CN203326117U - Compact-structure 16-element broadband substrate integration waveguide back chamber antenna array - Google Patents

Compact-structure 16-element broadband substrate integration waveguide back chamber antenna array Download PDF

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CN203326117U
CN203326117U CN2013203745939U CN201320374593U CN203326117U CN 203326117 U CN203326117 U CN 203326117U CN 2013203745939 U CN2013203745939 U CN 2013203745939U CN 201320374593 U CN201320374593 U CN 201320374593U CN 203326117 U CN203326117 U CN 203326117U
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substrate
integrated waveguide
cavity
antenna array
array
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关东方
钱祖平
张颖松
蔡洋
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PLA University of Science and Technology
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Abstract

一种结构紧凑的16元宽带基片集成波导背腔天线阵,包括:双面覆有金属层的介质基片,在介质基片上设有由金属化通孔构成的按照2*2阵列分布的基片集成波导背腔,在每个基片集成波导背腔中分别设有由金属化通孔构成的按照2*2阵列分布的基片集成波导子背腔,在2*2阵列分布的基片集成波导背腔的2*2阵列中心以及各个基片集成波导背腔的几何中心上分别设有感性耦合窗。通过调整缝隙距基片集成波导腔中心的偏移量来实现缝隙的辐射频率与腔的谐振频率分离,从而实现16个缝隙同相辐射,辐射增益叠加,且最大增益方向为正上方。

Figure 201320374593

A compact 16-element broadband substrate integrated waveguide cavity-backed antenna array, including: a dielectric substrate covered with metal layers on both sides, and on the dielectric substrate, there are metallized through-holes distributed in a 2*2 array. Substrate-integrated waveguide back cavities, in each substrate-integrated waveguide back cavity, there are substrate-integrated waveguide sub-cavities distributed in a 2*2 array, which are composed of metallized through holes, respectively. The center of the 2*2 array of chip-integrated waveguide back cavities and the geometric center of each substrate-integrated waveguide back cavity are respectively provided with inductive coupling windows. By adjusting the offset between the slot and the center of the substrate integrated waveguide cavity, the radiation frequency of the slot is separated from the resonant frequency of the cavity, so that 16 slots can radiate in phase, and the radiation gain is superimposed, and the maximum gain direction is directly above.

Figure 201320374593

Description

一种结构紧凑的16元宽带基片集成波导背腔天线阵A compact 16-element broadband substrate integrated waveguide cavity-backed antenna array

技术领域 technical field

本实用新型专利涉及一种结构紧凑的宽带背腔天线阵,尤其涉及一种结构紧凑的16元宽带基片集成波导背腔天线阵。  The utility model patent relates to a compact broadband cavity-backed antenna array, in particular to a compact 16-element broadband substrate integrated waveguide cavity-backed antenna array. the

背景技术 Background technique

基片集成波导(SIW)由于其自身低剖面,低损耗,易于与电路共面等优点被广泛应用于微波、毫米波器件中。近年来,出现了许多基于基片集成波导结构的天线,例如基片集成波导缝隙天线阵,基片集成波导背腔天线及其阵列等。基片集成波导背腔天线具有低剖面,高辐射性能,易于设计等优点。但是基片集成波导的低剖面决定了其高Q值,而Q值越高,天线的带宽越窄。展宽基片集成波导背腔天线的带宽已经成为了一个研究热点。传统的基片集成波导背腔天线阵由两部分组成,即馈电网络部分和辐射单元部分,需要设计专门馈电网络进行馈电,这不但增加了天线阵的面积,而且设计复杂。如何减少天线阵馈电网络的面积及复杂度成为大型阵列设计的一大难题。 Substrate integrated waveguide (SIW) is widely used in microwave and millimeter wave devices due to its low profile, low loss, and easy coplanarity with circuits. In recent years, many antennas based on substrate-integrated waveguide structures have emerged, such as substrate-integrated waveguide slot antenna arrays, substrate-integrated waveguide cavity-backed antennas and their arrays, and so on. The substrate-integrated waveguide cavity-backed antenna has the advantages of low profile, high radiation performance, and easy design. However, the low profile of the substrate integrated waveguide determines its high Q value, and the higher the Q value, the narrower the bandwidth of the antenna. Broadening the bandwidth of substrate-integrated waveguide cavity-backed antennas has become a research hotspot. The traditional substrate-integrated waveguide cavity-backed antenna array consists of two parts, namely, the feed network part and the radiation unit part. It is necessary to design a special feed network for feeding, which not only increases the area of the antenna array, but also complicates the design. How to reduce the area and complexity of the antenna array feed network has become a major problem in the design of large arrays.

实用新型内容 Utility model content

本实用新型的目的是提出一种结构紧凑的16元宽带基片集成波导背腔天线阵,该天线阵不但具有基片集成波导背腔天线的所有优点,而且不需要专门的馈电网络,具有紧凑的结构和较宽的阻抗带宽。 The purpose of this utility model is to propose a compact 16-element broadband substrate-integrated waveguide-backed cavity antenna array, which not only has all the advantages of the substrate-integrated waveguide-backed cavity antenna, but also does not require a special feed network, and Compact structure and wide impedance bandwidth.

为实现以上目的,本实用新型采用的技术方案如下: For realizing above object, the technical scheme that the utility model adopts is as follows:

一种结构紧凑的16元宽带基片集成波导背腔天线阵,包括:双面覆有金属层的介质基片,在介质基片上设有由金属化通孔构成的按照2*2阵列分布的基片集成波导背腔,在每个基片集成波导背腔中分别设有由金属化通孔构成的按照2*2阵列分布的基片集成波导子背腔,在2*2阵列分布的基片集成波导背腔的2*2阵列中心以及各个基片集成波导背腔的几何中心上分别设有感性耦合窗。 A compact 16-element broadband substrate integrated waveguide cavity-backed antenna array, including: a dielectric substrate covered with metal layers on both sides, and on the dielectric substrate, there are metallized through-holes distributed in a 2*2 array. Substrate-integrated waveguide back cavities, in each substrate-integrated waveguide back cavity, there are substrate-integrated waveguide sub-cavities distributed in a 2*2 array, which are composed of metallized through holes, respectively. The center of the 2*2 array of chip-integrated waveguide back cavities and the geometric center of each substrate-integrated waveguide back cavity are respectively provided with inductive coupling windows.

本天线阵由16个紧密相连的基片集成波导子背腔组成,采用同轴探针在天线阵中心位置馈电。能量通过5个感性耦合窗在16个腔中互相耦合,达到共振。在各基片集成波导背腔上表面开缝作为辐射单元,辐射缝隙偏离腔体中心,形成同相辐射。背腔既作为辐射单元,同时其本身又是馈电网络,这种新颖的天线阵结构不需要附加的馈电网络,结构非常紧凑,这种技术非常适合大型阵列天线的设计。通过调整缝隙距基片集成波导腔中心的偏移量来实现缝隙的辐射频率与腔的谐振频率分离,从而实现16个缝隙同相辐射,辐射增益叠加,且最大增益方向为正上方。通过调整缝隙的宽度来提高天线阵的阻抗带宽。采用同轴探针直接对腔体馈电,不需要馈电网络,结构紧凑,设计简单。 The antenna array is composed of 16 closely connected substrate-integrated waveguide sub-cavities, and a coaxial probe is used to feed power at the center of the antenna array. The energy is coupled to each other in 16 cavities through 5 inductive coupling windows to achieve resonance. The upper surface of each substrate integrated waveguide back cavity is slotted as a radiation unit, and the radiation slot deviates from the center of the cavity to form in-phase radiation. The back cavity not only serves as a radiation unit, but also serves as a feeding network. This novel antenna array structure does not require an additional feeding network, and the structure is very compact. This technology is very suitable for the design of large array antennas. By adjusting the offset between the slot and the center of the substrate integrated waveguide cavity, the radiation frequency of the slot is separated from the resonant frequency of the cavity, so that 16 slots can radiate in phase, and the radiation gain is superimposed, and the maximum gain direction is directly above. The impedance bandwidth of the antenna array is improved by adjusting the width of the slot. The coaxial probe is used to directly feed the cavity, no feeding network is required, the structure is compact, and the design is simple.

有益效果:Beneficial effect:

本实用新型的有益效果是,天线阵不但具有一般基片集成波导背腔天线低剖面、低损耗、易于与电路集成等优点,而且不需要馈电网络,结构简单、紧凑。同时其带宽比一般背腔天线(只有5%左右)展宽一倍以上,阻抗带宽达到12%。得益于基片集成波导的低损耗特性,该16元天线阵具有高增益的优点,最大增益达到17.3dB。  The beneficial effect of the utility model is that the antenna array not only has the advantages of low profile, low loss, and easy integration with circuits of general substrate integrated waveguide cavity-backed antennas, but also does not need a feeding network, and has a simple and compact structure. At the same time, its bandwidth is more than double that of ordinary cavity-backed antennas (only about 5%), and its impedance bandwidth reaches 12%. Thanks to the low-loss characteristics of the substrate-integrated waveguide, the 16-element antenna array has the advantage of high gain, with a maximum gain of 17.3dB. 

附图说明 Description of drawings

图1是本实用新型的正面结构示意图。图中1为基片集成波导背腔,由金属化通孔围成,2为辐射缝隙,3为感性耦合窗,4同轴探针,在天线阵中央馈电。 Fig. 1 is a schematic diagram of the front structure of the utility model. In the figure, 1 is the substrate integrated waveguide back cavity, surrounded by metallized through holes, 2 is the radiation slot, 3 is the inductive coupling window, and 4 is the coaxial probe, which is fed in the center of the antenna array.

图2是本实用新型的剖面结构示意图。图中4为同轴探针。 Fig. 2 is a schematic cross-sectional structure diagram of the utility model. Figure 4 is a coaxial probe.

图3是本实用新型天线阵回波损耗随偏移量变化示意图。 Fig. 3 is a schematic diagram of the variation of the return loss of the antenna array of the present invention with the offset.

图4是本实用新型天线阵回波损耗随缝隙宽度变化示意图。 Fig. 4 is a schematic diagram of the variation of the return loss of the antenna array of the present invention with the width of the slot.

图5 是本实用新型天线阵的仿真回波损耗示意图。 Fig. 5 is a schematic diagram of the simulated return loss of the antenna array of the present invention.

图6是本实用新型天线阵的仿真增益示意图。 Fig. 6 is a schematic diagram of simulation gain of the antenna array of the present invention.

图7是本实用新型天线阵的E面仿真方向图。 Fig. 7 is a simulation direction diagram of the E plane of the antenna array of the present invention.

图8是本实用新型天线阵的H面仿真方向图。  Fig. 8 is the H plane simulation direction diagram of the antenna array of the present invention. the

具体实施方式 Detailed ways

一种结构紧凑的16元宽带基片集成波导背腔天线阵,包括:双面覆有金属层的介质基片,在介质基片上设有由金属化通孔构成的按照2*2阵列分布的基片集成波导背腔,在每个基片集成波导背腔中分别设有由金属化通孔构成的按照2*2阵列分布的基片集成波导子背腔1,在2*2阵列分布的基片集成波导背腔的2*2阵列中心以及各个基片集成波导背腔的几何中心上分别设有感性耦合窗3。在本实施例中,在各基片集成波导子背腔1内设有辐射缝隙2且辐射缝隙2偏离基片集成波导子背腔1的中心,在2*2阵列分布的基片集成波导背腔的2*2阵列中心设有同轴探针4。 A compact 16-element broadband substrate integrated waveguide cavity-backed antenna array, including: a dielectric substrate covered with metal layers on both sides, and on the dielectric substrate, there are metallized through-holes distributed in a 2*2 array. Substrate-integrated waveguide back cavities, each substrate-integrated waveguide back-cavity is provided with substrate-integrated waveguide sub-cavities 1 composed of metallized through-holes distributed in a 2*2 array, and distributed in a 2*2 array Inductive coupling windows 3 are respectively provided at the center of the 2*2 array of substrate-integrated waveguide back cavities and the geometric center of each substrate-integrated waveguide back cavity. In this embodiment, a radiation slot 2 is provided in each substrate-integrated waveguide sub-cavity 1 and the radiation slot 2 deviates from the center of the substrate-integrated waveguide sub-cavity 1. The center of the 2*2 array of chambers is provided with a coaxial probe 4 .

下面结合附图和实施例对本实用新型作进一步说明。 Below in conjunction with accompanying drawing and embodiment the utility model is further described.

本天线阵由16个紧密相连的基片集成波导背腔1组成16元天线阵。基片集成波导背腔由金属化通孔围成,形成一种低剖面的易于集成的波导结构。通过5个感性耦合窗3,将16个腔互通,使能量可以在所有的腔中共振。在天线阵的中心位置采用同轴探针4馈电,如图1所示,这样能量就能对称,均匀的到达每个基片集成波导腔中,并且形成谐振。背腔既作为辐射单元,同时其本身也是馈电网络,这种新颖的天线阵结构不需要附加的馈电网络,结构非常紧凑,这种技术非常适合大型阵列天线的设计。在各基片集成波导背腔上表面开缝作为辐射单元。为了实现同相辐射,通过调整缝隙距基片集成波导腔中心的偏移量来实现缝隙的辐射频率与腔的谐振频率分离,这样可以使各个缝隙周围的电流保持同相,从而达到辐射增益叠加,且最大增益方向为正上方的目的。回波损耗随偏移量变化的曲线如图3所示,随着偏移量的增加,缝隙的辐射频率逐渐与腔体的谐振频率分离,当偏移量为2mm左右,带宽宽,匹配好。通过增加缝隙的宽度,优化缝隙的长宽比,从而展宽天线阵的阻抗带宽。回波损耗随缝隙宽度变化的曲线如图4所示,随着缝隙变宽,天线的带宽展宽,当缝隙宽度达到2mm时,宽度再增加,阻抗匹配会恶化。最终优化后的回波损耗曲线如图5所示,在19GHz到21.4GHz的频率范围内回波损耗小于-10dB,天线阻抗带宽达到12%,为一般背腔缝隙天线的两倍以上。天线阵的增益曲线如图6所示,得益于基片集成波导的低损耗特性,该16元天线阵具有高增益的优点,最大增益达到17.3dB。天线阵的归一化E面和H面方向图曲线如图7、8所示。E面半波束宽度为180,最大副瓣小于-14 dB,H面半波束为200,最大副瓣小于-18 dB,最大辐射方向为正上方。 The antenna array consists of 16 closely connected substrate-integrated waveguide back cavities 1 to form a 16-element antenna array. The substrate-integrated waveguide back cavity is surrounded by metallized through-holes, forming a waveguide structure with low profile and easy integration. Through five inductive coupling windows 3, the 16 cavities are communicated, so that energy can resonate in all cavities. The coaxial probe 4 is used to feed power at the center of the antenna array, as shown in Figure 1, so that the energy can reach each substrate integrated waveguide cavity symmetrically and uniformly, and form resonance. The back cavity not only acts as a radiation unit, but also serves as a feed network. This novel antenna array structure does not require an additional feed network, and the structure is very compact. This technology is very suitable for the design of large array antennas. The upper surface of each substrate integrated waveguide back cavity is slotted as a radiation unit. In order to achieve in-phase radiation, the radiation frequency of the slot is separated from the resonant frequency of the cavity by adjusting the offset of the slot from the center of the substrate integrated waveguide cavity, so that the current around each slot can be kept in the same phase, so as to achieve radiation gain superposition, and The direction of maximum gain is aimed directly above. The curve of the return loss changing with the offset is shown in Figure 3. With the increase of the offset, the radiation frequency of the slot is gradually separated from the resonant frequency of the cavity. When the offset is about 2mm, the bandwidth is wide and the matching is good. . By increasing the width of the slot and optimizing the aspect ratio of the slot, the impedance bandwidth of the antenna array is widened. The curve of the return loss changing with the slot width is shown in Figure 4. As the slot becomes wider, the bandwidth of the antenna expands. When the slot width reaches 2 mm, the impedance matching will deteriorate as the width increases. The final optimized return loss curve is shown in Figure 5. The return loss is less than -10dB in the frequency range from 19GHz to 21.4GHz, and the antenna impedance bandwidth reaches 12%, which is more than twice that of the general cavity-backed slot antenna. The gain curve of the antenna array is shown in Figure 6. Thanks to the low-loss characteristics of the substrate integrated waveguide, the 16-element antenna array has the advantage of high gain, with a maximum gain of 17.3dB. The normalized E-plane and H-plane pattern curves of the antenna array are shown in Figures 7 and 8. The E-plane half-beam width is 18 0 , the maximum sidelobe is less than -14 dB, the H-plane half-beam is 20 0 , the maximum sidelobe is less than -18 dB, and the maximum radiation direction is directly above.

在结构上,基片集成波导子背腔1的尺寸决定整个天线阵大致的工作范围,辐射缝隙2的长度决定天线阵的工作频率,而调整缝隙的位置可以实现同相辐射,调整缝隙的宽度可以展宽天线阵的带宽。感性耦合窗3的大小对整个天线的很多性能都有影响。耦合窗越大,腔体的Q值越低,这样天线阵的带宽就会展宽,但是如果耦合窗过大就会影响整个天线阵的匹配,使回波损耗恶化,能量不能很好的辐射出去。  Structurally, the size of the substrate-integrated waveguide sub-back cavity 1 determines the approximate working range of the entire antenna array, and the length of the radiation slot 2 determines the operating frequency of the antenna array. Adjusting the position of the slot can achieve in-phase radiation, and adjusting the width of the slot can Broaden the bandwidth of the antenna array. The size of the inductive coupling window 3 affects many performances of the entire antenna. The larger the coupling window, the lower the Q value of the cavity, so that the bandwidth of the antenna array will be widened, but if the coupling window is too large, it will affect the matching of the entire antenna array, worsen the return loss, and the energy cannot be radiated well. . the

在制造上,本天线阵在一块5mm×5mm的高频介质板上实现,介质板厚度为1.5mm, 介电常数为2.2。通过在介质板上打金属化通孔实现基片集成波导结构,基片集成波导子背腔1由金属化通孔围成。馈电部分采用同轴探针4在天线阵中央馈电,因为天线阵工作频率在20GHz左右,频率较高,为了保证天线阵的高性能,所以采用高频接头馈电。介质板上下表面覆铜,辐射缝隙2作为辐射单元,将覆铜部分腐蚀掉。因为铜长期放置在空气中,容易被氧化,为了保证天线长期使用,可以采用镀锡技术在铜皮的外部镀锡。 In manufacturing, the antenna array is implemented on a 5mm×5mm high-frequency dielectric board with a thickness of 1.5mm and a dielectric constant of 2.2. The substrate-integrated waveguide structure is realized by drilling metallized through-holes on the dielectric board, and the substrate-integrated waveguide sub-cavity 1 is surrounded by the metallized through-holes. The feeding part uses coaxial probe 4 to feed power in the center of the antenna array. Because the operating frequency of the antenna array is about 20GHz, the frequency is relatively high. In order to ensure the high performance of the antenna array, high-frequency connectors are used for feeding. Copper is coated on the upper and lower surfaces of the dielectric board, and the radiation slot 2 is used as a radiation unit to corrode the copper-clad part. Because copper is placed in the air for a long time, it is easy to be oxidized. In order to ensure the long-term use of the antenna, tinning technology can be used to plate the outside of the copper skin.

根据以上所述,便可实现本实用新型。 According to the above, the utility model can be realized.

Claims (3)

1.一种结构紧凑的16元宽带基片集成波导背腔天线阵,包括:双面覆有金属层的介质基片,其特征在于,在介质基片上设有由金属化通孔构成的按照2*2阵列分布的基片集成波导背腔,在每个基片集成波导背腔中分别设有由金属化通孔构成的按照2*2阵列分布的基片集成波导子背腔(1),在2*2阵列分布的基片集成波导背腔的2*2阵列中心以及各个基片集成波导背腔的几何中心上分别设有感性耦合窗(3)。 1. A 16-element broadband substrate integrated waveguide cavity-backed antenna array with a compact structure, comprising: a dielectric substrate covered with a metal layer on both sides, characterized in that, the dielectric substrate is provided with a metallized through hole according to Substrate-integrated waveguide back cavities distributed in 2*2 arrays, and substrate-integrated waveguide sub-cavities (1) composed of metallized through-holes distributed in a 2*2 array are arranged in each substrate-integrated waveguide back cavity , inductive coupling windows (3) are respectively provided at the center of the 2*2 array of substrate-integrated waveguide back cavities distributed in a 2*2 array and the geometric center of each substrate-integrated waveguide back cavity. 2.根据权利要求1所述的结构紧凑的16元宽带基片集成波导背腔天线阵,其特征在于,在各基片集成波导子背腔(1)内设有辐射缝隙(2)且辐射缝隙(2)偏离基片集成波导子背腔(1)的中心。 2. The compact 16-element broadband substrate-integrated waveguide cavity-backed antenna array according to claim 1, characterized in that a radiation slot (2) is provided in each substrate-integrated waveguide sub-cavity (1) and radiates The slot (2) deviates from the center of the substrate-integrated waveguide sub-back cavity (1). 3.根据权利要求1或2所述的结构紧凑的16元宽带基片集成波导背腔天线阵,其特征在于,在2*2阵列分布的基片集成波导背腔的2*2阵列中心设有同轴探针(4)。 3. The compact 16-element broadband substrate-integrated waveguide-backed cavity antenna array according to claim 1 or 2, characterized in that, the 2*2 array center of the substrate-integrated waveguide-backed cavity distributed in the 2*2 array is set There are coaxial probes (4).
CN2013203745939U 2013-06-27 2013-06-27 Compact-structure 16-element broadband substrate integration waveguide back chamber antenna array Expired - Fee Related CN203326117U (en)

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