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CN112164884B - Satellite-borne helical array antenna feed probe with multiple degrees of freedom and consistent amplitude and phase - Google Patents

Satellite-borne helical array antenna feed probe with multiple degrees of freedom and consistent amplitude and phase Download PDF

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CN112164884B
CN112164884B CN202010852066.9A CN202010852066A CN112164884B CN 112164884 B CN112164884 B CN 112164884B CN 202010852066 A CN202010852066 A CN 202010852066A CN 112164884 B CN112164884 B CN 112164884B
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feed
feeder
rod
helix
column
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CN112164884A (en
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艾永强
牛宝华
张振杰
王超
杨文丽
郑伟
穆楠
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Xian Institute of Space Radio Technology
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    • 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
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/28Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/288Satellite antennas
    • 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
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems

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  • Engineering & Computer Science (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Details Of Aerials (AREA)
  • Waveguide Aerials (AREA)

Abstract

The invention relates to a multi-degree-of-freedom amplitude-phase consistent spaceborne spiral array antenna feed probe, which comprises a feed rod and a feed column, wherein the feed rod is connected with the feed column; the upper end surface of the feed column is provided with a U-shaped groove, and the center of the feed column is provided with a V-shaped inner cavity; the feed pole is fixedly arranged in a conductor in the feed network, the feed column is embedded into the U-shaped groove by using the V-shaped inner cavity of the cylindrical positioning device at the top end of the feed pole, the end part of the spiral line is tangent to the excircle of the feed column, and the V-shaped groove is filled with solder in the welding process.

Description

一种多自由度幅相一致的星载螺旋阵列天线馈电探针A Spaceborne Helical Array Antenna Feeding Probe with Multiple Degrees of Freedom and Amplitude Consistent

技术领域technical field

本发明涉及一种多自由度幅相一致的星载螺旋阵列天线馈电探针,属于天线结构技术领域。The invention relates to a space-borne spiral array antenna feeding probe with consistent multi-degree-of-freedom amplitudes, and belongs to the technical field of antenna structures.

背景技术Background technique

螺旋阵列天线在波束赋型设计中对各螺旋单元幅相误差较为敏感,采用传统馈线与馈电探针搭接,螺旋线与馈电探针位置随机性较大,焊点形状不一致,幅相分布难以保证,需要进行近场幅相通道测试,需额外增加补偿相位环节,调试和测试周期很长,效率较低。The helical array antenna is more sensitive to the amplitude and phase error of each helical unit in the beamforming design. If the traditional feeder is used to overlap the feeder probe, the positions of the helix and the feeder probe are random, and the shapes of the solder joints are inconsistent. The distribution is difficult to guarantee. Near-field amplitude and phase channel testing is required, and an additional compensation phase link is required. The debugging and testing cycle is very long and the efficiency is low.

发明内容Contents of the invention

本发明解决的技术问题是:克服现有技术的不足,提供一种多自由度幅相一致的星载螺旋阵列天线馈电探针,提高产品的一致性、可靠性和可操作性。The technical problem solved by the present invention is to overcome the deficiencies of the prior art, provide a space-borne spiral array antenna feeding probe with consistent multi-degree-of-freedom amplitudes, and improve product consistency, reliability and operability.

本发明解决技术的方案是:一种多自由度幅相一致的星载螺旋阵列天线馈电探针,包括馈电杆和馈电柱;所述的馈电柱上端面设置U型槽,槽宽与嵌入螺旋线部分弦高相同,槽深与螺旋线直径相同,中心设置夹角为15゜±1゜V型内腔,底部设置圆柱凹槽与馈电杆凸台定位和调整U型槽方向;所述馈电杆装入馈电网络内导体固定,馈电柱使用圆柱凹槽与馈电杆顶端圆柱定位装入所述的V型内腔,调整U型槽方向与螺旋线方向一致,将螺旋线嵌入U型槽内,使螺旋线端部与馈电柱外圆相切,焊接过程中将焊料填充至馈电柱V型内腔内直至充满V型内腔。The technical solution of the present invention is: a space-borne spiral array antenna feeding probe with the same multi-degree-of-freedom amplitude, including a feeding rod and a feeding post; the upper end of the feeding post is provided with a U-shaped groove, and The width is the same as the chord height of the embedded helix, the groove depth is the same as the diameter of the helix, the center is set at an angle of 15°±1°V-shaped inner cavity, and the bottom is set with a cylindrical groove and a U-shaped groove for the positioning and adjustment of the feed rod boss Direction; the feeder rod is fixed in the conductor of the feeder network, and the feeder rod is positioned in the V-shaped inner cavity using a cylindrical groove and the top cylinder of the feeder rod, and the direction of the U-shaped groove is adjusted to be consistent with the direction of the helix , insert the helix into the U-shaped groove, so that the end of the helix is tangent to the outer circle of the feed post, and fill the solder into the V-shaped cavity of the feed post during the welding process until it fills the V-shaped cavity.

优选的,焊接馈电杆、馈电柱和螺旋线时焊点位于馈电柱内部V型槽内,焊点形状规则,多个焊点状态一致。Preferably, when welding the feed rod, the feed column and the helix, the welding spot is located in the V-shaped groove inside the feed column, the shape of the welding spot is regular, and the states of the plurality of welding spots are consistent.

优选的,所述的馈电杆顶端为螺纹设计。Preferably, the top end of the feed rod is threaded.

优选的,所述的馈电柱下端面设置观察孔兼排气孔,便于观察焊接状态和排气。Preferably, the lower end surface of the feeder column is provided with an observation hole and an exhaust hole, which is convenient for observing the welding state and exhausting.

优选的,所述的观察孔兼排气孔直径Φ0.6。Preferably, the diameter of the observation hole and exhaust hole is Φ0.6.

一种所述探针与星载侧馈螺旋天线的连接方法,步骤如下:A method for connecting the probe to the space-borne side-fed helical antenna, the steps are as follows:

(1)馈电网络和反射杯装入反射板后,将馈电杆通过螺纹连接装入馈电网络内导体固定,使用馈电杆上端平口施加固定力矩;(1) After the feed network and the reflector cup are loaded into the reflector, the feed rod is screwed into the inner conductor of the feed network and fixed, and the fixed torque is applied by using the flat opening on the upper end of the feed rod;

(2)将螺旋天线装入上述部件固定,馈电柱使用馈电杆顶端圆柱定位装入,调整馈电柱U型槽方向与螺旋线方向一致,将螺旋线嵌入U型槽,螺旋线端头与馈电柱相切;(2) Install the helical antenna into the above parts and fix it. The feeder column is positioned by the cylinder at the top of the feeder rod. Adjust the direction of the U-shaped groove of the feeder column to be consistent with the direction of the helix. The head is tangent to the feed column;

(3)焊接填充馈电柱V型槽,在焊接过程中通过观察孔观察焊料情况判断焊接状态,完成焊接。(3) Weld and fill the V-shaped groove of the feeder column. During the welding process, observe the solder through the observation hole to judge the welding state and complete the welding.

一种提升螺旋阵列天线工作效率的方法,按照上述连接方式将所述的探针与星载侧馈螺旋天线进行连接,以提高螺旋阵列天线的幅度方向图的对称性,减小螺旋阵列天线的相位中心波动。A method for improving the working efficiency of a helical array antenna. According to the above connection method, the probe is connected with the space-borne side-fed helical antenna, so as to improve the symmetry of the amplitude pattern of the helical array antenna and reduce the symmetry of the helical array antenna. Phase center fluctuations.

本发明与现有技术相比的有益效果是:The beneficial effect of the present invention compared with prior art is:

本发明采用馈电杆和馈电柱分体结构和螺旋线镶嵌焊接设计,焊接部位一致性好,焊接强度高,焊接方便,提高了焊接部位一致性、可靠性和可操作性,同时大幅提高了螺旋阵列天线的幅度方向图的对称性,减小了螺旋阵列天线的相位中心波动,提升了螺旋阵列天线的工作效率。The invention adopts the separate structure of the feed rod and the feed post and the design of the helical inlaid welding, which has good consistency of the welding parts, high welding strength, convenient welding, improves the consistency, reliability and operability of the welding parts, and greatly improves the The symmetry of the amplitude pattern of the helical array antenna is improved, the phase center fluctuation of the helical array antenna is reduced, and the working efficiency of the helical array antenna is improved.

该发明已应用于我国多个星载阵面天线,已经过通过力学、热冲击、热真空鉴定级考核和在轨使用,后续多个型号及预先研究课题的研制中参考了该发明中星载侧馈螺旋天线与馈电探针连接方式,本发明具有广泛的应用领域具备较好的市场竞争力。This invention has been applied to many space-borne array antennas in my country, and has passed the mechanical, thermal shock, and thermal vacuum appraisal level assessment and in-orbit use. The connection mode between the side-fed helical antenna and the feeding probe has wide application fields and good market competitiveness.

附图说明Description of drawings

图1侧馈螺旋天线与馈电探针连接示意图;Fig. 1 Schematic diagram of connection between side-fed helical antenna and feeding probe;

图2侧馈螺旋天线与馈电探针焊接前示意图;Fig. 2 Schematic diagram of side-fed helical antenna and feeding probe before welding;

图3侧馈螺旋天线与馈电探针焊接后示意图。Fig. 3 The schematic diagram of side-fed helical antenna and feeding probe after welding.

具体实施方式detailed description

下面结合实施例对本发明作进一步阐述。The present invention will be further elaborated below in conjunction with embodiment.

如图1所示,一种星载螺旋单元馈电探针结构与星载侧馈螺旋天线的连接方式,设计部件侧馈螺旋天线1,馈电柱2,馈电杆3,反射杯4,反射板5,馈电网络6和介质支撑7。本发明异于传统的螺旋线与馈电探针搭接焊接方式和压接方式,采用圆柱螺旋线嵌入U型槽馈电探针焊接方式,如图1所示。该连接方式馈电探针与馈电网络内导体间采用螺纹连接,由于馈电探针在螺纹加工中起始角度的随机性,导致馈电探针以固定力矩装入馈电网络后U型槽方向与螺旋线方向不一致的问题。为了避免上述问题将馈电探针分为馈电杆和馈电柱,馈电柱上端设有U型槽,馈电柱可以绕馈电杆轴线转任意角度安装,同时实现了螺旋线、馈电柱和馈电杆相对位置固定。馈电柱内腔采用V型设计,馈电杆顶端为螺纹设计,增大了焊接面积,增加焊接强度,焊接部位形状规则。焊接部位位于馈电柱V型内腔内,焊接部位形状规则,改善多个螺旋天线组阵时焊接部位的差异导致阻抗不一致的问题,且焊接部位可靠性明显高于传统连接方式。该侧馈螺旋天线与馈电探针连接方式具有结构简单,焊接方便,焊接状态一致性好,可靠性高的特点。馈电柱下端增加观察孔兼排气口,便于观察焊接状态和排气。As shown in Figure 1, a connection method between a space-borne helical unit feeding probe structure and a space-borne side-fed helical antenna, design components side-fed helical antenna 1, feeding column 2, feeding rod 3, reflective cup 4, Reflector 5 , feed network 6 and dielectric support 7 . The present invention is different from the traditional overlapping welding method and crimping method of the spiral wire and the feeding probe, and adopts the welding method of the cylindrical helical wire embedded in the U-shaped groove feeding probe, as shown in FIG. 1 . In this connection method, the feeding probe and the inner conductor of the feeding network are connected by threads. Due to the randomness of the starting angle of the feeding probe in the thread processing, the feeding probe is installed into the feeding network with a fixed torque and U-shaped. The problem that the groove direction does not coincide with the direction of the helix. In order to avoid the above problems, the feeding probe is divided into a feeding rod and a feeding column. There is a U-shaped groove on the upper end of the feeding column. The relative positions of the electric post and the feeder pole are fixed. The inner cavity of the feed column adopts a V-shaped design, and the top of the feed rod is designed with threads, which increases the welding area, increases the welding strength, and the shape of the welding part is regular. The welding part is located in the V-shaped inner cavity of the feeding column, and the shape of the welding part is regular, which improves the problem of inconsistent impedance caused by the difference of the welding part when multiple helical antennas are arrayed, and the reliability of the welding part is significantly higher than that of the traditional connection method. The connection mode of the side-fed helical antenna and the feeding probe has the characteristics of simple structure, convenient welding, good consistency of welding state and high reliability. An observation hole and an exhaust port are added at the lower end of the feed column to facilitate observation of welding status and exhaust.

一种星载侧馈螺旋天线与馈电探针连接方法如下:A connection method between a space-borne side-fed helical antenna and a feeding probe is as follows:

(1)馈电网络和反射杯装入反射板后,将馈电杆通过螺纹连接装入馈电网络内导体固定,使用馈电杆上端平口施加固定力矩;(1) After the feed network and the reflector cup are loaded into the reflector, the feed rod is screwed into the inner conductor of the feed network and fixed, and the fixed torque is applied by using the flat opening on the upper end of the feed rod;

(2)将螺旋天线装入上述部件固定,馈电柱使用馈电杆顶端圆柱定位装入,调整馈电柱U型槽方向与螺旋线方向一致,将螺旋线嵌入U型槽,螺旋线端头与馈电柱相切,如图2所示(2) Install the helical antenna into the above parts and fix it. The feeder column is positioned by the cylinder at the top of the feeder rod. Adjust the direction of the U-shaped groove of the feeder column to be consistent with the direction of the helix. The head is tangent to the feed column, as shown in Figure 2

(3)焊接填充馈电柱V型槽,在焊接过程中通过观察孔观察焊料情况判断焊接状态,焊接完毕后焊接部位如图3所示。(3) Weld and fill the V-shaped groove of the feeder column. During the welding process, observe the solder through the observation hole to judge the welding state. After the welding is completed, the welding position is shown in Figure 3.

按照上述方式将探针与螺旋阵列天线进行连接,以提高螺旋阵列天线的幅度方向图的对称性,减小螺旋阵列天线的相位中心波动,提高天线的工作效率。The probe is connected to the helical array antenna in the above manner, so as to improve the symmetry of the amplitude pattern of the helical array antenna, reduce the phase center fluctuation of the helical array antenna, and improve the working efficiency of the antenna.

本发明未详细说明部分属于本领域技术人员的公知常识。Parts not described in detail in the present invention belong to the common knowledge of those skilled in the art.

Claims (7)

1.一种多自由度幅相一致的星载螺旋阵列天线馈电探针,其特征在于:包括馈电杆和馈电柱;所述的馈电柱上端面设置U型槽,槽宽与嵌入螺旋线部分弦高相同,槽深与螺旋线直径相同,中心设置夹角为15゜±1゜V型内腔,底部设置圆柱凹槽,用于与馈电杆凸台定位和调整U型槽方向;所述馈电杆装入馈电网络内导体固定,馈电柱使用圆柱凹槽与馈电杆顶端圆柱定位装入所述的V型内腔,调整U型槽方向与螺旋线方向一致,将螺旋线嵌入U型槽内,使螺旋线端部与馈电柱外圆相切,焊接过程中将焊料填充至馈电柱V型内腔内直至充满V型内腔。1. A space-borne spiral array antenna feed probe with multiple degrees of freedom amplitudes consistent, is characterized in that: it includes a feed rod and a feed post; the upper end of the feed post is provided with a U-shaped groove, and the groove width is the same as The chord height of the part embedded in the helix is the same, the groove depth is the same as the diameter of the helix, and the center is set at an angle of 15゜±1゜V-shaped inner cavity, and a cylindrical groove is set at the bottom, which is used for positioning and adjusting the U-shape with the boss of the feeder rod Groove direction; the feeder rod is installed into the conductor of the feeder network to fix it, and the feeder rod is positioned into the V-shaped inner cavity using a cylindrical groove and a cylinder at the top of the feeder rod, and the direction of the U-shaped groove and the direction of the helix are adjusted. Consistently, insert the helix into the U-shaped groove so that the end of the helix is tangent to the outer circle of the feeder column. During the welding process, fill the solder into the V-shaped cavity of the feeder column until it is full of the V-shaped cavity. 2.根据权利要求1所述的探针,其特征在于:焊接馈电杆、馈电柱和螺旋线时焊点位于馈电柱内部V型槽内,焊点形状规则,多个焊点状态一致。2. The probe according to claim 1, characterized in that: when welding the feed rod, feed post and helix, the solder joints are located in the V-shaped groove inside the feed post, the solder joints have regular shapes, and the states of multiple solder joints unanimous. 3.根据权利要求1所述的探针,其特征在于:所述的馈电杆顶端为螺纹设计。3. The probe according to claim 1, characterized in that: the top end of the feed rod is threaded. 4.根据权利要求1所述的探针,其特征在于:所述的馈电柱下端面设置观察孔兼排气孔,便于观察焊接状态和排气。4. The probe according to claim 1, characterized in that: the lower end surface of the feed post is provided with an observation hole and an exhaust hole, which is convenient for observing the welding state and exhausting. 5.根据权利要求4所述的探针,其特征在于:所述的观察孔兼排气孔直径Φ0.6。5. The probe according to claim 4, characterized in that the diameter of the observation hole and exhaust hole is Φ0.6. 6.一种权利要求1所述探针与星载侧馈螺旋天线的连接方法,其特征在于步骤如下:6. a method for connecting probes and space-borne side-fed helical antennas according to claim 1, characterized in that the steps are as follows: (1)馈电网络和反射杯装入反射板后,将馈电杆通过螺纹连接装入馈电网络内导体固定,使用馈电杆上端平口施加固定力矩;(1) After the feed network and the reflector cup are loaded into the reflector, the feed rod is screwed into the inner conductor of the feed network to fix it, and the upper end of the feed rod is used to apply a fixed torque; (2)将螺旋天线装入上述反射杯固定,馈电柱使用馈电杆顶端圆柱定位装入,调整馈电柱U型槽方向与螺旋线方向一致,将螺旋线嵌入U型槽,螺旋线端头与馈电柱相切;(2) Put the helical antenna into the above-mentioned reflective cup and fix it. The feeder column is positioned by the cylinder at the top of the feeder rod. Adjust the direction of the U-shaped groove of the feeder column to be consistent with the direction of the helix. The end is tangent to the feeder column; (3)焊接填充馈电柱V型槽,在焊接过程中通过观察孔观察焊料情况判断焊接状态,完成焊接。(3) Weld and fill the V-shaped groove of the feeder column. During the welding process, observe the solder through the observation hole to judge the welding state and complete the welding. 7.一种提升螺旋阵列天线工作效率的方法,其特征在于按照权利要求6的连接方式将权利要求1所述的探针与星载侧馈螺旋天线进行连接,以提高螺旋阵列天线的幅度方向图的对称性,减小螺旋阵列天线的相位中心波动。7. A method for improving the working efficiency of the spiral array antenna is characterized in that the probe according to claim 1 is connected with the space-borne side-fed spiral antenna according to the connection method of claim 6, so as to improve the amplitude direction of the spiral array antenna The symmetry of the graph reduces the phase center fluctuation of the helical array antenna.
CN202010852066.9A 2020-08-21 2020-08-21 Satellite-borne helical array antenna feed probe with multiple degrees of freedom and consistent amplitude and phase Active CN112164884B (en)

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