The present disclosure relates to the antenna technology, and more particularly to an isolation structure of a large array antenna and an antenna.
An antenna system composed of many identical individual antennas, such as symmetrical antennas, arranged in accordance with certain rules, is called a large array antenna, which is also referred to as an antenna array. An independent radiating element in a large array antenna is called an array element or antenna element. With the development of large array antennas, a large array antenna may have more and more array elements.
With the development of large array antennas, a large array antenna may have more and more array elements, and there is an urgent problem to solve, i.e., how to isolate array elements therein so as to guarantee the isolation between the array elements and reduce the coupling of the array elements.
At present, the problem mentioned above may be solved by setting an isolation structure between array elements in a large array antenna. The following are two major types of set isolation structures.
A first isolation structure is as shown in
A second isolation structure is as shown in
Therefore, a simple and implementable isolation structure for a large array antenna that can improve the isolation of the large array antenna has not been developed yet until now.
Provided are simple and implementable isolation structures for a large array antenna.
In view of this, various embodiments of the present disclosure provide an isolation structure of a large array antenna that can improve the isolation of the large array antenna simply.
Various embodiments of the present disclosure also provides a large array antenna with a boundary structure that can improve the isolation of the large array antenna simply.
Embodiments of the present disclosure will be described below:
An isolation structure of a large array antenna may include a boundary plate 301 disposed between array elements 100 of the large array antenna. The boundary plate 301 has hollowed-out areas and is perpendicular to a plane where the array elements 100 are located.
The boundary plate 301 is made of a metal or a polymeric material.
The boundary plate 301 is designed with a printed circuit board (PCB).
The hollowed-out areas in the boundary plate 301 form sub-areas with staggered patterns in the boundary plate 301.
The staggered patterns are at least two layers of staggered patterns arranged with one on top of the other, in such a manner of being perpendicular to the plane where the array elements are located.
The at least two layers of staggered patterns are arranged continuously or discontinuously in a direction perpendicular to the plane where the array elements are located.
An antenna may include a plurality of array elements 100 arranged regularly and any isolation structure as described above.
As can be seen from the above, according to embodiments of the present disclosure, a boundary plate is disposed between array elements of a large array antenna. The boundary plate has hollowed-out areas and is perpendicular to a plane where the array elements are located. The hollowed-out areas of the boundary plate form sub-areas with staggered patterns in the boundary plate to allow a coupling path of signals of array elements generated at the boundary plate and a radiation path of the array elements to counteract with each other, thus weakening the coupling between the array elements and improving the isolation between the array elements, especially the isolation between 3-5 db array elements. Therefore, the isolation structure in accordance with the embodiments of the present disclosure can improve the isolation of the large array antenna simply.
To illustrate the objectives, technical solutions and advantages of the present disclosure more clearly, the present disclosure will be further described in detail with reference to drawings and by embodiments.
According to an embodiment of the present disclosure, a boundary plate is arranged between array elements of a large array antenna. The boundary plate has hollowed-out areas and is arranged in a plane that is perpendicular to the plane where the array elements are located. The hollowed-out areas of the boundary plate form sub-areas with staggered patterns in the boundary plate to allow a coupling path of signals of array elements generated at the boundary plate and a radiation path of the array elements to counteract with each other, thus weakening the coupling between the array elements and improving the isolation between the array elements, especially the isolation between 3-5 db array elements. Further, since the boundary plate has the hollowed-out areas and may not highly reflect the principal-direction electromagnetic field of the array elements, so the antenna pattern of the large array antenna may not be affected. The hollowed-out areas of the boundary plate according to the embodiment of the present disclosure include the sub-areas with staggered patterns, and the staggered patterns may be at least two layers of staggered patterns arranged with one on top of the other in such a manner of being perpendicular to the plane where the array elements are located, so that the boundary plate is not completely connected with the plane where the array elements are located. For example, the boundary plate is partially connected with the plane where the array elements are located. Thus, the surface wave backflow to the plane is interrupted, and the surface wave interference is reduced with no deterioration of third-order passive intermodulation level (PIM3) of the array elements.
Therefore, the structure in accordance with this embodiment of the present invention can improve the isolation of the large array antenna simply.
The boundary plate 301 illustrated in
The boundary plate 301 illustrated in
The hollowed-out areas in the boundary plate 301 illustrated in
In an embodiment of the present disclosure, since the boundary plate 301 has partial hollowed-out areas, another coupling path may be generated when array elements 100 transmit signals, which counteracts with a radiation path of the array elements 100, thereby weakening coupling and improving isolation, especially the isolation between 3-5 db array elements 100, wherein, the partial hollowed-out areas are constituted by sub-areas with special staggered patterns. The hollowed-out patterns are formed in the sub-areas. In an embodiment of the present disclosure, with low reflection of the principal-direction field of the array elements 100 and no effect on the antenna directional pattern, the boundary plate 301 may be manufactured to be higher than and perpendicular to the plane where the array elements 100 are located.
In an embodiment of the present disclosure, since the boundary plate 301 has partial hollowed-out areas that are constituted by the sub-areas with special staggered patterns in the boundary plate 301, a plurality of mutually transformational coupling paths can be generated when the array elements 100 transmit signals, thereby the principal-direction field is tightly restrained around the array elements 100.
In an embodiment of the present disclosure, the hollowed-out patterns formed by the sub-areas with staggered patterns in the boundary plate 301 may vary in type and size depending on different types or different frequencies of the array antennas. For example, as shown in
An embodiment of the present disclosure also provides an antenna including the boundary plate 301 and a plurality of array elements 100 isolated by the boundary plate 301.
It can be seen that in this embodiment of the present disclosure, with the use of the boundary plate 301 provided by the embodiments of the present disclosure in a large array antenna, the isolation between array elements is dramatically improved. Through simulation and actual measurement and by comparing with a 3.5 G multi-mode unit (MMU) antenna, it is found that homopolar isolation is improved by more than 5 dB and heteropolar isolation is improved by more than 6 dB.
The above embodiments are merely preferable embodiments of the present disclosure and are not for limiting the present disclosure. Any modification, equivalent substitution, improvement and the like in accordance with the spirit and principles of the present disclosure shall fall within the protection scope of the present disclosure.
Number | Date | Country | Kind |
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201810375894.0 | Apr 2018 | CN | national |
Filing Document | Filing Date | Country | Kind |
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PCT/KR2019/000216 | 1/7/2019 | WO | 00 |