WO2018010260A1 - Conformal spherical antenna array - Google Patents

Conformal spherical antenna array Download PDF

Info

Publication number
WO2018010260A1
WO2018010260A1 PCT/CN2016/096414 CN2016096414W WO2018010260A1 WO 2018010260 A1 WO2018010260 A1 WO 2018010260A1 CN 2016096414 W CN2016096414 W CN 2016096414W WO 2018010260 A1 WO2018010260 A1 WO 2018010260A1
Authority
WO
WIPO (PCT)
Prior art keywords
antenna
layer
layer skeleton
antenna array
skeleton
Prior art date
Application number
PCT/CN2016/096414
Other languages
French (fr)
Chinese (zh)
Inventor
兰伟
燕标
吴亚飞
Original Assignee
成都泰格微波技术股份有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 成都泰格微波技术股份有限公司 filed Critical 成都泰格微波技术股份有限公司
Publication of WO2018010260A1 publication Critical patent/WO2018010260A1/en

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome

Definitions

  • the present invention relates to conformal antenna arrays, and more particularly to a conformal spherical antenna array.
  • a conformal (elliptical) spherical antenna array can achieve a full range of hemispherical radiation. It has unparalleled advantages in many antenna systems. It can be used in ground communication systems, airborne and vehicle-mounted mobile systems, and can also be applied to radar, positioning and navigation.
  • conformal antenna arrays such as a cone array, a spherical array, a cylindrical array, and the like. It has the characteristics of a conventional planar antenna array, and there are many differences in its peers.
  • Planar arrays have been well established in many fields, but their scan angles are generally up to about 60°.
  • the spherical array can be covered in all directions. This works well in areas such as satellite tracking and communications. Conformal spherical arrays have great advantages in terms of size, power consumption, and cost under the same wide radiation angle.
  • the design of the spherical array is very demanding.
  • the array elements are not evenly distributed, and the pattern analysis becomes complicated. For an array with a large radius of curvature to obtain a low sidelobe pattern, the position of each element must be assigned so that all elements can effectively point to the specified direction.
  • the non-planar elements of the same plane are not neatly radiated, which may result in high cross-polarization.
  • An object of the present invention is to overcome the disadvantages of the prior art and to provide a conformal spherical antenna array having high radiation uniformity, low production cost, and good structural stability.
  • a conformal spherical antenna array comprising a radome An antenna array, a shield cover, a bottom plate and a supporting device, wherein the antenna array is mounted on the bottom plate, and the shielding cover is located between the antenna array and the bottom plate, the antenna cover covers the antenna array, and a ring is arranged on the bottom plate a slot, the lower edge of the radome is inserted into the annular groove, and is positioned by the locking positioning mechanism, the supporting device is installed at the bottom of the bottom plate, and the antenna array includes a first layer skeleton, a second layer skeleton, a third layer skeleton and an antenna, wherein the first layer skeleton, the second layer skeleton, and the third layer skeleton are all in the same ellipsoidal plane, and the inclination angle of each layer skeleton is different, the first layer skeleton, The second layer skeleton is tangent to the ellipsoid surface, and the third layer
  • the first layer of the skeleton is uniformly mounted with four antennas, the second layer of the skeleton is evenly mounted with eight antennas, and the third layer of the skeleton is evenly mounted with eleven antennas.
  • the top of the first layer skeleton is a dome structure, and a positioning device mounting hole is disposed on the top layer, a positioning device is installed in the mounting hole of the positioning device, and the positioning device is disposed in the positioning mounting hole.
  • the four positioning devices on the positioning column are positioned.
  • the first layer skeleton and the second layer skeleton are connected to each other, and the second layer skeleton and the third layer skeleton are connected with the weight reduction holes.
  • the outer sidewall of the bottom of the third layer skeleton is provided with a plurality of evenly distributed antenna frame mounts, and the antenna frame mount is provided with a threaded through hole, and the bottom plate is provided with an antenna frame
  • the antenna frame mounting hole corresponding to the mounting seat, and the third skeleton is fastened by a connecting screw installed in the antenna frame mounting seat and the antenna frame mounting hole.
  • the locking and positioning mechanism includes a locking screw, and a plurality of threaded through holes are formed in a sidewall of the annular groove, and a lower edge of the shielding cover is disposed with a threaded through hole.
  • the hole, the radome and the bottom plate are locked and locked by a locking screw locked in the threaded through hole and the positioning hole.
  • the support device is a support column, and the upper and lower ends of the support column are provided with a connection flange.
  • the supporting device is an L-shaped mounting seat, and the L-shaped mounting seat is provided with a stepped hole connected to the bottom plate and a fixed through hole for fixing the L-shaped mounting seat.
  • the bottom of the bottom plate is further provided with a joint seat and a waterproof breathable valve, and the waterproof breathable valve is located at the joint seat.
  • the present invention has the following advantages:
  • the conformal spherical antenna array of the present invention the antenna array is divided into three layers of skeletons, and the skeleton is hollowed out, which ensures the structural strength and reduces the weight of the skeleton, and the same is also reduced.
  • the skeleton consumables, and the skeleton is made by 3D printing technology. Compared with the traditional process, the processing efficiency is high, the processing precision is high, and the production cost is low.
  • Each layer has different inclination angles between the skeletons, thereby improving the uniformity of the antenna radiation, that is, the gain flatness in the scanning range, and the skeleton adopts a hollow structure, thereby ensuring the performance of the skeleton and reducing the material cost of the skeleton.
  • the weight; the first layer skeleton adopts a dome structure, thereby ensuring the uniformity of the force of the antenna mounting skeleton, thereby improving the stability of the antenna mounting skeleton, and the pitch angle of the antenna is adjustable, so that the antenna can be adjusted according to actual needs.
  • the elevation angle of the antenna array improves the versatility of the antenna array; the antenna array is installed by the support device, which can be different according to The environment is used in conjunction with the installation of different mounting accessories to enable the installation of the vehicle, the shipboard and the groundwork, thereby improving the versatility of the spherical antenna array.
  • Embodiment 1 is a schematic structural view of Embodiment 1;
  • Embodiment 2 is a schematic structural view of Embodiment 2;
  • FIG. 3 is a schematic structural view of an antenna array
  • FIG. 4 is a schematic view showing the connection of a first layer skeleton, a second layer skeleton, and a third layer skeleton;
  • FIG. 5 is a schematic structural view of an antenna
  • FIG. 6 is a perspective view of a bottom plate of the embodiment
  • FIG. 8 is a perspective view of a bottom plate of the second embodiment
  • FIG. 9 is a bottom view of the bottom plate of the second embodiment.
  • a conformal spherical antenna array includes a radome 13, an antenna array 14, a shield cover 15, a bottom plate 16, and a supporting device, and the antenna array 14 is mounted.
  • the shielding cover 15 is located between the antenna array 14 and the bottom plate 16
  • the radome 13 covers the antenna array 14, and the bottom plate 16 is provided with an annular groove 18, and the radome 13 is under the hood.
  • the edge is inserted into the annular groove 18 and is positioned by the locking and positioning mechanism.
  • the locking and positioning mechanism includes a locking screw 19, and the side wall of the annular groove 18 is provided with a plurality of threads.
  • the lower edge of the shielding cover 13 is provided with a positioning hole with a threaded through hole, and the locking screw lock between the radome 13 and the bottom plate 16 is locked in the threaded through hole and the positioning hole Tight positioning, in this way, the original end face sealing structure is changed, so that the sealing performance between the radome 13 and the bottom plate 16 is ensured, thereby ensuring the shielding effect of the shield cover 15, and improving the quality of the antenna array.
  • the support device is mounted on the bottom of the bottom plate 16,
  • the antenna array 14 includes a first layer skeleton 1, a second layer skeleton 2, a third layer skeleton 3, and an antenna 11, and the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton 3 are all in the same In the ellipsoidal plane, and the inclination angle of each layer of the skeleton is different, the first layer skeleton 1 and the second layer skeleton 2 are tangent to the ellipsoidal surface, and the third layer skeleton 3 and the second layer skeleton 1 have a tangent to the spherical tangent
  • the angle a, , preferably, the angle ⁇ of the tangential line is 10°.
  • the uniformity of the antenna radiation that is, the gain flatness within the scanning range can be improved.
  • the first layer skeleton 1, the second layer The layer skeleton 2 and the third layer skeleton 3 are not limited to the ellipsoidal surface, and may be a spherical surface.
  • the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton 3 are each provided with a plurality of antenna mounting holes. 4, a plurality of antenna support columns 6 are disposed on the skeleton around the antenna mounting hole 4, and the antenna 11 is provided with a mounting hole 12 corresponding to the antenna support column 6, and the antenna 11 is mounted by screws.
  • the antenna support column 6 is four Further, Jian antenna 11 is provided on the outer four projections, corresponding to the mounting holes 12 provided on the bump Jian, installation inch, the height of the antenna support pole 6 may be changed so as to be In order to change the elevation angle of the antenna unit by changing the height of the antenna support column 6, in order to satisfy the adjustment of the antenna support column 6, the antenna support column 6 and the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton 3 may be employed. The threaded connection is installed, and the height of the antenna support column 6 is adjusted by adjusting the amount of screwing of the antenna support column 6.
  • the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton are 3 Made by 3D printing technology, it has high processing efficiency, high processing precision and low production cost compared with traditional technology.
  • antennas 11 are uniformly mounted on the first layer skeleton 1, and eight antennas are evenly mounted on the second layer skeleton 2, and the third layer skeleton 3 is Ten antennas 11 are evenly mounted on the top, so the total number of antennas 11 is 23, and 23 antennas are the minimum number of units that meet the requirements.
  • the number of small units is required by the overall index, the number of units is Position, position, etc. are variables, cell spacing, ellipsoid size, etc. are constraints, and the unit pattern is equivalent to the point source pattern optimized by genetic algorithm. The specific ideas are as follows:
  • the antenna's metrics are required to analyze the required antenna element characteristics and the topology of the conformal antenna array.
  • the optimization unit algorithm is used to determine the required unit pattern, and then the conformal array topology layout is further optimized.
  • the antenna array operates in the S-band with a bandwidth of 10% and a scan range of -75° to 75° and an azimuth of 0°-360°.
  • the antenna array has a gain greater than 13dBi in the scan range and a gain flatness less than ldB.
  • the antenna array can support dual circular polarization mode at the same time, and its axial ratio is less than 3dB. Peer antennas should be able to simultaneously receive the capability of more than three satellites.
  • the antenna gain optimization must be greater than 13 dBi and the gain flatness is less than 1 dB over the entire upper half of the airspace.
  • the top of the first layer skeleton 1 is a dome structure, and the dome-shaped shape of the dome mechanism has the characteristics of four-sided force transmission, so that the wall thickness of the bracket can be satisfied on the basis of satisfying the same force.
  • the weight of the antenna mounting frame is reduced, and a positioning device mounting hole 5 is disposed at the top of the first layer frame 1.
  • the positioning device 10 is mounted in the positioning device mounting hole 5, and the positioning device 10 is set.
  • the four positioning device positioning posts 9 on the positioning mounting holes 5 are positioned.
  • the connecting rings of the first layer skeleton 1 and the second layer skeleton 2 and the connecting rings of the second layer skeleton 2 and the third layer skeleton 3 are each provided with a reduction
  • the heavy hole 8, that is, the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton 3 adopt a hollow design, which can not only reduce the weight of the antenna mounting skeleton, but also ensure the uniformity of the force of the antenna mounting skeleton. Thereby improving the stability of the antenna mounting skeleton.
  • the outer side wall of the bottom of the third layer frame 3 is provided with a plurality of evenly distributed antenna frame mounts 7, and the antenna frame mounts 7 are provided with threaded through holes, and the bottom plate 16 is disposed on the bottom plate 16 There is an antenna frame mounting hole 17 corresponding to the antenna frame mount 7, and the third frame 3 is fastened by a connecting screw mounted in the antenna frame mount 7 and the antenna frame mounting hole 17.
  • the bottom of the bottom plate 16 is further provided with a joint seat 23 and a waterproof gas permeable valve 22, the waterproof gas permeable valve 22 is located at one side of the joint seat 23, and the waterproof gas permeable valve 22 is provided with a waterproof gas permeable membrane.
  • the waterproof and breathable membrane is made of a polymer material, and the waterproof breathable valve 22 solves the respiratory effect of the conformal spherical antenna array.
  • the support device is a support column 20, and the upper and lower ends of the support column 20 are provided with a connection flange, and the connection between the support column 20 and the bottom plate 16 can be realized through the connection flange.
  • the same can also satisfy the support of the bottom plate 16, and the mounting ⁇ , the bottom of the support column 20 can be installed at the corresponding position to achieve stable installation of the conformal spherical antenna array.
  • Embodiment 2 is a diagrammatic representation of Embodiment 1
  • This embodiment is basically the same as the structure of the first embodiment. The only difference is that the structure of the supporting device is different. As shown in FIG. 2, FIG. 8 and FIG. 9, the supporting device is an L-shaped mounting seat 21, The L-shaped mounts 21 are pluralityed and evenly distributed on the lower surface of the bottom plate 16. Further, the L-shaped mounts 21 are provided with stepped holes connected to the bottom plate 16 and for fixing the L-shaped mounts. 21 fixed through hole, mounting ⁇ , L-shaped installation With the seat 21 fixed, a stable installation of the conformal spherical antenna array can be achieved.

Landscapes

  • Details Of Aerials (AREA)

Abstract

Disclosed in the present invention is a conformal spherical antenna array, comprising: a radome, an antenna array, a shielding cover, a base plate and a supporting apparatus; the antenna array is mounted on the base plate, and the shielding cover is located between the antenna array and the base plate; the radome covers the antenna array, and the bottom plate is provided with an annular groove; a lower edge of the radome is inserted into the annular groove and positioned by means of a locking and positioning mechanism; the support apparatus is mounted at a bottom portion of the bottom plate; the antenna array comprises: a first layer of frame, a second layer of frame, a third layer of frame and an antenna; the first layer of frame, the second layer of frame and the third layer of frame are all in a same ellipsoidal plane, and each layer of frame has a different inclination angle; the first layer of frame and the second layer of frame are tangent to the ellipsoidal plane; a spherical tangent of the second layer of frame and the third layer of frame has a tangent angle a. The present invention enjoys the following beneficial effects: highly uniform antenna radiation, low production cost and good structural stability.

Description

一种共形球面天线阵 技术领域  Conformal spherical antenna array
[0001] 本发明涉及共形天线阵, 特别是一种共形球面天线阵。  The present invention relates to conformal antenna arrays, and more particularly to a conformal spherical antenna array.
背景技术  Background technique
[0002] 共形 (椭) 球面天线阵可实现半球面全方位的辐射。 在众多天线系统中具有不 可比拟的优势。 可用于地面通信系统, 机载、 车载动中通系统, 同吋也能应用 于雷达、 定位、 导航领域。  [0002] A conformal (elliptical) spherical antenna array can achieve a full range of hemispherical radiation. It has unparalleled advantages in many antenna systems. It can be used in ground communication systems, airborne and vehicle-mounted mobile systems, and can also be applied to radar, positioning and navigation.
[0003] 共形天线阵有很多种类, 有锥形阵, 球面阵, 圆柱阵等。 它具备常规平面天线 阵的特性, 同吋也有很多不同之处。  [0003] There are many types of conformal antenna arrays, such as a cone array, a spherical array, a cylindrical array, and the like. It has the characteristics of a conventional planar antenna array, and there are many differences in its peers.
[0004] 平面阵已经很成熟应用于多个领域, 但其扫描角一般最多到 60°左右。 而球面 阵可以全方位覆盖。 这在卫星跟踪, 通信等领域能很好发挥作用。 在达到同样 宽辐射角度的条件下, 共形球面阵在体积、 功耗、 成本方面有很大的优势。 但 是球面阵的设计要求很高。 相对于平面阵, 其阵元分布不均匀, 方向图分析变 得复杂。 对于较大曲率半径的阵列要想获得低副瓣的方向图, 必须分配好各个 阵元的位置, 以使得所有阵元能够有效指向制定的方向。 同吋非平面的的阵元 辐射极化不整齐, 因此可能导致交叉极化很高。  [0004] Planar arrays have been well established in many fields, but their scan angles are generally up to about 60°. The spherical array can be covered in all directions. This works well in areas such as satellite tracking and communications. Conformal spherical arrays have great advantages in terms of size, power consumption, and cost under the same wide radiation angle. However, the design of the spherical array is very demanding. Compared with the planar array, the array elements are not evenly distributed, and the pattern analysis becomes complicated. For an array with a large radius of curvature to obtain a low sidelobe pattern, the position of each element must be assigned so that all elements can effectively point to the specified direction. The non-planar elements of the same plane are not neatly radiated, which may result in high cross-polarization.
[0005] (椭) 球面结构在加工方面难度较大, 且成本很高, 其设计难点主要有以下几 点: 1、 (椭) 球面共形天线单元特性及单元间的互耦分析困难, 2、 共形阵列 天线方向图综合困难, 3、 共形阵列天线极化控制困难, 4、 波束形成和控制复 杂, 5、 测试 (校准) 困难。  [0005] (Ellipse) Spherical structure is difficult in processing and costly. The design difficulties are as follows: 1. (Ellipse) Spherical conformal antenna element characteristics and mutual coupling analysis between units, 2 Conformal array antenna pattern is difficult to integrate. 3. Conformal array antenna polarization control is difficult. 4. Beamforming and control are complicated. 5. Testing (calibration) is difficult.
技术问题  technical problem
[0006] 本发明的目的在于克服现有技术的缺点, 提供一种天线辐射均匀度高、 生产成 本低和结构稳定性好的共形球面天线阵。  SUMMARY OF THE INVENTION An object of the present invention is to overcome the disadvantages of the prior art and to provide a conformal spherical antenna array having high radiation uniformity, low production cost, and good structural stability.
问题的解决方案  Problem solution
技术解决方案  Technical solution
[0007] 本发明的目的通过以下技术方案来实现: 一种共形球面天线阵, 它包括天线罩 、 天线阵、 屏蔽罩、 底板和支撑装置, 所述的天线阵安装在底板上, 且屏蔽罩 位于天线阵与底板之间, 所述的天线罩盖住天线阵, 且底板上幵设有一环形槽 , 所述的天线罩的下边缘插入环形槽内, 且通过锁紧定位机构定位, 所述的支 撑装置安装在底板的底部, 所述的天线阵包括第一层骨架、 第二层骨架、 第三 层骨架和天线, 所述的第一层骨架、 第二层骨架、 第三层骨架均在同一椭球面 内, 且每一层骨架的倾角均不相同, 所述的第一层骨架、 第二层骨架与椭球面 相切, 第三层骨架与第二层骨架球面切线具有切线夹角 a, 所述的第一层骨架、 第二层骨架、 第三层骨架上均幵设有多个天线安装孔, 所述的天线安装孔周围 的骨架上设置有多个天线支撑柱, 所述的天线上设置有与天线支撑柱对应的安 装孔, 所述的天线通过螺钉安装在天线支撑柱上。 The object of the invention is achieved by the following technical solution: A conformal spherical antenna array comprising a radome An antenna array, a shield cover, a bottom plate and a supporting device, wherein the antenna array is mounted on the bottom plate, and the shielding cover is located between the antenna array and the bottom plate, the antenna cover covers the antenna array, and a ring is arranged on the bottom plate a slot, the lower edge of the radome is inserted into the annular groove, and is positioned by the locking positioning mechanism, the supporting device is installed at the bottom of the bottom plate, and the antenna array includes a first layer skeleton, a second layer skeleton, a third layer skeleton and an antenna, wherein the first layer skeleton, the second layer skeleton, and the third layer skeleton are all in the same ellipsoidal plane, and the inclination angle of each layer skeleton is different, the first layer skeleton, The second layer skeleton is tangent to the ellipsoid surface, and the third layer skeleton and the second layer skeleton spherical tangent have a tangent angle a, and the first layer skeleton, the second layer skeleton, and the third layer skeleton are both provided with a plurality of An antenna mounting hole, a plurality of antenna supporting columns are disposed on the skeleton around the antenna mounting hole, and the antenna is provided with a mounting hole corresponding to the antenna supporting column, and the antenna is mounted on the antenna by screws Column.
[0008] 所述的第一层骨架上均匀安装有四个天线, 所述的第二层骨架上均匀安装有八 个天线, 所述的第三层骨架上均匀安装有十一个天线。  [0008] The first layer of the skeleton is uniformly mounted with four antennas, the second layer of the skeleton is evenly mounted with eight antennas, and the third layer of the skeleton is evenly mounted with eleven antennas.
[0009] 所述的第一层骨架的顶部为圆顶结构, 在其上幵设有一定位装置安装孔, 所述 的定位装置安装孔内安装有定位装置, 且定位装置通过设置在定位安装孔上的 四个定位装置定位柱定位。  [0009] The top of the first layer skeleton is a dome structure, and a positioning device mounting hole is disposed on the top layer, a positioning device is installed in the mounting hole of the positioning device, and the positioning device is disposed in the positioning mounting hole. The four positioning devices on the positioning column are positioned.
[0010] 所述的第一层骨架和第二层骨架的相接环上以及第二层骨架和第三层骨架的相 接环上均幵设有减重孔。  [0010] The first layer skeleton and the second layer skeleton are connected to each other, and the second layer skeleton and the third layer skeleton are connected with the weight reduction holes.
[0011] 所述的第三层骨架底部的外侧壁上设置有多个均匀分布的天线骨架安装座, 天 线骨架安装座上幵设有螺纹通孔, 所述的底板上幵设有与天线骨架安装座对应 的天线骨架安装孔, 第三次骨架通过安装在天线骨架安装座和天线骨架安装孔 内的连接螺钉紧固连接。  [0011] The outer sidewall of the bottom of the third layer skeleton is provided with a plurality of evenly distributed antenna frame mounts, and the antenna frame mount is provided with a threaded through hole, and the bottom plate is provided with an antenna frame The antenna frame mounting hole corresponding to the mounting seat, and the third skeleton is fastened by a connecting screw installed in the antenna frame mounting seat and the antenna frame mounting hole.
[0012] 所述的锁紧定位机构包括锁紧螺钉, 所述的环形槽的侧壁上幵设有多个螺纹通 孔, 所述的屏蔽罩的下边缘幵设有与螺纹通孔的定位孔, 所述的天线罩和底板 之间通过锁紧在螺纹通孔和定位孔内的锁紧螺钉锁紧定位。  [0012] The locking and positioning mechanism includes a locking screw, and a plurality of threaded through holes are formed in a sidewall of the annular groove, and a lower edge of the shielding cover is disposed with a threaded through hole. The hole, the radome and the bottom plate are locked and locked by a locking screw locked in the threaded through hole and the positioning hole.
[0013] 所述的支撑装置为支撑柱, 支撑柱的上下两端均设置有连接法兰。  [0013] The support device is a support column, and the upper and lower ends of the support column are provided with a connection flange.
[0014] 所述的支撑装置为 L形安装座, L形安装座上幵设有与底板连接的台阶孔以及用 以固定 L形安装座固定通孔。  [0014] The supporting device is an L-shaped mounting seat, and the L-shaped mounting seat is provided with a stepped hole connected to the bottom plate and a fixed through hole for fixing the L-shaped mounting seat.
[0015] 所述的底板的底部还设置有接头座和防水透气阀, 防水透气阀位于接头座的一 发明的有益效果 [0015] The bottom of the bottom plate is further provided with a joint seat and a waterproof breathable valve, and the waterproof breathable valve is located at the joint seat. Advantageous effects of the invention
有益效果  Beneficial effect
[0016] 本发明具有以下优点: 本发明的共形球面天线阵, 天线阵列分为三层骨架, 骨 架为缕空设计, 即保证了结构强度, 又降低了骨架的重量, 同吋也降低了骨架 的耗材, 而且骨架采用 3D打印技术制作, 与传统工艺相比, 其加工效率高、 加 工精度高和生产成本低, 在骨架上幵设有实现天线球面布阵的 23个天线安装孔 , 且每一层骨架之间具有不同的倾角, 从而改善了天线辐射的均匀性即扫描范 围内的增益平坦度, 且骨架采用缕空结构, 即保证了骨架的性能, 又降低了骨 架的用料成本和重量; 第一层骨架采用圆顶结构, 从而保证了天线安装骨架的 受力均匀性, 从而提高了天线安装骨架的稳定性, 并且天线的俯仰角度可调, 从而可根据实际需求, 调节天线的俯仰角, 提高天线阵列的通用性; 天线阵通 过支持装置安装, 可根据不同的使用环境配合安装不同的安装附件实现车载、 舰载以及地面工事的安装使用, 从而提高了该球面天线阵的通用性。  [0016] The present invention has the following advantages: The conformal spherical antenna array of the present invention, the antenna array is divided into three layers of skeletons, and the skeleton is hollowed out, which ensures the structural strength and reduces the weight of the skeleton, and the same is also reduced. The skeleton consumables, and the skeleton is made by 3D printing technology. Compared with the traditional process, the processing efficiency is high, the processing precision is high, and the production cost is low. 23 antenna mounting holes for implementing the antenna spherical array are arranged on the skeleton, and Each layer has different inclination angles between the skeletons, thereby improving the uniformity of the antenna radiation, that is, the gain flatness in the scanning range, and the skeleton adopts a hollow structure, thereby ensuring the performance of the skeleton and reducing the material cost of the skeleton. And the weight; the first layer skeleton adopts a dome structure, thereby ensuring the uniformity of the force of the antenna mounting skeleton, thereby improving the stability of the antenna mounting skeleton, and the pitch angle of the antenna is adjustable, so that the antenna can be adjusted according to actual needs. The elevation angle of the antenna array improves the versatility of the antenna array; the antenna array is installed by the support device, which can be different according to The environment is used in conjunction with the installation of different mounting accessories to enable the installation of the vehicle, the shipboard and the groundwork, thereby improving the versatility of the spherical antenna array.
对附图的简要说明  Brief description of the drawing
附图说明  DRAWINGS
[0017] 图 1为实施例一的结构示意图;  1 is a schematic structural view of Embodiment 1;
[0018] 图 2为实施例二的结构示意图; 2 is a schematic structural view of Embodiment 2;
[0019] 图 3为天线阵的结构示意图; 3 is a schematic structural view of an antenna array;
[0020] 图 4为第一层骨架、 第二层骨架、 第三层骨架的连接示意图;  4 is a schematic view showing the connection of a first layer skeleton, a second layer skeleton, and a third layer skeleton;
[0021] 图 5为天线的结构示意图;  [0021] FIG. 5 is a schematic structural view of an antenna;
[0022] 图 6为实施例一底板的立体示意图;  6 is a perspective view of a bottom plate of the embodiment;
[0023] 图 7为实施例一底板的仰视示意图;  7 is a bottom view of a bottom plate of the embodiment;
[0024] 图 8为实施例二底板的立体示意图;  8 is a perspective view of a bottom plate of the second embodiment;
[0025] 图 9为实施例二底板的仰视示意图;  9 is a bottom view of the bottom plate of the second embodiment; [0025] FIG.
[0026] 图中, 1-第一层骨架, 2-第二层骨架, 3-第三层骨架, 4-天线安装孔, 5-定位装 置安装孔, 6-天线支撑柱, 7-天线骨架安装座, 8-减重孔, 9-定位装置定位柱, 1 0-定位装置, 11-天线, 12-安装孔, 13-天线罩, 14-天线阵, 15-屏蔽罩, 16-底板 , 17-天线骨架安装孔, 18-环形槽, 19-锁紧螺钉, 20-支撑柱, 21-L形安装座, 2 2-防水透气阀, 23-接头座。 In the figure, 1-first layer skeleton, 2- second layer skeleton, 3-third layer skeleton, 4-antenna mounting hole, 5-positioning device mounting hole, 6-antenna support column, 7-antenna skeleton Mounting seat, 8-weight reducing hole, 9-positioning device positioning post, 1 0-positioning device, 11-antenna, 12-mounting hole, 13-radome, 14-antenna array, 15-shield, 16-base , 17-antenna skeleton mounting hole, 18-annular groove, 19-locking screw, 20-support column, 21-L-shaped mount, 2 2-waterproof breathable valve, 23-joint seat.
本发明的实施方式 Embodiments of the invention
[0027] 下面结合附图对本发明做进一步的描述, 本发明的保护范围不局限于以下所述 [0028] 实施例一:  [0027] The present invention will be further described below with reference to the accompanying drawings, and the scope of protection of the present invention is not limited to the following: [0028] Embodiment 1
[0029] 如图 1、 图 3〜图 7所示, 一种共形球面天线阵, 它包括天线罩 13、 天线阵 14、 屏 蔽罩 15、 底板 16和支撑装置, 所述的天线阵 14安装在底板 16上, 且屏蔽罩 15位 于天线阵 14与底板 16之间, 所述的天线罩 13盖住天线阵 14, 且底板 16上幵设有 一环形槽 18, 所述的天线罩 13的下边缘插入环形槽 18内, 且通过锁紧定位机构 定位, 在本实施例中, 所述的锁紧定位机构包括锁紧螺钉 19, 所述的环形槽 18 的侧壁上幵设有多个螺纹通孔, 所述的屏蔽罩 13的下边缘幵设有与螺纹通孔的 定位孔, 所述的天线罩 13和底板 16之间通过锁紧在螺纹通孔和定位孔内的锁紧 螺钉锁紧定位, 通过此种方式, 改变了原有端面密封结构, 从而使得天线罩 13 与底板 16之间的密封性能得到保证, 从而保证了屏蔽罩 15的屏蔽效果, 提高了 天线阵的质量, 所述的支撑装置安装在底板 16的底部, 所述的天线阵 14包括第 一层骨架 1、 第二层骨架 2、 第三层骨架 3和天线 11, 所述的第一层骨架 1、 第二 层骨架 2、 第三层骨架 3均在同一椭球面内, 且每一层骨架的倾角均不相同, 所 述的第一层骨架 1、 第二层骨架 2与椭球面相切, 第三层骨架 3与第二层骨架 1球 面切线具有切线夹角 a, , 优选的, 切线夹角 a为 10°, 通过这种方式, 可以改善 天线辐射的均匀性即扫描范围内的增益平坦度, 在实际过程中, 第一层骨架 1、 第二层骨架 2和第三层骨架 3并不仅限于椭球面, 也可以是球面, 所述的第一层 骨架 1、 第二层骨架 2、 第三层骨架 3上均幵设有多个天线安装孔 4, 所述的天线 安装孔 4周围的骨架上设置有多个天线支撑柱 6, 所述的天线 11上设置有与天线 支撑柱 6对应的安装孔 12, 所述的天线 11通过螺钉安装在天线支撑柱 6上, 在本 实施例中, 天线支撑柱 6为四个, 进一步的, 天线 11的外圆上幵设有四个凸块, 安装孔 12对应幵设在凸块上, 在安装吋, 天线支撑柱 6的高度可以改变, 从而可 以通过改变天线支撑柱 6的高度来改变天线单元的俯仰角, 为满足天线支撑柱 6 的调节, 可采用天线支撑柱 6与第一层骨架 1、 第二层骨架 2、 第三层骨架 3螺纹 连接的方式安装, 通过调整天线支撑柱 6的旋入量来调节天线支撑柱 6的高度, 在本实施例中, 所述的第一层骨架 1、 第二层骨架 2、 第三层骨架 3采用 3D打印技 术制作, 与传统工艺相比, 其加工效率高、 加工精度高和生产成本低。 [0029] As shown in FIG. 1, FIG. 3 to FIG. 7, a conformal spherical antenna array includes a radome 13, an antenna array 14, a shield cover 15, a bottom plate 16, and a supporting device, and the antenna array 14 is mounted. On the bottom plate 16, and the shielding cover 15 is located between the antenna array 14 and the bottom plate 16, the radome 13 covers the antenna array 14, and the bottom plate 16 is provided with an annular groove 18, and the radome 13 is under the hood. The edge is inserted into the annular groove 18 and is positioned by the locking and positioning mechanism. In the embodiment, the locking and positioning mechanism includes a locking screw 19, and the side wall of the annular groove 18 is provided with a plurality of threads. a through hole, the lower edge of the shielding cover 13 is provided with a positioning hole with a threaded through hole, and the locking screw lock between the radome 13 and the bottom plate 16 is locked in the threaded through hole and the positioning hole Tight positioning, in this way, the original end face sealing structure is changed, so that the sealing performance between the radome 13 and the bottom plate 16 is ensured, thereby ensuring the shielding effect of the shield cover 15, and improving the quality of the antenna array. The support device is mounted on the bottom of the bottom plate 16, The antenna array 14 includes a first layer skeleton 1, a second layer skeleton 2, a third layer skeleton 3, and an antenna 11, and the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton 3 are all in the same In the ellipsoidal plane, and the inclination angle of each layer of the skeleton is different, the first layer skeleton 1 and the second layer skeleton 2 are tangent to the ellipsoidal surface, and the third layer skeleton 3 and the second layer skeleton 1 have a tangent to the spherical tangent The angle a, , preferably, the angle θ of the tangential line is 10°. In this way, the uniformity of the antenna radiation, that is, the gain flatness within the scanning range can be improved. In the actual process, the first layer skeleton 1, the second layer The layer skeleton 2 and the third layer skeleton 3 are not limited to the ellipsoidal surface, and may be a spherical surface. The first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton 3 are each provided with a plurality of antenna mounting holes. 4, a plurality of antenna support columns 6 are disposed on the skeleton around the antenna mounting hole 4, and the antenna 11 is provided with a mounting hole 12 corresponding to the antenna support column 6, and the antenna 11 is mounted by screws. On the antenna support column 6, in this embodiment, the antenna support column 6 is four Further, Jian antenna 11 is provided on the outer four projections, corresponding to the mounting holes 12 provided on the bump Jian, installation inch, the height of the antenna support pole 6 may be changed so as to be In order to change the elevation angle of the antenna unit by changing the height of the antenna support column 6, in order to satisfy the adjustment of the antenna support column 6, the antenna support column 6 and the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton 3 may be employed. The threaded connection is installed, and the height of the antenna support column 6 is adjusted by adjusting the amount of screwing of the antenna support column 6. In this embodiment, the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton are 3 Made by 3D printing technology, it has high processing efficiency, high processing precision and low production cost compared with traditional technology.
[0030] 在本实施例中, 所述的第一层骨架 1上均匀安装有四个天线 11, 所述的第二层 骨架 2上均匀安装有八个天线, 所述的第三层骨架 3上均匀安装有十一个天线 11 , 因此天线 11总计 23个, 而 23个天线, 是满足要求下得到的最小单元数, 而这 个虽小单元数是在整体指标的要求下, 以单元个数、 位置等为变量, 单元间距 、 椭球大小等为约束条件, 将单元方向图等效成点源方向图用遗传算法进行优 化而得到的, 其具体思路如下:  [0030] In this embodiment, four antennas 11 are uniformly mounted on the first layer skeleton 1, and eight antennas are evenly mounted on the second layer skeleton 2, and the third layer skeleton 3 is Ten antennas 11 are evenly mounted on the top, so the total number of antennas 11 is 23, and 23 antennas are the minimum number of units that meet the requirements. However, although the number of small units is required by the overall index, the number of units is Position, position, etc. are variables, cell spacing, ellipsoid size, etc. are constraints, and the unit pattern is equivalent to the point source pattern optimized by genetic algorithm. The specific ideas are as follows:
[0031] 首先从系统指标出发, 分解出共形天线所需达到的指标要求。 然后, 从天线的 指标要求分析所需的天线单元特性以及共形天线阵列的拓扑结构。 进而通过优 化算法确定所需的单元方向图, 然后进一步对共形阵列拓扑结构布局进行优化 。 天线阵列工作在 S波段, 带宽为 10%, 扫描范围为俯仰角 -75°到 75°, 方位角 0°- 360°。 天线阵列在扫描范围内的增益要大于 13dBi, 增益平坦度小于 ldB。 天线 阵列能同吋支持双圆极化工作模式, 且其轴比小于 3dB。 同吋天线应该能同吋接 受多于三个卫星情报的能力。  [0031] First, starting from the system index, the index requirements required for the conformal antenna are decomposed. Then, the antenna's metrics are required to analyze the required antenna element characteristics and the topology of the conformal antenna array. Then, the optimization unit algorithm is used to determine the required unit pattern, and then the conformal array topology layout is further optimized. The antenna array operates in the S-band with a bandwidth of 10% and a scan range of -75° to 75° and an azimuth of 0°-360°. The antenna array has a gain greater than 13dBi in the scan range and a gain flatness less than ldB. The antenna array can support dual circular polarization mode at the same time, and its axial ratio is less than 3dB. Peer antennas should be able to simultaneously receive the capability of more than three satellites.
[0032] 显然, 对一个共形相控阵来说, 其首先应该被限制在一定的空间上, 在这里我 们限定其范围在一个直径小于 300mm的半球内。 同吋为了节约共形相控阵天线 的成本, 单元数和其位置是我们优化的一个重要变量。 其增益和增益平坦度是 非常重要的优化目标。 首先, 拟定一个天线单元方向图, 现在有两个变量: 每 个单元的位置坐标 (x, y, z)和天线单元的总数 N。 阵列的每个单元不能相交, 其大 小在限定在半球的半径必须小于 R, 也就是说, 每一个单元的坐标控制在一定的 范围之内。 另外, 在整个上半空域, 天线增益的优化结果必须大于 13 dBi, 并且 增益平坦度小于 1 dB。 我们使用遗传算法对单元的分布以及单元数量进行优化。 如果这个拟定的单元方向图不能优化出满足要求的结构, 对单元天线的方向图 进行调整, 选择一个新的方向图重新进行优化。 在优化目标达到我们要求之后 , 我们按着拟定的方向图去设计我们所需的单元方向图, 将此设计好的天线单 元按照优化的拓扑结构进行排布, 最后利用全波分析软件进行整体分析和优化 [0032] Obviously, for a conformal phased array, it should first be confined to a certain space, where we define its range in a hemisphere with a diameter of less than 300 mm. In order to save the cost of the conformal phased array antenna, the number of cells and their position are an important variable for our optimization. Its gain and gain flatness are very important optimization goals. First, to develop an antenna element pattern, there are now two variables: the position coordinates (x, y, z) of each unit and the total number N of antenna elements. Each cell of the array cannot intersect, and its radius must be less than R in the radius defined in the hemisphere, that is, the coordinates of each cell are controlled within a certain range. In addition, the antenna gain optimization must be greater than 13 dBi and the gain flatness is less than 1 dB over the entire upper half of the airspace. We use genetic algorithms to optimize the distribution of the elements and the number of elements. If the proposed unit pattern cannot optimize the structure that satisfies the requirements, adjust the pattern of the unit antenna and select a new pattern to re-optimize. After the optimization goal reaches our requirements We design the required unit pattern according to the proposed pattern, arrange the designed antenna unit according to the optimized topology, and finally use the full-wave analysis software for overall analysis and optimization.
[0033] 所述的第一层骨架 1的顶部为圆顶结构, 其圆顶机构的穹拱式的造型具有四周 传力的特点, 这样能在满足相同受力的基础上将支架的壁厚尽量减薄, 从而降 低天线安装骨架的重量, 在第一层骨架 1的顶部幵设有一定位装置安装孔 5, 所 述的定位装置安装孔 5内安装有定位装置 10, 且定位装置 10通过设置在定位安装 孔 5上的四个定位装置定位柱 9定位。 [0033] The top of the first layer skeleton 1 is a dome structure, and the dome-shaped shape of the dome mechanism has the characteristics of four-sided force transmission, so that the wall thickness of the bracket can be satisfied on the basis of satisfying the same force. As far as possible, the weight of the antenna mounting frame is reduced, and a positioning device mounting hole 5 is disposed at the top of the first layer frame 1. The positioning device 10 is mounted in the positioning device mounting hole 5, and the positioning device 10 is set. The four positioning device positioning posts 9 on the positioning mounting holes 5 are positioned.
[0034] 在本实施例中, 所述的第一层骨架 1和第二层骨架 2的相接环上以及第二层骨架 2和第三层骨架 3的相接环上均幵设有减重孔 8, 即第一层骨架 1、 第二层骨架 2和 第三层骨架 3采用缕空设计, 这样不仅可以降低天线安装骨架的重量, 而且还可 保证天线安装骨架的受力均匀性, 从而提高了天线安装骨架的稳定性。  [0034] In the embodiment, the connecting rings of the first layer skeleton 1 and the second layer skeleton 2 and the connecting rings of the second layer skeleton 2 and the third layer skeleton 3 are each provided with a reduction The heavy hole 8, that is, the first layer skeleton 1, the second layer skeleton 2, and the third layer skeleton 3 adopt a hollow design, which can not only reduce the weight of the antenna mounting skeleton, but also ensure the uniformity of the force of the antenna mounting skeleton. Thereby improving the stability of the antenna mounting skeleton.
[0035] 所述的第三层骨架 3底部的外侧壁上设置有多个均匀分布的天线骨架安装座 7, 天线骨架安装座 7上幵设有螺纹通孔, 所述的底板 16上幵设有与天线骨架安装座 7对应的天线骨架安装孔 17, 第三次骨架 3通过安装在天线骨架安装座 7和天线骨 架安装孔 17内的连接螺钉紧固连接。  [0035] The outer side wall of the bottom of the third layer frame 3 is provided with a plurality of evenly distributed antenna frame mounts 7, and the antenna frame mounts 7 are provided with threaded through holes, and the bottom plate 16 is disposed on the bottom plate 16 There is an antenna frame mounting hole 17 corresponding to the antenna frame mount 7, and the third frame 3 is fastened by a connecting screw mounted in the antenna frame mount 7 and the antenna frame mounting hole 17.
[0036] 在本实施例中, 所述的底板 16的底部还设置有接头座 23和防水透气阀 22, 防水 透气阀 22位于接头座 23的一侧, 防水透气阀 22内设置有防水透气膜, 该防水透 气膜为高分子材料制成, 防水透气阀 22解决了共形球面天线阵的呼吸效应。  [0036] In the embodiment, the bottom of the bottom plate 16 is further provided with a joint seat 23 and a waterproof gas permeable valve 22, the waterproof gas permeable valve 22 is located at one side of the joint seat 23, and the waterproof gas permeable valve 22 is provided with a waterproof gas permeable membrane. The waterproof and breathable membrane is made of a polymer material, and the waterproof breathable valve 22 solves the respiratory effect of the conformal spherical antenna array.
[0037] 在本实施例中, 所述的支撑装置为支撑柱 20, 支撑柱 20的上下两端均设置有连 接法兰, 通过连接法兰可实现支撑柱 20与底板 16之间的连接, 同吋也可满足底 板 16的支撑, 安装吋, 将支撑柱 20的底部安装在对应的位置上即可实现共形球 面天线阵的稳固安装。  [0037] In the embodiment, the support device is a support column 20, and the upper and lower ends of the support column 20 are provided with a connection flange, and the connection between the support column 20 and the bottom plate 16 can be realized through the connection flange. The same can also satisfy the support of the bottom plate 16, and the mounting 吋, the bottom of the support column 20 can be installed at the corresponding position to achieve stable installation of the conformal spherical antenna array.
[0038] 实施例二:  [0038] Embodiment 2:
[0039] 本实施例与实施例一结构基本相同, 唯一不同点在于支撑装置结构不同, 如图 2、 图 8和图 9所示, 所述的支撑装置为 L形安装座 21, 所述的 L形安装座 21为多个 , 且均匀分布在底板 16的下表面上, 进一步的, 所述的 L形安装座 21上幵设有与 底板 16连接的台阶孔以及用以固定 L形安装座 21固定通孔, 安装吋, 将 L形安装 座 21固定, 就可实现共形球面天线阵的稳固安装。 [0039] This embodiment is basically the same as the structure of the first embodiment. The only difference is that the structure of the supporting device is different. As shown in FIG. 2, FIG. 8 and FIG. 9, the supporting device is an L-shaped mounting seat 21, The L-shaped mounts 21 are pluralityed and evenly distributed on the lower surface of the bottom plate 16. Further, the L-shaped mounts 21 are provided with stepped holes connected to the bottom plate 16 and for fixing the L-shaped mounts. 21 fixed through hole, mounting 吋, L-shaped installation With the seat 21 fixed, a stable installation of the conformal spherical antenna array can be achieved.
在上述实施例中, 可以根据不同的使用环境配合安装不同的安装附件实现车载 、 舰载以及地面工事的安装使用。  In the above embodiments, different installation accessories can be installed according to different usage environments to realize the installation and use of the vehicle, the shipboard, and the groundwork.

Claims

权利要求书 Claim
[权利要求 1] 一种共形球面天线阵, 其特征在于: 它包括天线罩 (13) 、 天线阵 (  [Claim 1] A conformal spherical antenna array, comprising: a radome (13), an antenna array (
14) 、 屏蔽罩 (15) 、 底板 (16) 和支撑装置, 所述的天线阵 (14) 安装在底板 (16) 上, 且屏蔽罩 (15) 位于天线阵 (14) 与底板 (16 ) 之间, 所述的天线罩 (13) 盖住天线阵 (14) , 且底板 (16) 上幵 设有一环形槽 (18) , 所述的天线罩 (13) 的下边缘插入环形槽 (18 ) 内, 且通过锁紧定位机构定位, 所述的支撑装置安装在底板 (16) 的底部, 所述的天线阵 (14) 包括第一层骨架 (1) 、 第二层骨架 (2 ) 、 第三层骨架 (3) 和天线 (11) , 所述的第一层骨架 (1) 、 第二 层骨架 (2) 、 第三层骨架 (3) 均在同一椭球面内, 且每一层骨架的 倾角均不相同, 所述的第一层骨架 (1) 、 第二层骨架 (2) 与椭球面 相切, 第三层骨架 (3) 与第二层骨架 (1) 球面切线具有切线夹角 a , 所述的第一层骨架 (1) 、 第二层骨架 (2) 、 第三层骨架 (3) 上 均幵设有多个天线安装孔 (4) , 所述的天线安装孔 (4) 周围的骨架 上设置有多个天线支撑柱 (6) , 所述的天线 (11) 上设置有与天线 支撑柱 (6) 对应的安装孔 (12) , 所述的天线 (11) 通过螺钉安装 在天线支撑柱 (6) 上。  14), a shield (15), a bottom plate (16) and a supporting device, the antenna array (14) is mounted on the bottom plate (16), and the shielding cover (15) is located at the antenna array (14) and the bottom plate (16) Between the radome (13) covers the antenna array (14), and the bottom plate (16) is provided with an annular groove (18), and the lower edge of the radome (13) is inserted into the annular groove (18). Inside, and positioned by the locking positioning mechanism, the supporting device is installed at the bottom of the bottom plate (16), and the antenna array (14) includes a first layer skeleton (1) and a second layer skeleton (2), The third layer skeleton (3) and the antenna (11), the first layer skeleton (1), the second layer skeleton (2), and the third layer skeleton (3) are all in the same ellipsoidal plane, and each layer The inclination angles of the skeleton are different, the first layer skeleton (1) and the second layer skeleton (2) are tangent to the ellipsoid surface, and the third layer skeleton (3) and the second layer skeleton (1) have a tangent to the spherical tangent. The angle a, the first layer skeleton (1), the second layer skeleton (2), and the third layer skeleton (3) are uniformly distributed a plurality of antenna mounting holes (4) are disposed, and a plurality of antenna supporting columns (6) are disposed on the skeleton around the antenna mounting holes (4), and the antenna (11) is provided with an antenna supporting column ( 6) Corresponding mounting hole (12), the antenna (11) is mounted on the antenna support column (6) by screws.
[权利要求 2] 根据权利要求 1所述的一种共形球面天线阵, 其特征在于: 所述的第 一层骨架 (1) 上均匀安装有四个天线 (11) , 所述的第二层骨架 (2 ) 上均匀安装有八个天线, 所述的第三层骨架 (3) 上均匀安装有十 一个天线 ( 11) 。  [Claim 2] A conformal spherical antenna array according to claim 1, wherein: the first layer skeleton (1) is uniformly mounted with four antennas (11), and the second Eight antennas are evenly mounted on the layer skeleton (2), and eleven antennas (11) are evenly mounted on the third layer skeleton (3).
[权利要求 3] 根据权利要求 2所述的一种共形球面天线阵, 其特征在于: 所述的第 一层骨架 (1) 的顶部为圆顶结构, 在其上幵设有一定位装置安装孔 (5) , 所述的定位装置安装孔 (5) 内安装有定位装置 (10) , 且定 位装置 (10) 通过设置在定位安装孔 (5) 上的四个定位装置定位柱 (9) 定位。  [Claim 3] A conformal spherical antenna array according to claim 2, wherein: the top of the first layer skeleton (1) has a dome structure, and a positioning device is mounted thereon. a positioning device (10) is mounted in the positioning device mounting hole (5), and the positioning device (10) is positioned by the four positioning devices (9) disposed on the positioning mounting hole (5) Positioning.
[权利要求 4] 根据权利要求 3所述的一种共形球面天线阵, 其特征在于: 所述的第 一层骨架 (1) 和第二层骨架 (2) 的相接环上以及第二层骨架 (2) 和第三层骨架 (3) 的相接环上均幵设有减重孔 (8) 。 [Claim 4] A conformal spherical antenna array according to claim 3, characterized in that: the first layer skeleton (1) and the second layer skeleton (2) are connected to each other on the ring and the second Layer skeleton (2) A lightening hole (8) is provided on the connecting ring of the third layer skeleton (3).
根据权利要求 4所述的一种共形球面天线阵, 其特征在于: 所述的第 三层骨架 (3) 底部的外侧壁上设置有多个均匀分布的天线骨架安装 座 (7) , 天线骨架安装座 (7) 上幵设有螺纹通孔, 所述的底板 (16 ) 上幵设有与天线骨架安装座 (7) 对应的天线骨架安装孔 (17) , 第三次骨架 (3) 通过安装在天线骨架安装座 (7) 和天线骨架安装孔A conformal spherical antenna array according to claim 4, characterized in that: the outer side wall of the bottom of the third layer skeleton (3) is provided with a plurality of evenly distributed antenna frame mounts (7), the antenna The frame mounting seat (7) is provided with a threaded through hole, and the bottom plate (16) is provided with an antenna frame mounting hole (17) corresponding to the antenna frame mounting seat (7), and a third skeleton (3) By mounting on the antenna frame mount (7) and antenna frame mounting holes
(17) 内的连接螺钉紧固连接。 (17) The connection screws inside are fastened.
根据权利要求 1或 5所述的一种共形球面天线阵, 其特征在于: 所述的 锁紧定位机构包括锁紧螺钉 (19) , 所述的环形槽 (18) 的侧壁上幵 设有多个螺纹通孔, 所述的屏蔽罩 (13) 的下边缘幵设有与螺纹通孔 的定位孔, 所述的天线罩 (13) 和底板 (16) 之间通过锁紧在螺纹通 孔和定位孔内的锁紧螺钉锁紧定位。 A conformal spherical antenna array according to claim 1 or 5, wherein: said locking positioning mechanism comprises a locking screw (19), and said side wall of said annular groove (18) is provided There are a plurality of threaded through holes, and the lower edge of the shielding cover (13) is provided with a positioning hole with a threaded through hole, and the radome (13) and the bottom plate (16) are locked in the threaded passage. The locking screw in the hole and the positioning hole is locked and positioned.
根据权利要求 6所述的一种共形球面天线阵, 其特征在于: 所述的支 撑装置为支撑柱 (20) , 支撑柱 (20) 的上下两端均设置有连接法兰 根据权利要求 1所述的一种共形球面天线阵, 其特征在于: 所述的支 撑装置为 L形安装座 (21) , L形安装座 (21) 上幵设有与底板 (16 ) 连接的台阶孔以及用以固定 L形安装座 (21) 固定通孔。 The conformal spherical antenna array according to claim 6, wherein: the support device is a support column (20), and the upper and lower ends of the support column (20) are provided with a connecting flange according to claim 1. The conformal spherical antenna array is characterized in that: the supporting device is an L-shaped mounting seat (21), and the L-shaped mounting seat (21) has a stepped hole connected to the bottom plate (16) and It is used to fix the L-shaped mount (21) to fix the through hole.
根据权利要求 1所述的一种共形球面天线阵, 其特征在于: 所述的底 板 (16) 的底部还设置有接头座 (23) 和防水透气阀 (22) , 防水透 A conformal spherical antenna array according to claim 1, wherein: the bottom plate (16) is further provided with a joint seat (23) and a waterproof breathable valve (22) at the bottom of the bottom plate (16).
PCT/CN2016/096414 2016-07-12 2016-08-23 Conformal spherical antenna array WO2018010260A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201610545262.5A CN106025578B (en) 2016-07-12 2016-07-12 A kind of conformal spherical antenna battle array
CN201610545262.5 2016-07-12

Publications (1)

Publication Number Publication Date
WO2018010260A1 true WO2018010260A1 (en) 2018-01-18

Family

ID=57109440

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2016/096414 WO2018010260A1 (en) 2016-07-12 2016-08-23 Conformal spherical antenna array

Country Status (2)

Country Link
CN (1) CN106025578B (en)
WO (1) WO2018010260A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111817027A (en) * 2020-06-29 2020-10-23 西南电子技术研究所(中国电子科技集团公司第十研究所) Method for designing vehicle-carrying platform special-shaped curved surface conformal array antenna

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106025541B (en) * 2016-07-12 2018-12-04 成都泰格微电子研究所有限责任公司 A kind of good conformal spherical antenna battle array of shield effectiveness
CN105958216B (en) * 2016-07-12 2019-01-22 成都泰格微电子研究所有限责任公司 A kind of conformal antenna array
CN106025490B (en) * 2016-07-12 2019-01-22 成都泰格微电子研究所有限责任公司 A kind of conformal antenna mounting framework
CN107196051B (en) * 2017-07-11 2023-05-23 中国电子科技集团公司第十四研究所 Intelligent skin antenna structure based on three-dimensional printing
CN108376823B (en) * 2018-03-26 2023-10-13 广东通宇通讯股份有限公司 Waterproof and breathable antenna device supporting multi-polarization installation of antenna
CN112490690B (en) * 2019-09-11 2022-12-20 英业达科技有限公司 Antenna structure and operation method thereof
CN111564690A (en) * 2020-02-27 2020-08-21 湖南迈克森伟电子科技有限公司 Antenna array element assembly and ground satellite receiving terminal based on same
CN113904096B (en) * 2021-12-09 2022-02-22 河北晶禾电子技术股份有限公司 Miniaturized anti-interference antenna array

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4792808A (en) * 1982-12-14 1988-12-20 Harris Corp. Ellipsoid distribution of antenna array elements for obtaining hemispheric coverage
US5905466A (en) * 1991-11-08 1999-05-18 Teledesic Llc Terrestrial antennas for satellite communication system
US20140292612A1 (en) * 2010-12-07 2014-10-02 Thales Protective ballistic radome for a satellite antenna
CN105612657A (en) * 2013-07-18 2016-05-25 艾伯特复合材料公司 Advanced composite radome and method of manufacturing same

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN205828676U (en) * 2016-07-12 2016-12-21 成都泰格微电子研究所有限责任公司 A kind of conformal spherical antenna battle array

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4792808A (en) * 1982-12-14 1988-12-20 Harris Corp. Ellipsoid distribution of antenna array elements for obtaining hemispheric coverage
US5905466A (en) * 1991-11-08 1999-05-18 Teledesic Llc Terrestrial antennas for satellite communication system
US20140292612A1 (en) * 2010-12-07 2014-10-02 Thales Protective ballistic radome for a satellite antenna
CN105612657A (en) * 2013-07-18 2016-05-25 艾伯特复合材料公司 Advanced composite radome and method of manufacturing same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111817027A (en) * 2020-06-29 2020-10-23 西南电子技术研究所(中国电子科技集团公司第十研究所) Method for designing vehicle-carrying platform special-shaped curved surface conformal array antenna
CN111817027B (en) * 2020-06-29 2022-04-01 西南电子技术研究所(中国电子科技集团公司第十研究所) Method for designing vehicle-carrying platform special-shaped curved surface conformal array antenna

Also Published As

Publication number Publication date
CN106025578A (en) 2016-10-12
CN106025578B (en) 2019-01-18

Similar Documents

Publication Publication Date Title
WO2018010260A1 (en) Conformal spherical antenna array
WO2018010259A1 (en) Conformal antenna array
US11967775B2 (en) Lens antenna system
US20230231324A1 (en) Multi-band lens antenna system
CN107959121B (en) Based on artificial dielectric cylindrical lens sector multibeam antenna
US6987489B2 (en) Electronically scanning direction finding antenna system
WO2018010258A1 (en) Conformal antenna mounting frame
WO2018010257A1 (en) Conformal spherical antenna array having good shielding results
CN205828676U (en) A kind of conformal spherical antenna battle array
CN103022728B (en) Method for designing partial-feed paraboloid multi-beam antenna feed array
CN111585042B (en) Multi-beam dielectric lens antenna and manufacturing method thereof
WO2014071866A1 (en) Reflective array surface and reflective array antenna
CN209282410U (en) A kind of high calibre efficiency multipolarization plane reflection type orbital angular momentum antenna
US5012256A (en) Array antenna
CN210040509U (en) Luneberg lens array and satellite antenna
WO2022152139A1 (en) Multi-beam lens antenna and active lens antenna system
CN105552572A (en) Dual-polarized conical medium feed source symmetrical medium filled cylindrical lens antenna
CN105633584B (en) Logarithm period feed battle array based on satellite multi-beam antenna stereoeffect layout
CN105428821A (en) Dual polarization circular cone medium feed source asymmetrical medium packing column lens antenna
CN205828664U (en) The conformal spherical antenna battle array that a kind of shield effectiveness is good
CN111817027B (en) Method for designing vehicle-carrying platform special-shaped curved surface conformal array antenna
Cheng et al. Satellite ground stations with electronic beam steering
US20230036249A1 (en) Multibeam antenna
CN107634339B (en) High-directivity umbrella-shaped convex surface common reflector antenna based on super surface
Pirinoli et al. Multifocal approach for reflectarray antenna for DTH applications

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 16908585

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 16908585

Country of ref document: EP

Kind code of ref document: A1