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CN114725667B - A Magnetoelectric Dipole Antenna for Autopilot Radar - Google Patents

A Magnetoelectric Dipole Antenna for Autopilot Radar Download PDF

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CN114725667B
CN114725667B CN202210347994.9A CN202210347994A CN114725667B CN 114725667 B CN114725667 B CN 114725667B CN 202210347994 A CN202210347994 A CN 202210347994A CN 114725667 B CN114725667 B CN 114725667B
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antenna
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CN114725667A (en
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布迪诺
张波
屈世伟
杨仕文
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University of Electronic Science and Technology of China
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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
    • H01PWAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P5/00Coupling devices of the waveguide type
    • H01P5/08Coupling devices of the waveguide type for linking dissimilar lines or devices
    • H01P5/10Coupling devices of the waveguide type for linking dissimilar lines or devices for coupling balanced lines or devices with unbalanced lines or devices
    • H01P5/103Hollow-waveguide/coaxial-line transitions
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/32Adaptation for use in or on road or rail vehicles
    • H01Q1/3208Adaptation for use in or on road or rail vehicles characterised by the application wherein the antenna is used
    • H01Q1/3233Adaptation for use in or on road or rail vehicles characterised by the application wherein the antenna is used particular used as part of a sensor or in a security system, e.g. for automotive radar, navigation systems
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/48Earthing means; Earth screens; Counterpoises
    • 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
    • H01Q13/00Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
    • H01Q13/10Resonant slot antennas
    • H01Q13/106Microstrip slot antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems
    • H01Q21/0075Stripline fed arrays
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04Resonant antennas
    • H01Q9/0407Substantially flat resonant element parallel to ground plane, e.g. patch antenna
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q9/00Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
    • H01Q9/04Resonant antennas
    • H01Q9/0407Substantially flat resonant element parallel to ground plane, e.g. patch antenna
    • H01Q9/0464Annular ring patch
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

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  • Engineering & Computer Science (AREA)
  • Computer Security & Cryptography (AREA)
  • Radar, Positioning & Navigation (AREA)
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  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

本发明公开一种应用于自动驾驶雷达的磁电偶极子天线,属于天线工程技术领域。该磁电偶极子天线由五层PCB板和四层半固化片所构成,其集成度高,稳定性强,具有平面结构易于共形,适用于自动驾驶MIMO雷达。该磁电偶极子天线阵列由辐射部分,功分器部分和波导转同轴结构部分三部分构成,通过耦合拓宽了天线的阻抗带宽。该天线通过添加可调节哑元阵列和调整单元间距的方式实现了3dB波束宽度可调,满足自动驾驶MIMO雷达对天线的性能需求。

Figure 202210347994

The invention discloses a magnetoelectric dipole antenna applied to an automatic driving radar, which belongs to the technical field of antenna engineering. The magnetoelectric dipole antenna is composed of a five-layer PCB board and a four-layer prepreg. It has high integration, strong stability, and a planar structure that is easy to conform to, and is suitable for autonomous driving MIMO radars. The magnetoelectric dipole antenna array is composed of three parts: a radiation part, a power divider part and a waveguide-to-coaxial structure part, and the impedance bandwidth of the antenna is widened through coupling. The antenna realizes the adjustable 3dB beam width by adding an adjustable dummy array and adjusting the unit spacing, which meets the performance requirements of the autonomous driving MIMO radar for the antenna.

Figure 202210347994

Description

一种应用于自动驾驶雷达的磁电偶极子天线A Magnetoelectric Dipole Antenna for Autopilot Radar

技术领域technical field

本发明属于天线工程技术领域,涉及一种磁电偶极子天线,应用背景为自动驾驶MIMO雷达,其具有集成度高、宽频带、3dB波束宽度可控的特点。The invention belongs to the technical field of antenna engineering, and relates to a magnetoelectric dipole antenna. The application background is MIMO radar for automatic driving, which has the characteristics of high integration, wide frequency band, and controllable 3dB beam width.

背景技术Background technique

磁电偶极子天线通过在天线辐射口径上构造磁极子和电极子来得到在E面和H面对称的方向图,同时其双谐振点可以满足宽带匹配。自动驾驶MIMO雷达对天线的3dB波束宽度有着严格的要求,例如在论文“Patch Array Antenna Using a Dual Coupled FeedingStructure for 79GHz Automotive Radar Applications”中,实现了ZX平面8.1°的3dB波束宽度,ZY平面内70°的波束宽度;在论文“Hybrid thin film multilayer antenna forautomotive radar at 77GHz”中,实现了H面40°、E面12°的3dB波束宽度。此外,在77GHz频段,加工工艺的限制也是对天线设计的一大挑战,最近LTCC工艺在此汽车雷达领域被广泛研究,例如在论文“A 79-GHz resonant laminated waveguide slotted array antennausing novel shaped slots in LTCC”中,一个基于LTCC工艺的波导缝隙天线被提出,其通过谐振方式工作;在论文“A 79-GHz radar sensor in LTCC technology using gridarray antennas”中,提出了一款应用于79GHz雷达的网格阵列天线。但是由于材料损耗等原因,LTCC工艺所加工的天线效率较低,通常在30%以下,因此低损耗的PCB工艺也常被用于毫米波频段。例如在论文“A low-cost and high-gain 60-GHz differential phasedarray antenna in PCB process”中,一个宽带多层的相控阵天线被提出,它基于PCB工艺加工,最终实现了90%的辐射效率。The magnetoelectric dipole antenna obtains a symmetrical pattern on the E plane and the H plane by constructing magnetic poles and poles on the antenna radiation aperture, and its double resonance point can meet broadband matching. MIMO radar for autonomous driving has strict requirements on the 3dB beamwidth of the antenna. For example, in the paper "Patch Array Antenna Using a Dual Coupled FeedingStructure for 79GHz Automotive Radar Applications", a 3dB beamwidth of 8.1° in the ZX plane is achieved, and 70° in the ZY plane. ° beamwidth; in the paper "Hybrid thin film multilayer antenna for automotive radar at 77GHz", a 3dB beamwidth of 40° on the H plane and 12° on the E plane was achieved. In addition, in the 77GHz frequency band, the limitation of processing technology is also a major challenge to antenna design. Recently, LTCC technology has been widely studied in this field of automotive radar, for example in the paper "A 79-GHz resonant laminated waveguide slotted array antenna using novel shaped slots in LTCC In ", a waveguide slot antenna based on LTCC technology was proposed, which works by resonance; in the paper "A 79-GHz radar sensor in LTCC technology using gridarray antennas", a grid array applied to 79GHz radar was proposed antenna. However, due to material loss and other reasons, the efficiency of the antenna processed by the LTCC process is low, usually below 30%, so the low-loss PCB process is often used in the millimeter wave frequency band. For example, in the paper "A low-cost and high-gain 60-GHz differential phasedarray antenna in PCB process", a broadband multi-layer phased array antenna is proposed, which is based on the PCB process and finally achieves a radiation efficiency of 90%. .

发明内容Contents of the invention

本发明在背景技术的基础上,提出了一种应用于自动驾驶雷达的新型磁电偶极子天线阵列,采用多层PCB板的结构,集成度高,频带宽,3dB波束宽度可调,和自动驾驶雷达所需求的天线性能十分吻合。On the basis of background technology, the present invention proposes a novel magnetoelectric dipole antenna array applied to automatic driving radar, which adopts the structure of multi-layer PCB board, has high integration, wide frequency band, and adjustable 3dB beam width, and The antenna performance required for autonomous driving radar is a good match.

本发明采用的技术方案如下:The technical scheme that the present invention adopts is as follows:

一种应用于自动驾驶雷达的磁电偶极子天线,该天线由下至上依次堆叠:第一层金属地第一层介质板、第二层金属地、第一层半固化片、第三层金属地、第二层介质板、第二层半固化片、第四层金属地、第三层介质板、第三层半固化片、第五层金属地、第四层介质板、第四层半固化片、第六层金属地、第五层介质板;A magnetoelectric dipole antenna applied to automatic driving radar, the antenna is stacked from bottom to top: the first layer of metal ground, the first layer of dielectric board, the second layer of metal ground, the first layer of prepreg, and the third layer of metal ground , The second layer of dielectric board, the second layer of prepreg, the fourth layer of metal ground, the third layer of dielectric board, the third layer of prepreg, the fifth layer of metal ground, the fourth layer of dielectric board, the fourth layer of prepreg, the sixth layer of metal Ground and fifth layer dielectric board;

第五层介质板上表面设置屏蔽腔金属环,该屏蔽腔金属环为环状贴片,屏蔽腔金属环对应位置均匀设置一圈屏蔽腔金属孔,用于连接屏蔽腔金属环与第六层金属地;屏蔽腔金属环的环状结构内设置多组磁电偶极子金属贴片,每组包括阵列为2×2的4个贴片,4个贴片相对的角相互连通,每个贴片对应位置设置一个磁电偶极子金属孔,用于连接贴片与第六层金属地;The metal ring of the shielding cavity is set on the upper surface of the dielectric plate of the fifth layer. The metal ring of the shielding cavity is a ring-shaped patch, and a circle of metal holes of the shielding cavity is evenly arranged at the corresponding position of the metal ring of the shielding cavity, which is used to connect the metal ring of the shielding cavity and the sixth layer. Metal ground; multiple groups of magnetoelectric dipole metal patches are set in the annular structure of the metal ring of the shielding cavity, each group includes 4 patches in an array of 2×2, and the opposite corners of the 4 patches are connected to each other, each A magnetoelectric dipole metal hole is set at the corresponding position of the patch, which is used to connect the patch and the sixth layer of metal ground;

所述第六层金属地上开设有耦合缝,一组磁电偶极子金属贴片对应一条耦合缝;A coupling seam is opened on the metal ground of the sixth layer, and a group of magnetoelectric dipole metal patches corresponds to a coupling seam;

所述第四层介质板上表面设置有叉形微带馈线,一条耦合缝对应一个叉形微带馈线,叉形微带馈线包括U形耦合区和位于U形底部向U形开口的反方向凸起的馈电区,耦合缝的两端正好与耦合区U形结构的两臂重叠,馈电区对应位置设置馈线输入孔,用于连接位于第三层介质板上表面的第二功分器贴片;第五层金属地上开设有用于穿过馈线输入孔的金属孔,保证馈线输入孔不与第五层金属地接触;A fork-shaped microstrip feeder is provided on the upper surface of the fourth layer dielectric plate, and one coupling slot corresponds to a fork-shaped microstrip feeder. The fork-shaped microstrip feeder includes a U-shaped coupling area and a U-shaped bottom located in the opposite direction to the U-shaped opening. In the raised feeding area, the two ends of the coupling slit just overlap with the two arms of the U-shaped structure of the coupling area, and the corresponding position of the feeding area is provided with a feeder input hole for connecting the second power divider located on the upper surface of the third layer dielectric board. There are metal holes for passing through the feeder input hole on the fifth layer of metal ground, so as to ensure that the feeder input hole does not contact the fifth layer of metal ground;

所述第三层介质板上表面的多个第二功分器贴片,第二功分器贴片每个输出孔对应连接一个馈线输入孔;A plurality of second power divider patches on the upper surface of the third layer dielectric board, each output hole of the second power divider patch is correspondingly connected to a feeder input hole;

所述第二层介质板上表面设置有一个第一功分器贴片,第一功分器贴片的每个输出孔对应连接一个第二功分器贴片的输出孔,且不与第四层金属地接触;第一功分器贴片贴片只包括一个输入孔;A first power divider patch is provided on the upper surface of the second layer dielectric board, and each output hole of the first power divider patch is correspondingly connected to an output hole of a second power divider patch, and is not connected with the first power divider patch. Four-layer metal ground contact; the first power divider patch only includes one input hole;

所述第一层金属地和第二层金属地开设有方形的空心区域,空心区域周围设置有一圈波导腔金属孔,该波导腔金属孔连通第一层金属地和第二层金属地;第二层金属地开设的空心区域尺寸大于第一层金属地上开设的空心区域;第二层金属地上空心区域内设置有矩形耦合贴片,矩形耦合贴片的边缘部设置波导腔输出孔,该波导腔输出孔与第一功分器贴片输入孔连接,并不与第三层金属地接触;The metal ground of the first layer and the metal ground of the second layer are provided with a square hollow area, and a circle of waveguide cavity metal holes is arranged around the hollow area, and the metal hole of the waveguide cavity communicates with the metal ground of the first layer and the metal ground of the second layer; The size of the hollow area on the second layer of metal ground is larger than that on the first layer of metal ground; a rectangular coupling patch is arranged in the hollow area on the second layer of metal ground, and a waveguide cavity output hole is set on the edge of the rectangular coupling patch. The cavity output hole is connected to the patch input hole of the first power divider, and is not in contact with the metal ground of the third layer;

波导腔金属孔围成的区域为磁电偶极子天线的输入。The area enclosed by the metal hole of the waveguide cavity is the input of the magnetoelectric dipole antenna.

进一步的,所述多组磁电偶极子金属贴片设置成一列,这一列磁电偶极子金属贴片的两侧各设置一列哑元阵列,该哑元阵列结构与磁电偶极子金属贴片相同,哑元阵列中每个磁电偶极子金属贴片对应一个耦合缝,再对应一个叉形微带馈线,但哑元阵列对应的叉形微带馈线的馈电区的馈线输入孔直接连接第五层金属地。Further, the plurality of groups of magnetoelectric dipole metal patches are arranged in a row, and a column of dummy arrays is respectively arranged on both sides of the row of magnetoelectric dipole metal patches, and the structure of the dummy array is the same as that of the magnetoelectric dipoles. The metal patch is the same, each magnetoelectric dipole metal patch in the dummy array corresponds to a coupling slot, and then corresponds to a fork-shaped microstrip feeder, but the feeder of the feeder area of the fork-shaped microstrip feeder corresponding to the dummy array The input hole is directly connected to the fifth layer metal ground.

本发明采用多层PCB板结构,易于加工,集成度高,具有平面结构,易于共形。通过耦合馈电的方式磁电偶极子阵列的阻抗带宽,通过添加可调节哑元和调整单元间距的方式实现了3dB波束宽度可调,满足自动驾驶MIMO雷达对天线的性能需求。磁电偶极子天线阵列的辐射结构为磁电偶极子,磁电偶极子的中部交叉相接可以改良天线的阻抗匹配性能。除了馈电阵列外,阵列两侧还添加了哑元辐射结构,哑元辐射结构的馈线接地,通过调整接地点可以调节哑元的反射相位,进而实现对水平方向3dB波束宽度的调节。所述磁电偶极子天线阵列的波导转同轴结构是由方形金属贴片和金属孔构成的围腔以及和功分器输入端相接的金属孔构成,通过耦合的方式实现波导场到同轴场的转变。The invention adopts a multi-layer PCB board structure, which is easy to process, has high integration, has a planar structure, and is easy to be conformal. The impedance bandwidth of the magnetoelectric dipole array is coupled and fed, and the 3dB beam width is adjustable by adding adjustable dummy elements and adjusting the unit spacing, which meets the performance requirements of the autonomous driving MIMO radar for the antenna. The radiation structure of the magnetoelectric dipole antenna array is magnetoelectric dipoles, and the middle parts of the magnetoelectric dipoles are cross-connected to improve the impedance matching performance of the antenna. In addition to the feed array, a dummy radiation structure is added on both sides of the array. The feeder of the dummy radiation structure is grounded. By adjusting the ground point, the reflection phase of the dummy can be adjusted, thereby realizing the adjustment of the 3dB beam width in the horizontal direction. The waveguide-to-coaxial structure of the magnetoelectric dipole antenna array is composed of a surrounding cavity composed of a square metal patch and a metal hole and a metal hole connected to the input end of the power divider, and the waveguide field is realized by coupling. Transformation of the coaxial field.

附图说明Description of drawings

图1为本发明磁电偶极子天线阵列分解3D视图。Fig. 1 is an exploded 3D view of the magnetoelectric dipole antenna array of the present invention.

图2为本发明磁电偶极子天线阵列侧视图。Fig. 2 is a side view of the magnetoelectric dipole antenna array of the present invention.

图3为本发明磁电偶极子天线阵列关键结构俯视图。其中图3(a)为未添加哑元的天线辐射结构俯视图,图3(b)为天线的叉形馈线和H形耦合开槽的俯视图,图3(c)为一分二功分器的俯视图,图3(d)为波导转同轴结构的俯视图。Fig. 3 is a top view of the key structure of the magnetoelectric dipole antenna array of the present invention. Among them, Fig. 3(a) is the top view of the antenna radiation structure without adding dummy elements, Fig. 3(b) is the top view of the fork-shaped feeder and H-shaped coupling slot of the antenna, and Fig. 3(c) is the structure of the one-to-two power splitter Top view, Figure 3(d) is a top view of the waveguide-to-coaxial structure.

图4为此天线哑元阵列示意图。其中图4(a)为添加哑元后的阵列辐射结构俯视图,图4(b)为哑元阵列叉形馈线接地的变化示意图。FIG. 4 is a schematic diagram of the antenna dummy array. Figure 4(a) is a top view of the array radiation structure after adding dummy elements, and Figure 4(b) is a schematic diagram of the grounding change of the dummy array fork feeder.

图5为此天线的图3(b)结构24在不同长度情况下水平面增益方向图。FIG. 5 is a horizontal plane gain pattern of the antenna structure 24 in FIG. 3( b ) with different lengths.

图6为此天线的回波损耗随频率变化图。Figure 6 shows the variation of return loss with frequency for this antenna.

图7为此天线的图3(b)结构24=0.45mm时的增益方向图。Fig. 7 is the gain pattern of the structure 24 = 0.45mm in Fig. 3(b) of this antenna.

图2中结构1为第一层金属地,结构2为第一层介质板,结构3为第二层金属地,结构4为第一层半固化片,结构5为第三层金属地,结构6为第二层介质板,结构7为第二层半固化篇,结构8为第四层金属地,结构9为第三层介质板,结构10为第三层半固化片,结构11为第五层金属地,结构12为第四层介质板,结构13为第四层半固化片,结构14为第六层金属地,结构15为第五层介质板。图3(a)中结构16为屏蔽腔金属环,结构17为屏蔽腔金属孔,结构18为磁电偶极子金属孔,结构19为磁电偶极子金属贴片,结构20为金属连接处。图3(b)中结构21为耦合缝,结构22为叉形微带馈线,结构23为馈线输入孔。图3(c)中结构25为功分器输出孔,结构26为功分器输入孔,结构27为第二功分器贴片。图3(d)中结构28为波导腔金属孔,结构29为矩形耦合贴片,结构30为波导腔输出孔,结构31为上层金属地缺少处。图4(a)中结构32为哑元阵列。图4(b)中结构33为接地点。In Figure 2, structure 1 is the first layer of metal ground, structure 2 is the first layer of dielectric board, structure 3 is the second layer of metal ground, structure 4 is the first layer of prepreg, structure 5 is the third layer of metal ground, and structure 6 is The second layer of dielectric board, structure 7 is the second layer of prepreg, structure 8 is the fourth layer of metal ground, structure 9 is the third layer of dielectric board, structure 10 is the third layer of prepreg, structure 11 is the fifth layer of metal ground , structure 12 is the fourth layer of dielectric board, structure 13 is the fourth layer of prepreg, structure 14 is the sixth layer of metal ground, and structure 15 is the fifth layer of dielectric board. In Fig. 3 (a), structure 16 is the metal ring of the shielding cavity, structure 17 is the metal hole of the shielding cavity, structure 18 is the metal hole of the magnetoelectric dipole, structure 19 is the metal patch of the magnetoelectric dipole, and structure 20 is the metal connection place. In FIG. 3( b ), structure 21 is a coupling slot, structure 22 is a fork-shaped microstrip feeder, and structure 23 is a feeder input hole. In Fig. 3(c), structure 25 is the output hole of the power divider, structure 26 is the input hole of the power divider, and structure 27 is the patch of the second power divider. In FIG. 3( d ), structure 28 is the metal hole of the waveguide cavity, structure 29 is the rectangular coupling patch, structure 30 is the output hole of the waveguide cavity, and structure 31 is the missing part of the upper layer metal. The structure 32 in Fig. 4(a) is a dummy array. The structure 33 in Fig. 4(b) is the grounding point.

具体实施方式Detailed ways

本实施例中磁电偶极子天线阵列分解3D视图如图1,天线工作在W频段,其由5层介质板和4层用于粘接的半固化片胶构成。介质板的材料为RO3003,相对介电常数为3。半固化片材料为RLP30,相对介电常数为3。天线阵列中天线单元的间距为2.4mm。图2为磁电偶极子天线阵列侧视图,其中所有的金属地层厚度都为0.03mm,第一、五层介质板2、15厚度为0.508mm,第二、三、四层介质板6、9、12厚度为0.254mm,所有的半固化片层厚度都为0.111mm。The exploded 3D view of the magnetoelectric dipole antenna array in this embodiment is shown in Figure 1. The antenna works in the W frequency band and consists of 5 layers of dielectric boards and 4 layers of prepreg for bonding. The material of the dielectric board is RO3003, and the relative permittivity is 3. The prepreg material is RLP30 with a relative dielectric constant of 3. The pitch of the antenna elements in the antenna array is 2.4mm. Fig. 2 is a side view of the magnetoelectric dipole antenna array, wherein all the metal formations have a thickness of 0.03mm, the thickness of the first and fifth dielectric plates 2 and 15 is 0.508mm, and the second, third and fourth dielectric plates 6, The thickness of 9 and 12 is 0.254mm, and the thickness of all prepreg layers is 0.111mm.

本实施例中磁电偶极子天线阵列关键结构俯视图如图3。图3(a)为未添加哑元的天线辐射结构俯视图,屏蔽腔金属环16宽度为0.8mm,屏蔽金属孔17直径为0.5mm,此屏蔽腔可以减少天线阵列同MIMO系统中其他组件的耦合,进而减少耦合对天线性能的恶化,磁电偶极子金属孔18、磁电偶极子金属铁片19、金属连接处20为构成磁电偶极子的部分,磁电偶极子金属孔18直径为0.4mm,磁电偶极子金属贴片19边长为0.8mm,金属连接处20可以很大程度地改善天线的匹配性能,它的宽度为0.1mm。图3(b)为天线的叉形馈线和H形耦合开槽的俯视图,其中耦合缝21的宽度为0.1mm,H形两侧延长部分长度为0.19mm,开槽整体的长度为0.8mm,其中叉形微带馈线22的叉形开口宽度为0.82mm,微带线整体宽度为0.11mm,切角部分为直角三角形,直角边长为0.1mm,馈线输入孔23为金属化通孔,它的直径为0.2mm,它和下层的功分器输出端相连,其在微带线层金属焊盘单边宽度0.1mm,为了方便连接,叉形微带馈线22中输入部分的宽度同金属化通孔添加焊盘后的直径相同,通过叉形馈线,可以更好地将电磁场耦合到H形开槽的两端,使得在开槽层有环绕H形开槽两端的电流,进而将能量向上耦合到天线辐射结构上,H形开槽得长度影响电流路径的长度,进而可以影响天线的中心工作频率,其中金属过孔到叉形馈线开口的部分24由金属贴片组成,长度为0.35mm。图3(c)为一分二功分器的俯视图,一分二功分器共有两种类型,分别起到将能量一分二和二分四的作用,两种功分器结构相同细节尺寸不同,其中功分器输出孔25直径为0.2mm,其为功分器的输出端,同上层结构的输入端相连,功分器输入孔26直径为0.2mm,其为功分器的输入端,同下层结构的输出端相连,功分器贴片27和功分器输出孔25的两个金属焊盘一同构成了功分器的微带线部分,两种功分器的尺寸仅在功分器贴片27的长度和宽度上有区别,一分二功分器的功分器贴片27长度为4.8mm宽度为0.1mm,二分四功分器的功分器贴片27长度为2.4mm,宽度为0.5mm,两级功分器通过级联的方式构成了一分四功分器。图3(d)为波导转同轴结构的俯视图,其由两层刻蚀掉矩形的金属地板贴片以及一些金属孔和一个矩形金属耦合贴片构成,其中波导腔金属孔28直径为0.2mm,矩形耦合贴片29的长度为1.5mm,宽度为0.9mm,波导腔输出孔30与功分器的输入端相接,直径为0.2mm,上层金属地缺少处31可以看到上下两层金属贴片地板上刻蚀掉的部分宽度不同,下层的金属地板所刻蚀的矩形宽度为1.27mm,长度为2.54毫米,而上层金属地板所刻蚀掉的矩形宽度比下层宽了0.26mm,这样做的目的是因为此矩形腔体会形成电磁谐振,从而恶化天线的匹配性能,拓宽上层所刻蚀的矩形宽度可以将此谐振移至更低的频率,改善天线阵列的匹配性能。The top view of the key structure of the magnetoelectric dipole antenna array in this embodiment is shown in Fig. 3 . Figure 3(a) is a top view of the antenna radiation structure without adding dummy elements. The metal ring 16 of the shielding cavity has a width of 0.8mm, and the diameter of the shielding metal hole 17 is 0.5mm. This shielding cavity can reduce the coupling between the antenna array and other components in the MIMO system , and then reduce the deterioration of the coupling to the performance of the antenna, the magnetoelectric dipole metal hole 18, the magnetoelectric dipole metal iron sheet 19, and the metal connection 20 are the parts that constitute the magnetoelectric dipole, and the magnetoelectric dipole metal hole The diameter of 18 is 0.4mm, the side length of magnetoelectric dipole metal patch 19 is 0.8mm, and the metal connection 20 can greatly improve the matching performance of the antenna, and its width is 0.1mm. Fig. 3(b) is a top view of the fork-shaped feeder and the H-shaped coupling slot of the antenna, wherein the width of the coupling slot 21 is 0.1 mm, the length of the extensions on both sides of the H-shape is 0.19 mm, and the overall length of the slot is 0.8 mm. Wherein the width of the fork-shaped opening of the fork-shaped microstrip feeder 22 is 0.82mm, the overall width of the microstrip line is 0.11mm, the cut corner part is a right-angled triangle, and the length of the right-angled side is 0.1mm, and the feeder input hole 23 is a metallized through hole. The diameter of the fork-shaped microstrip feeder 22 is 0.2mm, and it is connected to the output end of the power divider on the lower layer. Its width on one side of the metal pad on the microstrip line layer is 0.1mm. The diameter of the through hole after adding the pad is the same. Through the fork-shaped feeder, the electromagnetic field can be better coupled to the two ends of the H-shaped slot, so that there is a current around the two ends of the H-shaped slot in the slot layer, and then the energy is upward. Coupled to the radiation structure of the antenna, the length of the H-shaped slot affects the length of the current path, which in turn can affect the central operating frequency of the antenna. The part 24 from the metal via to the fork-shaped feeder opening is composed of a metal patch with a length of 0.35mm . Figure 3(c) is a top view of the one-to-two power divider. There are two types of one-to-two power dividers, which respectively play the role of dividing energy into two and two into four. The two power dividers have the same structure and different details. , wherein the power splitter output hole 25 has a diameter of 0.2 mm, which is the output end of the power splitter, and is connected with the input end of the superstructure, and the power splitter input hole 26 has a diameter of 0.2 mm, which is the input end of the power splitter. Connected to the output end of the lower structure, the power divider patch 27 and the two metal pads of the power divider output hole 25 together constitute the microstrip line part of the power divider, and the size of the two power dividers is only in the power divider There are differences in the length and width of the patch 27, the length of the patch 27 of the splitter patch 27 of the one-to-two splitter is 4.8mm and the width is 0.1mm, and the splitter patch 27 of the splitter patch 27 of the splitter is 2.4mm in length , the width is 0.5mm, and the two-stage power divider is cascaded to form a one-point four-power divider. Figure 3(d) is a top view of the waveguide-to-coaxial structure, which is composed of two layers of etched rectangular metal floor patches, some metal holes and a rectangular metal coupling patch, in which the diameter of the waveguide cavity metal hole 28 is 0.2mm , the length of the rectangular coupling patch 29 is 1.5 mm, the width is 0.9 mm, the output hole 30 of the waveguide cavity is connected to the input end of the power divider, and the diameter is 0.2 mm, and the upper and lower metal layers can be seen at the missing part 31 of the upper layer metal The width of the etched part on the patch floor is different. The width of the rectangle etched on the lower metal floor is 1.27mm, and the length is 2.54mm, while the width of the rectangle etched on the upper metal floor is 0.26mm wider than that of the lower layer. The purpose of doing this is because the rectangular cavity will form electromagnetic resonance, which will deteriorate the matching performance of the antenna. Widening the width of the etched rectangle on the upper layer can move this resonance to a lower frequency and improve the matching performance of the antenna array.

本实施例中天线哑元阵列示意图如图4。图4(a)为添加哑元后的阵列辐射结构俯视图,其中哑元阵列32的位置在中心阵列两侧各1.95mm,哑元阵列仅保留原阵列的第1、2和3层结构,因为叉形馈电结构接地,所以略去其下层的金属结构部分。图4(b)为哑元阵列叉形馈线接地的变化示意图,接地点33为金属通孔,直径为0.2mm,在哑元阵列中使其与地板相接,再通过调整金属过孔到叉形馈线开口的部分24的长度,可以对其反相位进行调节,进而达到调整天线阵面相位分布的目的,来控制水平角度的3dB波束宽度。A schematic diagram of an antenna dummy array in this embodiment is shown in FIG. 4 . Figure 4(a) is a top view of the radiation structure of the array after adding dummy elements, in which the position of the dummy element array 32 is 1.95mm on both sides of the central array, and the dummy element array only retains the first, second and third layer structures of the original array, because The fork feed structure is grounded, so the metal structure part of the lower layer is omitted. Figure 4(b) is a schematic diagram of the grounding change of the dummy array fork-shaped feeder. The grounding point 33 is a metal through hole with a diameter of 0.2 mm. The length of the part 24 of the shaped feeder opening can be adjusted for its reverse phase, thereby achieving the purpose of adjusting the phase distribution of the antenna front to control the 3dB beamwidth of the horizontal angle.

图5给出了此天线的金属过孔到叉形馈线开口的部分24在不同长度情况下水平面增益方向图,可以看到随着金属过孔到叉形馈线开口的部分24的长度变长,天线的水平面3dB波束宽度也在逐渐变宽,可以根据自动驾驶MIMO雷达的需要选择合适的尺寸。Fig. 5 shows the horizontal plane gain pattern of the antenna at different lengths from the metal via hole to the fork-shaped feeder opening. It can be seen that as the length of the metal via to the fork-shaped feeder opening 24 becomes longer, The horizontal 3dB beam width of the antenna is also gradually widening, and an appropriate size can be selected according to the needs of the MIMO radar for autonomous driving.

图6给出了此天线的回波损耗随频率变化图,并且包含金属过孔到叉形馈线开口的部分24在不同长度下的多种情况,金属过孔到叉形馈线开口的部分24对天线回波损耗性能影响较小,天线阵列在74.5~80GHz(甚至更高频率)都可以实现回波损耗小于10dB。Figure 6 shows the return loss of the antenna as a function of frequency, and includes a variety of situations at different lengths of the part 24 from the metal via to the fork-shaped feeder opening, and the part 24 from the metal via to the fork-shaped feeder opening is The performance of the antenna return loss is less affected, and the antenna array can achieve a return loss of less than 10dB at 74.5-80GHz (or even higher frequencies).

图7给出了此天线的金属过孔到叉形馈线开口的部分24=0.45mm时的增益方向图,此时天线在水平面内的3dB波束宽度为-10.38°~9.47°,在垂直面内的3dB波束宽度为-52.42°~52.37°,符合自动驾驶MIMO雷达对天线的性能需求。Figure 7 shows the gain pattern of the antenna from the metal via to the fork-shaped feeder opening at 24 = 0.45mm. At this time, the 3dB beamwidth of the antenna in the horizontal plane is -10.38°~9.47°, and in the vertical plane The 3dB beam width is -52.42°~52.37°, which meets the performance requirements of MIMO radar for autonomous driving.

可以实现宽频带、高增益、水平面±50°~±55°的3dB波束宽度、垂直面±10°的3dB波束宽度。其特征在于:分为天线、功分器、波导转同轴结构三个部分;在于:天线部分由三层PCB板构成,最顶层的PCB板用于实现辐射,第二层和第三层PCB板用于耦合馈电;在于:功分器部分由四层PCB板构成,三个一分二功分器相接构成一分四功分器;在于:波导转同轴结构由两层PCB板构成,其尺寸可与WR-10波导相匹配。天线结构由改良的磁电偶极子构成,磁电偶极子辐射贴片中心相接可改善天线的阻抗匹配性能,拓宽天线的阻抗带宽。磁电偶极子周围存在由矩形环贴片和金属孔构成的围腔结构,围腔结构可以减少MIMO系统中的其他组件对天线的耦合干扰,减少集成应用下电磁干扰对天线性能的恶化。磁电偶极子通过耦合馈电,由叉形微带线向H形开槽耦合电磁场,再耦合到磁电偶极子辐射结构上,通过耦合的方式可以改善天线的阻抗匹配性能,拓宽天线的阻抗匹配带宽,进而增大天线抵抗公差带来的误差的能力。磁电偶极子阵列在竖直方向上通过控制单元间距来实现了垂直面±10°的3dB波束宽度,这可以提高天线增益,增大自动驾驶MIMO雷达的探测距离。磁电偶极子阵列在水平方向的阵列两侧添加可调反射相位的哑元阵列,进而改变天线阵面的辐射相位分布,控制水平方向的3dB波束宽度在±50°~±55°,增大自动驾驶MIMO雷达的探测角度。磁电偶极子由一分四功分器馈电构成1×4阵列,一分四功分器由三个一分二功分器级联构成,一分二功分器采用了同轴转微带线的结构,占用水平空间小。为了进行测量,为天线阵列添加了波导转同轴结构,通过耦合的方式完成了波导场转化为微带场,再转化为同轴场,并完成了其中的阻抗变换,使天线得以完成测量。It can realize broadband, high gain, 3dB beamwidth of ±50°~±55° in the horizontal plane, and 3dB beamwidth of ±10° in the vertical plane. It is characterized in that: it is divided into three parts: antenna, power divider, and waveguide to coaxial structure; in that: the antenna part is composed of three layers of PCB boards, the top PCB board is used to realize radiation, the second and third layers of PCB The board is used for coupling and feeding; because: the power splitter part is composed of four-layer PCB boards, and three one-two power splitters are connected to form one-point four-power splitter; because: the waveguide-to-coaxial structure is composed of two-layer PCB boards Composition, its size can be matched with WR-10 waveguide. The antenna structure is composed of improved magnetoelectric dipoles, and the centers of the magnetoelectric dipole radiation patches can improve the impedance matching performance of the antenna and widen the impedance bandwidth of the antenna. There is a surrounding cavity structure composed of rectangular ring patches and metal holes around the magnetoelectric dipole. The surrounding cavity structure can reduce the coupling interference of other components in the MIMO system to the antenna, and reduce the deterioration of antenna performance caused by electromagnetic interference in integrated applications. The magnetoelectric dipole is fed through coupling, and the electromagnetic field is coupled from the fork-shaped microstrip line to the H-shaped slot, and then coupled to the magnetoelectric dipole radiation structure. The impedance matching performance of the antenna can be improved by coupling, and the antenna can be widened. The impedance matching bandwidth of the antenna increases the ability of the antenna to resist the error caused by the tolerance. The magnetoelectric dipole array achieves a 3dB beamwidth of ±10° in the vertical plane by controlling the cell spacing in the vertical direction, which can improve the antenna gain and increase the detection range of the MIMO radar for autonomous driving. The magnetoelectric dipole array adds dummy arrays with adjustable reflection phases on both sides of the array in the horizontal direction, thereby changing the radiation phase distribution of the antenna array, and controlling the 3dB beamwidth in the horizontal direction to ±50°~±55°, increasing the Detection angle of MIMO radar for large autonomous driving. The magnetoelectric dipole is fed by a one-to-four power divider to form a 1×4 array. The one-to-four power divider is composed of three one-to-two power dividers cascaded. The structure of the microstrip line occupies a small horizontal space. For measurement, a waveguide-to-coaxial structure is added to the antenna array, and the waveguide field is converted into a microstrip field and then into a coaxial field through coupling, and the impedance transformation is completed, so that the antenna can complete the measurement.

Claims (2)

1.一种应用于自动驾驶雷达的磁电偶极子天线,该天线由下至上依次堆叠:第一层金属地、第一层介质板、第二层金属地、第一层半固化片、第三层金属地、第二层介质板、第二层半固化片、第四层金属地、第三层介质板、第三层半固化片、第五层金属地、第四层介质板、第四层半固化片、第六层金属地、第五层介质板;1. A magnetoelectric dipole antenna applied to automatic driving radar, the antenna is stacked from bottom to top: the first layer of metal ground, the first layer of dielectric board, the second layer of metal ground, the first layer of prepreg, the third layer The first layer of metal ground, the second layer of dielectric board, the second layer of prepreg, the fourth layer of metal ground, the third layer of dielectric board, the third layer of prepreg, the fifth layer of metal ground, the fourth layer of dielectric board, the fourth layer of prepreg, the fourth layer of Six layers of metal ground, fifth layer of dielectric board; 第五层介质板上表面设置屏蔽腔金属环,该屏蔽腔金属环为环状贴片,屏蔽腔金属环对应位置均匀设置一圈屏蔽腔金属孔,用于连接屏蔽腔金属环与第六层金属地;屏蔽腔金属环的环状结构内设置多组磁电偶极子金属贴片,每组包括阵列为2×2的4个贴片,4个贴片相对的角相互连通,每个贴片对应位置设置一个磁电偶极子金属孔,用于连接贴片与第六层金属地;The metal ring of the shielding cavity is set on the upper surface of the dielectric plate of the fifth layer. The metal ring of the shielding cavity is a ring-shaped patch, and a circle of metal holes of the shielding cavity is evenly arranged at the corresponding position of the metal ring of the shielding cavity, which is used to connect the metal ring of the shielding cavity and the sixth layer. Metal ground; multiple groups of magnetoelectric dipole metal patches are set in the annular structure of the metal ring of the shielding cavity, each group includes 4 patches in an array of 2×2, and the opposite corners of the 4 patches are connected to each other, each A magnetoelectric dipole metal hole is set at the corresponding position of the patch, which is used to connect the patch and the sixth layer of metal ground; 所述第六层金属地上开设有耦合缝,一组磁电偶极子金属贴片对应一条耦合缝;A coupling seam is opened on the metal ground of the sixth layer, and a group of magnetoelectric dipole metal patches corresponds to a coupling seam; 所述第四层介质板上表面设置有叉形微带馈线,一条耦合缝对应一个叉形微带馈线,叉形微带馈线包括U形耦合区和位于U形底部向U形开口的反方向凸起的馈电区,耦合缝的两端正好与耦合区U形结构的两臂重叠,馈电区对应位置设置馈线输入孔,用于连接位于第三层介质板上表面的第二功分器贴片;第五层金属地上开设有用于穿过馈线输入孔的金属孔,保证馈线输入孔不与第五层金属地接触;A fork-shaped microstrip feeder is provided on the upper surface of the fourth layer dielectric plate, and one coupling slot corresponds to a fork-shaped microstrip feeder. The fork-shaped microstrip feeder includes a U-shaped coupling area and a U-shaped bottom located in the opposite direction to the U-shaped opening. In the raised feeding area, the two ends of the coupling slit just overlap with the two arms of the U-shaped structure of the coupling area, and the corresponding position of the feeding area is provided with a feeder input hole for connecting the second power divider located on the upper surface of the third layer dielectric board. There are metal holes for passing through the feeder input hole on the fifth layer of metal ground, so as to ensure that the feeder input hole does not contact the fifth layer of metal ground; 所述第三层介质板上表面的多个第二功分器贴片,第二功分器贴片每个输出孔对应连接一个馈线输入孔;A plurality of second power divider patches on the upper surface of the third layer dielectric board, each output hole of the second power divider patch is correspondingly connected to a feeder input hole; 所述第二层介质板上表面设置有一个第一功分器贴片,第一功分器贴片的每个输出孔对应连接一个第二功分器贴片的输入孔,且不与第四层金属地接触;第一功分器贴片只包括一个输入孔;A first power divider patch is provided on the upper surface of the second layer dielectric board, and each output hole of the first power divider patch is connected to an input hole of a second power divider patch, and is not connected with the first power divider patch. Four-layer metal ground contact; the first power divider patch only includes one input hole; 所述第一层金属地和第二层金属地开设有方形的空心区域,空心区域周围设置有一圈波导腔金属孔,该波导腔金属孔连通第一层金属地和第二层金属地;第二层金属地开设的空心区域尺寸大于第一层金属地上开设的空心区域;第二层金属地上空心区域内设置有矩形耦合贴片,矩形耦合贴片的边缘部设置波导腔输出孔,该波导腔输出孔与第一功分器贴片输入孔连接,并不与第三层金属地接触;The metal ground of the first layer and the metal ground of the second layer are provided with a square hollow area, and a circle of waveguide cavity metal holes is arranged around the hollow area, and the metal hole of the waveguide cavity communicates with the metal ground of the first layer and the metal ground of the second layer; The size of the hollow area on the second layer of metal ground is larger than that on the first layer of metal ground; a rectangular coupling patch is arranged in the hollow area on the second layer of metal ground, and a waveguide cavity output hole is set on the edge of the rectangular coupling patch. The cavity output hole is connected to the patch input hole of the first power divider, and is not in contact with the metal ground of the third layer; 波导腔金属孔围成的区域为磁电偶极子天线的输入。The area enclosed by the metal hole of the waveguide cavity is the input of the magnetoelectric dipole antenna. 2.如权利要求1所述的一种应用于自动驾驶雷达的磁电偶极子天线,其特征在于,所述多组磁电偶极子金属贴片设置成一列,这一列磁电偶极子金属贴片的两侧各设置一列哑元阵列,该哑元阵列结构与磁电偶极子金属贴片相同,哑元阵列中每个磁电偶极子金属贴片对应一个耦合缝,再对应一个叉形微带馈线,但哑元阵列对应的叉形微带馈线的馈电区的馈线输入孔直接连接第五层金属地。2. A kind of magnetoelectric dipole antenna that is applied to automatic driving radar as claimed in claim 1, is characterized in that, described multiple groups of magnetoelectric dipole metal patches are arranged in a row, and the row of magnetoelectric dipoles A row of dummy element arrays are respectively arranged on both sides of the sub-metal patch, and the structure of the dummy element array is the same as that of the magnetoelectric dipole metal patch, and each magnetoelectric dipole metal patch in the dummy element array corresponds to a coupling slot, and then Corresponds to a fork-shaped microstrip feeder, but the feeder input hole of the feeder area of the fork-shaped microstrip feeder corresponding to the dummy array is directly connected to the fifth-layer metal ground.
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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107681262A (en) * 2017-09-12 2018-02-09 北京邮电大学 A kind of low section magnetoelectricity dipole antenna based on bending magnetic wall
CN107819203A (en) * 2017-09-29 2018-03-20 深圳大学 A Magnetoelectric Dipole Antenna Based on a Metasurface Dielectric Plate
CN109346837A (en) * 2018-09-28 2019-02-15 电子科技大学 An Ultra-Broadband Wide-Angle Scanning Phased Array Based on Magnetoelectric Dipole Antennas
CN111180886A (en) * 2020-03-03 2020-05-19 南京锐码毫米波太赫兹技术研究院有限公司 Miniaturized broadband dual-polarized magnetoelectric dipole millimeter-wave side-fire antenna and its array
CN112313836A (en) * 2019-11-22 2021-02-02 深圳市大疆创新科技有限公司 Millimeter wave antenna, antenna assembly, millimeter wave radar system and movable platform
WO2021021017A1 (en) * 2019-08-01 2021-02-04 National University Of Singapore A dipole antenna, an antenna array, and a method of fabricating the dipole antenna and the antenna array
CN113937510A (en) * 2021-09-29 2022-01-14 北京理工大学 A hybrid-fed Ka-band magnetoelectric dipole antenna array

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206301945U (en) * 2016-12-30 2017-07-04 广东盛路通信科技股份有限公司 A kind of multilayer planar aerial array
CN113078459B (en) * 2021-03-03 2022-03-15 电子科技大学 A Low Profile Broadband Circularly Polarized Magnetoelectric Dipole Antenna
CN113871861B (en) * 2021-09-29 2024-02-13 东南大学 4-bit electronic beam scanning planar antenna array

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107681262A (en) * 2017-09-12 2018-02-09 北京邮电大学 A kind of low section magnetoelectricity dipole antenna based on bending magnetic wall
CN107819203A (en) * 2017-09-29 2018-03-20 深圳大学 A Magnetoelectric Dipole Antenna Based on a Metasurface Dielectric Plate
CN109346837A (en) * 2018-09-28 2019-02-15 电子科技大学 An Ultra-Broadband Wide-Angle Scanning Phased Array Based on Magnetoelectric Dipole Antennas
WO2021021017A1 (en) * 2019-08-01 2021-02-04 National University Of Singapore A dipole antenna, an antenna array, and a method of fabricating the dipole antenna and the antenna array
CN112313836A (en) * 2019-11-22 2021-02-02 深圳市大疆创新科技有限公司 Millimeter wave antenna, antenna assembly, millimeter wave radar system and movable platform
CN111180886A (en) * 2020-03-03 2020-05-19 南京锐码毫米波太赫兹技术研究院有限公司 Miniaturized broadband dual-polarized magnetoelectric dipole millimeter-wave side-fire antenna and its array
CN113937510A (en) * 2021-09-29 2022-01-14 北京理工大学 A hybrid-fed Ka-band magnetoelectric dipole antenna array

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