The present invention relates to a comb polarizer suitable for millimeter band applications; and, more particularly, to a millimeter band comb polarizer having a comparative simple structure allowing an easy manufacturing process, less manufacturing and testing cost, and applicable for other bands, by embodying a polarizer transforming a linear polarization to a circular polarization with a comb shaped conductive plate (comb conductive plate) interposed between two half waveguides.
Conventionally, satellite communication frequency bands, an L-band, a C-band, and a Ku-band, were used to provide a wideband satellite multimedia service. Due to the restricted frequency bandwidth of the satellite communication frequency, the satellite frequency band has been replaced with a millimeter band for the satellite communication to provide a wideband multimedia service. The millimeter wave is an electromagnetic wave having a frequency in a range from about 30 to 300 GHz. That is, the millimeter wave denotes an electromagnetic wave having a millimeter wavelength.
The present invention relates to a circular polarizer having a new structure. The circular polarizer is one of major parts used for a satellite communication antenna power-feed system. The circular polarizer transforms a linear polarization to a left circular polarization or a right circular polarization.
Various conventional methods were introduced to embody a conventional circular polarizer. For example, according to a first conventional method, a circular polarizer is embodied by inserting a conductive iris structure in a rectangular or circular waveguide. According to a second conventional method, a circular polarizer is embodied by inserting conductive poles in a rectangular or circular waveguide. In a third conventional method, a circular polarizer is embodied by inserting a dielectric plate in a rectangular or circular waveguide. In a fourth conventional method, a circular polarizer is embodied by inserting a rectangular groove formed on an outer surface of a circular waveguide.
Since the conventional circular polarizers have complicated structures as described above, it is very difficult to manufacture the conventional circular polarizer for millimeter band applications. The complicated manufacturing process of the conventional circular polarizer is the major factor to increase the manufacturing cost and the testing cost. Particularly, the conventional circular polarizer having the dielectric plate has shortcomings. The conventional circular polarizer having the dielectric plate has the electric characteristic varying according to peripheral temperature characteristic, and cannot be used for dual band application.
Technical Problem
An embodiment of the present invention is directed to providing a comb polarizer, suitable for millimeter band applications, having a comparative simple structure allowing an easy manufacturing process, a less manufacturing and testing cost, and applicable for other bands, by embodying a polarizer transforming a linear polarization to a circular polarization with a comb shaped conductive plate (comb conductive plate) interposed between two half waveguides.
Other objects and advantages of the present invention can be understood by the following description, and become apparent with reference to the embodiments of the present invention. Also, it is obvious to those skilled in the art of the present invention that the objects and advantages of the present invention can be realized by the means as claimed and combinations thereof.
Technical Solution
In accordance with an aspect of the present invention, there is provided a comb polarizer suitable for millimeter band applications including: a waveguide having an aperture side formed of two separable half waveguides, and a comb shaped conductive unit having a plurality of cogs interposed between two half waveguides for transforming a linear polarized signal to a circular polarized signal.
Advantageous Effects
According to the present invention, a circular polarizer is embodied by interposing a com conductive plate between two half circular waveguides using a conventional circular waveguide as it is. Therefore, the circular polarizer according to the present embodiment has a simple structure that allows an easy manufacturing process, less manufacturing and testing cost, and applicable for other bands.
The simple structure of the circular polarizer according to the present invention can significantly reduce the manufacturing cost and the testing cost although the circular polarizer is manufactured for millimeter band applications that require a complicated and fine manufacturing process and test.
The circular polarizer according to the present embodiment can be used as a single and a dual band circular polarizer for various applications including the conventional satellite or mobile communication antenna system. Due to such an advantage, it may give great economical benefit to the related field.
Although the circular polarizer according to the present embodiment includes no tuning elements for controlling performance, the electric performance thereof can be optimized by controlling the size of the comb cog. Also, it can be used for single or dual band design according to needs.
The advantages, features and aspects of the invention will become apparent from the following description of the embodiments with reference to the accompanying drawings, which is set forth hereinafter.
As shown in
The comb circular polarizer according to the present embodiment also includes input and output flanges 13 of a circular polarizer used to connect to other circular waveguide type parts, fixing pins 14 for fixing two conductive plates 12 at a predetermined position, and screws 15 for fastening two half circular waveguides and two comb conductive plates.
Each of the comb conductive plates 12 has a symmetric shape in a longitudinal axis and an abscissa axis and includes comb cogs regularly formed, as shown in
That is, a linear polarized signal, which enters to a plane formed by a pair of the conductive plates 12 inserted between the circular waveguides 11 at an offset of about +45° or −45°, includes vertical component and horizontal component to the comb conductive plate plane in a vector. The vertical component propagates without passing through the comb structure. On the contrary, the horizontal component propagates passing through the comb structure. As a result, the phase delay is induced. In order to induce circular polarization, the differential phase shift between the vertical and horizontal components of the input signal must be +90° at an operating band. Therefore, the number of comb cogs and the size of each comb cog must be optimized for making the required differential phase shift.
As shown in
Also, the propagation constant becomes converged as the frequency of the vertical input signal increase like as the propagation constant variation in a circular waveguide. On the contrary, the horizontal input signal becomes diffused because the resonant frequency induced from the comb structure restricts the horizontal input signal.
In order to drive the comb circular polarizer for dual band as shown in
Δφ=Δβ1·L=Δβ2·L=90° Eq. 1
In Eq. 1, Δβ=(βpi−βvi) where i=1,2. Δβ denotes a relative propagation constant, and βpi and βvi denote the propagation constants of the horizontal input signal and the vertical input signal, respectively. i is each of the operating frequencies, L denotes the length of a comb cog delaying a phase, fcv and fcp denotes cut-off frequencies of the vertical and horizontal input signals, and fc and fr denote cut-off frequency of a circular waveguide and resonant frequencies induced from the comb cog structure. f1 and f2 denote denotes dual operating frequencies.
The designing parameters, a radius R of a circular waveguide, the number N of comb cogs, a thickness T, a length L1, a gap L2 between combs, and heights L3 to L6, are optimally decided according to an operating frequency. Particularly, the comb cogs disposed at the input/output end of the comb conductive plate are tapered to gradually increase to the center thereof so as to have the same height L6 of the cogs disposed at the center for impedance matching of the input/output signals. In order to match the input/output impedances, the heights of cogs gradually increase from the input/output ends to the center within a predetermined region only, for example, from the input/output ends to L3 to L6. The heights of cogs in other regions are same.
The electrical performance of the comb circular polarizer is decided by the designing parameters. Particularly, the radius R of the circular waveguide must be decided not to propagate high-order modes such as TM11, TE31, TM21, and TE12 modes. Since the second-order modes such as TM01, TE21, and TE01 modes are attenuated by the symmetric structure of the comb structure, they do not influence to decide the diameter of the circular waveguide. Therefore, the operating frequency range of the circular waveguide is decided by a resonant frequency induced based on the radius R of the circular waveguide and the comb structure like as Eq. 2.
In Eq. 2, R is a radius of a circular waveguide, K1 and K2 are parameters related to TE11 and TM11 modes. For example, K1=3.413, and K2=1.640. For example, when a radius (R) is 5.335 mmm, the operating frequency band must be in a range from about 16.5 GHz<f<34.3 GHz.
As an example, the results of simulations of using a dual band satellite communication circular polarizer using a comb circular polarizer according to an embodiment of the present invention will be described hereinafter. The dual band frequency reflected to design is about 20.355 to 21.155 GHz (Band 1, K_band) and 30.085˜30.885 GHz (Band 2, Ka_band).
In order to optimally design the comb circular polarizer, a CST Microwave Studio™, a commercial designing simulator, is used. Table 1 shows the optimal designing parameter of the comb circular polarizer having a differential phase shift of 90°±5° in the given dual bands.
In the
The graph of
As shown in
As shown, spherical and circular waveguide adaptors have superior return loss characteristics of less than −30 dB, and the measurement result includes the return loss characteristics of the spherical and circular waveguide adaptors.
In the graph of
The relative phase different characteristics of the comb circular polarizer according to the present embodiment can be replaced with the cross polarization characteristics. In order to measure the cross polarization characteristics, a rotation detection method can be used as shown in
The test device using the rotation detection method, as shown in
If N test frequencies fT1, fT2, . . . , fTN input to the input SMA (or K) connector—spherical waveguide transformer (SRW-T1) 71, a vertical basic mode signal is generated at the P1 boundary. Then, the liner signal passes through the spherical-circular waveguide transformer (RCW-T2) 72 and is transformed to a vertical basic mode signal in the circular waveguide at the P2 boundary side.
The vertical basic mode signal passes through the circular waveguide (CWG) 73 and enters to the comb structure of the prototype circular waveguide (POL) 74 at 45° inclined. Then, the linear polarized signal passes through the comb circular polarizer POL 74 and then, the circular polarization signal is generated at the P4 boundary.
The rotary joint and linear polarized filter (RJ-LPF) 75 detects linear polarized signals from the generated circular polarized signal at various rotation angles. In
The difference ΔAdB between the maximum value and the minimum value in the measuring results of each test frequency denotes an axial ratio characteristic like as Eq. 3.
ΔAdB=max[L1(fTi):LM(fTi)]−min[L1(fTi):LM(fTi)], i=1,2, . . . , N. Eq. 3
In Eq. 3, max[L1(fTi):LM(fTi)] denotes M levels detected at the output end. That is, it is the maximum value selected from L1(fTi), L2(fTi), . . . LM(fTi). min[L1(fTi):LM(fTi)] denotes a minimum value. i denotes N testing frequencies. The axial ratio characteristics may be transited to a cross polarization level using Eq. 4.
In Eq. 4, K is given as
As shown in the measuring result of
The present application contains subject matter related to Korean patent application No. 2006-0114041, filed in the Korean Intellectual Property Office on Nov. 17, 2006, the entire contents of which is incorporated herein by reference.
While the present invention has been described with respect to certain preferred embodiments, it will be apparent to those skilled in the art that various changes and modifications may be made without departing from the scope of the invention as defined in the following claims.
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