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CN109994822B - High-power microwave space beam swept planar array antenna - Google Patents

High-power microwave space beam swept planar array antenna Download PDF

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CN109994822B
CN109994822B CN201910303976.9A CN201910303976A CN109994822B CN 109994822 B CN109994822 B CN 109994822B CN 201910303976 A CN201910303976 A CN 201910303976A CN 109994822 B CN109994822 B CN 109994822B
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waveguide
rectangular waveguide
circular
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CN109994822A (en
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袁成卫
余龙舟
张强
孙云飞
郝冬青
许亮
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National University of Defense Technology
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • 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
    • H01Q21/061Two dimensional planar arrays
    • 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
    • H01Q21/08Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a rectilinear path
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/26Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture
    • H01Q3/30Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array
    • H01Q3/32Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture varying the relative phase between the radiating elements of an array by mechanical means

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Abstract

本发明公开了一种高功率微波空间波束可扫平面阵列天线。本发明由N个基于矩形波导窄边缝隙电桥的旋转调节式移相器、N个连接波导、N路高功率微波一维波束可扫直线阵列、N个移相器相位控制单元、M个直线阵列的螺旋线内导体的驱动控制单元组成。每路直线阵列的辐射单元数目为M,在x轴方向,第n1辐射单元到第nM辐射单元构成第n行辐射单元;在y轴方向,第1m辐射单元到第Nm辐射单元构成第m列辐射单元;第m螺旋线内导体驱动控制单元控制第m列辐射单元;第n移相器相位控制单元调节第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的输出相位。本发明在实现波束扫描的基础上,具有较高的口面效率,所需控制电机的数量只要M+N。

Figure 201910303976

The invention discloses a high-power microwave space beam scannable plane array antenna. The invention consists of N rotary adjustable phase shifters based on rectangular waveguide narrow-side slot bridges, N connection waveguides, N high-power microwave one-dimensional beam sweepable linear arrays, N phase shifter phase control units, M It is composed of the drive control unit of the inner conductor of the helix of the linear array. The number of radiation elements in each linear array is M. In the x-axis direction, the n1th radiation element to the nMth radiation element constitute the nth row of radiation elements; in the y-axis direction, the 1mth radiation element to the Nmth radiation element constitute the mth column. The radiation unit; the m-th helix inner conductor drive control unit controls the m-th column of radiation units; the n-th phase shifter phase control unit adjusts the output phase of the n-th rotary adjustable phase shifter based on the rectangular waveguide narrow-side slot bridge. On the basis of realizing beam scanning, the present invention has higher oral surface efficiency, and the number of required control motors is only M+N.

Figure 201910303976

Description

高功率微波空间波束可扫平面阵列天线High-power microwave space beam swept planar array antenna

技术领域technical field

本发明涉及一种高功率微波技术领域的天线,尤其是一种具有空间波束扫描能力的高功率微波平面阵列天线。The invention relates to an antenna in the field of high-power microwave technology, in particular to a high-power microwave plane array antenna with space beam scanning capability.

背景技术Background technique

高功率微波天线是高功率微波系统的终端,其性能对高功率微波系统的辐照能力有重要影响。随着高功率微波技术的发展,迫切要求高功率微波天线具有空间波束扫描的能力。现有的经过模式转换由喇叭辐射的双曲口面天线可通过两个旋转轴实现波束扫描,但是这种天线口面效率低,不能实现与平台的共形设计;高功率微波径向线螺旋阵列天线具有GW级的功率容量,通过控制单元(一般为步进电机)控制螺旋辐射单元内导体的空间方位角,可实现一定范围的空间波束扫描,但是对于一个拥有M×N个辐射单元的系统来讲,需要M×N数量的控制单元来控制螺旋辐射单元内导体的旋转,导致伺服系统复杂,众多的控制单元导致制造天线所需的成本较高。因此,发明一种具有较高口面效率,同时具有较少数量控制单元的高功率微波空间波束可扫平面阵列天线具有重要的应用价值。The high-power microwave antenna is the terminal of the high-power microwave system, and its performance has an important influence on the irradiation ability of the high-power microwave system. With the development of high-power microwave technology, high-power microwave antennas are urgently required to have the ability to scan spatial beams. The existing hyperbolic surface antenna radiated by the horn after mode conversion can realize beam scanning through two rotation axes, but the efficiency of the antenna surface is low, and the conformal design with the platform cannot be realized; the high-power microwave radial line helix The array antenna has a power capacity of GW level. The spatial azimuth angle of the conductor in the helical radiation unit is controlled by the control unit (usually a stepper motor), and a certain range of spatial beam scanning can be achieved. In terms of the system, M×N control units are required to control the rotation of the conductors in the helical radiation unit, which leads to a complicated servo system, and many control units lead to higher costs for manufacturing the antenna. Therefore, the invention of a high-power microwave spatial beam swept planar array antenna with high aperture efficiency and a small number of control units has important application value.

发明内容SUMMARY OF THE INVENTION

本发明要解决的技术问题是提供一种具有较高口面效率,同时具有较少数量控制单元的高功率微波空间波束可扫平面阵列天线。The technical problem to be solved by the present invention is to provide a high-power microwave spatial beam swept planar array antenna with higher aperture efficiency and fewer control units.

本发明由五部分组成,它们分别是N(20<N<100)个基于矩形波导窄边缝隙电桥的旋转调节式移相器,即第一基于矩形波导窄边缝隙电桥的旋转调节式移相器,第二基于矩形波导窄边缝隙电桥的旋转调节式移相器,第三基于矩形波导窄边缝隙电桥的旋转调节式移相器,…第n(1≤n≤N)基于矩形波导窄边缝隙电桥的旋转调节式移相器,…第N基于矩形波导窄边缝隙电桥的旋转调节式移相器;N个连接波导,即第一连接波导,第二连接波导,第三连接波导,…第n连接波导,…第N连接波导;N路高功率微波一维波束可扫直线阵列,即第一高功率微波一维波束可扫直线阵列,第二高功率微波一维波束可扫直线阵列,第三高功率微波一维波束可扫直线阵列,…第n高功率微波一维波束可扫直线阵列,…第N高功率微波一维波束可扫直线阵列,(每路高功率微波一维波束可扫直线阵列的辐射单元数目为M,相邻辐射单元沿x轴方向的间距为d),第n路高功率微波一维波束可扫直线阵的辐射单元沿x轴方向依次为第n1辐射单元,第n2辐射单元,第n3辐射单元…第nm(1≤m≤M)辐射单元…第nM辐射单元。在x轴方向,第n1辐射单元到第nM辐射单元构成第n行辐射单元;在y轴方向,第1m辐射单元到第Nm辐射单元构成第m列辐射单元);N个移相器相位控制单元,即第一移相器相位控制单元,第二移相器相位控制单元,第三移相器相位控制单元,…第n移相器相位控制单元,…第N移相器相位控制单元;M个高功率微波一维波束可扫直线阵列的螺旋线内导体的驱动控制单元,即第一螺旋线内导体驱动控制单元,第二螺旋线内导体驱动控制单元,第三螺旋线内导体驱动控制单元,…第m螺旋线内导体驱动控制单元,…第M螺旋线内导体驱动控制单元。(每一个螺旋线内导体驱动控制单元控制对应列的辐射单元,即第m螺旋线内导体驱动控制单元控制第m列辐射单元)。第n基于矩形波导窄边缝隙电桥的旋转调节式移相器与第n高功率微波一维波束可扫直线阵列由第n连接波导连接,三者一起沿x轴方向构成第n路直线阵列。N路直线阵列结构完全相同,平行地沿y轴在空间中排列构成平面阵列,相邻两路直线阵列在y轴方向的间距为s。第n基于矩形波导窄边缝隙电桥的旋转调节式移相器由第n移相器相位控制单元来调节输出相位。第n行的螺旋线内导体依次为第n行第一螺旋线内导体3n31…第n行第m螺旋线内导体3n3m…第n行第M螺旋线内导体3n3M;第m列螺旋线内导体依次为第m列第1螺旋线内导体313m,第m列第2螺旋线内导体323m…第m列第n螺旋线内导体3n3m…第m列第N螺旋线内导体3N3m。The present invention consists of five parts, which are respectively N (20<N<100) rotary-adjustable phase shifters based on rectangular waveguide narrow-side slot bridges, namely the first rotary-adjustable phase shifters based on rectangular-waveguide narrow-side slot bridges Phase shifter, second rotary adjustable phase shifter based on rectangular waveguide narrow-side slot bridge, third rotary adjustable phase shifter based on rectangular waveguide narrow-side slot bridge, ... nth (1≤n≤N) Rotational Adjustable Phase Shifter Based on Rectangular Waveguide Narrow Side Slot Bridge, ... Nth Rotation Adjustable Phase Shifter Based on Rectangular Waveguide Narrow Side Slot Bridge; N connection waveguides, namely the first connection waveguide and the second connection waveguide , the third connecting waveguide, ...the nth connecting waveguide, ...the Nth connecting waveguide; 1D beam scannable linear array, third high power microwave 1D beam scannable linear array, ...nth high power microwave 1D beam scannable linear array, ...Nth high power microwave 1D beam scannable linear array, ( The number of radiation elements of each high-power microwave one-dimensional beam scannable linear array is M, and the distance between adjacent radiation elements along the x-axis direction is d). The x-axis direction is the n1th radiation unit, the n2th radiation unit, the n3th radiation unit...the nm (1≤m≤M) radiation unit...the nMth radiation unit. In the x-axis direction, the n1th radiation unit to the nMth radiation unit constitute the nth row radiation unit; in the y-axis direction, the 1mth radiation unit to the Nmth radiation unit constitute the mth column radiation unit); N phase shifters phase control Units, namely the first phase shifter phase control unit, the second phase shifter phase control unit, the third phase shifter phase control unit,...the nth phase shifter phase control unit,...the Nth phase shifter phase control unit; M high-power microwave one-dimensional beam scannable linear arrays of drive control units for the inner conductors of the helix, namely the first helix inner conductor drive control unit, the second helix inner conductor drive control unit, and the third helix inner conductor drive control unit control unit, ... mth inner conductor drive control unit, ... mth inner conductor drive control unit. (The inner conductor drive control unit of each spiral controls the radiation units of the corresponding column, that is, the m-th inner conductor drive control unit of the spiral controls the radiation units of the mth column). The nth rotary adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide and the nth high-power microwave one-dimensional beam scannable linear array are connected by the nth connecting waveguide, and the three together form the nth linear array along the x-axis direction . The N-way linear arrays have exactly the same structure, and are arranged in parallel along the y-axis in space to form a plane array, and the distance between the adjacent two-way linear arrays in the y-axis direction is s. The output phase of the nth phase shifter based on the narrow side slot bridge of the rectangular waveguide is adjusted by the phase control unit of the nth phase shifter. The spiral inner conductor of the nth row is the first spiral inner conductor of the nth row 3n31...the nth row of the mth spiral inner conductor 3n3m...the nth row of the Mth spiral inner conductor 3n3M; the mth column of the spiral inner conductor The order is the m-th column first spiral inner conductor 313m, the m-th column second spiral inner conductor 323m... m-th column n-th spiral inner conductor 3n3m... m-th column N-th spiral inner conductor 3N3m.

微波由第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第一移相器端口注入,第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第二移相器端口与第n连接波导的输入端口相连。第n移相器相位控制单元与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第一旋转关节和第二旋转关节相连。第n连接波导的输出端口与第n高功率微波一维波束可扫直线阵列的输入端口相连,第n高功率微波一维波束可扫直线阵列的第二端口外接匹配负载。第n高功率微波一维波束可扫直线阵列的第m个辐射单元的螺旋线内导体与第m螺旋线内导体驱动控制单元相连,第1高功率微波一维波束可扫直线阵列的第m个辐射单元的螺旋线内导体到第N高功率微波一维波束可扫直线阵列的第m个辐射单元的螺旋线内导体定义为第m列螺旋线内导体。Microwaves are injected from the first phase shifter port of the nth rotary-adjustable phase shifter based on the rectangular waveguide narrow-side slot bridge, and the second phase shifter of the n-th rotary-adjustable phase shifter based on the rectangular waveguide narrow-side slot bridge The filter port is connected to the input port of the nth connecting waveguide. The phase control unit of the nth phase shifter is connected with the first rotation joint and the second rotation joint of the nth rotation-adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide. The output port of the nth connecting waveguide is connected to the input port of the nth high-power microwave one-dimensional beam scannable linear array, and the second port of the nth high-power microwave one-dimensional beam scannable linear array is connected to an external matching load. The inner conductor of the helix of the mth radiation unit of the nth high-power microwave one-dimensional beam can scan the linear array is connected to the drive control unit of the mth helix inner conductor, and the first high-power microwave one-dimensional beam can scan the mth of the linear array. The helical inner conductors of the radiating elements to the helical inner conductors of the m-th radiating element of the Nth high-power microwave one-dimensional beam-scannable linear array are defined as the m-th column helical inner conductors.

基于矩形波导窄边缝隙电桥的旋转调节式移相器由矩形波导窄边缝隙电桥、第一相位调节臂和第二相位调节臂构成。第一相位调节臂与矩形波导窄边缝隙电桥的第三电桥端口相连,第二相位调节臂与矩形波导窄边缝隙电桥的第四电桥端口相连。第一相位调节臂由第一线转圆极化器和第一旋转关节构成;第二相位调节臂由第二线转圆极化器和第二旋转关节构成。第一线转圆极化器和第二线转圆极化器结构完全相同;第一旋转关节和第二旋转关节结构完全相同。微波由矩形波导窄边缝隙电桥第一电桥端口注入,由矩形波导窄边缝隙电桥的第二电桥端口输出。The rotary-adjustable phase shifter based on a rectangular waveguide narrow-side slot bridge is composed of a rectangular waveguide narrow-side slot bridge, a first phase adjustment arm and a second phase adjustment arm. The first phase adjustment arm is connected to the third bridge port of the rectangular waveguide narrow-side slot bridge, and the second phase adjustment arm is connected to the fourth bridge port of the rectangular waveguide narrow-side slot bridge. The first phase adjusting arm is composed of a first wire-rotating circular polarizer and a first rotary joint; the second phase regulating arm is composed of a second wire-rotating circular polarizer and a second rotary joint. The structures of the first line-to-circular polarizer and the second line-to-circular polarizer are identical; the structures of the first rotary joint and the second rotary joint are identical. Microwaves are injected from the first bridge port of the rectangular waveguide narrow-side slot bridge, and output from the second bridge port of the rectangular waveguide narrow-side slot bridge.

矩形波导窄边缝隙电桥是由金属材料制成的空腔,金属壁厚为T(T>1.5mm)。矩形波导窄边缝隙电桥的第一电桥端口、第二电桥端口、第三电桥端口、第四电桥端口均为矩形波导,四个端口的矩形波导的内腔的宽边长度均为a,窄边长度均为b。The rectangular waveguide narrow-side slot bridge is a cavity made of metal material, and the metal wall thickness is T (T>1.5mm). The first bridge port, the second bridge port, the third bridge port, and the fourth bridge port of the narrow-side slot bridge of the rectangular waveguide are all rectangular waveguides, and the lengths of the broad sides of the inner cavity of the rectangular waveguide of the four ports are all is a, and the length of the narrow side is b.

矩形波导窄边缝隙电桥由第一电桥端口、第二电桥端口、第三电桥端口、第四电桥端口四个端口,第一微波传输通道、第二微波传输通道、第三微波传输通道、第四微波传输通道四路微波传输通道,和中央耦合区构成。第一电桥端口与第一微波传输通道相通,第二电桥端口与第二微波传输通道相通,第一微波传输通道和第二微波传输通道均与中央耦合区相通,中央耦合区与第三微波传输通道和第四微波传输通道相通,第三微波传输通道与第三电桥端口相通,第四微波传输通道与第四电桥端口相通,第一微波传输通道和第二微波传输通道的两条轴线之间的垂直距离为h,中央耦合区的长度为L1',第三微波传输通道和第四微波传输通道均拐了90度弯,拐弯处倒圆角的内半径均为R1',拐弯处倒圆角的外半径为R2',R1'和R2'可通过电磁仿真软件优化得到,优化的目标是拐弯引起的反射为零。第三微波传输通道P18和第四微波传输通道的轴线的水平距离为L,要求2a<L<3a。The rectangular waveguide narrow-side slot bridge is composed of four ports: a first bridge port, a second bridge port, a third bridge port, and a fourth bridge port, a first microwave transmission channel, a second microwave transmission channel, and a third microwave transmission channel. The transmission channel, the fourth microwave transmission channel, four microwave transmission channels, and the central coupling area are formed. The first electric bridge port is communicated with the first microwave transmission channel, the second electric bridge port is communicated with the second microwave transmission channel, the first microwave transmission channel and the second microwave transmission channel are both communicated with the central coupling area, and the central coupling area is communicated with the third microwave transmission channel. The microwave transmission channel is communicated with the fourth microwave transmission channel, the third microwave transmission channel is communicated with the third electric bridge port, the fourth microwave transmission channel is communicated with the fourth electric bridge port, and the two microwave transmission channels of the first microwave transmission channel and the second microwave transmission channel are communicated with each other. The vertical distance between the axes of the bars is h, the length of the central coupling region is L 1 ', the third microwave transmission channel and the fourth microwave transmission channel are both turned 90 degrees, and the inner radius of the rounded corners at the corners are both R 1 '', the outer radius of the rounded corner at the corner is R 2 ', R 1 ' and R 2 ' can be optimized by electromagnetic simulation software, and the optimization goal is that the reflection caused by the corner is zero. The horizontal distance between the axes of the third microwave transmission channel P18 and the fourth microwave transmission channel is L, and it is required that 2a<L<3a.

第一线转圆极化器由注入端口,圆波导,第一波导脊,第二波导脊和末端端口组成。注入端口由金属封口,中心留有矩形缺口与矩形波导窄边缝隙电桥的第三电桥端口相连,矩形缺口宽边长度为a,窄边长度为b。圆波导的金属壁厚度为T,内圆直径为R'(λ0/2.61>R'>λ0/3.41)。第一波导脊与第二波导脊结构完全相同,两个波导脊关于z轴对称,PP'为连接两个波导脊脊腹面中心的线段,它表示两个波导脊之间的距离w(λ0/2.61>w>λ0/3.41,且w<R'),PP'在注入端口平面上的投影为OQ'(坐标原点位于注入端口的中心),OQ'与x轴的夹角为α(α=45°)。末端端口与第一旋转关节相连。The first linear-to-circular polarizer consists of an injection port, a circular waveguide, a first waveguide ridge, a second waveguide ridge and an end port. The injection port is sealed by metal, and a rectangular gap is left in the center to connect with the third bridge port of the narrow-side slot bridge of the rectangular waveguide. The length of the wide side of the rectangular gap is a, and the length of the narrow side is b. The thickness of the metal wall of the circular waveguide is T, and the diameter of the inner circle is R' (λ 0 /2.61>R'>λ 0 /3.41). The structure of the first waveguide ridge is exactly the same as that of the second waveguide ridge, and the two waveguide ridges are symmetrical about the z-axis. /2.61>w>λ 0 /3.41, and w<R'), the projection of PP' on the plane of the injection port is OQ' (the origin of the coordinates is at the center of the injection port), and the angle between OQ' and the x-axis is α ( α=45°). The end port is connected to the first rotary joint.

第一波导脊与第二波导脊形状相同,形状像一个马鞍,波导脊的脊背的长度为d2,波导脊的脊腹长度为d1。第一波导脊和第二波导脊的背部(长度为d1)与圆波导内壁紧密接触。The first waveguide ridge has the same shape as the second waveguide ridge, shaped like a saddle, the length of the back of the waveguide ridge is d 2 , and the length of the belly of the waveguide ridge is d 1 . The backs (length d 1 ) of the first waveguide ridge and the second waveguide ridge are in close contact with the inner wall of the circular waveguide.

第一旋转关节由圆柱形底板和窄金属板构成,窄金属板焊接在圆柱形底板中央。圆柱形底板的半径为R0'(R0'=L/2),厚度为w1(w1>2mm)。窄金属板的长度为Ls(Ls=λ0/4,其中λ0为圆极化TE11模式在圆波导内传输的波导波长),宽度为R',厚度为w2(1mm<w2<4mm)。窄金属板沿z轴方向的两个侧面倒圆角,圆角半径为R'/2。窄金属板从第一线转圆极化器的末端端口插入第一线转圆极化器的圆波导内,圆柱形底板将第一线转圆极化器的末端端口封口。第一旋转关节可绕对称轴(即z轴)旋转。The first rotary joint is composed of a cylindrical base plate and a narrow metal plate, and the narrow metal plate is welded in the center of the cylindrical base plate. The cylindrical base plate has a radius R 0 ' (R 0 '=L/2) and a thickness w 1 (w 1 >2mm). The length of the narrow metal plate is Ls (Ls=λ 0 /4, where λ 0 is the waveguide wavelength of the circularly polarized TE 11 mode propagating in the circular waveguide), the width is R', and the thickness is w 2 (1mm<w 2 < 4mm). The two sides of the narrow metal plate along the z-axis are rounded with a radius of R'/2. The narrow metal plate is inserted into the circular waveguide of the first linear-to-circular polarizer from the end port of the first linear-to-circular polarizer, and the cylindrical base plate seals the end port of the first linear-to-circular polarizer. The first rotation joint is rotatable about the axis of symmetry (ie, the z-axis).

基于矩形波导窄边缝隙电桥的旋转调节式移相器的第一旋转关节和第二旋转关节在初始状态下,两块窄金属板之间存在一个夹角,夹角大小为γ。In the initial state of the first rotary joint and the second rotary joint of the rotary adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide, there is an included angle between the two narrow metal plates, and the size of the included angle is γ.

第n连接波导的两端端口为矩形波导,第n连接波导输入端口的矩形波导的外尺寸为a×b,与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第二移相器端口相连,二者的波导尺寸相同,第n连接波导输出端口的矩形波导的外尺寸为a2×b2,与第n高功率微波一维波束可扫直线阵列的输入端口的尺寸相同。第n连接波导中央为连接两个端口的波导渐变过渡段,过渡段的长度为L,可通过电磁仿真软件(如CST Microwave Studio)优化得到,优化的目标是传输反射为零。过渡段的横截面保持为矩形,宽边尺寸由a过渡到a2,窄边尺寸由b过渡到b2The ports at both ends of the n-th connecting waveguide are rectangular waveguides, and the outer dimension of the rectangular waveguide connecting the input port of the n-th waveguide is a×b. The port of the phase shifter is connected, and the waveguide size of the two is the same. The outer dimension of the rectangular waveguide connected to the output port of the nth waveguide is a 2 ×b 2 , which is the same as the size of the input port of the nth high-power microwave one-dimensional beam-sweepable linear array. same. The center of the nth connecting waveguide is the gradual transition section of the waveguide connecting the two ports. The length of the transition section is L, which can be optimized by electromagnetic simulation software (such as CST Microwave Studio). The optimization goal is zero transmission reflection. The cross-section of the transition section remains rectangular, the width of the broad side transitions from a to a 2 , and the size of the narrow side transitions from b to b 2 .

高功率微波一维波束可扫直线阵列是全金属结构,由两部分构成,第一部分是矩形波导,第二部分是辐射单元构成的一维直线阵列。微波由矩形波导的注入端注入,矩形波导的输出端外接匹配负载。一维直线阵列由M(一般而言:20<M<500)个辐射单元构成,相邻辐射单元间距为d,沿x轴方向安装在矩形波导窄边上。辐射单元构成的一维直线阵列按矩形波导的注入端向输出端的方向依次为第一辐射单元,第二辐射单元,第三辐射单元…第m辐射单元…第M辐射单元,其中1≤m≤M。The high-power microwave one-dimensional beam swept linear array is an all-metal structure and consists of two parts, the first part is a rectangular waveguide, and the second part is a one-dimensional linear array composed of radiating elements. The microwave is injected from the injection end of the rectangular waveguide, and the output end of the rectangular waveguide is connected to a matching load. The one-dimensional linear array is composed of M (generally: 20<M<500) radiating elements, the spacing between adjacent radiating elements is d, and they are installed on the narrow side of the rectangular waveguide along the x-axis direction. The one-dimensional linear array formed by the radiation elements is the first radiation unit, the second radiation unit, the third radiation unit...the mth radiation unit...the Mth radiation unit in the direction from the injection end to the output end of the rectangular waveguide, where 1≤m≤ M.

矩形波导的矩形截面的内尺寸宽边长度为a2,窄边长度为b2,矩形波导的四个侧面(即除注入端、输出端所在的面的另外四个面)金属壁厚均为T。矩形波导的第一侧面中央挖有M个圆形通孔,圆形通孔按矩形波导的注入端向输出端的方向依次为矩形波导第一侧面的第一圆形通孔,矩形波导第一侧面的第二圆形通孔,矩形波导第一侧面的第三圆形通孔…矩形波导第一侧面的第m圆形通孔…矩形波导第一侧面的第M圆形通孔。矩形波导第一侧面的第一圆形通孔到第M圆形通孔的半径均为R1(R1<b2/2),矩形波导第一侧面的第一圆形通孔的圆心与注入端的距离为s0(s0>d/2),矩形波导第一侧面的第m圆形通孔的圆心与注入端的距离为s0+(m-1)d,相邻的第一圆形通孔圆心间距为d。与矩形波导的第一侧面相对的矩形波导第二侧面中央挖有2M个圆形通孔,圆形通孔按矩形波导的注入端向输出端的方向依次为矩形波导第二侧面的第一圆形通孔,矩形波导第二侧面的第二圆形通孔,矩形波导第二侧面的第三圆形通孔,矩形波导第二侧面的第四圆形通孔…矩形波导第二侧面的第2m-1圆形通孔,矩形波导第二侧面的第2m圆形通孔,…矩形波导第二侧面第2M-1圆形通孔,矩形波导第二侧面第2M圆形通孔。矩形波导第二侧面的第1,3…2m-1…2M-1圆形通孔的半径均为R2,矩形波导第二侧面的第一圆形通孔的圆心与注入端的距离为s0,矩形波导第二侧面的第2m-1圆形通孔的圆心与注入端的距离为s0+(m-1)d;矩形波导第二侧面的第2m圆形通孔的半径为rm,矩形波导第二侧面的第二圆形通孔的圆心与注入端的距离为s1,矩形波导第二侧面的第2m圆形通孔的圆心与注入端的距离为sm,满足sm-s0-(m-1)d≈λ0/4,其中λ0为微波在矩形波导内传输的波导波长。The inner dimension of the rectangular cross-section of the rectangular waveguide is a 2 , the length of the narrow side is b 2 , and the metal wall thickness of the four sides of the rectangular waveguide (that is, the other four sides except the injection end and the output end) are T. M circular through holes are dug in the center of the first side of the rectangular waveguide. The circular through holes are the first circular through holes on the first side of the rectangular waveguide in the direction from the injection end to the output end of the rectangular waveguide. The second circular through hole of the rectangular waveguide, the third circular through hole on the first side of the rectangular waveguide...the mth circular through hole on the first side of the rectangular waveguide...the Mth circular through hole on the first side of the rectangular waveguide. The radii from the first circular through hole on the first side of the rectangular waveguide to the M-th circular through hole are all R 1 (R 1 <b 2 /2), and the center of the first circular through hole on the first side of the rectangular waveguide is The distance from the injection end is s 0 (s 0 >d/2), the distance between the center of the m-th circular through hole on the first side of the rectangular waveguide and the injection end is s 0 +(m-1)d, and the adjacent first circle The distance between the centers of the through holes is d. 2M circular through holes are dug in the center of the second side of the rectangular waveguide opposite to the first side of the rectangular waveguide. Through hole, second circular through hole on the second side of the rectangular waveguide, third circular through hole on the second side of the rectangular waveguide, fourth circular through hole on the second side of the rectangular waveguide...2m on the second side of the rectangular waveguide -1 circular via, 2mth circular via on the second side of the rectangular waveguide, ... 2M-1 circular via on the second side of the rectangular waveguide, 2M circular via on the second side of the rectangular waveguide. The radii of the first, 3...2m-1...2M-1 circular through holes on the second side of the rectangular waveguide are all R 2 , and the distance between the center of the first circular through hole on the second side of the rectangular waveguide and the injection end is s 0 , the distance between the center of the 2m-1 circular through hole on the second side of the rectangular waveguide and the injection end is s 0 +(m-1)d; the radius of the 2m-th circular through hole on the second side of the rectangular waveguide is r m , The distance between the center of the second circular through hole on the second side of the rectangular waveguide and the injection end is s 1 , and the distance between the center of the second circular through hole on the second side of the rectangular waveguide and the injection end is s m , satisfying s m -s 0 -(m-1)d≈λ 0 /4, where λ 0 is the waveguide wavelength of the microwave propagating in the rectangular waveguide.

本发明的第一辐射单元,第二辐射单元,第三辐射单元…第m辐射单元…第M辐射单元的组成成分相同(均包含反射消除杆,螺旋线内导体和耦合腔三部分)。以第m辐射单元为例,第m辐射单元由第m反射消除杆,第m螺旋线内导体和第m耦合腔三部分组成。第m反射消除杆通过矩形波导第二侧面的第2m圆形通孔完全插入矩形波导内,顶端与矩形波导第一侧面内壁接触;第m耦合腔一端由矩形波导第一侧面的第m圆形通孔插入矩形波导以固定在矩形波导上;第m螺旋线内导体经过第m耦合腔插入矩形波导内,由矩形波导第二侧面的第2m-1圆形通孔穿过矩形波导,外接步进电机,穿出矩形波导的长度为h'。The composition of the first radiation unit, the second radiation unit, the third radiation unit...the mth radiation unit...the Mth radiation unit of the present invention is the same (all including the reflection elimination rod, the inner conductor of the helix and the coupling cavity). Taking the mth radiation unit as an example, the mth radiation unit is composed of the mth reflection cancellation rod, the mth helix inner conductor and the mth coupling cavity. The m-th reflection cancellation rod is completely inserted into the rectangular waveguide through the 2m-th circular through hole on the second side of the rectangular waveguide, and the tip is in contact with the inner wall of the first side of the rectangular waveguide; The through hole is inserted into the rectangular waveguide to be fixed on the rectangular waveguide; the inner conductor of the m-th helix is inserted into the rectangular waveguide through the m-th coupling cavity, and the 2m-1 circular through hole on the second side of the rectangular waveguide passes through the rectangular waveguide, and the external step Into the motor, the length of the rectangular waveguide is h'.

第m反射消除杆的形状为圆柱体,半径等于rm。第m反射消除杆通过矩形波导第二侧面的第2m圆形通孔插入矩形波导内,一端顶在矩形波导第一侧面内壁,另一端嵌在矩形波导第二侧面的第2m圆形通孔内,第1反射消除杆到第M反射消除杆的长度均为a2+T。The m-th reflection cancelling rod has the shape of a cylinder with a radius equal to r m . The mth reflection cancellation rod is inserted into the rectangular waveguide through the 2mth circular through hole on the second side of the rectangular waveguide. , the lengths from the first reflection cancellation rod to the M reflection cancellation rod are a 2 +T.

第一螺旋线内导体到第M螺旋线内导体的结构完全相同。第m螺旋线内导体由一段直圆柱体,一段与直圆柱体垂直的半圆环和一段螺旋线构成,直圆柱体是一根金属棒,直径为2R2,直圆柱体的长度为L1(L1长度约为两倍矩形波导宽边a2长度,直圆柱体的一端从矩形波导第二侧面的第2m-1圆形通孔穿过矩形波导,外接步进电机。半圆环和螺旋线的总高度为L2;半圆环的圆环直径为L3/2,螺旋线2m23为等螺旋半径等螺距的一段螺旋线,螺旋线的螺旋外直径为L3。半圆环的初始段切线与x轴的夹角定义为螺旋线内导体的空间方位角,用αm表示,αm代表第m螺旋线内导体的空间方位,在直线阵列中,相邻两个螺旋线内导体的空间方位角度差为一个常量P,即αmm-1=P,其中1<m≤M。The structures of the inner conductor of the first helix to the inner conductor of the Mth helix are completely the same. The inner conductor of the m-th helix consists of a straight cylinder, a semi-circle perpendicular to the straight cylinder and a helix. The straight cylinder is a metal rod with a diameter of 2R 2 and the length of the straight cylinder is L 1 (The length of L 1 is about twice the length of the broad side a 2 of the rectangular waveguide, and one end of the right cylinder passes through the 2m-1 circular through hole on the second side of the rectangular waveguide, and is connected to a stepping motor. The semicircular ring and The total height of the helix is L 2 ; the diameter of the semicircular ring is L 3 /2, the helix 2m23 is a helix with equal helix radius and equal pitch, and the outer diameter of the helix is L 3 . The angle between the initial segment tangent and the x-axis is defined as the spatial azimuth angle of the conductor in the helix, denoted by α m , where α m represents the spatial azimuth of the conductor in the mth helix. The spatial azimuth angle difference of the conductors is a constant P, that is, α mm-1 =P, where 1<m≤M.

第m耦合腔的外形一端为圆柱凸台另一端为长方体,圆柱凸台的外半径为R1,凸台的高度为H1。第m耦合腔的内部挖有四个不同形状的孔,从圆柱凸台向长方体的方向依次为第一孔,第二孔,第三孔,第四孔,四个孔连通在一起构成微波传输的通道。第一孔由内孔和外孔构成,两个孔的高度均为H1,内孔截面形状为半径为R2的圆形,第m螺旋线内导体即通过该孔插入波导内,外孔近似半环形,内半径为R3,外半径为R4,外孔的圆心角为

Figure GDA0002444055660000051
外孔的对称轴与x轴的夹角定义为耦合腔的旋转角,用θm表示。第二孔2m34的高度为H2-H1,第二孔的轮廓由两段弧线构成,尺寸较大的圆弧线的半径为R4,对应的圆心角为
Figure GDA0002444055660000053
尺寸较小弧线的半径为R5,对应的圆心角为
Figure GDA0002444055660000052
第二孔的对称轴与x轴的夹角也为θm,第一耦合腔到第M耦合腔结构的尺寸除了耦合腔的旋转角θm不同外,其它结构尺寸均相同。第三孔的高度H3-H2,截面形状为圆形,圆形半径为R5。第四孔的高度H4-H3,截面形状为圆形,圆形半径为R6。One end of the shape of the mth coupling cavity is a cylindrical boss and the other end is a cuboid, the outer radius of the cylindrical boss is R 1 , and the height of the boss is H 1 . There are four holes of different shapes dug inside the mth coupling cavity, the first hole, the second hole, the third hole, and the fourth hole are in sequence from the cylindrical boss to the cuboid, and the four holes are connected together to form a microwave transmission channel. The first hole is composed of an inner hole and an outer hole. The heights of the two holes are H 1 . The cross-sectional shape of the inner hole is a circle with a radius of R 2. The inner conductor of the m-th helix is inserted into the waveguide through this hole. Approximate semi-circular shape, the inner radius is R 3 , the outer radius is R 4 , and the central angle of the outer hole is
Figure GDA0002444055660000051
The angle between the symmetry axis of the outer hole and the x-axis is defined as the rotation angle of the coupling cavity, represented by θ m . The height of the second hole 2m34 is H 2 -H 1 , the contour of the second hole is composed of two arcs, the radius of the larger arc is R 4 , and the corresponding central angle is
Figure GDA0002444055660000053
The radius of the arc with the smaller size is R 5 , and the corresponding central angle is
Figure GDA0002444055660000052
The angle between the symmetry axis of the second hole and the x-axis is also θ m , and the dimensions of the structures from the first coupling cavity to the M-th coupling cavity are the same except for the rotation angle θ m of the coupling cavity. The height of the third hole is H 3 -H 2 , the cross-sectional shape is a circle, and the radius of the circle is R 5 . The height of the fourth hole is H 4 -H 3 , the cross-sectional shape is a circle, and the radius of the circle is R 6 .

第n移相器相位控制单元为一个可旋转的轴承,轴承外接步进电机,由步进电机驱动绕自身轴(即z轴)旋转。可旋转轴承与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第一旋转关节和第二旋转关节具有相同的外直径R'0(R'0>R'),第n移相器相位控制单元与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第一旋转关节和第二旋转关节相连(三者通过外围的齿轮啮合,这里不作具体结构介绍,只介绍其原理)。第n移相器相位控制单元外接步进电机,绕z轴旋转,即带动第一旋转关节和第二旋转关节同步旋转。由基于矩形波导窄边缝隙电桥的旋转调节式移相器可知,第n移相器相位控制单元每旋转θn,同步地带动第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第一旋转关节和第二旋转关节绕相同方向旋转θn,因此移相器的输出相位改变2θn。高功率微波空间波束可扫平面阵列天线的工作状态要求相邻两路直线阵列的移相器的旋转角度差

Figure GDA0002444055660000061
为一个常量,即
Figure GDA0002444055660000062
因此相邻两路直线阵列的馈入相位差也应为常量,即馈入相位差等于相邻两路直线阵列的移相器的旋转角度差。The phase control unit of the nth phase shifter is a rotatable bearing, and the bearing is connected to a stepping motor, which is driven by the stepping motor to rotate around its own axis (ie, the z-axis). The rotatable bearing has the same outer diameter R' 0 (R' 0 >R') as the first rotary joint and the second rotary joint of the n-th rectangular waveguide narrow-side slot bridge-based rotary adjustable phase shifter, and the n-th The phase shifter phase control unit is connected with the first rotary joint and the second rotary joint of the nth rotary adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide (the three are meshed by the peripheral gears, and the specific structure is not introduced here. Only the principle is introduced). The phase control unit of the nth phase shifter is connected to a stepping motor, and rotates around the z-axis, that is, drives the first rotary joint and the second rotary joint to rotate synchronously. It can be seen from the rotary-adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide that every time the phase control unit of the n-th phase shifter rotates by θ n , it synchronously drives the n-th rotational-adjustable phase-shifter based on the narrow-side slot bridge of the rectangular waveguide. The first and second rotary joints of the phase shifter rotate around the same direction by θ n , so the output phase of the phase shifter changes by 2θ n . The working state of the high-power microwave space beam swept planar array antenna requires the rotation angle difference of the phase shifters of the two adjacent linear arrays
Figure GDA0002444055660000061
is a constant, that is
Figure GDA0002444055660000062
Therefore, the feeding phase difference of the two adjacent linear arrays should also be constant, that is, the feeding phase difference is equal to the rotation angle difference of the phase shifters of the adjacent two linear arrays.

第m螺旋线内导体驱动控制单元由第m带齿轮的滑动平板(这里介绍原理,所有的齿轮结构均不作描述)和N个带齿轮的轴承构成,N个带齿轮的轴承沿y轴方向依次为第m1轴承,第m2轴承,第m3轴承…第mn轴承…第mN轴承,上述轴承沿y轴方向依次与第m列的N个辐射单元的螺旋线内导体(即第m列螺旋线内导体)紧密相连,轴承的旋转将带动螺旋线内导体跟着一起旋转。每一个轴承的外直径为r(d/2>r>R2),滑动平板和轴承的齿轮啮合在一起,轴承的齿轮与滑动平板的齿轮尺寸相同。第m螺旋线内导体驱动控制单元的一端由步进电机驱动沿y轴方向移动hm,从而带动第m1轴承到第Nm轴承都旋转2hm/r弧度,同时带动第m列螺旋线内导体的空间方位角旋转2hm/r弧度,这个旋转角大小由所需的波束指向确定。在x轴方向上相邻螺旋线内导体驱动控制单元被外接步进电机驱动的长度差为一个常量Δh=hm-hm-1,因此在x轴方向相邻列螺旋线内导体的空间方位角差也为一个常量,设为

Figure GDA0002444055660000063
Figure GDA0002444055660000064
The m-th helical inner conductor drive control unit is composed of the m-th geared sliding plate (the principle is introduced here, all gear structures are not described) and N geared bearings, and the N geared bearings are in turn along the y-axis direction. For the m1th bearing, the m2th bearing, the m3th bearing...the mnth bearing...the mNth bearing, the above bearings are sequentially connected with the inner conductors of the spirals of the N radiation units in the mth row along the y-axis direction (that is, the inner conductors of the helix in the mth row). The conductors) are closely connected, and the rotation of the bearing will drive the inner conductor of the helix to rotate along with it. The outer diameter of each bearing is r (d/2>r>R 2 ), the sliding plate and the gear of the bearing are meshed together, and the gear of the bearing is the same size as the gear of the sliding plate. One end of the m-th helix inner conductor drive control unit is driven by a stepping motor to move h m along the y-axis direction, thereby driving the m1th bearing to the Nmth bearing to rotate by 2h m /r radians, and at the same time driving the mth row of helix inner conductors The spatial azimuth is rotated by 2h m /r radians, and the size of this rotation angle is determined by the desired beam pointing. In the x-axis direction, the length difference between the adjacent helix inner conductor drive control units driven by the external stepping motor is a constant Δh=h m -h m-1 , so the space of the conductors in the adjacent column helix in the x-axis direction The azimuth difference is also a constant, set to
Figure GDA0002444055660000063
Have
Figure GDA0002444055660000064

所述结构参数所满足的条件和设计步骤如下:The conditions and design steps satisfied by the structural parameters are as follows:

一、确定基于矩形波导窄边缝隙电桥的旋转调节式移相器的结构参数1. Determining the structural parameters of the rotary adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide

1)确定矩形波导窄边缝隙电桥基本参数。四路微波传输通道对应的矩形波导尺寸a和b根据实际应用需要设计。为了满足TE10模在其中传输,一般满足λ/2<a<λ,b<λ/2,λ为微波在自由空间中的波长;第一微波传输通道和第二微波传输通道的两条轴线之间的垂直距离即中央耦合区的高度h满足仅传输矩形波导TE10和TE20模式的要求,即λ<h+a<1.5λ,中央耦合区的长度L1'满足两个模式的相位差为π/2,即1) Determine the basic parameters of the rectangular waveguide narrow-side slot bridge. The dimensions a and b of the rectangular waveguide corresponding to the four microwave transmission channels are designed according to practical application requirements. In order to satisfy the transmission of the TE 10 mode in it, it generally satisfies λ/2<a<λ, b<λ/2, where λ is the wavelength of the microwave in free space; the two axes of the first microwave transmission channel and the second microwave transmission channel The vertical distance between them, i.e. the height h of the central coupling region, satisfies the requirement of transmitting only the TE 10 and TE 20 modes of the rectangular waveguide, that is, λ<h+a<1.5λ, and the length L 1 ' of the central coupling region satisfies the phase of the two modes The difference is π/2, i.e.

Figure GDA0002444055660000071
Figure GDA0002444055660000071

其中k为微波的自由空间波数。倒角R1'和R2'可通过电磁仿真软件(如CSTMicrowave Studio)优化得到,优化的目的是使得微波传输通道的反射为零。where k is the free-space wavenumber of the microwave. The chamfers R 1 ' and R 2 ' can be optimized by electromagnetic simulation software (such as CSTMicrowave Studio), and the purpose of optimization is to make the reflection of the microwave transmission channel zero.

2)确定线转圆极化器的参数。波导脊的尺寸d1和d2以及2个波导脊之间的距离w可通过电磁仿真软件(如CST Microwave Studio)优化得到,优化的目的是使圆极化器注入线极化的TE11模式后,输出为圆极化的TE11模式,圆极化TE11模式的轴比为1。2) Determine the parameters of the line-to-circular polarizer. The dimensions d 1 and d 2 of the waveguide ridges and the distance w between the 2 waveguide ridges can be optimized by electromagnetic simulation software (such as CST Microwave Studio), and the purpose of optimization is to inject the linearly polarized TE 11 mode into the circular polarizer After that, the output is the circularly polarized TE 11 mode, and the axial ratio of the circularly polarized TE 11 mode is 1.

3)两个旋转关节的初始状态的角度差γ由下式确定3) The angle difference γ of the initial state of the two rotary joints is determined by the following formula

Figure GDA0002444055660000072
Figure GDA0002444055660000072

二、确定高功率微波一维波束可扫直线阵列结构参数2. Determine the structural parameters of the high-power microwave one-dimensional beam scannable linear array

1)确定波导基本参数。矩形缝隙波导的尺寸a2和b2根据实际应用需要设计。为了满足TE10模在其中传输,一般满足λ/2<a2<λ,b2<λ/2,λ为微波在自由空间中的波长;壁厚T根据强度和保证功率容量的需要,一般取T≥1.5mm。1) Determine the basic parameters of the waveguide. The dimensions a 2 and b 2 of the rectangular slot waveguide are designed according to practical application requirements. In order to meet the transmission of TE 10 mode in it, generally λ/2<a 2 <λ, b 2 <λ/2, λ is the wavelength of microwave in free space; the wall thickness T is generally based on the strength and the need to ensure power capacity. Take T≥1.5mm.

2)耦合腔的第一孔的外孔尺寸在空间许可的范围内,为保证一定的功率容量要求,一般要求:R4-R3>1.50mm,同时要求R3>3.00mm,高度H1,H2和圆心角

Figure GDA0002444055660000075
的确定方法是:在保证功率容量的前提下,其取值由电磁仿真软件(如CST Microwave Studio)仿真得到,优化的目标是尺寸参数能使耦合腔的第一孔工作在谐振状态,等效电导随频率变化的曲线在中心频点获得极大值。2) The size of the outer hole of the first hole of the coupling cavity is within the range allowed by the space. In order to ensure a certain power capacity requirement, the general requirement is: R 4 -R 3 >1.50mm, and at the same time, R 3 >3.00mm, height H 1 , H2 and the central angle
Figure GDA0002444055660000075
The determination method is: on the premise of ensuring the power capacity, its value is simulated by electromagnetic simulation software (such as CST Microwave Studio), and the optimization goal is that the size parameters can make the first hole of the coupling cavity work in the resonant state, equivalent to The curve of conductance versus frequency obtains a maximum value at the center frequency.

3)确定第m耦合腔的旋转角θm。本发明的耦合电场强度由θm确定,外孔的等效电导gm随着θm(0<θm<90°)的增加而增大。直线阵列中第m个辐射单元的理论归一化等效电导与口径分布有关,gm理论计算公式为3) Determine the rotation angle θ m of the mth coupling cavity. The coupling electric field strength of the present invention is determined by θ m , and the equivalent conductance g m of the outer hole increases with the increase of θ m (0<θ m <90°). The theoretical normalized equivalent conductance of the mth radiating element in the linear array is related to the aperture distribution, and the theoretical calculation formula of g m is:

Figure GDA0002444055660000073
Figure GDA0002444055660000073

其中,

Figure GDA0002444055660000074
αe为波导衰减常数,d为相邻辐射单元之间的间距,Ei为第i(1≤i≤m)个辐射单元的电场强度,由口径电场分布确定。η为天线辐射效率,一般取1>η>0.95。通过电磁仿真软件计算提取得到耦合腔的等效电导随耦合腔的旋转角度的关系后(即任意一个角度对应一个等效电导数值),根据公式(3),利用插值法即可得直线阵列中各个辐射单元(1—M)的耦合腔的旋转角度θm。in,
Figure GDA0002444055660000074
α e is the attenuation constant of the waveguide, d is the spacing between adjacent radiation elements, and E i is the electric field intensity of the i-th (1≤i≤m) radiation element, which is determined by the aperture electric field distribution. η is the radiation efficiency of the antenna, generally 1>η>0.95. After calculating and extracting the relationship between the equivalent conductance of the coupled cavity and the rotation angle of the coupled cavity through electromagnetic simulation software (that is, any angle corresponds to an equivalent conductance value), according to formula (3), the linear array can be obtained by interpolation method. The rotation angle θ m of the coupling cavity of each radiation element (1-M).

4)确定耦合腔和螺旋线内导体结构参数。辐射单元间距d决定了波束扫描范围,在空间允许的情况下,尽量缩小d可以增大波束扫描范围,d满足4) Determine the structural parameters of the coupling cavity and the conductor in the helix. The radiation unit spacing d determines the beam scanning range. If space allows, reducing d as much as possible can increase the beam scanning range. d satisfies

Figure GDA0002444055660000081
Figure GDA0002444055660000081

其中ρ0为波束偏离天线辐射口面法向的最大角。螺旋线内导体半径与矩形波导第二侧面的第1,3…2m-1…2M-1圆形通孔的半径相等,均为R2,要求0<R2<R3-1。圆形凸台高度H1等于波导壁厚T。耦合腔和螺旋线内导体的其它结构参数,包括H3,H4,L1,L2,L3,R6和R5可由电磁仿真软件(如CST Microwave Studio)优化得到。优化的目标是辐射单元的反射在工作频点接近0,轴比(辐射电场在与微波传输方向垂直的平面上两个正交方向上的电场比值)在螺旋线的轴向上接近1,这就保证了螺旋线内导体和耦合腔构成的辐射单元工作在轴向模式状态。另外要求H4-H1≈0.75λ。where ρ 0 is the maximum angle that the beam deviates from the normal direction of the antenna radiation port. The radius of the inner conductor of the helix is equal to the radius of the 1st, 3...2m-1...2M-1 circular through holes on the second side of the rectangular waveguide, both are R 2 , and 0<R 2 <R 3 -1 is required. The circular boss height H1 is equal to the waveguide wall thickness T. Other structural parameters of the coupled cavity and the inner conductor of the helix, including H 3 , H 4 , L 1 , L 2 , L 3 , R 6 and R 5 , can be optimized by electromagnetic simulation software (such as CST Microwave Studio). The optimization goal is that the reflection of the radiation element is close to 0 at the operating frequency, and the axial ratio (the ratio of the electric field of the radiation electric field in two orthogonal directions on a plane perpendicular to the microwave transmission direction) is close to 1 in the axial direction of the helix. This ensures that the radiation element formed by the inner conductor of the helix and the coupling cavity works in the axial mode state. In addition, H 4 -H 1 ≈ 0.75λ is required.

5)反射消除杆的尺寸确定。第m个反射消除杆的半径等于rm,满足反射消除杆在矩形波导内引起的反射与第m个耦合腔和第m个螺旋线内导体引起的反射幅度相等,具体数值可由电磁仿真软件(如CST Microwave Studio)仿真计算比较得到。第m个反射消除杆的位置sm满足第m反射消除杆引起的反射波相位和第m个耦合腔和第m个螺旋线内导体引起的反射相位相差180度,这就使得反射消除杆,耦合腔和螺旋线内导体引起的反射相互抵消,尺寸具体数值同理可由电磁仿真软件仿真计算比较得到。5) The size of the reflection eliminating rod is determined. The radius of the m-th reflection cancellation rod is equal to r m , which satisfies that the reflection caused by the reflection cancellation rod in the rectangular waveguide is equal to the reflection amplitude caused by the m-th coupling cavity and the m-th helix inner conductor. The specific value can be determined by the electromagnetic simulation software ( Such as CST Microwave Studio) simulation calculation and comparison. The position s m of the m-th reflection cancellation rod satisfies the phase difference of the reflected wave caused by the m-th reflection cancellation rod and the reflection phase caused by the m-th coupling cavity and the m-th helix inner conductor, which makes the reflection cancellation rod, The reflections caused by the coupling cavity and the inner conductor of the helix cancel each other out, and the specific value of the size can be calculated and compared by the electromagnetic simulation software for the same reason.

6)螺旋线内导体外接步进电机,M个辐射单元构成的直线阵列共需要M个步进电机,第m个步进电机控制第m螺旋线内导体绕其直圆柱体的轴线(即是螺旋线的轴线)旋转。定义直线阵列天线的辐射主波束的方向与口面法向(即图1中的z轴)的夹角为ρ,直线阵列天线沿x轴方向相邻螺旋线内导体旋转后的空间方位角度αm差P由波束方向ρ决定,P与ρ的关系如下6) The inner conductor of the helix is connected to an external stepping motor. The linear array composed of M radiation units requires M stepping motors in total. the axis of the helix) rotates. Define the angle between the direction of the radiated main beam of the linear array antenna and the normal direction of the mouth (that is, the z-axis in Figure 1) as ρ, and the spatial azimuth angle α of the linear array antenna after the rotation of the conductor in the adjacent helix along the x-axis direction The m difference P is determined by the beam direction ρ, and the relationship between P and ρ is as follows

Figure GDA0002444055660000082
Figure GDA0002444055660000082

其中k为自由空间波数,β为矩形波导波导传播常数,其计算式为where k is the free-space wave number, and β is the propagation constant of the rectangular waveguide, which is calculated as

Figure GDA0002444055660000083
Figure GDA0002444055660000083

基于矩形波导窄边缝隙电桥的旋转调节式移相器的工作原理是:高功率微波从注入端口注入到矩形波导窄边缝隙电桥内,经过中央耦合区后分成两路幅度相同,分别由矩形波导窄边缝隙电桥的第三和第四通道注入第一和第二相位调节臂;每一路矩形波导传输通道内传输的TE10模式的线极化微波注入到线转圆极化器的圆波导后,被转换成圆极化波向前传输,旋转关节的功能是改变圆极化波的左右旋特性(即将左旋圆极化波转换成右旋圆极化波,或者将右旋圆极化波转换成左旋圆极化波)。被矩形波导窄边缝隙电桥分成两路传输的微波经过旋转关节的圆柱形底板反射后,反射相位与旋转关节空间方位有关。初始状态下,两个旋转关节的角度差γ用来弥补两路微波传输路径不同的相位差。因此,在上述初始条件下,两路反射微波分别再次通过矩形波导窄边缝隙电桥的第三和第四传输通道时,反射波相位与旋转关节的空间方位有关,满足上述条件后,反射波将全部从矩形波导窄边缝隙电桥的第二电桥端口输出。定义同步将两个旋转关节绕各自的对称轴沿同一个方向旋转的角度为Δθ,实施上述旋转后,则反射微波的相位将改变2Δθ。The working principle of the rotary-adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide is as follows: the high-power microwave is injected into the narrow-side slot bridge of the rectangular waveguide from the injection port, and after passing through the central coupling area, it is divided into two paths with the same amplitude. The third and fourth channels of the narrow-side slot bridge of the rectangular waveguide are injected into the first and second phase adjustment arms; the linearly polarized microwave of the TE 10 mode transmitted in each channel of the rectangular waveguide transmission channel is injected into the linear-to-circular polarizer. After the circular waveguide, it is converted into a circularly polarized wave and transmitted forward. The function of the rotating joint is to change the left and right rotation characteristics of the circularly polarized wave (that is, to convert the left-handed circularly polarized wave into a right-handed circularly polarized wave, or to convert the right-handed circularly polarized wave into a right-handed circularly polarized wave. The polarized wave is converted into a left-handed circularly polarized wave). After the microwaves divided into two transmissions by the narrow-side slot bridge of the rectangular waveguide are reflected by the cylindrical base plate of the rotary joint, the reflection phase is related to the spatial orientation of the rotary joint. In the initial state, the angle difference γ of the two rotating joints is used to compensate for the different phase differences between the two microwave transmission paths. Therefore, under the above initial conditions, when the two reflected microwaves pass through the third and fourth transmission channels of the rectangular waveguide narrow-side slot bridge again, the phase of the reflected wave is related to the spatial orientation of the rotating joint. After the above conditions are met, the reflected wave All will be output from the second bridge port of the rectangular waveguide narrow-side slot bridge. The angle at which the two rotary joints rotate in the same direction around their respective axes of symmetry is defined as Δθ. After the above rotation is performed, the phase of the reflected microwave will change by 2Δθ.

高功率微波一维波束可扫直线阵列的工作过程为:高功率微波从矩形波导的注入端馈入到矩形波导内,沿x轴方向传输,由于耦合腔第一孔的外孔切断矩形波导第一侧面上的电流,使得能量从矩形波导耦合到耦合腔,从而通过螺旋线内导体和耦合腔构成的辐射单元向自由空间辐射。矩形波导内的传输反射可通过反射消除杆抵消。微波经过辐射单元构成的一维直线阵辐射后,少部分剩余的能量被外接的匹配负载吸收,整个天线工作在行波状态。螺旋线内导体工作在轴向模状态,辐射圆极化波,圆极化波的辐射相位与螺旋线内导体的空间方位角度αm有关。通过外接的步进电机控制螺旋线内导体旋转来调节直线阵列天线螺旋线内导体的空间方位角度αm,即调节直线阵列天线各个辐射单元沿x轴的相位分布,从而实现波束扫描的功能。The working process of the high-power microwave one-dimensional beam swept linear array is as follows: the high-power microwave is fed into the rectangular waveguide from the injection end of the rectangular waveguide and transmitted along the x-axis direction. The current on one side causes the energy to be coupled from the rectangular waveguide to the coupling cavity, thereby radiating to the free space through the radiating element formed by the conductor in the helix and the coupling cavity. Transmission reflections within the rectangular waveguide can be canceled by reflection cancellation rods. After the microwave is radiated by the one-dimensional linear array formed by the radiation unit, a small part of the remaining energy is absorbed by the external matching load, and the whole antenna works in the traveling wave state. The inner conductor of the helix works in the axial mode state and radiates circularly polarized waves. The radiation phase of the circularly polarized wave is related to the spatial azimuth angle α m of the inner conductor of the helix. An external stepping motor controls the rotation of the inner conductor of the helix to adjust the spatial azimuth angle α m of the inner conductor of the helix of the linear array antenna, that is, to adjust the phase distribution of each radiating element of the linear array antenna along the x-axis, so as to realize the function of beam scanning.

因此,高功率微波由第1到第N基于矩形波导窄边缝隙电桥的旋转调节式移相器到的N个第一移相器端口等幅等相位地注入,经过N个基于矩形波导窄边缝隙电桥的旋转调节式移相器相位控制单元调节后使得注入到高功率微波一维波束可扫直线阵列的微波形成沿y轴方向的等差相位分布,相邻行的高功率微波一维波束可扫直线阵列的注入相位差为

Figure GDA0002444055660000092
辐射单元的螺旋线内导体经过M个螺旋线内导体驱动控制单元调节后,沿x轴方向形成梯度相位差分布,相邻列的相位差为
Figure GDA0002444055660000093
微波中剩余的少部分能量被匹配负载吸收,整个天线工作在行波状态。每个控制单元对应由一个步进电机驱动,因此该高功率微波空间波束可扫平面阵列天线所需的步进电机数目为M+N。最大波束指向与
Figure GDA0002444055660000094
Figure GDA0002444055660000095
有关:Therefore, the high-power microwaves are injected with equal amplitude and equal phase from the first to the Nth first to Nth first phase shifters based on the rectangular waveguide narrow-side slot bridge to the N ports of the first phase shifter. The phase control unit of the rotary adjustable phase shifter of the side-slot bridge is adjusted so that the microwave injected into the high-power microwave one-dimensional beam-sweepable linear array forms an equidistant phase distribution along the y-axis direction. The injection phase difference of the dimensional beam scannable linear array is
Figure GDA0002444055660000092
After the inner conductor of the helix of the radiation unit is adjusted by the M driving control units of the inner conductor of the helix, a gradient phase difference distribution is formed along the x-axis direction, and the phase difference of the adjacent columns is
Figure GDA0002444055660000093
A small part of the energy remaining in the microwave is absorbed by the matching load, and the entire antenna works in a traveling wave state. Each control unit is correspondingly driven by a stepping motor, so the number of stepping motors required by the high-power microwave space beam swept planar array antenna is M+N. Maximum beam pointing and
Figure GDA0002444055660000094
and
Figure GDA0002444055660000095
related:

Figure GDA0002444055660000091
Figure GDA0002444055660000091

其中ρ为辐射主波束与高功率微波空间波束可扫平面阵列天线口面法向(即z轴)的夹角,

Figure GDA0002444055660000096
为主波束在x-o-y平面投影与x轴夹角,β为高功率微波一维波束可扫直线阵列矩形波导中的波导传播常数,k为自由空间波数。通过步进电机调整
Figure GDA0002444055660000101
Figure GDA0002444055660000102
即可实现空间波束扫描。where ρ is the angle between the main radiating beam and the normal direction (ie, the z-axis) of the swept planar array antenna of the high-power microwave space beam,
Figure GDA0002444055660000096
is the angle between the projection of the main beam on the xoy plane and the x-axis, β is the waveguide propagation constant of the high-power microwave one-dimensional beam sweepable linear array rectangular waveguide, and k is the free-space wave number. Adjusted by stepper motor
Figure GDA0002444055660000101
and
Figure GDA0002444055660000102
Spatial beam scanning can be achieved.

与现有技术相比,采用本发明可以达到以下技术效果:Compared with the prior art, the following technical effects can be achieved by adopting the present invention:

1)、采用阵列天线的形式,天线口面为平面,便于共形设计,由高功率微波一维波束可扫直线阵列天线的设计可知,天线口面电场幅度容易控制,具有较高的口面效率;1) In the form of an array antenna, the antenna surface is flat, which is convenient for conformal design. From the design of a high-power microwave one-dimensional beam swept linear array antenna, it can be seen that the electric field amplitude of the antenna surface is easy to control and has a higher surface. efficiency;

2)、采用整路整列控制阵列相位的方式,使得所需的控制电机的数量由传统的相控阵天线的M×N缩减到M+N,大大降低了天线的制造成本。2) Using the method of controlling the phase of the array in the whole way and in the whole column, the number of required control motors is reduced from M×N of the traditional phased array antenna to M+N, which greatly reduces the manufacturing cost of the antenna.

附图说明Description of drawings

图1为本发明总体系统示意图;Fig. 1 is the overall system schematic diagram of the present invention;

图2为本发明一单路直线阵列结构示意图;2 is a schematic structural diagram of a single-channel linear array of the present invention;

图3为本发明的基于矩形波导窄边缝隙电桥的旋转调节式移相器整体结构示意图;3 is a schematic diagram of the overall structure of a rotary adjustable phase shifter based on a rectangular waveguide narrow-side slot bridge according to the present invention;

图4为本发明的基于矩形波导窄边缝隙电桥的旋转调节式移相器的矩形波导窄边缝隙电桥结构示意图;4 is a schematic structural diagram of a rectangular waveguide narrow-side slot bridge based on a rotary-adjustable phase shifter based on a rectangular waveguide narrow-side slot bridge of the present invention;

图5本发明的基于矩形波导窄边缝隙电桥的旋转调节式移相器的矩形波导窄边缝隙电桥剖面结构正视图;5 is a front view of the cross-sectional structure of the rectangular waveguide narrow-side slot bridge of the rotary-adjustable phase shifter based on the rectangular waveguide narrow-side slot bridge of the present invention;

图6为本发明的基于矩形波导窄边缝隙电桥的旋转调节式移相器的线转圆极化器结构示意图;6 is a schematic structural diagram of a linear-to-circular polarizer of a rotary-adjustable phase shifter based on a rectangular waveguide narrow-side slot bridge according to the present invention;

图7为本发明的基于矩形波导窄边缝隙电桥的旋转调节式移相器的波导脊形状示意图;7 is a schematic diagram of the shape of the waveguide ridge of the rotary adjustable phase shifter based on the rectangular waveguide narrow-side slot bridge of the present invention;

图8为本发明的基于矩形波导窄边缝隙电桥的旋转调节式移相器的旋转关节结构示意图;FIG. 8 is a schematic structural diagram of a rotary joint of a rotary adjustable phase shifter based on a rectangular waveguide narrow-side slot bridge according to the present invention;

图9为本发明的基于矩形波导窄边缝隙电桥的旋转调节式移相器的旋转关节工作条件的初始状态示意图;Fig. 9 is the initial state schematic diagram of the working condition of the rotary joint of the rotary adjustable phase shifter based on the rectangular waveguide narrow-side slot bridge of the present invention;

图10为本发明连接波导结构示意图;FIG. 10 is a schematic diagram of the connecting waveguide structure of the present invention;

图11为本发明的高功率微波一维波束可扫直线阵列的整体结构断裂示图;FIG. 11 is a schematic diagram of the overall structure of the high-power microwave one-dimensional beam scannable linear array of the present invention;

图12为本发明的高功率微波一维波束可扫直线阵列的矩形波导的结构示意图。图2(a)是矩形波导的左视图,图2(b)是矩形波导的俯视图,图2(c)是矩形波导的仰视图;FIG. 12 is a schematic structural diagram of the rectangular waveguide of the high-power microwave one-dimensional beam sweepable linear array of the present invention. Fig. 2(a) is a left side view of the rectangular waveguide, Fig. 2(b) is a top view of the rectangular waveguide, and Fig. 2(c) is a bottom view of the rectangular waveguide;

图13为本发明的高功率微波一维波束可扫直线阵列的第m辐射单元结构示意图;13 is a schematic structural diagram of the mth radiation unit of the high-power microwave one-dimensional beam scannable linear array of the present invention;

图14为本发明的高功率微波一维波束可扫直线阵列的第m螺旋线内导体结构示意图,图4(a)是第m螺旋线内导体的正视图,图4(b)是第m螺旋线内导体的俯视图;14 is a schematic diagram of the structure of the inner conductor of the m-th helix of the high-power microwave one-dimensional beam scannable linear array of the present invention, FIG. 4(a) is a front view of the inner conductor of the m-th helix, and FIG. 4(b) is the m-th helix. Top view of the inner conductor of the helix;

图15为本发明的高功率微波一维波束可扫直线阵列的第m耦合腔结构示意图,图15(a)是第m耦合腔立体图,图15(b)是第m耦合腔沿图15(a)中的NN'轴的剖面视图,图15(c)是第m耦合腔沿图15(b)中BB'截面视图,图15(d)是第m耦合腔沿图51(b)中AA'截面视图;FIG. 15 is a schematic diagram of the structure of the m-th coupling cavity of the high-power microwave one-dimensional beam scannable linear array of the present invention, FIG. 15(a) is a perspective view of the m-th coupling cavity, and FIG. a) is a cross-sectional view of the NN' axis, Fig. 15(c) is a cross-sectional view of the m-th coupling cavity along BB' in Fig. 15(b), and Fig. 15(d) is a cross-sectional view of the m-th coupling cavity along Fig. 51(b) AA' section view;

图16为本发明移相器的输出相位调整原理示意图;FIG. 16 is a schematic diagram of the output phase adjustment principle of the phase shifter of the present invention;

图17为本发明螺旋线内导体相位调节原理示意图。FIG. 17 is a schematic diagram of the principle of phase adjustment of the inner conductor of the helix of the present invention.

具体实施方式Detailed ways

本发明高功率微波空间波束可扫平面阵列天线系统结构示意图如图1所示,本发明由五部分组成,它们分别是N(20<N<100)个基于矩形波导窄边缝隙电桥的旋转调节式移相器1,即第一基于矩形波导窄边缝隙电桥的旋转调节式移相器11,第二基于矩形波导窄边缝隙电桥的旋转调节式移相器12,第三基于矩形波导窄边缝隙电桥的旋转调节式移相器13,…第n(1≤n≤N)基于矩形波导窄边缝隙电桥的旋转调节式移相器1n,…第N基于矩形波导窄边缝隙电桥的旋转调节式移相器1N;N个连接波导2,即第一连接波导21,第二连接波导22,第三连接波导23,…第n连接波导2n,…第N连接波导2N;N路高功率微波一维波束可扫直线阵列3,即第一高功率微波一维波束可扫直线阵列31,第二高功率微波一维波束可扫直线阵列32,第三高功率微波一维波束可扫直线阵列33,…第n高功率微波一维波束可扫直线阵列3n,…第N高功率微波一维波束可扫直线阵列3N,(每路高功率微波一维波束可扫直线阵列的辐射单元数目为M—图1中用小圆表示,其中50<M<500,相邻辐射单元沿x轴方向的间距为d,第n路高功率微波一维波束可扫直线阵的辐射单元沿x轴方向依次为第n1辐射单元n1,第n2辐射单元n2,第n3辐射单元n3…第nm(1≤m≤M)辐射单元nm…第nM辐射单元nM。在x轴方向,第n1辐射单元n1到第nM辐射单元nM构成第n行辐射单元;在y轴方向,第1m辐射单元1m到第Nm辐射单元Nm构成第m列辐射单元);N个移相器相位控制单元4,即第一移相器相位控制单元41,第二移相器相位控制单元42,第三移相器相位控制单元43,…第n移相器相位控制单元4n,…第N移相器相位控制单元4N;M个高功率微波一维波束可扫直线阵列的螺旋线内导体的驱动控制单元5,即第一螺旋线内导体驱动控制单元51,第二螺旋线内导体驱动控制单元52,第三螺旋线内导体驱动控制单元53,…第m螺旋线内导体驱动控制单元5m,…第M螺旋线内导体驱动控制单元5M。(螺旋线内导体驱动控制单元在图1中用虚线表示,每一个螺旋线内导体驱动控制单元控制对应列的辐射单元,即第m螺旋线内导体驱动控制单元5m控制第m列辐射单元)。第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n与第n高功率微波一维波束可扫直线阵列3n由第n连接波导2n连接,三者一起沿x轴方向构成第n路直线阵列。N路直线阵列结构完全相同,平行地沿y轴在空间中排列构成平面阵列,相邻两路直线阵列在y轴方向的间距为s。第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n由第n移相器相位控制单元4n来调节输出相位。The schematic diagram of the structure of the high-power microwave space beam swept planar array antenna system of the present invention is shown in Figure 1. The present invention consists of five parts, which are N (20<N<100) rotations based on rectangular waveguide narrow-side slot bridges. Adjustable phase shifter 1, namely the first rotary adjustable phase shifter 11 based on rectangular waveguide narrow-side slot bridges, the second rotary adjustable phase shifter 12 based on rectangular waveguide narrow-side slot bridges, and the third based on rectangular Rotational Adjustable Phase Shifter for Waveguide Narrow Side Slot Bridge 13,...nth (1≤n≤N) Rotation Adjustable Phase Shifter 1n Based on Rectangular Waveguide Narrow Side Slot Bridge 1n,...Nth Rectangular Waveguide Narrow Side Based Rotational Adjustable Phase Shifter 1N of the Slot Bridge; N connecting waveguides 2, namely the first connecting waveguide 21, the second connecting waveguide 22, the third connecting waveguide 23,...the nth connecting waveguide 2n,...the Nth connecting waveguide 2N ; N high-power microwave one-dimensional beams can scan the linear array 3, that is, the first high-power microwave one-dimensional beam can scan the linear array 31, the second high-power microwave one-dimensional beam can scan the linear array 32, and the third high-power microwave one-dimensional beam can scan the linear array 32. One-dimensional beam scannable linear array 33, ... nth high-power microwave one-dimensional beam scannable linear array 3n, ... Nth high-power microwave one-dimensional beam scannable linear array 3N, (each high-power microwave one-dimensional beam scans a straight line The number of radiation elements of the array is M—represented by small circles in Figure 1, where 50<M<500, the spacing between adjacent radiation elements along the x-axis direction is d, and the nth high-power microwave one-dimensional beam can scan the linear array. The radiation units along the x-axis direction are the n1th radiation unit n1, the n2th radiation unit n2, the n3th radiation unit n3...the nm (1≤m≤M) radiation unit nm...the nMth radiation unit nM. In the x-axis direction, The n1th radiation unit n1 to the nMth radiation unit nM constitute the nth row radiation unit; in the y-axis direction, the 1mth radiation unit 1m to the Nmth radiation unit Nm constitute the mth column radiation unit); N phase shifter phase control units 4, that is, the first phase shifter phase control unit 41, the second phase shifter phase control unit 42, the third phase shifter phase control unit 43,...the nth phase shifter phase control unit 4n,...the Nth phase shifter Phase control unit 4N; drive control unit 5 for M high-power microwave one-dimensional beam sweepable linear arrays of helix inner conductors, namely first helix inner conductor drive control unit 51, second helix inner conductor drive control unit 52 , the third helix inner conductor drive control unit 53, ... the mth helix inner conductor drive control unit 5m, ... the Mth helix inner conductor drive control unit 5M. (The inner conductor drive control unit in the helix is represented by a dotted line in FIG. 1, each inner conductor drive control unit in the helix controls the radiation units in the corresponding column, that is, the mth inner conductor drive control unit 5m controls the mth column of radiation units) . The nth rotary-adjustable phase shifter 1n based on the narrow-side slot bridge of the rectangular waveguide and the nth high-power microwave one-dimensional beam scannable linear array 3n are connected by the nth connecting waveguide 2n, and the three together form the nth Road line array. The N-way linear arrays have exactly the same structure, and are arranged in parallel along the y-axis in space to form a plane array, and the distance between the adjacent two-way linear arrays in the y-axis direction is s. The output phase of the n-th rotary-adjustable phase shifter 1 n based on the rectangular waveguide narrow-side slot bridge is adjusted by the n-th phase shifter phase control unit 4 n.

图2为本发明高功率微波空间波束可扫平面阵列天线的第n路直线阵列沿y轴方向的正视图。微波由第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n的第一移相器端口1n1注入,第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n的第二移相器端口1n2与第n连接波导2n的输入端口相连。第n移相器相位控制单元4n与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n的第一旋转关节P22和第二旋转关节P32相连。第n连接波导2n的输出端口与第n高功率微波一维波束可扫直线阵列3n的输入端口3n1相连,第n高功率微波一维波束可扫直线阵列3n的第二端口3n2外接匹配负载。第n高功率微波一维波束可扫直线阵列3n的第m个辐射单元的螺旋线内导体3n3m与第m螺旋线内导体驱动控制单元5m相连,第1高功率微波一维波束可扫直线阵列31的第m个辐射单元1m的螺旋线内导体313m到第N高功率微波一维波束可扫直线阵列3N的第m个辐射单元Nm的螺旋线内导体3N3m定义为第m列螺旋线内导体。FIG. 2 is a front view of the nth linear array of the high-power microwave space beam swept planar array antenna along the y-axis direction of the present invention. The microwave is injected from the first phase shifter port 1n1 of the nth rotary adjustable phase shifter 1n based on the rectangular waveguide narrow-side slot bridge, and the nth of the rotary adjustable phase shifter 1n based on the rectangular waveguide narrow-side slot bridge is injected. The second phase shifter port 1n2 is connected to the input port of the nth connecting waveguide 2n. The nth phase shifter phase control unit 4n is connected to the first rotation joint P22 and the second rotation joint P32 of the nth rotation-adjustable phase shifter 1n based on the rectangular waveguide narrow-side slot bridge. The output port of the nth connecting waveguide 2n is connected to the input port 3n1 of the nth high-power microwave one-dimensional beam scannable linear array 3n, and the second port 3n2 of the nth high-power microwave one-dimensional beam scannable linear array 3n is connected to an external matching load. The spiral inner conductor 3n3m of the m-th radiating element of the n-th high-power microwave one-dimensional beam can scan the linear array 3n is connected to the m-th spiral inner conductor drive control unit 5m, and the first high-power microwave one-dimensional beam can scan the linear array The spiral inner conductor of the m-th radiation element 1m of 31 313m to the N-th high-power microwave one-dimensional beam-scannable linear array 3N The spiral inner conductor of the m-th radiation element Nm of 3N is defined as the m-th column spiral inner conductor 3N3m .

如图3所示,第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n由矩形波导窄边缝隙电桥P1、第一相位调节臂P2和第二相位调节臂P3构成。第一相位调节臂P2与矩形波导窄边缝隙电桥的第三电桥端口P13相连,第二相位调节臂P3与矩形波导窄边缝隙电桥P1的第四电桥端口P14相连。第一相位调节臂P2由第一线转圆极化器P21和第一旋转关节P22构成;第二相位调节臂P3由第二线转圆极化器P31和第二旋转关节P32构成。第一线转圆极化器P21和第二线转圆极化器P31结构完全相同;第一旋转关节P22和第二旋转关节P32结构完全相同。微波由矩形波导窄边缝隙电桥第一电桥端口P11注入,由矩形波导窄边缝隙电桥的第二电桥端口P12输出。As shown in FIG. 3 , the nth rotary-adjustable phase shifter 1 n based on a rectangular waveguide narrow-side slot bridge is composed of a rectangular waveguide narrow-side slot bridge P1 , a first phase adjustment arm P2 and a second phase adjustment arm P3 . The first phase adjusting arm P2 is connected to the third bridge port P13 of the rectangular waveguide narrow-side slot bridge, and the second phase adjusting arm P3 is connected to the fourth bridge port P14 of the rectangular waveguide narrow-side slot bridge P1. The first phase adjustment arm P2 is composed of a first linear circular polarizer P21 and a first rotary joint P22; the second phase adjustment arm P3 is composed of a second linear circular polarizer P31 and a second rotary joint P32. The structures of the first line-to-circular polarizer P21 and the second line-to-circular polarizer P31 are identical; the structures of the first rotary joint P22 and the second rotary joint P32 are identical. Microwaves are injected from the first bridge port P11 of the rectangular waveguide narrow-side slot bridge, and output from the second bridge port P12 of the rectangular waveguide narrow-side slot bridge.

沿图3中的x-o-z平面(NN'轴)截断,矩形波导窄边缝隙电桥P1结构如图4所示。矩形波导窄边缝隙电桥P1是由金属材料制成的空腔,金属壁厚为T(T>1.5mm)。矩形波导窄边缝隙电桥P1的第一电桥端口P11、第二电桥端口P12、第三电桥端口P13、第四电桥端口P14均为矩形波导,四个端口的矩形波导的内腔的宽边长度均为a,窄边长度均为b。Cut along the x-o-z plane (NN' axis) in Fig. 3, the structure of the rectangular waveguide narrow-side slot bridge P1 is shown in Fig. 4. The rectangular waveguide narrow-side slot bridge P1 is a cavity made of metal material, and the metal wall thickness is T (T>1.5mm). The first bridge port P11, the second bridge port P12, the third bridge port P13, and the fourth bridge port P14 of the narrow-side slot bridge P1 of the rectangular waveguide are all rectangular waveguides, and the inner cavity of the four-port rectangular waveguide The length of the broad side is a, and the length of the narrow side is b.

沿图3中的x-o-z平面(即MM'轴)剖开矩形波导窄边缝隙电桥,如图5所示。矩形波导窄边缝隙电桥P1由第一电桥端口P11、第二电桥端口P12、第三电桥端口P13、第四电桥端口P14四个端口,第一微波传输通道P15、第二微波传输通道P16、第三微波传输通道P18、第四微波传输通道P19四路微波传输通道,和中央耦合区P17构成。第一电桥端口P11与第一微波传输通道P15相通,第二电桥端口P12与第二微波传输通道P16相通,第一微波传输通道P15和第二微波传输通道P16均与中央耦合区P17相通,中央耦合区P17与第三微波传输通道P18和第四微波传输通道P19相通,第三微波传输通道P18与第三电桥端口P13相通,第四微波传输通道P19与第四电桥端口P14相通,第一微波传输通道P15和第二微波传输通道P16的两条轴线之间的垂直距离为h,中央耦合区P17的长度为L1',第三微波传输通道P18和第四微波传输通道P19均拐了90度弯,拐弯处倒圆角的内半径均为R1',拐弯处倒圆角的外半径为R2',R1'和R2'可通过电磁仿真软件优化得到,优化的目标是拐弯引起的反射为零。第三微波传输通道P18和第四微波传输通道P19的轴线的水平距离为L,要求2a<L<3a。The rectangular waveguide narrow-side slot bridge is cut along the xoz plane in FIG. 3 (ie, the MM' axis), as shown in FIG. 5 . The rectangular waveguide narrow-side slot bridge P1 consists of four ports: the first bridge port P11, the second bridge port P12, the third bridge port P13, the fourth bridge port P14, the first microwave transmission channel P15, the second microwave The transmission channel P16, the third microwave transmission channel P18, the fourth microwave transmission channel P19 are four microwave transmission channels, and the central coupling area P17 is formed. The first bridge port P11 communicates with the first microwave transmission channel P15, the second bridge port P12 communicates with the second microwave transmission channel P16, and both the first microwave transmission channel P15 and the second microwave transmission channel P16 communicate with the central coupling area P17 , the central coupling area P17 communicates with the third microwave transmission channel P18 and the fourth microwave transmission channel P19, the third microwave transmission channel P18 communicates with the third electric bridge port P13, and the fourth microwave transmission channel P19 communicates with the fourth electric bridge port P14 , the vertical distance between the two axes of the first microwave transmission channel P15 and the second microwave transmission channel P16 is h, the length of the central coupling region P17 is L 1 ′, the third microwave transmission channel P18 and the fourth microwave transmission channel P19 All turned 90 degrees, the inner radius of the rounded corners at the corners is R 1 ', and the outer radius of the rounded corners at the corners is R 2 ', R 1 ' and R 2 ' can be optimized by electromagnetic simulation software. The goal is to have zero reflections due to cornering. The horizontal distance between the axes of the third microwave transmission channel P18 and the fourth microwave transmission channel P19 is L, and it is required that 2a<L<3a.

如图6所示,第一线转圆极化器P21由注入端口P211,圆波导P212,第一波导脊P213,第二波导脊P214和末端端口P215组成。注入端口P211由金属封口,中心留有矩形缺口与矩形波导窄边缝隙电桥的第三电桥端口P13相连,矩形缺口宽边长度为a,窄边长度为b。圆波导P212的金属壁厚度为T,内圆直径为R'(λ0/2.61>R'>λ0/3.41)。第一波导脊P213与第二波导脊P214结构完全相同,两个波导脊关于z轴对称,PP'为连接两个波导脊脊腹面中心的线段,它表示两个波导脊之间的距离w(λ0/2.61>w>λ0/3.41,且w<R),PP'在x-o-y平面上的投影为OQ'(坐标原点位于注入端口211的中心),OQ'与x轴的夹角为α(α=45°)。末端端口P215与第一旋转关节P22相连。As shown in FIG. 6 , the first linear-to-circular polarizer P21 is composed of an injection port P211 , a circular waveguide P212 , a first waveguide ridge P213 , a second waveguide ridge P214 and an end port P215 . The injection port P211 is sealed by metal, and a rectangular gap is left in the center to connect with the third bridge port P13 of the rectangular waveguide narrow-side slot bridge. The length of the wide side of the rectangular gap is a, and the length of the narrow side is b. The thickness of the metal wall of the circular waveguide P212 is T, and the diameter of the inner circle is R' (λ 0 /2.61>R'>λ 0 /3.41). The structures of the first waveguide ridge P213 and the second waveguide ridge P214 are exactly the same. The two waveguide ridges are symmetrical about the z-axis. λ 0 /2.61>w>λ 0 /3.41, and w<R), the projection of PP' on the xoy plane is OQ' (the coordinate origin is located at the center of the injection port 211 ), and the angle between OQ' and the x-axis is α (α=45°). The end port P215 is connected to the first rotary joint P22.

如图7所示,第一波导脊P213与第二波导脊P214形状相同,形状像一个马鞍,波导脊的脊背的长度为d2,波导脊的脊腹长度为d1。第一波导脊P213和第二波导脊P214的背部(长度为d1)与圆波导P212内壁紧密接触。As shown in FIG. 7 , the first waveguide ridge P213 and the second waveguide ridge P214 have the same shape as a saddle, the length of the back of the waveguide ridge is d 2 , and the length of the belly of the waveguide ridge is d 1 . The backs (length d 1 ) of the first waveguide ridge P213 and the second waveguide ridge P214 are in close contact with the inner wall of the circular waveguide P212.

如图8所示,第一旋转关节P22由圆柱形底板P221和窄金属板P222构成,窄金属板P222焊接在圆柱形底板P221中央。圆柱形底板的半径为R0'(R0'=L/2),厚度为w1(w1>2mm)。窄金属板P222的长度为Ls(Ls=λ0/4,其中λ0为圆极化TE11模式在圆波导内传输的波导波长),宽度为R',厚度为w2(1mm<w2<4mm)。窄金属板P222沿z轴方向的两个侧面倒圆角,圆角半径为R'/2。窄金属板P222从第一线转圆极化器的末端端口P215插入第一线转圆极化器的圆波导212内,圆柱形底板P221将第一线转圆极化器的末端端口P215封口。第一旋转关节P22可绕对称轴(即z轴)旋转。As shown in FIG. 8 , the first rotary joint P22 is composed of a cylindrical bottom plate P221 and a narrow metal plate P222, and the narrow metal plate P222 is welded to the center of the cylindrical bottom plate P221. The cylindrical base plate has a radius R 0 ' (R 0 '=L/2) and a thickness w 1 (w 1 >2mm). The length of the narrow metal plate P222 is Ls (Ls=λ 0 /4, where λ 0 is the waveguide wavelength of the circularly polarized TE 11 mode propagating in the circular waveguide), the width is R', and the thickness is w 2 (1mm<w 2 <4mm). The two side surfaces of the narrow metal plate P222 along the z-axis direction are rounded with a corner radius of R'/2. The narrow metal plate P222 is inserted into the circular waveguide 212 of the first linear-to-circular polarizer from the end port P215 of the first linear-to-circular polarizer, and the cylindrical base plate P221 seals the end port P215 of the first linear-to-circular polarizer . The first rotation joint P22 is rotatable around the axis of symmetry (ie, the z-axis).

图9为基于矩形波导窄边缝隙电桥的旋转调节式移相器的旋转关节工作条件的初始状态示意图;图9(a)是图8中第一旋转关节P22的右视图,图9(b)是第二旋转关节P32的右视图。本发明的第一旋转关节P22和第二旋转关节P32在初始状态下,两块窄金属板之间存在一个夹角,夹角大小为γ。Figure 9 is a schematic diagram of the initial state of the working conditions of the rotary joint of the rotary adjustment type phase shifter based on the rectangular waveguide narrow-side slot bridge; Figure 9(a) is a right side view of the first rotary joint P22 in Figure 8, Figure 9(b ) is a right side view of the second rotary joint P32. In the initial state of the first rotary joint P22 and the second rotary joint P32 of the present invention, there is an included angle between the two narrow metal plates, and the size of the included angle is γ.

图10为本发明第n连接波导2n的放大结构示意图,第n连接波导2n的两端端口为矩形波导,第n连接波导输入端口2n1的外尺寸为a×b,与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第二移相器端口1n2相连,二者的波导尺寸相同,第n连接波导输出端口2n2的外尺寸为a2×b2,与第n高功率微波一维波束可扫直线阵列的输入端口3n1的尺寸相同。第n连接波导中央为连接两个端口的波导渐变过渡段,过渡段的长度为Lx,可通过电磁仿真软件(如CST Microwave Studio)优化得到,优化的目标是传输反射为零。过渡段的横截面保持为矩形,宽边尺寸由a过渡到a2,窄边尺寸由b过渡到b210 is an enlarged schematic view of the nth connecting waveguide 2n of the present invention, the ports at both ends of the nth connecting waveguide 2n are rectangular waveguides, the outer dimension of the input port 2n1 of the nth connecting waveguide is a×b, and the nth connecting waveguide is narrow based on the rectangular waveguide. The second phase shifter port 1n2 of the rotary adjustable phase shifter of the side-slot bridge is connected, and the waveguide size of the two is the same. The input ports 3n1 of the microwave one-dimensional beam scannable linear array have the same size. The center of the nth connecting waveguide is the gradual transition section of the waveguide connecting the two ports. The length of the transition section is L x , which can be optimized by electromagnetic simulation software (such as CST Microwave Studio). The optimization goal is zero transmission reflection. The cross-section of the transition section remains rectangular, the width of the broad side transitions from a to a 2 , and the size of the narrow side transitions from b to b 2 .

如图11所示,高功率微波一维波束可扫直线阵列3n是全金属结构,由两部分构成,第一部分是矩形波导L1,第二部分是辐射单元构成的一维直线阵列L2。微波由矩形波导的注入端L11注入,矩形波导的输出端L12外接匹配负载。一维直线阵列由M(一般而言:20<M<500)个辐射单元构成,相邻辐射单元间距为d(0.5λ<d<λ,其中λ为微波在自由空间的波长),沿x轴方向安装在矩形波导窄边上。辐射单元按矩形波导的注入端L11向输出端L12的方向依次为第一辐射单元L21,第二辐射单元L22,第三辐射单元L23,第四辐射单元L24,第五辐射单元L25…第m辐射单元L2m…第M-6辐射单元L2M-6…第M-4辐射单元L2M-4…第M-2辐射单元L2M-2,第M辐射单元L2M,其中1≤m≤M。As shown in FIG. 11 , the high-power microwave one-dimensional beam scannable linear array 3n is an all-metal structure and consists of two parts, the first part is a rectangular waveguide L1, and the second part is a one-dimensional linear array L2 composed of radiating elements. The microwave is injected by the injection end L11 of the rectangular waveguide, and the output end L12 of the rectangular waveguide is connected to a matching load. A one-dimensional linear array consists of M (generally: 20<M<500) radiation elements, and the spacing between adjacent radiation elements is d (0.5λ<d<λ, where λ is the wavelength of microwave in free space), along x The axial direction is installed on the narrow side of the rectangular waveguide. According to the direction from the injection end L11 of the rectangular waveguide to the output end L12, the radiation units are the first radiation unit L21, the second radiation unit L22, the third radiation unit L23, the fourth radiation unit L24, the fifth radiation unit L25...the mth radiation unit Units L2m...M-6th radiation unit L2M-6...M-4th radiation unit L2M-4...M-2th radiation unit L2M-2, Mth radiation unit L2M, where 1≤m≤M.

如图12所示,矩形波导L1的矩形截面的内尺寸宽边长度为a2,窄边长度为b2,矩形波导的四个侧面(即除注入端L11、输出端L12所在的面的另外四个面)金属壁厚均为T。矩形波导的第一侧面L13中央挖有M个圆形通孔,圆形通孔按矩形波导的注入端L11向输出端L12的方向依次为矩形波导第一侧面的第一圆形通孔L131,矩形波导第一侧面的第二圆形通孔L132,矩形波导第一侧面的第三圆形通孔L133…矩形波导第一侧面的第m圆形通孔L13m…矩形波导第一侧面的第M-2圆形通孔L13M-2,矩形波导第一侧面的第M-1圆形通孔L13M-1,矩形波导第一侧面的第M圆形通孔L13M。矩形波导第一侧面的第一圆形通孔L131到第M圆形通孔L13M的半径均为R1(R1<b2/2),矩形波导第一侧面的第一圆形通孔L131的圆心与注入端L11的距离为s0(s0>d/2),矩形波导第一侧面的第m圆形通孔L13m的圆心与注入端L11的距离为s0+(m-1)d,相邻的第一圆形通孔圆心间距为d。与矩形波导的第一侧面L13相对的矩形波导第二侧面L14中央挖有2M个圆形通孔,圆形通孔按矩形波导的注入端L11向输出端L12的方向依次为矩形波导第二侧面的第一圆形通孔L1411,矩形波导第二侧面的第二圆形通孔L1421,矩形波导第二侧面的第三圆形通孔L1412,矩形波导第二侧面的第四圆形通孔L1422…矩形波导第二侧面的第2m-1圆形通孔L141m,矩形波导第二侧面的第2m圆形通孔L142m,…矩形波导第二侧面的第2M-5圆形通孔L141M-2,矩形波导第二侧面的第2M-4圆形通孔L142M-2,矩形波导第二侧面的第2M-3圆形通孔L141M-1,矩形波导第二侧面的第2M-2圆形通孔L142M-1,矩形波导第二侧面第2M-1圆形通孔L141M,矩形波导第二侧面第2M圆形通孔L142M。矩形波导第二侧面的第1,3…2m-1…2M-1圆形通孔的半径均为R2,矩形波导第二侧面的第一圆形通孔的圆心与注入端L11的距离为s0,矩形波导第二侧面的第2m-1圆形通孔的圆心与注入端L11的距离为s0+(m-1)d;矩形波导第二侧面的第2m圆形通孔的半径为rm,矩形波导第二侧面的第二圆形通孔的圆心与注入端L11的距离为s1,矩形波导第二侧面的第2m圆形通孔的圆心与注入端L11的距离为sm,满足sm-s0-(m-1)d≈λ0/4,其中λ0为微波在矩形波导L1内传输的波导波长。As shown in FIG. 12 , the inner dimension of the rectangular cross-section of the rectangular waveguide L1 has a wide side length a 2 and a narrow side length b 2 . Four sides) the metal wall thickness is T. M circular through holes are dug in the center of the first side L13 of the rectangular waveguide, and the circular through holes are the first circular through holes L131 on the first side of the rectangular waveguide in the direction from the injection end L11 of the rectangular waveguide to the output end L12. The second circular through hole L132 on the first side of the rectangular waveguide, the third circular through hole L133 on the first side of the rectangular waveguide...the mth circular through hole L13m on the first side of the rectangular waveguide...the Mth circular through hole L13m on the first side of the rectangular waveguide -2 The circular through hole L13M-2, the M-1th circular through hole L13M-1 on the first side of the rectangular waveguide, and the M-th circular through hole L13M on the first side of the rectangular waveguide. The radii of the first circular through hole L131 on the first side of the rectangular waveguide to the M-th circular through hole L13M are all R 1 (R 1 <b 2 /2), and the first circular through hole L131 on the first side of the rectangular waveguide is The distance between the center of the circle and the injection end L11 is s 0 (s 0 >d/2), and the distance between the center of the m-th circular through hole L13m on the first side of the rectangular waveguide and the injection end L11 is s 0 +(m-1) d, the distance between the centers of adjacent first circular through holes is d. 2M circular through holes are dug in the center of the second side L14 of the rectangular waveguide opposite to the first side L13 of the rectangular waveguide. The first circular through hole L1411 of the rectangular waveguide, the second circular through hole L1421 of the second side of the rectangular waveguide, the third circular through hole L1412 of the second side of the rectangular waveguide, and the fourth circular through hole L1422 of the second side of the rectangular waveguide ...the 2m-1th circular through hole L141m on the second side of the rectangular waveguide, the 2mth circular through hole L142m on the second side of the rectangular waveguide, ...the 2M-5th circular through hole L141M-2 on the second side of the rectangular waveguide, The 2M-4 circular through hole L142M-2 on the second side of the rectangular waveguide, the 2M-3 circular through hole L141M-1 on the second side of the rectangular waveguide, and the 2M-2 circular through hole on the second side of the rectangular waveguide L142M-1, the 2M-1 circular through hole L141M on the second side of the rectangular waveguide, and the 2M circular through hole L142M on the second side of the rectangular waveguide. The radii of the first, 3...2m-1...2M-1 circular through holes on the second side of the rectangular waveguide are all R 2 , and the distance between the center of the first circular through hole on the second side of the rectangular waveguide and the injection end L11 is s 0 , the distance between the center of the 2m-1th circular through hole on the second side of the rectangular waveguide and the injection end L11 is s 0 +(m-1)d; the radius of the 2mth circular through hole on the second side of the rectangular waveguide is s 0 +(m-1)d; is r m , the distance between the center of the second circular through hole on the second side of the rectangular waveguide and the injection end L11 is s 1 , and the distance between the center of the 2mth circular through hole on the second side of the rectangular waveguide and the injection end L11 is s m , which satisfies s m -s 0 -(m-1)d≈λ 0 /4, where λ 0 is the waveguide wavelength for microwave transmission in the rectangular waveguide L1.

本发明的第一辐射单元L21,第二辐射单元L22,第三辐射单元L23…第m辐射单元2m…第M辐射单元2M的结构相同(均包含反射消除杆,螺旋线内导体和耦合腔三部分)。如图13所示,以第m辐射单元L2m为例,第m辐射单元L2m由第m反射消除杆L2m1,第m螺旋线内导体L2m2和第m耦合腔L2m3三部分组成。第m反射消除杆L2m1通过矩形波导第二侧面的第2m圆形通孔L142m完全插入矩形波导L1内,顶端与矩形波导第一侧面L13内壁接触;第m耦合腔L2m3一端由矩形波导第一侧面的第m圆形通孔L13m插入矩形波导L1以固定在矩形波导L1上;第m螺旋线内导体L2m2经过第m耦合腔插入矩形波导L1内,由矩形波导第二侧面的第2m-1圆形通孔L141m穿过矩形波导L1,外接步进电机,穿出矩形波导L1的长度为h'。The first radiating unit L21, the second radiating unit L22, the third radiating unit L23...the mth radiating unit 2m...the Mth radiating unit 2M of the present invention have the same structures (all include a reflection cancellation rod, a helix inner conductor and a coupling cavity three part). As shown in Fig. 13, taking the mth radiation unit L2m as an example, the mth radiation unit L2m consists of the mth reflection cancellation rod L2m1, the mth helix inner conductor L2m2 and the mth coupling cavity L2m3. The m-th reflection cancellation rod L2m1 is completely inserted into the rectangular waveguide L1 through the 2m-th circular through hole L142m on the second side of the rectangular waveguide, and the tip is in contact with the inner wall of the first side L13 of the rectangular waveguide; one end of the m-th coupling cavity L2m3 is connected by the first side of the rectangular waveguide. The mth circular through hole L13m is inserted into the rectangular waveguide L1 to be fixed on the rectangular waveguide L1; the mth helix inner conductor L2m2 is inserted into the rectangular waveguide L1 through the mth coupling cavity, and the 2m-1th circle on the second side of the rectangular waveguide is inserted into the rectangular waveguide L1 The shaped through hole L141m passes through the rectangular waveguide L1 and is connected to a stepping motor, and the length passing through the rectangular waveguide L1 is h'.

第m反射消除杆L2m1的形状为圆柱体,半径等于rm。第m反射消除杆L2m1通过矩形波导第二侧面的第2m圆形通孔L142m插入矩形波导L1内,一端顶在矩形波导第一侧面L13内壁,另一端嵌在矩形波导第二侧面的第2m圆形通孔L142m内,第一反射消除杆L211,第二反射消除杆L221,…,第m反射消除杆L2m1,…,第M反射消除杆L2M1的长度均为a2+T。The m-th reflection cancelling rod L2m1 is in the shape of a cylinder with a radius equal to r m . The m-th reflection cancellation rod L2m1 is inserted into the rectangular waveguide L1 through the 2m-th circular through hole L142m on the second side of the rectangular waveguide. In the through hole L142m, the lengths of the first reflection cancellation rod L211, the second reflection cancellation rod L221, ..., the mth reflection cancellation rod L2m1, ..., and the Mth reflection cancellation rod L2M1 are all a 2 +T.

如图14所示,第m螺旋线内导体L2m2由一段直圆柱体L2m21,一段与直圆柱体L2m21垂直的半圆环L2m22和一段螺旋线L2m23构成,直圆柱体L2m21是一根金属棒,直径为2R2,直圆柱体L2m21的长度为L1(L1长度约为两倍矩形波导宽边a2长度,直圆柱体L2m21的一端从矩形波导第二侧面的第2m-1圆形通孔L141m穿过矩形波导L1,外接步进电机。半圆环L2m22和螺旋线L2m23的总高度为L2;半圆环L2m22的圆环直径为L3/2,螺旋线L2m23为等螺旋半径等螺距的一段螺旋线,螺旋线L2m23的螺旋外直径为L3。半圆环L2m22的初始段切线与x轴的夹角为αm,αm代表第m螺旋线内导体L2m2的空间方位,在直线阵列中,相邻两个螺旋线内导体的空间方位角度差为一个常量P,即αmm-1=P,其中1<m≤M。上述结构参数L1,L2,和L3均由电磁仿真软件(如CST Microwave Studio)优化得到,优化的目标是螺旋线的辐射在轴向上的轴比为零,反射接近零。As shown in Figure 14, the inner conductor L2m2 of the mth helix is composed of a straight cylinder L2m21, a semicircle L2m22 perpendicular to the straight cylinder L2m21, and a helix L2m23. The straight cylinder L2m21 is a metal rod with a diameter of is 2R 2 , the length of the straight cylinder L2m21 is L 1 (the length of L 1 is about twice the length of the broad side a 2 of the rectangular waveguide, and one end of the straight cylinder L2m21 extends from the 2m-1 circular through hole on the second side of the rectangular waveguide. L141m passes through the rectangular waveguide L1 and is connected to a stepping motor. The total height of the semicircular ring L2m22 and the helix L2m23 is L2 ; The outer diameter of the helix L2m23 is L 3 . The angle between the initial segment tangent of the semicircular ring L2m22 and the x-axis is α m , where α m represents the spatial orientation of the conductor L2m2 in the mth helix. In the array, the spatial azimuth angle difference of the inner conductors of two adjacent spirals is a constant P, namely α mm-1 =P, where 1<m≤M. The above-mentioned structural parameters L 1 , L 2 , and L 3 are optimized by electromagnetic simulation software (such as CST Microwave Studio). The optimization goal is that the axial ratio of the radiation of the helix in the axial direction is zero, and the reflection is close to zero.

如图15(a)所示,第m耦合腔L2m3的外形一端为圆柱凸台L2m31,另一端为长方体L2m32,圆柱凸台的外半径为R1,凸台的高度为H1。沿图15(a)中的NN'截断,第m耦合腔L2m3的正视图如图15(b)所示。第m耦合腔L2m3的内部挖有四个不同形状的孔,从圆柱凸台L2m31向长方体2m32的方向依次为第一孔L2m33,第二孔L2m34,第三孔L2m35,第四孔L2m36,四个孔连通在一起构成微波传输的通道。沿图15(b)AA'方向截断,得到第一孔L2m33的截面俯视图如图15(d)所示,第一孔L2m33由内孔L2m331和外孔L2m332构成,两个孔的高度均为H1,内孔2m331截面形状为半径为R2的圆形,第m螺旋线内导体L2m2即通过内孔插入波导内,外孔L2m332近似半环形,内半径为R3,外半径为R4,外孔L2m332的圆心角为

Figure GDA0002444055660000161
外孔L2m332的对称轴CC'与x轴的夹角定义为耦合腔的旋转角,用θm表示。沿图15(b)BB'轴截断,得到第二孔L2m34的截面俯视图如图15(d)所示,第二孔L2m34的高度为H2-H1,第二孔L2m34的轮廓由两段弧线构成,尺寸较大的圆弧线的半径为R4,对应的圆心角为
Figure GDA0002444055660000163
尺寸较小弧线的半径为R5,对应的圆心角为
Figure GDA0002444055660000162
第二孔L2m34的对称轴DD'与x轴的夹角也为θm,第一耦合腔L213到第M耦合腔L2M3结构的尺寸除了耦合腔的旋转角θm不同外,其它结构尺寸均相同。第三孔L2m35的高度H3-H2,截面形状为圆形,圆形半径为R5。第四孔L2m36的高度H4-H3,截面形状为圆形,圆形半径为R6。As shown in Figure 15(a), the m-th coupling cavity L2m3 has a cylindrical boss L2m31 at one end and a rectangular parallelepiped L2m32 at the other end, the outer radius of the cylindrical boss is R 1 , and the height of the boss is H 1 . Cut along NN' in Fig. 15(a), the front view of the m-th coupling cavity L2m3 is shown in Fig. 15(b). Four holes of different shapes are dug inside the m-th coupling cavity L2m3. The direction from the cylindrical boss L2m31 to the cuboid 2m32 is the first hole L2m33, the second hole L2m34, the third hole L2m35, the fourth hole L2m36, and four holes. The holes are connected together to form a channel for microwave transmission. 15(b) AA', the cross-sectional top view of the first hole L2m33 is obtained as shown in Fig. 15(d). 1. The cross-sectional shape of the inner hole 2m331 is a circle with a radius of R 2. The inner conductor L2m2 of the m-th helix is inserted into the waveguide through the inner hole. The central angle of the outer hole L2m332 is
Figure GDA0002444055660000161
The angle between the symmetry axis CC' of the outer hole L2m332 and the x-axis is defined as the rotation angle of the coupling cavity, which is represented by θ m . 15(b) along the BB' axis, the cross-sectional top view of the second hole L2m34 is obtained as shown in FIG. 15(d). The arc is formed, the radius of the larger arc is R 4 , and the corresponding central angle is
Figure GDA0002444055660000163
The radius of the arc with the smaller size is R 5 , and the corresponding central angle is
Figure GDA0002444055660000162
The angle between the symmetry axis DD' of the second hole L2m34 and the x-axis is also θ m . The dimensions of the structures from the first coupling cavity L213 to the M-th coupling cavity L2M3 are the same except for the rotation angle θ m of the coupling cavity. . The height of the third hole L2m35 is H 3 -H 2 , the cross-sectional shape is a circle, and the circle radius is R 5 . The height of the fourth hole L2m36 is H 4 -H 3 , the cross-sectional shape is a circle, and the radius of the circle is R 6 .

图16为本发明的移相器相位调节原理示意图。第n移相器相位控制单元4n为一个可旋转的轴承,轴承外接步进电机,由步进电机驱动绕自身轴(即z轴)旋转。可旋转轴承与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n的第一旋转关节P22和第二旋转关节P32具有相同的外直径R'0,第n移相器相位控制单元4n与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n的第一旋转关节P22和第二旋转关节P32相连(三者通过外围的齿轮啮合)。第n移相器相位控制单元4n外接步进电机,绕z轴旋转,即带动第一旋转关节P22和第二旋转关节P32同步旋转。由基于矩形波导窄边缝隙电桥的旋转调节式移相器可知,第n移相器相位控制单元4n每旋转θn,同步地带动第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n的第一旋转关节P22和第二旋转关节P32绕相同方向旋转θn,因此移相器的输出相位改变2θn。高功率微波空间波束可扫平面阵列天线的工作状态要求相邻两路直线阵列的移相器的旋转角度差为一个常量,即

Figure GDA0002444055660000171
因此相邻两路直线阵列的馈入相位差也应为常量,即馈入相位差等于相邻两路直线阵列的移相器的旋转角度差:
Figure GDA0002444055660000172
FIG. 16 is a schematic diagram of the phase adjustment principle of the phase shifter of the present invention. The phase control unit 4n of the nth phase shifter is a rotatable bearing, the bearing is connected to a stepping motor, and is driven by the stepping motor to rotate around its own axis (ie, the z-axis). The rotatable bearing has the same outer diameter R' 0 as the first rotary joint P22 and the second rotary joint P32 of the nth rotary adjustable phase shifter 1n based on the narrow side slot bridge of the rectangular waveguide, and the nth phase shifter phase control The unit 4n is connected with the first rotation joint P22 and the second rotation joint P32 of the nth rotation-adjustable phase shifter 1n based on the narrow-side slot bridge of the rectangular waveguide (the three are meshed by peripheral gears). The nth phase shifter phase control unit 4n is externally connected to a stepping motor, and rotates around the z-axis, that is, drives the first rotating joint P22 and the second rotating joint P32 to rotate synchronously. It can be known from the rotationally adjustable phase shifter based on the rectangular waveguide narrow-side slot bridge that the nth phase shifter phase control unit 4n rotates θ n synchronously to drive the nth rotationally adjustable phase shifter based on the rectangular waveguide narrow-side slot bridge. The first rotary joint P22 and the second rotary joint P32 of the phaser 1n rotate in the same direction by θ n , so that the output phase of the phase shifter changes by 2θ n . The working state of the high-power microwave space beam swept planar array antenna requires that the rotation angle difference of the phase shifters of the two adjacent linear arrays be a constant, namely
Figure GDA0002444055660000171
Therefore, the feeding phase difference of the two adjacent linear arrays should also be constant, that is, the feeding phase difference is equal to the rotation angle difference of the phase shifters of the adjacent two linear arrays:
Figure GDA0002444055660000172

图17为本发明直线阵列的相位调节原理示意图。第m螺旋线内导体驱动控制单元5m由第m带齿轮的滑动平板5m2和N个带齿轮的轴承构成,N个带齿轮的轴承沿y轴方向依次为第m1轴承5m11,第m2轴承5m12,第m3轴承5m13…第mn轴承5m1n…第mN轴承5m1N,上述轴承沿y轴方向依次与第m列的N个辐射单元的螺旋线内导体(即螺旋线内导体313m到螺旋线内导体3N3m)紧密相连,轴承的旋转将带动螺旋线内导体跟着一起旋转。每一个轴承的外直径为r(d/2>r>R2),滑动平板和轴承的齿轮啮合在一起,轴承的齿轮与滑动平板的齿轮尺寸相同。第m螺旋线内导体驱动控制单元5m的一端5m3由步进电机驱动沿y轴方向移动hm,从而带动第m1轴承5m11到第Nm轴承5m1N都旋转2hm/r弧度,同时带动第m列螺旋线内导体的空间方位角旋转2hm/r弧度。在x轴方向上相邻螺旋线内导体驱动控制单元被外接步进电机驱动的长度差为一个常量Δh=hm-hm-1,因此在x轴方向相邻列螺旋线内导体的空间方位角差也为一个常量,设为

Figure GDA0002444055660000173
Figure GDA0002444055660000174
FIG. 17 is a schematic diagram of the phase adjustment principle of the linear array of the present invention. The m-th helical inner conductor drive control unit 5m is composed of the m-th geared sliding plate 5m2 and N geared bearings. The N geared bearings are the m1th bearing 5m11 and the m2th bearing 5m12 in sequence along the y-axis direction. The m3th bearing 5m13...the mnth bearing 5m1n...the mNth bearing 5m1N, the above bearings are sequentially connected to the helical inner conductors of the mth row of N radiation units along the y-axis direction (that is, the helical inner conductor 313m to the helical inner conductor 3N3m) Closely connected, the rotation of the bearing will drive the inner conductor of the helix to rotate along with it. The outer diameter of each bearing is r (d/2>r>R 2 ), the sliding plate and the gear of the bearing are meshed together, and the gear of the bearing is the same size as the gear of the sliding plate. One end 5m3 of the inner conductor drive control unit 5m of the mth helix is driven by the stepping motor to move h m along the y-axis direction, thereby driving the m1th bearing 5m11 to the Nmth bearing 5m1N to rotate by 2h m /r radians, and at the same time driving the mth row The spatial azimuth of the conductors in the helix is rotated by 2h m /r radians. In the x-axis direction, the length difference between the adjacent helix inner conductor drive control units driven by the external stepping motor is a constant Δh=h m -h m-1 , so the space of the conductors in the adjacent column helix in the x-axis direction The azimuth difference is also a constant, set to
Figure GDA0002444055660000173
Have
Figure GDA0002444055660000174

因此,高功率微波由第1到第N基于矩形波导窄边缝隙电桥的旋转调节式移相器11到1N的第一移相器端口等幅等相位地注入,经过N个基于矩形波导窄边缝隙电桥的旋转调节式移相器11到1N的相位控制单元41到4N调节后使得注入到高功率微波一维波束可扫直线阵列的微波形成沿y轴方向的等差相位分布,相邻行的高功率微波一维波束可扫直线阵列的注入相位差为

Figure GDA00024440556600001715
辐射单元的螺旋线内导体经过M个螺旋线内导体驱动控制单元调节后,沿x轴方向形成梯度相位差分布,相邻列的相位差为
Figure GDA0002444055660000175
微波中剩余的少部分能量被匹配负载吸收,整个天线工作在行波状态。每个控制单元对应由一个步进电机驱动,因此该高功率微波空间波束可扫平面阵列天线所需的步进电机数目为M+N。增益最大波束指向
Figure GDA0002444055660000176
Figure GDA0002444055660000177
Figure GDA0002444055660000178
有关。(参考公式(7))Therefore, high-power microwaves are injected with equal amplitude and equal phase from the first to Nth first to Nth first phase shifter ports of the rotary adjustable phase shifters 11 to 1N based on rectangular waveguide narrow-side slot bridges. The phase control units 41 to 4N of the rotary adjustable phase shifters 11 to 1N of the side-slot bridge are adjusted so that the microwaves injected into the high-power microwave one-dimensional beam-sweepable linear array form an equidistant phase distribution along the y-axis direction. The injection phase difference of the high-power microwave one-dimensional beam scannable linear array in the adjacent row is
Figure GDA00024440556600001715
After the inner conductor of the helix of the radiation unit is adjusted by the M driving control units of the inner conductor of the helix, a gradient phase difference distribution is formed along the x-axis direction, and the phase difference of the adjacent columns is
Figure GDA0002444055660000175
A small part of the energy remaining in the microwave is absorbed by the matching load, and the entire antenna works in a traveling wave state. Each control unit is correspondingly driven by a stepping motor, so the number of stepping motors required by the high-power microwave space beam swept planar array antenna is M+N. Gain maximum beam pointing
Figure GDA0002444055660000176
and
Figure GDA0002444055660000177
and
Figure GDA0002444055660000178
related. (Refer to formula (7))

其中ρ为辐射主波束与高功率微波空间波束可扫平面阵列天线口面法向(即z轴)的夹角,

Figure GDA0002444055660000179
为主波束在x-o-y平面投影与x轴夹角,β为高功率微波一维波束可扫直线阵列矩形波导中的波导传播常数,k为自由空间波数。因此在波束扫描的过程中需要波束指向某一空间方位
Figure GDA00024440556600001710
时,通过(7)式即可算出
Figure GDA00024440556600001711
Figure GDA00024440556600001712
进而根据
Figure GDA00024440556600001713
Figure GDA00024440556600001714
计算得到移相器和螺旋线内导体的工作状态,通过步进电机调整实现上述状态后,即可引导波束指向所需要的角度,此即为波束扫描的原理。where ρ is the angle between the main radiating beam and the normal direction (ie, the z-axis) of the swept planar array antenna of the high-power microwave space beam,
Figure GDA0002444055660000179
is the angle between the projection of the main beam on the xoy plane and the x-axis, β is the waveguide propagation constant of the high-power microwave one-dimensional beam sweepable linear array rectangular waveguide, and k is the free-space wave number. Therefore, in the process of beam scanning, the beam needs to be pointed to a certain spatial orientation
Figure GDA00024440556600001710
, it can be calculated by formula (7)
Figure GDA00024440556600001711
and
Figure GDA00024440556600001712
and then according to
Figure GDA00024440556600001713
and
Figure GDA00024440556600001714
The working state of the phase shifter and the inner conductor of the helix is obtained by calculation. After the above state is achieved by adjusting the stepper motor, the beam can be directed to the required angle, which is the principle of beam scanning.

下面以工作在X波段中心频点8.4GHz的系统为例,基于矩形波导窄边缝隙电桥的旋转调节式移相器的输出矩形波导尺寸为a=24mm,b=12mm,高功率微波一维波束可扫直线阵列天线的矩形波导的尺寸为a2=30mm,b2=15mm。相邻辐射单元在x轴方向的间距为d=0.63λ=22.5mm,相邻两路直线阵列在y轴方向上间距也为s=0.63λ=22.5mm时,

Figure GDA0002444055660000181
Figure GDA0002444055660000182
可由步进电机驱动在0到360度变化,根据(4)式可计算得到波束扫描范围,在x-o-z和y-o-z平面上最大波束指向均达到±35°。Taking the system operating at the center frequency of X-band at 8.4GHz as an example, the output rectangular waveguide of the rotary adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide is a=24mm, b=12mm, and the high-power microwave one-dimensional The dimensions of the rectangular waveguide of the beam-scannable linear array antenna are a 2 =30mm, b 2 =15mm. When the spacing between adjacent radiating elements in the x-axis direction is d=0.63λ=22.5mm, and the spacing between two adjacent linear arrays in the y-axis direction is also s=0.63λ=22.5mm,
Figure GDA0002444055660000181
and
Figure GDA0002444055660000182
It can be driven by a stepping motor to change from 0 to 360 degrees. According to the formula (4), the beam scanning range can be calculated, and the maximum beam pointing on the xoz and yoz planes can reach ±35°.

Claims (15)

1.一种高功率微波空间波束可扫平面阵列天线,其特征在于高功率微波空间波束可扫平面阵列天线由五部分组成,它们分别是N个基于矩形波导窄边缝隙电桥的旋转调节式移相器,即第一基于矩形波导窄边缝隙电桥的旋转调节式移相器(11),第二基于矩形波导窄边缝隙电桥的旋转调节式移相器(12),第三基于矩形波导窄边缝隙电桥的旋转调节式移相器(13),…第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n),…第N基于矩形波导窄边缝隙电桥的旋转调节式移相器(1N);N个连接波导,即第一连接波导(21),第二连接波导(22),第三连接波导(23),…第n连接波导(2n),…第N连接波导(2N);N路高功率微波一维波束可扫直线阵列,即第一高功率微波一维波束可扫直线阵列(31),第二高功率微波一维波束可扫直线阵列(32),第三高功率微波一维波束可扫直线阵列(33),…第n高功率微波一维波束可扫直线阵列(3n),…第N高功率微波一维波束可扫直线阵列(3N),每路高功率微波一维波束可扫直线阵列的辐射单元数目为M,相邻辐射单元沿x轴方向的间距为d,第n路高功率微波一维波束可扫直线阵的辐射单元沿x轴方向依次为第n1辐射单元,第n2辐射单元,第n3辐射单元…第nm辐射单元…第nM辐射单元;在x轴方向,第n1辐射单元到第nM辐射单元)构成第n行辐射单元;在y轴方向,第1m辐射单元到第Nm辐射单元构成第m列辐射单元;N个移相器相位控制单元,即第一移相器相位控制单元(41),第二移相器相位控制单元(42),第三移相器相位控制单元(43),…第n移相器相位控制单元(4n),…第N移相器相位控制单元(4N);M个高功率微波一维波束可扫直线阵列的螺旋线内导体的驱动控制单元,即第一螺旋线内导体驱动控制单元(51),第二螺旋线内导体驱动控制单元(52),第三螺旋线内导体驱动控制单元(53),…第m螺旋线内导体驱动控制单元(5m),…第M螺旋线内导体驱动控制单元(5M),第m螺旋线内导体驱动控制单元(5m)控制第m列辐射单元;第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n)与第n高功率微波一维波束可扫直线阵列(3n)由第n连接波导(2n)连接,三者一起沿x轴方向构成第n路直线阵列;N路直线阵列结构完全相同,平行地沿y轴在空间中排列构成平面阵列,相邻两路直线阵列在y轴方向的间距为s;第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n)由第n移相器相位控制单元(4n)来调节输出相位;其中1≤n≤N,1≤m≤M,N和M均为正整数;第n行的螺旋线内导体依次为第n行第一螺旋线内导体(3n31)…第n行第m螺旋线内导体(3n3m)…第n行第M螺旋线内导体(3n3M);第m列螺旋线内导体依次为第m列第1螺旋线内导体(313m),第m列第2螺旋线内导体(323m)…第m列第n螺旋线内导体(3n3m)…第m列第N螺旋线内导体(3N3m);1. A high-power microwave space beam swept planar array antenna is characterized in that the high-power microwave space beam swept planar array antenna is made up of five parts, and they are respectively N based on the rotary adjustment type of the rectangular waveguide narrow-side slot bridge. Phase shifters, namely, a first rotary-adjustable phase shifter (11) based on a rectangular waveguide narrow-side slot bridge, a second rotary-adjustable phase shifter (12) based on a rectangular waveguide narrow-side slot bridge, and a third based on Rotational Adjustable Phase Shifter for Rectangular Waveguide Narrow Side Slot Bridge Rotationally adjustable phase shifter of the bridge (1N); N connection waveguides, namely the first connection waveguide (21), the second connection waveguide (22), the third connection waveguide (23), ... the nth connection waveguide (2n) , ... Nth connecting waveguide (2N); N high-power microwave one-dimensional beams can scan a linear array, that is, the first high-power microwave one-dimensional beam can scan a linear array (31), and the second high-power microwave one-dimensional beam can scan Linear array (32), third high-power microwave one-dimensional beam scannable linear array (33), ... nth high-power microwave one-dimensional beam scannable linear array (3n), ... Nth high-power microwave one-dimensional beam scannable linear array (3n) Linear array (3N), the number of radiation elements of the linear array that can be scanned by each high-power microwave one-dimensional beam is M, the distance between adjacent radiation elements along the x-axis direction is d, and the nth high-power microwave one-dimensional beam can scan a straight line The radiation units of the array are sequentially the n1th radiation unit, the n2th radiation unit, the n3th radiation unit...the nmth radiation unit...the nMth radiation unit along the x-axis direction; in the x-axis direction, the n1th radiation unit to the nMth radiation unit) constitute the nth row of radiation units; in the y-axis direction, the mth radiation unit to the Nmth radiation unit constitute the mth column of radiation units; N phase shifter phase control units, namely the first phase shifter phase control unit (41), The second phase shifter phase control unit (42), the third phase shifter phase control unit (43),...the nth phase shifter phase control unit (4n),...the Nth phase shifter phase control unit (4N); The drive control units for the inner conductors of the spirals of the M high-power microwave one-dimensional beam scannable linear arrays, namely the first spiral inner conductor drive control unit (51), the second spiral inner conductor drive control unit (52), the first spiral inner conductor drive control unit (52), Triple helix inner conductor drive control unit (53), ... mth helix inner conductor drive control unit (5m), ... Mth helix inner conductor drive control unit (5M), mth helix inner conductor drive control unit ( 5m) Control the m-th row of radiation units; the n-th rotary-adjustable phase shifter based on the narrow-side slot bridge of the rectangular waveguide (1n) and the n-th high-power microwave one-dimensional beam-scannable linear array (3n) are connected by the n-th waveguide (2n) connected, the three together form the nth linear array along the x-axis direction; the N-channel linear arrays have exactly the same structure, and are arranged in parallel along the y-axis in space to form a plane array, and the two adjacent linear arrays are in the y-axis direction. The spacing is s; the nth is based on the rotational adjustment of the narrow-side slot bridge of the rectangular waveguide. The segmental phase shifter (1n) is adjusted by the nth phase shifter phase control unit (4n) to adjust the output phase; wherein 1≤n≤N, 1≤m≤M, N and M are both positive integers; The inner conductor of the spiral is the first spiral inner conductor of the nth row (3n31)…the nth row of the mth spiral inner conductor (3n3m)…the nth row of the Mth spiral inner conductor (3n3M); the mth column of the spiral The inner conductors are the first spiral inner conductor (313m) in the mth column, the second spiral inner conductor in the mth column (323m)...the mth column and the nth spiral inner conductor (3n3m)...the mth column Nth spiral Inner conductor (3N3m); 微波由第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n)的第一移相器端口(1n1)注入,第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n)的第二移相器端口(1n2)与第n连接波导(2n)的输入端口(2n1)相连;第n移相器相位控制单元(4n)与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n)的第一旋转关节(P22)和第二旋转关节(P32)相连;第n连接波导(2n)的输出端口(2n2)与第n高功率微波一维波束可扫直线阵列(3n)的输入端口(3n1)相连,第n高功率微波一维波束可扫直线阵列(3n)的第二端口(3n2)外接匹配负载;第n高功率微波一维波束可扫直线阵列(3n)的第m个辐射单元的螺旋线内导体(3n3m)与第m螺旋线内导体驱动控制单元(5m)相连,第1高功率微波一维波束可扫直线阵列(31)的第m个辐射单元(1m)的螺旋线内导体(313m)到第N高功率微波一维波束可扫直线阵列(3N)的第m个辐射单元(Nm)的螺旋线内导体(3N3m)定义为第m列螺旋线内导体;Microwaves are injected from the first phase shifter port (1n1) of the nth rotary-adjustable phase shifter (1n) based on the rectangular waveguide narrow-side slot bridge, and the n-th rotary-adjustable phase shifter based on the rectangular-waveguide narrow-side slot bridge The second phase shifter port (1n2) of the device (1n) is connected to the input port (2n1) of the nth connecting waveguide (2n); The first rotary joint (P22) of the rotary adjustable phase shifter (1n) of the electric bridge is connected with the second rotary joint (P32); the output port (2n2) of the nth connection waveguide (2n) is connected with the nth high-power microwave one. The input port (3n1) of the 2D beam scannable linear array (3n) is connected, and the second port (3n2) of the nth high-power microwave one-dimensional beam scannable linear array (3n) is connected to an external matching load; the nth high-power microwave one-dimensional The helix inner conductor (3n3m) of the mth radiating element of the beam scannable linear array (3n) is connected to the mth helix inner conductor drive control unit (5m), and the first high-power microwave one-dimensional beam scannable linear array ( 31) The inner conductor of the helix (313m) of the mth radiation element (1m) to the inner conductor of the helix of the mth radiation element (Nm) of the Nth high-power microwave one-dimensional beam scannable linear array (3N) ( 3N3m) is defined as the inner conductor of the m-th column spiral; 第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n)由矩形波导窄边缝隙电桥(P1)、第一相位调节臂(P2)和第二相位调节臂(P3)构成;第一相位调节臂(P2)与矩形波导窄边缝隙电桥的第三电桥端口(P13)相连,第二相位调节臂(P3)与矩形波导窄边缝隙电桥(P1)的第四电桥端口(P14)相连;第一相位调节臂(P2)由第一线转圆极化器(P21)和第一旋转关节(P22)构成;第二相位调节臂(P3)由第二线转圆极化器(P31)和第二旋转关节(P32)构成;第一线转圆极化器(P21)和第二线转圆极化器(P31)结构完全相同,第一旋转关节(P22)和第二旋转关节(P32)结构完全相同;微波由矩形波导窄边缝隙电桥第一电桥端口(P11)注入,由矩形波导窄边缝隙电桥的第二电桥端口(P12)输出;The nth rotary-adjustable phase shifter (1n) based on a rectangular waveguide narrow-side slot bridge is composed of a rectangular waveguide narrow-side slot bridge (P1), a first phase adjustment arm (P2) and a second phase adjustment arm (P3) ; The first phase adjustment arm (P2) is connected to the third bridge port (P13) of the rectangular waveguide narrow-side slot bridge, and the second phase adjustment arm (P3) is connected to the fourth of the rectangular waveguide narrow-side slot bridge (P1). The bridge port (P14) is connected; the first phase adjustment arm (P2) is composed of the first wire-rotating circular polarizer (P21) and the first rotary joint (P22); the second phase-adjusting arm (P3) is formed by the second wire-rotating The circular polarizer (P31) and the second rotary joint (P32) are composed; the first wire-to-circular polarizer (P21) and the second wire-to-circular polarizer (P31) have the same structure, and the first rotary joint (P22) The structure is exactly the same as that of the second rotary joint (P32); microwaves are injected from the first bridge port (P11) of the rectangular waveguide narrow-side slot bridge, and output from the second bridge port (P12) of the rectangular waveguide narrow-side slot bridge; 矩形波导窄边缝隙电桥(P1)是由金属材料制成的空腔,由矩形波导窄边缝隙电桥第一电桥端口(P11)(P11)、第二电桥端口(P12)、第三电桥端口(P13)、第四电桥端口(P14)四个端口,第一微波传输通道(P15)、第二微波传输通道(P16)、第三微波传输通道(P18)、第四微波传输通道(P19)四路微波传输通道、中央耦合区(P17)构成;矩形波导窄边缝隙电桥第一电桥端口(P11)(P11)、第二电桥端口(P12)、第三电桥端口(P13)、第四电桥端口(P14)均为矩形波导,四个端口的矩形波导的内腔的宽边长度均为a,窄边长度均为b;第一微波传输通道(P15)和第二微波传输通道(P16)的两条轴线之间的垂直距离为h,中央耦合区(P17)的长度为L1',第三微波传输通道(P18)和第四微波传输通道(P19)的轴线的水平距离为L;The rectangular waveguide narrow-side slot bridge (P1) is a cavity made of metal material. Three bridge ports (P13), fourth bridge ports (P14) four ports, the first microwave transmission channel (P15), the second microwave transmission channel (P16), the third microwave transmission channel (P18), the fourth microwave transmission channel The transmission channel (P19) consists of four microwave transmission channels and the central coupling area (P17); the rectangular waveguide narrow-side slot bridge is composed of the first bridge port (P11) (P11), the second bridge port (P12), and the third bridge port (P12). The bridge port (P13) and the fourth bridge port (P14) are both rectangular waveguides, and the length of the broad side of the inner cavity of the rectangular waveguide of the four ports is a, and the length of the narrow side is both b; the first microwave transmission channel (P15 ) and the vertical distance between the two axes of the second microwave transmission channel (P16) is h, the length of the central coupling region (P17) is L 1 ', the third microwave transmission channel (P18) and the fourth microwave transmission channel ( The horizontal distance of the axis of P19) is L; 第一线转圆极化器(P21)由注入端口(P211),圆波导(P212),第一波导脊(P213),第二波导脊(P214)和末端端口(P215)组成;注入端口(P211)由金属封口,中心留有矩形缺口与矩形波导窄边缝隙电桥的第三电桥端口(P13)相连,矩形缺口宽边长度为a,窄边长度为b;圆波导(P212)的内圆直径为R';第一波导脊(P213)与第二波导脊(P214)形状结构完全相同,两个波导脊关于z轴对称;末端端口(P215)与第一旋转关节(P22)相连;The first line-to-circular polarizer (P21) consists of an injection port (P211), a circular waveguide (P212), a first waveguide ridge (P213), a second waveguide ridge (P214) and an end port (P215); the injection port ( P211) is sealed by metal, and there is a rectangular gap in the center, which is connected to the third bridge port (P13) of the narrow-side slot bridge of the rectangular waveguide. The length of the wide side of the rectangular gap is a, and the length of the narrow side is b; The inner circle diameter is R'; the first waveguide ridge (P213) has the same shape and structure as the second waveguide ridge (P214), and the two waveguide ridges are symmetrical about the z-axis; the end port (P215) is connected to the first rotary joint (P22) ; 第一波导脊(P213)与第二波导脊(P214)形状像一个马鞍,波导脊的脊背的长度为d2,波导脊的脊腹长度为d1;第一波导脊(P213)和第二波导脊(P214)的背部与圆波导(P212)内壁接触;连接两个波导脊脊腹面中心的线段PP'在x-o-y平面上的投影OQ'与x轴的夹角为α=45°,坐标原点O位于注入端口(P211)的中心;The first waveguide ridge (P213) and the second waveguide ridge (P214) are shaped like a saddle, the length of the back of the waveguide ridge is d 2 , and the length of the belly of the waveguide ridge is d 1 ; the first waveguide ridge (P213) and the second The back of the waveguide ridge (P214) is in contact with the inner wall of the circular waveguide (P212); the angle between the projection OQ' of the line segment PP' connecting the centers of the ventral surfaces of the two waveguide ridge ridges on the xoy plane and the x-axis is α=45°, the origin of the coordinates O is located in the center of the injection port (P211); 第一旋转关节(P22)由圆柱形底板(P221)和窄金属板(P222)构成,窄金属板(P222)焊接在圆柱形底板(P221)中央;窄金属板(P222)从第一线转圆极化器的末端端口(P215)插入第一线转圆极化器的圆波导(P212)内,圆柱形底板(P221)将第一线转圆极化器的末端端口(P215)封口;第一旋转关节(P22)可绕对称轴即z轴旋转;The first rotary joint (P22) consists of a cylindrical base plate (P221) and a narrow metal plate (P222). The narrow metal plate (P222) is welded in the center of the cylindrical base plate (P221); The end port (P215) of the circular polarizer is inserted into the circular waveguide (P212) of the first linear-to-circular polarizer, and the cylindrical base plate (P221) seals the end port (P215) of the first linear-to-circular polarizer; The first rotary joint (P22) can rotate around the axis of symmetry, that is, the z-axis; 第一旋转关节(P22)和第二旋转关节(P32)在初始状态下,窄金属板(P222)和第二旋转关节(P32)的窄金属板之间存在一个夹角,此夹角命名为第一旋转关节(P22)和第二旋转关节(P32)的初始状态的角度差,大小为γ;In the initial state of the first rotary joint (P22) and the second rotary joint (P32), there is an included angle between the narrow metal plate (P222) and the narrow metal plate of the second rotary joint (P32), which is named as The angle difference between the initial states of the first rotary joint (P22) and the second rotary joint (P32), and the magnitude is γ; 第n连接波导(2n)的两端端口为矩形波导,第n连接波导输入端口2n1的外尺寸为a×b,与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器的第二移相器端口(1n2)相连,二者的波导尺寸相同,第n连接波导(2n)的输出端口(2n2)的外尺寸为a2×b2,与第n高功率微波一维波束可扫直线阵列的输入端口(3n1)的尺寸相同;The ports at both ends of the nth connecting waveguide (2n) are rectangular waveguides, the outer dimension of the input port 2n1 of the nth connecting waveguide is a × b, and the The two phase shifter ports (1n2) are connected, and the waveguide dimensions of the two are the same. The outer dimension of the output port (2n2) of the n-th connection waveguide (2n) is a 2 ×b 2 , which is compatible with the n-th high-power microwave one-dimensional beam. The input port (3n1) of the sweep line array has the same size; 高功率微波一维波束可扫直线阵列(3n)是全金属结构,由两部分构成,第一部分是矩形波导(L1),第二部分是辐射单元构成的一维直线阵列(L2);一维直线阵列由M个辐射单元构成,M为正整数,相邻辐射单元间距为d,沿x轴方向安装在矩形波导(L1)窄边上;M个辐射单元按矩形波导的注入端(L11)向输出端(L12)的方向依次为第一辐射单元(L21),第二辐射单元(L22),第三辐射单元(L23)…第m辐射单元(L2m)…第M辐射单元(L2M),其中1≤m≤M;The high-power microwave one-dimensional beam-scannable linear array (3n) is an all-metal structure and consists of two parts, the first part is a rectangular waveguide (L1), and the second part is a one-dimensional linear array (L2) composed of radiating elements; one-dimensional The linear array is composed of M radiating elements, M is a positive integer, and the distance between adjacent radiating elements is d, and is installed on the narrow side of the rectangular waveguide (L1) along the x-axis direction; The direction to the output end (L12) is the first radiation unit (L21), the second radiation unit (L22), the third radiation unit (L23)...the mth radiation unit (L2m)...the Mth radiation unit (L2M), where 1≤m≤M; 矩形波导(L1)的矩形截面的内尺寸宽边长度为a2,窄边长度为b2,矩形波导的四个侧面即除注入端(L11)、输出端(L12)所在的面的另外四个面壁厚均为T;矩形波导的第一侧面(L13)中央挖有M个圆形通孔,圆形通孔按矩形波导的注入端(L11)向输出端(L12)的方向依次为矩形波导第一侧面的第一圆形通孔(L131),矩形波导第一侧面的第二圆形通孔(L132),矩形波导第一侧面的第三圆形通孔(L133)…矩形波导第一侧面的第m圆形通孔(L13m)…矩形波导第一侧面的第M-2圆形通孔(L13M-2),矩形波导第一侧面的第M-1圆形通孔(L13M-1),矩形波导第一侧面的第M圆形通孔(L13M);矩形波导第一侧面的第一圆形通孔(L131)到第M圆形通孔(L13M)的半径均为R1,矩形波导第一侧面的第一圆形通孔(L131)的圆心与注入端(L11)的距离为s0,相邻的矩形波导第一侧面的第一圆形通孔圆心间距为d;与矩形波导的第一侧面(L13)相对的矩形波导第二侧面(L14)中央挖有2M个圆形通孔,圆形通孔按矩形波导的注入端(L11)向输出端(L12)的方向依次为矩形波导第二侧面的第一圆形通孔(L1411),矩形波导第二侧面的第二圆形通孔(L1421),矩形波导第二侧面的第三圆形通孔(L1412),矩形波导第二侧面的第四圆形通孔(L1422)…矩形波导第二侧面的第2m-1圆形通孔(L141m),矩形波导第二侧面的第2m圆形通孔(L142m)…矩形波导第二侧面的第2M-5圆形通孔(L141M-2),矩形波导第二侧面的第2M-4圆形通孔(L142M-2),矩形波导第二侧面的第2M-3圆形通孔(L141M-1),矩形波导第二侧面的第2M-2圆形通孔(L142M-1),矩形波导第二侧面第2M-1圆形通孔(L141M),矩形波导第二侧面第2M圆形通孔(L142M);矩形波导第二侧面的第1,3…2m-1…2M-1圆形通孔的半径均为R2,矩形波导第二侧面的第一圆形通孔(L1411)的圆心与注入端(L11)的距离为s0,矩形波导第二侧面的第2m-1圆形通孔(L141m)的圆心与注入端(L11)的距离为s0+(m-1)d;矩形波导第二侧面的第2m圆形通孔(L142m)的半径为rm,矩形波导第二侧面的第二圆形通孔(L1421)的圆心与注入端(L11)的距离为s1,矩形波导第二侧面的第2m圆形通孔(L142m)的圆心与注入端(L11)的距离为smThe inner dimension of the rectangular cross-section of the rectangular waveguide (L1) is a 2 , and the length of the narrow side is b 2 . The wall thickness of each surface is T; M circular through holes are dug in the center of the first side (L13) of the rectangular waveguide, and the circular through holes are rectangular in the direction from the injection end (L11) to the output end (L12) of the rectangular waveguide. The first circular through hole (L131) on the first side of the waveguide, the second circular through hole (L132) on the first side of the rectangular waveguide, the third circular through hole (L133) on the first side of the rectangular waveguide... The mth circular through hole on one side (L13m)...the M-2 circular through hole (L13M-2) on the first side of the rectangular waveguide, the M-1 circular through hole on the first side of the rectangular waveguide (L13M- 1), the Mth circular through hole (L13M) on the first side of the rectangular waveguide; the radii from the first circular through hole (L131) to the Mth circular through hole (L13M) on the first side of the rectangular waveguide are all R 1 , the distance between the center of the first circular through hole (L131) on the first side of the rectangular waveguide and the injection end (L11) is s 0 , and the distance between the centers of the first circular through holes on the first side of the adjacent rectangular waveguide is d; 2M circular through holes are dug in the center of the second side (L14) of the rectangular waveguide opposite to the first side (L13) of the rectangular waveguide. The directions are the first circular via (L1411) on the second side of the rectangular waveguide, the second circular via (L1421) on the second side of the rectangular waveguide, and the third circular via (L1412) on the second side of the rectangular waveguide , the fourth circular via (L1422) on the second side of the rectangular waveguide...the 2m-1 circular via (L141m) on the second side of the rectangular waveguide, the 2m-th circular via (L142m) on the second side of the rectangular waveguide …the 2M-5 circular via (L141M-2) on the second side of the rectangular waveguide, the 2M-4 circular via (L142M-2) on the second side of the rectangular waveguide, the 2M- 3 circular through holes (L141M-1), 2M-2 circular through holes on the second side of the rectangular waveguide (L142M-1), 2M-1 circular through holes on the second side of the rectangular waveguide (L141M), rectangular waveguides The 2M circular through hole (L142M) on the second side; the radii of the 1st, 3...2m-1...2M-1 circular through holes on the second side of the rectangular waveguide are all R 2 . The distance between the center of the circular through hole (L1411) and the injection end (L11) is s 0 , and the distance between the center of the circular through hole (L141m) on the second side of the rectangular waveguide and the injection end (L11) is s 0 +(m-1)d; the radius of the 2mth circular through hole (L142m) on the second side of the rectangular waveguide is r m , the center and injection end of the second circular through hole (L1421) on the second side of the rectangular waveguide (L11) with distance s 1 , rectangle The distance between the center of the 2mth circular through hole (L142m) on the second side of the waveguide and the injection end (L11) is s m ; 第一辐射单元(L21),第二辐射单元(L22),第三辐射单元(L23),第四辐射单元(L24),第五辐射单元(L25),…第m辐射单元(L2m)…第M-6辐射单元(L2M-6)…第M-4辐射单元(L2M-4)…第M-2辐射单元(L2M-2)…第M辐射单元(L2M)的结构相同;第m辐射单元(L2m)由第m反射消除杆(L2m1),第m螺旋线内导体(L2m2)和第m耦合腔(L2m3)三部分组成;第m反射消除杆(L2m1)通过矩形波导第二侧面的第2m圆形通孔(L142m)完全插入矩形波导(L1)内,顶端与矩形波导第一侧面(L13)内壁接触;第m耦合腔(L2m3)一端由矩形波导第一侧面的第m圆形通孔(L13m)插入矩形波导(L1)以固定在矩形波导(L1)上;第m螺旋线内导体(L2m2)经过第m耦合腔插入矩形波导(L1)内,由矩形波导第二侧面的第2m-1圆形通孔(L141m)穿过矩形波导(L1),外接步进电机,穿出矩形波导(L1)的长度为h';The first radiation unit (L21), the second radiation unit (L22), the third radiation unit (L23), the fourth radiation unit (L24), the fifth radiation unit (L25),...the mth radiation unit (L2m)...the M-6 radiation unit (L2M-6)...M-4th radiation unit (L2M-4)...M-2th radiation unit (L2M-2)...Mth radiation unit (L2M) has the same structure; mth radiation unit (L2m) consists of the mth reflection cancellation rod (L2m1), the mth helix inner conductor (L2m2) and the mth coupling cavity (L2m3); the mth reflection cancellation rod (L2m1) passes through the second side of the rectangular waveguide. The 2m circular through hole (L142m) is completely inserted into the rectangular waveguide (L1), and the top is in contact with the inner wall of the first side (L13) of the rectangular waveguide; one end of the m-th coupling cavity (L2m3) is connected by the m-th circular hole on the first side of the rectangular waveguide. The hole (L13m) is inserted into the rectangular waveguide (L1) to be fixed on the rectangular waveguide (L1); the m-th helix inner conductor (L2m2) is inserted into the rectangular waveguide (L1) through the m-th coupling cavity, and the m A 2m-1 circular through hole (L141m) passes through the rectangular waveguide (L1), an external stepping motor is connected, and the length passing through the rectangular waveguide (L1) is h'; 第m反射消除杆(L2m1)的形状为圆柱体,半径等于rm;第m反射消除杆(L2m1)通过矩形波导第二侧面的第2m圆形通孔(L142m)插入矩形波导(L1)内,一端顶在矩形波导第一侧面(L13)内壁,另一端嵌在矩形波导第二侧面的第2m圆形通孔(L142m)内;The mth reflection cancellation rod (L2m1) is in the shape of a cylinder with a radius equal to r m ; the mth reflection cancellation rod (L2m1) is inserted into the rectangular waveguide (L1) through the 2mth circular through hole (L142m) on the second side of the rectangular waveguide , one end is on the inner wall of the first side (L13) of the rectangular waveguide, and the other end is embedded in the 2mth circular through hole (L142m) on the second side of the rectangular waveguide; M个螺旋线内导体的结构完全相同;第m螺旋线内导体(L2m2)由一段直圆柱体(L2m21),一段与直圆柱体(L2m21)垂直的半圆环(L2m22)和一段螺旋线(L2m23)构成,直圆柱体(L2m21)是一根金属棒,直圆柱体(L2m21)的长度为L1,直圆柱体(L2m21)的一端从矩形波导第二侧面的第2m-1圆形通孔(L141m)穿过矩形波导(L1),外接步进电机;半圆环(L2m22)和螺旋线(L2m23)的总高度为L2;半圆环(L2m22)的圆环直径为L3/2,螺旋线(L2m23)为等螺旋半径等螺距的一段螺旋线,L3为螺旋线(L2m23)的螺旋外直径;半圆环(L2m22)的初始段切线与x轴的夹角为αm,αm代表第m螺旋线内导体(L2m2)的空间方位;相邻两个螺旋线内导体的空间方位角度差为一个常量P,即αmm-1=P;The inner conductors of the M spirals have exactly the same structure; the inner conductor of the mth spiral (L2m2) consists of a straight cylinder (L2m21), a semicircle (L2m22) perpendicular to the straight cylinder (L2m21), and a helix (L2m22). L2m23), the straight cylinder (L2m21) is a metal rod, the length of the straight cylinder (L2m21) is L 1 , and one end of the straight cylinder (L2m21) passes through the 2m-1 circle on the second side of the rectangular waveguide. The hole (L141m) passes through the rectangular waveguide (L1), and the stepper motor is externally connected; the total height of the semi-circular ring (L2m22) and the helix (L2m23) is L 2 ; the diameter of the semi-circular ring (L2m22) is L 3 / 2. The helix (L2m23) is a helix with equal helix radius and equal pitch, L3 is the helix outer diameter of the helix (L2m23); the angle between the initial segment tangent of the semicircle (L2m22) and the x-axis is α m , α m represents the spatial orientation of the m-th helix inner conductor (L2m2); the spatial azimuth angle difference of the inner conductors of the two adjacent spirals is a constant P, that is, α mm-1 =P; 第m耦合腔(L2m3)的外形一端为圆柱凸台(L2m31),另一端为长方体(L2m32),圆柱凸台的外半径为R1,凸台的高度为H1;沿NN'方向截断,第m耦合腔(L2m3)的内部挖有四个不同形状的孔,从圆柱凸台(L2m31)向长方体(L2m32)的方向依次为第一孔(L2m33),第二孔(L2m34),第三孔(L2m35),第四孔(L2m36),四个孔连通在一起构成微波传输的通道;沿AA'方向截断,得到第一孔(L2m33)的截面,第一孔(L2m33)由内孔(L2m331)和外孔(L2m332)构成,内孔(L2m331)和外孔(L2m332)的高度均为H1,内孔(L2m331)截面形状为半径为R2的圆形,第m螺旋线内导体(L2m2)即通过内孔插入波导内,外孔(L2m332)近似半环形,内半径为R3,外半径为R4,外孔(L2m332)的圆心角为
Figure FDA0002546121150000051
外孔(L2m332)的对称轴CC'与x轴的夹角定义为耦合腔的旋转角,用θm表示,0<θm<90°;第二孔(L2m34)的高度为H2-H1,第二孔(L2m34)的轮廓由两段弧线构成,尺寸较大的圆弧线的半径为R4,对应的圆心角为
Figure FDA0002546121150000052
尺寸较小弧线的半径为R5,对应的圆心角为
Figure FDA0002546121150000053
第二孔(L2m34)的对称轴DD'与x轴的夹角大小与耦合腔的旋转角θm相同,第一耦合腔(L213)到第M耦合腔(L2M3)结构的尺寸除了耦合腔的旋转角θm不同外,其它结构尺寸均相同;第三孔(L2m35)的高度H3-H2,截面形状为圆形,圆形半径为R5;第四孔(L2m36)的高度H4-H3,截面形状为圆形,圆形半径为R6
The m-th coupling cavity (L2m3) has a cylindrical boss (L2m31) at one end and a cuboid (L2m32) at the other end, the outer radius of the cylindrical boss is R 1 , and the height of the boss is H 1 ; Four holes of different shapes are dug inside the mth coupling cavity (L2m3), from the cylindrical boss (L2m31) to the cuboid (L2m32) are the first hole (L2m33), the second hole (L2m34), the third hole The hole (L2m35), the fourth hole (L2m36), the four holes are connected together to form a microwave transmission channel; cut along the AA' direction to obtain the section of the first hole (L2m33), the first hole (L2m33) is composed of an inner hole ( L2m331) and an outer hole (L2m332), the heights of the inner hole (L2m331) and the outer hole (L2m332) are both H 1 , the cross-sectional shape of the inner hole (L2m331) is a circle with a radius of R 2 , and the m-th spiral inner conductor (L2m2) is inserted into the waveguide through the inner hole, the outer hole (L2m332) is approximately semi-circular, the inner radius is R 3 , the outer radius is R 4 , and the central angle of the outer hole (L2m332) is
Figure FDA0002546121150000051
The angle between the symmetry axis CC' of the outer hole (L2m332) and the x-axis is defined as the rotation angle of the coupling cavity, represented by θ m , 0<θ m <90°; the height of the second hole (L2m34) is H 2 -H 1. The contour of the second hole (L2m34) consists of two arcs, the radius of the arc with a larger size is R 4 , and the corresponding central angle is
Figure FDA0002546121150000052
The radius of the arc with the smaller size is R 5 , and the corresponding central angle is
Figure FDA0002546121150000053
The angle between the symmetry axis DD' of the second hole ( L2m34 ) and the x-axis is the same as the rotation angle θm of the coupling cavity. Except for the different rotation angle θ m , other structural dimensions are the same; the height H 3 -H 2 of the third hole (L2m35), the cross-sectional shape is a circle, and the radius of the circle is R 5 ; the height H 4 of the fourth hole (L2m36) -H 3 , the cross-sectional shape is a circle, and the radius of the circle is R 6 ;
第n移相器相位控制单元(4n)为一个可旋转的轴承,轴承外接步进电机,由步进电机驱动绕自身轴旋转,第n移相器相位控制单元(4n)外接步进电机,绕z轴旋转,即带动第一旋转关节(P22)和第二旋转关节(P32)同步旋转;第n移相器相位控制单元(4n)每旋转θn,同步地带动第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n)的第一旋转关节(P22)和第二旋转关节(P32)绕相同方向旋转θn,移相器的输出相位改变2θnThe nth phase shifter phase control unit (4n) is a rotatable bearing, the bearing is externally connected to a stepping motor, and is driven by the stepping motor to rotate around its own axis, and the nth phase shifter phase control unit (4n) is externally connected to the stepping motor, Rotating around the z-axis, that is, driving the first rotary joint (P22) and the second rotary joint (P32) to rotate synchronously; every time the nth phase shifter phase control unit (4n) rotates by θ n , synchronously drives the nth th The first rotary joint (P22) and the second rotary joint (P32) of the rotary-adjustable phase shifter (1n) of the side-slit bridge rotate around the same direction by θ n , and the output phase of the phase shifter changes by 2θ n ; 第m螺旋线内导体驱动控制单元(5m)由第m带齿轮的滑动平板(5m2)和N个带齿轮的轴承构成,N个带齿轮的轴承沿y轴方向依次为第m1轴承(5m11),第m2轴承(5m12),第m3轴承(5m13)…第mn轴承(5m1n)…第mN轴承(5m1N),上述轴承沿y轴方向依次与第m列的N个辐射单元的螺旋线内导体紧密相连,轴承的旋转将带动螺旋线内导体跟着一起旋转;滑动平板和轴承的齿轮啮合在一起,轴承的齿轮与滑动平板的齿轮尺寸相同;The m-th helical inner conductor drive control unit (5m) is composed of the m-th geared sliding plate (5m2) and N geared bearings. The N geared bearings are the m1th bearing (5m11) in the y-axis direction. , the m2th bearing (5m12), the m3th bearing (5m13)...the mnth bearing (5m1n)...the mNth bearing (5m1N), the above bearings are sequentially connected to the helical inner conductor of the mth row of N radiation units along the y-axis direction Closely connected, the rotation of the bearing will drive the inner conductor of the helix to rotate along with it; the sliding plate and the gear of the bearing are meshed together, and the gear of the bearing is the same size as the gear of the sliding plate; 高功率微波由第1到第N基于矩形波导窄边缝隙电桥的旋转调节式移相器(11)到(1N)的矩形波导窄边缝隙电桥第一电桥端口(P11)注入,经过第一移相器相位控制单元(41)到第N移相器相位控制单元(4N)调节后使得注入到高功率微波一维波束可扫直线阵列的微波形成沿y轴方向的等差相位分布,相邻行的高功率微波一维波束可扫直线阵列的注入相位差为
Figure FDA0002546121150000062
辐射单元的螺旋线内导体经过M个螺旋线内导体驱动控制单元调节后,沿x轴方向形成梯度相位差分布,相邻列的相位差为
Figure FDA0002546121150000063
微波中剩余的少部分能量被匹配负载吸收,整个天线工作在行波状态。
High-power microwaves are injected from the first bridge ports (P11) of the rectangular waveguide narrow-side slot bridges (11) to (1N) based on the rotary-adjustable phase shifters (11) to (1N) of the rectangular-waveguide narrow-side slot bridges, and pass through After adjustment by the first phase shifter phase control unit (41) to the Nth phase shifter phase control unit (4N), the microwaves injected into the high-power microwave one-dimensional beam scannable linear array form an equidistant phase distribution along the y-axis direction , the injection phase difference of the high-power microwave one-dimensional beam scannable linear array of adjacent rows is
Figure FDA0002546121150000062
After the inner conductor of the helix of the radiation unit is adjusted by the M driving control units of the inner conductor of the helix, a gradient phase difference distribution is formed along the x-axis direction, and the phase difference of the adjacent columns is
Figure FDA0002546121150000063
A small part of the energy remaining in the microwave is absorbed by the matching load, and the entire antenna works in a traveling wave state.
2.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述N满足20<N<100,辐射单元个数M满足20<M<500;相邻辐射单元间距为d满足0.5λ<d<λ,其中λ为微波在自由空间的波长。2. The high-power microwave space beam swept planar array antenna according to claim 1, characterized in that said N satisfies 20<N<100, and the number M of radiation units satisfies 20<M<500; the distance between adjacent radiation units 0.5λ<d<λ is satisfied for d, where λ is the wavelength of microwave in free space. 3.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第n基于矩形波导窄边缝隙电桥的旋转调节式移相器1n的矩形波导窄边缝隙电桥(P1)、圆波导(P212)金属壁厚度为T,高功率微波一维波束可扫直线阵列(3n)的矩形波导(L1)的四个侧面的金属壁厚度也为T,T>1.5mm。3. The high-power microwave space beam swept planar array antenna according to claim 1, characterized in that the nth rectangular waveguide narrow-side slot circuit based on the rotation-adjustable phase shifter 1n of the rectangular-waveguide narrow-side slot bridge The metal wall thickness of the bridge (P1) and circular waveguide (P212) is T, and the metal wall thickness of the four sides of the rectangular waveguide (L1) of the high-power microwave one-dimensional beam sweepable linear array (3n) is also T, T>1.5 mm. 4.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述矩形波导窄边缝隙电桥(P1)的第一电桥端口(P11)、第二电桥端口(P12)、第三电桥端口(P13)、第四电桥端口(P14)的内腔的宽边长度a满足λ/2<a<λ,窄边长度b满足b<λ/2,λ为微波在自由空间中的波长;第一微波传输通道(P15)和第二微波传输通道(P16)的两条轴线之间的垂直距离h满足λ<h+a<1.5λ,中央耦合区(P17)的长度L1'满足以下公式4. The high-power microwave space beam swept planar array antenna according to claim 1, characterized in that the first bridge port (P11) and the second bridge port of the rectangular waveguide narrow-side slot bridge (P1) (P12), the third bridge port (P13), the fourth bridge port (P14), the broad side length a of the inner cavity satisfies λ/2<a<λ, the narrow side length b satisfies b<λ/2, λ is the wavelength of microwave in free space; the vertical distance h between the two axes of the first microwave transmission channel (P15) and the second microwave transmission channel (P16) satisfies λ<h+a<1.5λ, the central coupling region ( The length L 1 ' of P17) satisfies the following formula
Figure FDA0002546121150000061
Figure FDA0002546121150000061
其中k为微波的自由空间波数;所述矩形波导窄边缝隙电桥(P1)的第三微波传输通道(P18)和第四微波传输通道(P19)均拐90度弯,拐弯处倒圆角的内半径均为R1',拐弯处倒圆角的外半径为R2';R1'和R2'通过电磁仿真软件优化得到,优化的目的是使得微波传输通道的反射为零。where k is the free-space wave number of the microwave; the third microwave transmission channel (P18) and the fourth microwave transmission channel (P19) of the rectangular waveguide narrow-side slot bridge (P1) both turn 90 degrees, and the corners are rounded The inner radii are R 1 ', and the outer radius of the rounded corners is R 2 '; R 1 ' and R 2 ' are optimized by electromagnetic simulation software, and the purpose of optimization is to make the reflection of the microwave transmission channel zero.
5.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第一线转圆极化器(P21)的圆波导(P212)的内圆直径R'满足:λ0/2.61>R'>λ0/3.41,λ0为圆极化TE11模式在圆波导内传输的波导波长;所述第一波导脊(P213)与第二波导脊(P214)的尺寸d1和d2以及第一波导脊(P213)与第二波导脊(P214)之间的距离w即连接两个波导脊顶面中心的线段PP'的长度通过电磁仿真软件优化得到,优化的目的是使圆极化器注入线极化的TE11模式后,输出为圆极化的TE11模式,圆极化TE11模式的轴比为1;第一波导脊(P213)与第二波导脊(P214)之间的距离w满足λ0/2.61>w>λ0/3.41且w<R',λ0为圆极化TE11模式在圆波导内传输的波导波长。5. high-power microwave space beam swept planar array antenna as claimed in claim 1, it is characterized in that the inner circle diameter R ' of the circular waveguide (P212) of described first line rotating circular polarizer (P21) satisfies: λ 0 /2.61>R'>λ 0 /3.41, λ 0 is the waveguide wavelength of the circularly polarized TE 11 mode propagating in the circular waveguide; the dimensions of the first waveguide ridge (P213) and the second waveguide ridge (P214) d 1 and d 2 and the distance w between the first waveguide ridge (P213) and the second waveguide ridge (P214), that is, the length of the line segment PP' connecting the centers of the top surfaces of the two waveguide ridges, are optimized by electromagnetic simulation software. The optimized The purpose is to inject the circular polarizer into the linearly polarized TE 11 mode, and the output is the circularly polarized TE 11 mode, and the axial ratio of the circularly polarized TE 11 mode is 1; the first waveguide ridge (P213) and the second waveguide The distance w between the ridges (P214) satisfies λ 0 /2.61>w>λ 0 /3.41 and w<R', where λ 0 is the waveguide wavelength of the circularly polarized TE 11 mode propagating in the circular waveguide. 6.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第一旋转关节(P22)的圆柱形底板(P221)的直径R'0,要求R'0=L/2,厚度w1>2mm;所述窄金属板(P222)的长度s=λ0/4,其中λ0为圆极化TE11模式在圆波导内传输的波导波长,宽度等于R',厚度w2满足1mm<w2<4mm;第一旋转关节(P22)的窄金属板(P222)沿z轴方向的两个侧面倒圆角,圆角半径为R'/2;第一旋转关节(P22)和第二旋转关节(P32)的初始状态的角度差γ由下式确定6. The high-power microwave space beam swept planar array antenna according to claim 1, characterized in that the diameter R' 0 of the cylindrical base plate (P221) of the first rotary joint (P22) requires R' 0 = L/2, thickness w 1 >2mm; the length of the narrow metal plate (P222) s=λ 0 /4, where λ 0 is the waveguide wavelength of the circularly polarized TE 11 mode propagating in the circular waveguide, and the width is equal to R' , the thickness w 2 satisfies 1mm<w 2 <4mm; the two sides of the narrow metal plate (P222) of the first rotary joint (P22) along the z-axis are rounded, and the fillet radius is R'/2; the first rotation The angle difference γ of the initial state of the joint (P22) and the second rotary joint (P32) is determined by the following formula
Figure FDA0002546121150000071
Figure FDA0002546121150000071
其中,k为自由空间波数,3a>L>2a,h为第一微波传输通道(P15)和第二微波传输通道(P16)的两条轴线之间的垂直距离,a为矩形波导的内腔的宽边长度。where k is the free space wave number, 3a>L>2a, h is the vertical distance between the two axes of the first microwave transmission channel (P15) and the second microwave transmission channel (P16), and a is the inner cavity of the rectangular waveguide of the broadside length.
7.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第n连接波导(2n)的过渡段的长度为L通过电磁仿真软件优化得到,优化的目标是传输反射为零,过渡段的横截面保持为矩形,宽边尺寸由a过渡到a2,窄边尺寸由b过渡到b27. The high-power microwave space beam swept planar array antenna as claimed in claim 1, wherein the length of the transition section of the nth connecting waveguide (2n) is that L is optimized by electromagnetic simulation software, and the optimized target is The transmission reflection is zero, the cross-section of the transition segment remains rectangular, the broad side dimension transitions from a to a 2 , and the narrow side dimension transitions from b to b 2 . 8.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述高功率微波一维波束可扫直线阵列(3n)的矩形波导(L1)上的第一侧面的第一圆形通孔(L131)的半径为R1满足R1<b2/2;矩形波导(L1)第一侧面的第一圆形通孔(L131)的圆心与注入端(L11)的距离s0满足s0>d/2,矩形波导第一侧面的第m圆形通孔(L13m)的圆心与注入端(L11)的距离为s0+(m-1)d;矩形波导第二侧面的第2m圆形通孔(L142m)的圆心与注入端(L11)的距离sm满足sm-s0-(m-1)d≈λ0/4,其中λ0为微波在矩形波导(L1)内传输的波导波长;矩形波导(L1)的尺寸a2和b2满足λ/2<a2<λ,b2<λ/2,λ为微波在自由空间中的波长。8. The high-power microwave space beam swept planar array antenna according to claim 1, characterized in that the high-power microwave one-dimensional beam swept linear array (3n) on the rectangular waveguide (L1) on the first side surface The radius of the first circular through hole (L131) is R 1 to satisfy R 1 <b 2 /2; The distance s 0 satisfies s 0 >d/2, and the distance between the center of the m-th circular through hole (L13m) on the first side of the rectangular waveguide and the injection end (L11) is s 0 +(m-1)d; The distance s m between the center of the 2mth circular through hole (L142m) on the two sides and the injection end (L11) satisfies s m -s 0 -(m-1)d≈λ 0 /4, where λ 0 is the microwave in the rectangular The waveguide wavelength transmitted in the waveguide (L1); the dimensions a 2 and b 2 of the rectangular waveguide (L1) satisfy λ/2<a 2 <λ, b 2 <λ/2, where λ is the wavelength of the microwave in free space. 9.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第m螺旋线内导体(L2m2)的结构参数L1,L2和L3均由电磁仿真软件优化得到,优化的目标是螺旋线的辐射在轴向上的轴比为零,反射接近零;所述直圆柱体(L2m21)的直径与矩形波导第二侧面的第1,3…2m-1…2M-1圆形通孔的直径2R2相同,R2的尺寸要求0<R2<R3-1。9. The high-power microwave space beam swept planar array antenna according to claim 1, wherein the structural parameters L 1 , L 2 and L 3 of the m-th helix inner conductor (L2m2) are all determined by electromagnetic simulation software The optimization is obtained, and the optimization goal is that the axial ratio of the radiation of the helix in the axial direction is zero, and the reflection is close to zero; the diameter of the right cylinder (L2m21) is the same as the second side of the rectangular waveguide. ... 2M-1 circular through holes have the same diameter as 2R 2 , and the size of R 2 requires 0<R 2 <R 3 -1. 10.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第m耦合腔(L2m3)的参数满足:R4-R3>1.50mm,同时要求R3>3.00mm,高度H1,H2和圆心角
Figure FDA0002546121150000084
的确定方法是:在保证功率容量的前提下,其取值由电磁仿真软件仿真得到,优化的目标是尺寸参数能使第m耦合腔(L2m3)的第一孔(L2m33)工作在谐振状态,等效电导随频率变化的曲线在中心频点获得极大值;第m耦合腔(L2m3)第一孔(L2m33)的外孔的等效电导gm随着θm的增加而增大,gm理论计算公式为
10. The high-power microwave space beam swept planar array antenna as claimed in claim 1, wherein the parameter of the mth coupling cavity (L2m3) satisfies: R 4 -R 3 >1.50mm, while requiring R 3 > 3.00mm, height H 1 , H 2 and central angle
Figure FDA0002546121150000084
The determination method is: on the premise of ensuring the power capacity, its value is obtained by the electromagnetic simulation software, and the optimization goal is to make the first hole (L2m33) of the mth coupling cavity (L2m3) work in the resonance state, The curve of equivalent conductance versus frequency obtains a maximum value at the center frequency point; the equivalent conductance g m of the outer hole of the first hole (L2m33) of the mth coupling cavity (L2m3) increases with the increase of θ m , and g The theoretical formula for m is
Figure FDA0002546121150000081
Figure FDA0002546121150000081
其中,
Figure FDA0002546121150000082
αe为波导衰减常数,d为相邻辐射单元之间的间距,Ei为第i个辐射单元的电场强度,1≤i≤m,η为天线辐射效率,取1>η>0.95,通过电磁仿真软件仿真提取得到耦合腔结构的耦合电导gm随θm的参数后,利用插值法即可得到θm
in,
Figure FDA0002546121150000082
α e is the attenuation constant of the waveguide, d is the spacing between adjacent radiating elements, E i is the electric field strength of the ith radiating element, 1≤i≤m, η is the antenna radiation efficiency, take 1>η>0.95, pass After the parameters of the coupling conductance g m of the coupled cavity structure with the θ m are obtained by the electromagnetic simulation software, θ m can be obtained by the interpolation method.
11.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述辐射单元间距d与最大波束指向角的关系如下式所示11. The high-power microwave space beam swept planar array antenna according to claim 1, wherein the relationship between the radiating element spacing d and the maximum beam pointing angle is shown in the following formula
Figure FDA0002546121150000083
Figure FDA0002546121150000083
其中ρ0为波束偏离天线辐射口面法向的最大角;圆形凸台高度H1等于波导壁厚T;耦合腔和螺旋线内导体的其它结构参数,包括H3,H4,L1,L2,L3,R6和R5由电磁仿真软件优化得到,优化的目标是辐射单元的反射在工作频点接近0,轴比即辐射电场在与微波传输方向垂直的平面上两个正交方向上的电场比值在螺旋线的轴向上接近1,且要求H4-H1≈0.75λ。where ρ 0 is the maximum angle that the beam deviates from the normal direction of the antenna radiation port; the height H 1 of the circular boss is equal to the wall thickness T of the waveguide; other structural parameters of the coupling cavity and the conductor in the helix, including H 3 , H 4 , L 1 , L 2 , L 3 , R 6 and R 5 are optimized by electromagnetic simulation software. The optimization goal is that the reflection of the radiating element is close to 0 at the operating frequency, and the axial ratio is that the radiation electric field is on a plane perpendicular to the microwave transmission direction. The electric field ratio in the orthogonal direction is close to 1 in the axial direction of the helix, and requires H 4 -H 1 ≈ 0.75λ.
12.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第m反射消除杆(L2m1)的长度为a2+T,第m个反射消除杆(L2m1)的半径等于rm,满足反射消除杆在矩形波导内引起的反射与第m个耦合腔和第m个螺旋线内导体引起的反射幅度相等,rm具体数值由电磁仿真软件仿真计算比较得到;第m个反射消除杆的位置sm满足第m反射消除杆引起的反射波相位和第m个耦合腔和第m个螺旋线内导体引起的反射相位相差180度,尺寸具体数值由电磁仿真软件仿真计算比较得到。12. The high-power microwave space beam swept planar array antenna according to claim 1, wherein the mth reflection cancellation rod (L2m1) has a length of a 2 +T, and the mth reflection cancellation rod (L2m1) The radius of r m is equal to r m , which satisfies that the reflection caused by the reflection eliminating rod in the rectangular waveguide is equal to the reflection amplitude caused by the m-th coupling cavity and the m-th helix inner conductor. The specific value of r m is obtained by the electromagnetic simulation software simulation calculation and comparison; The position s m of the m-th reflection cancellation rod satisfies the phase difference of the reflected wave caused by the m-th reflection cancellation rod and the reflection phase caused by the m-th coupling cavity and the m-th helix inner conductor. The specific value of the size is determined by the electromagnetic simulation software. The simulation calculation is compared. 13.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述M个辐射单元构成的直线阵列外接M个步进电机,第m螺旋线内导体穿出矩形波导(L1)的长度h'尺寸由步进电机的尺寸确定,要求穿出部分与步进电机之间能够实现有效连接配合;第m个步进电机控制第m螺旋线内导体绕螺旋线的轴线旋转;定义直线阵列天线的辐射主波束的方向与口面法向的夹角为ρ,直线阵列天线沿x轴方向相邻螺旋线内导体旋转后的空间方位角度αm差P由波束方向ρ决定,P与ρ的关系如下13. The high-power microwave space beam swept planar array antenna according to claim 1, wherein the linear array formed by the M radiating elements is connected to M stepping motors, and the inner conductor of the mth helix passes through a rectangular waveguide. The size of the length h' of (L1) is determined by the size of the stepper motor, and it is required to achieve effective connection and cooperation between the piercing part and the stepper motor; the mth stepper motor controls the axis of the mth helix inner conductor around the helix Rotation; define the angle between the direction of the radiated main beam of the linear array antenna and the normal direction of the mouth as ρ, and the spatial azimuth angle α m difference P of the linear array antenna after the rotation of the conductor in the adjacent helix along the x-axis direction is determined by the beam direction ρ It is decided that the relationship between P and ρ is as follows
Figure FDA0002546121150000091
Figure FDA0002546121150000091
其中k为自由空间波数,β为矩形波导波导传播常数,其计算式为where k is the free-space wave number, and β is the propagation constant of the rectangular waveguide, which is calculated as
Figure FDA0002546121150000092
Figure FDA0002546121150000092
14.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第n移相器相位控制单元(4n)与第n基于矩形波导窄边缝隙电桥的旋转调节式移相器(1n)的第一旋转关节(P22)和第二旋转关节(P32)具有相同的外直径,均为R'0,相邻两路直线阵列的移相器的旋转角度差
Figure FDA0002546121150000093
为一个常量,即
Figure FDA0002546121150000094
θn为第n移相器相位控制单元4n旋转的角度,θn-1为第n-1移相器相位控制单元(4n-1)旋转的角度。
14. The high-power microwave space beam swept planar array antenna according to claim 1, characterized in that the nth phase shifter phase control unit (4n) and the nth are based on the rotation adjustment of the rectangular waveguide narrow-side slot bridge The first rotary joint (P22) and the second rotary joint (P32) of the phase shifter (1n) have the same outer diameter, both of which are R' 0 , and the rotation angles of the phase shifters of the two adjacent linear arrays are different.
Figure FDA0002546121150000093
is a constant, that is
Figure FDA0002546121150000094
θ n is the angle at which the n-th phase shifter phase control unit 4n rotates, and θ n-1 is the angle at which the n-1th phase shifter phase control unit ( 4n-1 ) rotates.
15.如权利要求1所述的高功率微波空间波束可扫平面阵列天线,其特征在于所述第m螺旋线内导体驱动控制单元(5m)的每一个轴承的外直径为r满足d/2>r>R2;第m螺旋线内导体驱动控制单元(5m)的一端(5m3)由步进电机驱动沿y轴方向移动hm,从而带动第m1轴承(5m11)到第Nm轴承(5m1N)都旋转2hm/r弧度,同时带动第m列螺旋线内导体的空间方位角旋转2hm/r弧度;在x轴方向上相邻螺旋线内导体驱动控制单元被外接步进电机驱动的长度差为一个常量Δh=hm-hm-1,在x轴方向相邻列螺旋线内导体的空间方位角差也为一个常量,设为
Figure FDA0002546121150000095
Figure FDA0002546121150000096
增益最大波束指向
Figure FDA0002546121150000097
Figure FDA0002546121150000098
Figure FDA0002546121150000099
有关:
15. The high-power microwave space beam swept planar array antenna according to claim 1, wherein the outer diameter of each bearing of the m-th helix inner conductor drive control unit (5m) is that r satisfies d/2 >r>R 2 ; one end (5m3) of the mth helix inner conductor drive control unit (5m) is driven by the stepping motor to move h m along the y-axis direction, thereby driving the m1th bearing (5m11) to the Nmth bearing (5m1N ) are rotated by 2h m /r radians, and at the same time drive the spatial azimuth angle of the inner conductors of the m-th column to rotate 2h m /r radians; in the x-axis direction, the adjacent helix inner conductor drive control unit is driven by an external stepping motor. The length difference is a constant Δh=h m -h m-1 , and the spatial azimuth difference of the conductors in the adjacent columns of the helix in the x-axis direction is also a constant, set as
Figure FDA0002546121150000095
Have
Figure FDA0002546121150000096
Gain maximum beam pointing
Figure FDA0002546121150000097
and
Figure FDA0002546121150000098
and
Figure FDA0002546121150000099
related:
Figure FDA00025461211500000910
Figure FDA00025461211500000910
其中ρ为辐射主波束与高功率微波空间波束可扫平面阵列天线口面法向即z轴的夹角,
Figure FDA00025461211500000911
为主波束在x-o-y平面投影与x轴夹角,β为高功率微波一维波束可扫直线阵列矩形波导中的波导传播常数,k为自由空间波数。
where ρ is the angle between the main radiating beam and the high-power microwave space beam swept planar array antenna, that is, the normal direction of the mouth, that is, the z-axis,
Figure FDA00025461211500000911
is the angle between the projection of the main beam on the xoy plane and the x-axis, β is the waveguide propagation constant of the high-power microwave one-dimensional beam sweepable linear array rectangular waveguide, and k is the free-space wave number.
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