金属材质制成的片状体,其设于该载体1内部并位于该第一辐射体2下方且近邻该载体1的顶面11。该第二辐射体3上具有一第三端部31及一第四端部32。该第一辐射体2与该第二辐射体3的部分辐射体呈平行重叠的耦合关系,使该第一辐射体2的第一端部21与该第二辐射体3的第三端部31呈反方向设立在该载体1内部。 The second radiator 3 is a plate-shaped body made of metal material, which is disposed inside the carrier 1 , below the first radiator 2 and adjacent to the top surface 11 of the carrier 1 . The second radiator 3 has a third end portion 31 and a fourth end portion 32 . The first radiator 2 and part of the second radiator 3 are in a parallel overlapping coupling relationship, so that the first end 21 of the first radiator 2 and the third end 31 of the second radiator 3 It is set up inside the carrier 1 in the opposite direction.

该电磁能隙(Electromagnetic Band-gap,EBG)4,为由金属材质制成的片状体,其设于该载体1内部并位于该第二辐射体3下方且近邻顶面11。该电磁能隙4能反射接收信号供该第一辐射体2及该第二辐射体3接收,可增加天线指向性,增加天线辐射效率及缩小天线尺寸,相对可以降低SAR值,降低天线辐射对人体的伤害。 The electromagnetic band-gap (EBG) 4 is a sheet-shaped body made of metal material, which is disposed inside the carrier 1 below the second radiator 3 and adjacent to the top surface 11 . The electromagnetic energy gap 4 can reflect and receive signals for the first radiator 2 and the second radiator 3 to receive, which can increase the directivity of the antenna, increase the radiation efficiency of the antenna and reduce the size of the antenna, relatively can reduce the SAR value, and reduce the impact of antenna radiation on the antenna. human injury.

该电极部5,为由金属材质制成的构件,其由一上电极部51及一下电极部52组成。该上电极部51设于该载体1的顶面11,该下电极部52设于该载体1的底面12上,该下电极部52供天线模组可以表面粘着在基板(图中未示)上。 The electrode part 5 is a member made of metal material, which is composed of an upper electrode part 51 and a lower electrode part 52 . The upper electrode part 51 is arranged on the top surface 11 of the carrier 1, and the lower electrode part 52 is arranged on the bottom surface 12 of the carrier 1. The lower electrode part 52 is used for the antenna module to be surface-bonded on the substrate (not shown in the figure). superior.

该电连接部6,为由金属材质制成的构件,其由一第一电连接部61及一第二电连接部62组成,并设于该载体1的二侧面13上。该第一电连接部61电性连结右侧边的该上电极部51、第二辐射体3的第四端部32及右侧边的下电极部52。该第二电连接部62电性连结左侧边的上电极部51、第一辐射体2的第二端部22及左侧边的下电极部52电性连结。 The electrical connection portion 6 is a component made of metal material, which is composed of a first electrical connection portion 61 and a second electrical connection portion 62 , and is disposed on two side surfaces 13 of the carrier 1 . The first electrical connection portion 61 is electrically connected to the upper electrode portion 51 on the right side, the fourth end portion 32 of the second radiator 3 and the lower electrode portion 52 on the right side. The second electrical connection portion 62 is electrically connected to the upper electrode portion 51 on the left side, the second end portion 22 of the first radiator 2 and the lower electrode portion 52 on the left side.

该图案层7,其设于该载体1的顶面11上,该图案层7可以印刷天线的型号、公司商标图案。 The pattern layer 7 is arranged on the top surface 11 of the carrier 1 , and the pattern layer 7 can be printed with patterns of antenna models and company trademarks.

上述该第一辐射体2及该第二辐射体3的部分平行重叠的耦合关系,是以辐射体的耦合面积及耦合距离关系,形成二耦合电容彼此相配合调变(如调整二耦合电容大小来控制频率高低,可适用于2.4GHZ或1.575GHZ的天线),从而达到预定的目标阻抗、共振频率、频宽与辐射效应,且可有效缩小天线尺寸。 The above-mentioned coupling relationship of the first radiator 2 and the partial parallel overlap of the second radiator 3 is based on the coupling area and coupling distance relationship of the radiator to form two coupling capacitors that are coordinated and modulated (such as adjusting the size of the two coupling capacitors) To control the frequency level, it can be applied to 2.4GHZ or 1.575GHZ antenna), so as to achieve the predetermined target impedance, resonance frequency, bandwidth and radiation effect, and can effectively reduce the size of the antenna.

请参阅图4、图5,为本实用新型的基板及天线模组组合正面及背面示意图。如图所示:本实用新型的高指向性的天线模组10在运用时,将该天线模组10电性连结在一无净空区的基板8上做说明。 Please refer to FIG. 4 and FIG. 5 , which are front and back schematic diagrams of the combination of the substrate and the antenna module of the present invention. As shown in the figure: when the high directivity antenna module 10 of the present invention is in use, the antenna module 10 is electrically connected to a substrate 8 with no clearance area for illustration.

该基板8正面上具有一第一金属层81及一第一镂空部82,该第一镂空部82两侧的第一金属层81上具有一第一接点811及一第二接点812。该第一接点811的一侧电性连结有一微带馈入线83,该微带馈入线83由第一微带馈入线831及第二微带馈入线832组成,该微带馈入线83的两侧上各具有一第二镂空部84并与该第一金属层81分隔。另外,该基板8的背面具有一第二金属层85,该第二金属层85上无净空区。 The substrate 8 has a first metal layer 81 and a first hollow portion 82 on the front surface, and the first metal layer 81 on both sides of the first hollow portion 82 has a first contact 811 and a second contact 812 . One side of the first contact 811 is electrically connected to a microstrip feed-in line 83, which is composed of a first microstrip feed-in line 831 and a second microstrip feed-in line 832. Two sides of the incoming line 83 respectively have a second hollow portion 84 separated from the first metal layer 81 . In addition, the back surface of the substrate 8 has a second metal layer 85 , and there is no clearance area on the second metal layer 85 .

在天线模组10与该基板8电性连结时,该天线模组10的载体1的底面11上右侧及左侧的下电极部52电性连结在该第一金属层81的第一接点811及第二接点812上。该第一微带馈入线831与该第二微带馈入线832之间电性连结一耦合元件(图中未示),且在第二微带馈入线832上电性连结有一铜轴电缆线(图中未示)。 When the antenna module 10 is electrically connected to the substrate 8, the right and left lower electrode portions 52 on the bottom surface 11 of the carrier 1 of the antenna module 10 are electrically connected to the first contact of the first metal layer 81. 811 and the second contact 812. A coupling element (not shown) is electrically connected between the first microstrip feed-in line 831 and the second microstrip feed-in line 832, and a copper is electrically connected to the second microstrip feed-in line 832. Shaft cables (not shown in the figure).

在天线模组10接收信号后,经该第二接点812传至该微带馈入线83上,由该微带馈入线83传至该铜轴电缆线(图中未示)上,以便铜轴电缆线可将信号传至该装置(图中未示)的主机板上。 After the antenna module 10 receives the signal, it is transmitted to the microstrip feed-in line 83 through the second contact 812, and is transmitted to the copper axis cable (not shown) by the microstrip feed-in line 83, so that Copper cables carry the signal to the motherboard of the device (not shown).

请参阅图6,为本实用新型天线模组在1.575GHZ时的XZ平面的辐射场型示意图。如图所示:在频率为1.575GHZ时,主波瓣大小(Main lobe magnitude)在3.3dBi,主波瓣方向(Main lobe direction)在2.0deg,角宽度(Angular width)在3dB时为93.0 deg,旁波瓣准位(side lobe level在-3.0dB。 Please refer to FIG. 6 , which is a schematic diagram of the radiation field pattern on the XZ plane of the antenna module of the present invention at 1.575 GHZ. As shown in the figure: when the frequency is 1.575GHZ, the main lobe magnitude (Main lobe magnitude) is 3.3dBi, the main lobe direction (Main lobe direction) is 2.0deg, and the angular width (Angular width) is 93.0 deg when it is 3dB , the side lobe level is at -3.0dB.

请参阅图7,为本实用新型天线模组在1.575GHZ时的YZ平面的辐射场型示意图。如图所示:在频率为1.575GHZ时,主波瓣大小(Main lobe magnitude)在3.6dBi,主波瓣方向(Main lobe direction)在26.0deg,角宽度(Angular width)在3dB时为222.8 deg。 Please refer to FIG. 7 , which is a schematic diagram of the radiation field pattern of the YZ plane of the antenna module of the present invention at 1.575 GHZ. As shown in the figure: when the frequency is 1.575GHZ, the main lobe magnitude (Main lobe magnitude) is 3.6dBi, the main lobe direction (Main lobe direction) is 26.0deg, and the angular width (Angular width) is 222.8 deg when it is 3dB .

请参阅图8,为本实用新型天线模组在1.575GHZ时的XY平面的辐射场型示意图。如图所示:在频率为1.575GHZ时,主波瓣大小(Main lobe magnitude)在2.7dBi,主波瓣方向(Main lobe direction)在273.0deg,角宽度(Angular width)在3dB时为116.2 deg,旁波瓣准位(side lobe level)在-4.5dB。 Please refer to FIG. 8 , which is a schematic diagram of the XY plane radiation pattern of the antenna module of the present invention at 1.575 GHz. As shown in the figure: when the frequency is 1.575GHZ, the main lobe magnitude (Main lobe magnitude) is 2.7dBi, the main lobe direction (Main lobe direction) is 273.0deg, and the angular width (Angular width) is 116.2 deg when it is 3dB , the side lobe level is -4.5dB.

请参阅图9,为本实用新型天线模组的反射系数比较示意图。如图所示:S1频率在1.456GHZ时为-13.438dB,S2频率在1.4749GHZ时为-12.416dB,S3频率在1.4953GHZ时为-12.096dB,S4频率在1.5278GHZ时为-11.842dB,S5频率在1.5814GHZ时为-10.974dB,S6频率在1.5957GHZ时为-10.85dB,S7频率在1.626GHZ时为-10.491dB,S8频率在1.6579GHZ时为-9.9802dB,S9频率在1.6925GHZ时为-9.6347dB。 Please refer to FIG. 9 , which is a schematic diagram of comparison of reflection coefficients of the antenna module of the present invention. As shown in the figure: S1 frequency is -13.438dB at 1.456GHZ, S2 frequency is -12.416dB at 1.4749GHZ, S3 frequency is -12.096dB at 1.4953GHZ, S4 frequency is -11.842dB at 1.5278GHZ, S5 The frequency is -10.974dB at 1.5814GHZ, the S6 frequency is -10.85dB at 1.5957GHZ, the S7 frequency is -10.491dB at 1.626GHZ, the S8 frequency is -9.9802dB at 1.6579GHZ, and the S9 frequency is 1.6925GHZ -9.6347dB.

请参阅图10,为本实用新型天线模组在2.48时的XZ平面的辐射场型示意图。如图所示:在频率为2.48GHZ时,主波瓣大小(Main lobe magnitude)在1.9dBi,主波瓣方向(Main lobe direction)在19.0deg,角宽度(Angular width)在3dB时为180.0 deg。 Please refer to FIG. 10 , which is a schematic diagram of the radiation field pattern on the XZ plane of the antenna module of the present invention at 2.48. As shown in the figure: when the frequency is 2.48GHZ, the main lobe magnitude (Main lobe magnitude) is 1.9dBi, the main lobe direction (Main lobe direction) is 19.0deg, and the angular width (Angular width) is 180.0 deg at 3dB .

请参阅图11,为本实用新型天线模组在2.48GHZ时的YZ平面的辐射场型示意图。如图所示:在频率为2.48GHZ时,主波瓣大小(Main lobe magnitude)在1.5dBi,主波瓣方向(Main lobe direction)在4.0deg,角宽度(Angular width)在3dB时为151.6 deg,旁波瓣准位(side lobe level)在-4.2dB。 Please refer to FIG. 11 , which is a schematic diagram of the radiation field pattern of the YZ plane of the antenna module of the present invention at 2.48GHZ. As shown in the figure: when the frequency is 2.48GHZ, the main lobe magnitude (Main lobe magnitude) is 1.5dBi, the main lobe direction (Main lobe direction) is 4.0deg, and the angular width (Angular width) is 151.6 deg when it is 3dB , the side lobe level is -4.2dB.

请参阅图12,为本实用新型的天线模组在2.4GHZ时的XY平面的辐射场型示意图。如图所示:在频率为2.48GHZ时,主波瓣大小(Main lobe magnitude)在0.6dBi,主波瓣方向(Main lobe direction)在327.0deg,角宽度(Angular width)在3dB时为216.5deg,旁波瓣准位(side lobe level)在-4.2dB。 Please refer to FIG. 12 , which is a schematic diagram of the XY plane radiation pattern of the antenna module of the present invention at 2.4GHZ. As shown in the figure: when the frequency is 2.48GHZ, the main lobe magnitude (Main lobe magnitude) is 0.6dBi, the main lobe direction (Main lobe direction) is 327.0deg, and the angular width (Angular width) is 216.5deg when it is 3dB , the side lobe level is -4.2dB.

请参阅图13、图14、图15,为本实用新型天线模组运用在具有净空区的基板正面及背面与天线模组运用在有净空区及无净空区的反射系数比较示意图。如图所示:在天线模组10电性连结于该基板8的正面有一第一金属面81上时,该天线模组10对应该基板8的背面具有一第二金属层85及一第三镂空部86,该第三镂空部86为净空区且对应该天线模组10。 Please refer to Fig. 13, Fig. 14, and Fig. 15, which are schematic diagrams comparing the reflection coefficients of the antenna module of the present invention applied on the front and back of the substrate with clearance area and the antenna module applied in the clearance area and no clearance area. As shown in the figure: when the antenna module 10 is electrically connected to a first metal surface 81 on the front side of the substrate 8, the antenna module 10 has a second metal layer 85 and a third metal layer 85 corresponding to the back side of the substrate 8. The hollow part 86 , the third hollow part 86 is a clearance area and corresponds to the antenna module 10 .

在有无净空区的使用时对天线的频率影响很大,因此本实用新型做了有无净空区的比较。在净空区尺寸为5×4㎜时,频率为1.8822 GHZ、-18.6dB。在净空区尺寸为5×2㎜时,频率为2.2145 GHZ、-10.9dB。在净空区尺寸为5×6㎜时,频率为1.6465 GHZ、-10.7dB。在无净空区时,频率为2.4734 GHZ、-7.9dB。 The frequency of the antenna is greatly affected by the use of the clearance area or not, so the utility model has made a comparison with or without the clearance area. When the headroom size is 5×4㎜, the frequency is 1.8822 GHZ, -18.6dB. When the headroom size is 5×2㎜, the frequency is 2.2145 GHZ, -10.9dB. When the headroom size is 5×6㎜, the frequency is 1.6465 GHZ, -10.7dB. When there is no headroom, the frequency is 2.4734 GHZ, -7.9dB.

以上所述,仅为本实用新型的较佳实施例,并非用以限定本实用新型的专利保护范围,其它运用本实用新型专利精神所作的等效变化,均应同理属于本实用新型的专利保护范围。 The above is only a preferred embodiment of the utility model, and is not intended to limit the scope of protection of the utility model patent. Other equivalent changes made by using the spirit of the utility model patent should all belong to the utility model patent in the same way. protected range.

Claims (12)

1. the antenna modules of a high directivity is characterized in that, comprising:
One carrier has an end face, a bottom surface and two side faces at least on it;
One first radiant body, it is located at this carrier inside neighbour end face, has a first end and the second end on this first radiant body;
One second radiant body, it is located at this carrier inside and is positioned at the end face of this first radiant body below and this carrier of neighbour, has one the 3rd end and one the 4th end on this second radiant body;
One electromagnetic band gap, it is located at this carrier inside and is positioned at this second radiant body below and neighbour's end face;
One electrode part, it is located at this end face and bottom surface;
One electrical connection section, it is located on the two side faces of this carrier, and electrically connect electrode part, the second end of first radiant body and the 4th end of second radiant body;
Wherein, the partial parallel of this first radiant body and this second radiant body is overlapping, and the 3rd end of the first end of this first radiant body and this second radiant body is and is built up in the other direction this carrier inside.
2. antenna modules as claimed in claim 1 is characterized in that, this carrier is the ceramic substrate of multilayer or the rectangular semiconductor antenna component that glass mat is formed.
3. antenna modules as claimed in claim 2 is characterized in that, the plates of this first radiant body for being made by metal material.
4. antenna modules as claimed in claim 3 is characterized in that, the plates of this second radiant body for being made by metal material.
5. antenna modules as claimed in claim 4 is characterized in that, the plates of this electromagnetic band gap for being made by metal material.
6. antenna modules as claimed in claim 5 is characterized in that, the member of this electrode part for making by metal material, by a top electrode portion and once electrode part form, this top electrode portion is located at this end face, this bottom electrode portion is located on this bottom surface.
7. antenna modules as claimed in claim 6, it is characterized in that, the member of this electrical connection section for making by metal material, form by one first electrical connection section and one second electrical connection section, this top electrode portion of this this end face of first electrical connection section electrically connect and this bottom surface one side and this bottom electrode portion, this top electrode portion of this this end face of second electrical connection section electrically connect and this bottom surface opposite side and this bottom electrode portion.
8. antenna modules as claimed in claim 7 is characterized in that, more includes a patterned layer, and this patterned layer is located on the end face of this carrier.
9. antenna modules as claimed in claim 8, it is characterized in that, more include a substrate, have a first metal layer and one first hollow-out parts at least one surface of this substrate, have one first contact and one second contact on the first metal layer of these first hollow-out parts both sides, one side electrically connect of this first contact has a little band feed-in line, this little band feed-in line is made up of first little band feed-in line and second little band feed-in line, respectively has second hollow-out parts of separating with this first metal layer on the both sides of this little band feed-in line.
10. antenna modules as claimed in claim 9, it is characterized in that, the bottom electrode portion electrically connect of this carrier bottom surface is on first contact and second contact of this first metal layer, electrically connect has a coupling element between this first little band feed-in line and this second little band feed-in line, and electrically connect has a coaxial cable line on this second little band feed-in line.
11. antenna modules as claimed in claim 8, it is characterized in that, more include a substrate, have a first metal layer and one first hollow-out parts on this substrate front side, have one first contact and one second contact on the first metal layer of these first hollow-out parts both sides, one side electrically connect of this first contact has a little band feed-in line, this little band feed-in line is made up of first little band feed-in line and second little band feed-in line, respectively has second hollow-out parts of separating with this first metal layer on the both sides of this little band feed-in line; And this substrate back has one second metal level.
12. antenna modules as claimed in claim 11, it is characterized in that, the bottom electrode portion electrically connect of this carrier bottom surface is on first contact and second contact of this first metal layer, and to the 3rd hollow-out parts that should substrate back, electrically connect one coupling element between this first little band feed-in line and this second little band feed-in line, and electrically connect has a coaxial cable line on this second little band feed-in line.
CN 201220726501 2012-12-25 2012-12-25 High Directivity Antenna Module Expired - Lifetime CN203103496U (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103904415A (en) * 2012-12-25 2014-07-02 昌泽科技有限公司 High-directivity antenna module
CN105514593A (en) * 2014-09-24 2016-04-20 佳邦科技股份有限公司 Antenna structure

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103904415A (en) * 2012-12-25 2014-07-02 昌泽科技有限公司 High-directivity antenna module
CN105514593A (en) * 2014-09-24 2016-04-20 佳邦科技股份有限公司 Antenna structure
CN105514593B (en) * 2014-09-24 2019-04-09 佳邦科技股份有限公司 Antenna structure

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