Patent Description:
Currently, a radome in a conventional base station antenna design system mainly includes three parts: a radiation array unit, a reflection panel used to define a direction, and a feeding system that is mounted on the reflection panel and provides an amplitude and a phase for the radiation array unit. The reflection panel is generally used as a carrier platform, and both the radiation array unit and the feeding network are connected to and mounted on the reflection panel.

For an antenna applied to a higher-order Multi Input Multi Output technical scenario, the conventional antenna structure form has a relatively complex structure design and requires more assembly hours, and an error is easily caused because many assembly components exist; therefore, consistency is also affected.

An existing design scheme provides a feeding system that includes an air microstrip, and in the feeding system, a reflection panel is used as a ground plane, which simplifies design to some extent. However, the air microstrip in this design scheme has obvious defects, that is, backward radiation is large, a voltage standing wave ratio is not stable, and being greater than a frequency band of <NUM>; higher requirements are imposed on production and assembly, and therefore, the air microstrip is difficult to use.

<CIT> relates to an antenna structure. The antenna structure comprises a dual polarized radiating element, a triplate line and a connected relation between the dual polarized radiating element and the triplate line.

<CIT> discloses an antenna radiator, wherein each element radiator includes a node, a first ring connected to the node and a second ring connected to the node and disposed inside of and coplanar with the first ring.

<CIT> discloses an antenna assembly including a reflector, wherein the reflector includes a first ground plane, a second ground plane below and spaced apart from the reflector.

This application provides an antenna system according to appended claims <NUM> to <NUM>, to simplify assembly of the antenna system and improve stability and consistency of the antenna system.

A strip line ground plane is used as a reflective surface of a radiating element, and therefore, no independent reflective surface needs to be disposed, so that a structure of an antenna system is simplified. In addition, radiation baluns are electrically connected to the strip line ground plane, and all of feeding inner cores of radiation arms that are in a same polarization direction in the radiating element are electrically connected to one inner conductor, that is, a strip line of a strip line feeding system feeds the radiation arms in the same polarization direction one by one. Therefore, a feeding manner of an array antenna can be optimized very conveniently, assembly time is greatly reduced, quantities of welding points and cables are reduced, and because of reduced quantities of welding points and cables, consistency and reliability of the antenna system are improved.

The following describes specific embodiments of the present invention in detail with reference to accompanying drawings. It should be understood that the specific implementation manners described herein are merely used to describe and explain the present invention but are not intended to limit the present invention.

As shown in <FIG>, and <FIG>, <FIG> is a schematic diagram of a side cross section of a connection between a radiating element and a strip line in an antenna system according to an example and embodiments of the present invention, <FIG> is a schematic diagram of a side cross section of a connection between a radiating element and a strip line in an antenna system according to an embodiment of the present invention, and <FIG> is a schematic structural diagram of an antenna system according to an embodiment of the present invention.

An embodiment of the present invention provides an antenna system, and the antenna system includes:.

In the foregoing embodiment, a strip line ground plane 01a is used as a reflective surface of a radiating element <NUM>, and therefore, no independent reflective surface needs to be disposed, so that a structure of an antenna system is simplified. In addition, radiation baluns 00c are electrically connected to the strip line ground plane 01a, and all of feeding inner cores 00b of radiation arms 00a that are in a same polarization direction in the radiating element <NUM> are electrically connected to one inner conductor 01b, that is, a strip line <NUM> of a strip line feeding system feeds the radiation arms 00a in the same polarization direction one by one. Therefore, a feeding manner of an existing array antenna can be optimized very conveniently, and assembly time is greatly reduced. In a prior-art structure, feeding inner cores of each radiating element are corresponding to one inner conductor. By comparison, quantities of welding points and cables used to connect inner conductors are reduced, and therefore, consistency and reliability are improved.

To facilitate understanding of the embodiments of the present invention, the following describes in detail a structure of the antenna system with reference to specific embodiments.

As shown in <FIG>, the antenna system provided in the embodiments may include a radome <NUM>, where the radome <NUM> covers the strip line and the radiating element <NUM>.

The radiating element in the antenna system provided in the embodiments is a dual-polarization radiating element, and the following describes the radiating element in detail with reference to specific embodiments.

As shown in <FIG> is a schematic diagram of a side cross section of a connection between a radiating element and a strip line, and in this example, the radiating element is a single-polarization radiating element.

Specifically, as shown in <FIG>, a radiating element <NUM> includes radiation arms 00a in a same polarization direction, the radiation arm 00a is fastened on the top of a radiation balun 00c, and the radiation arm 00a is corresponding to a feeding inner core 00b that electrically feeds the radiation arm 00a, where the radiation arm 00a may be connected, in an electrical coupling manner or a welding manner, to the feeding inner core 00b corresponding to the radiation arm 00a for feeding. A strip line <NUM> has a hollow cavity 01c that is corresponding to the foregoing radiation arms 00a, and the strip line <NUM> has a strip line ground plane 01a that is corresponding to the radiation arms 00a in the same polarization direction. As shown in <FIG>, the strip line ground plane 01a is an upper sidewall of the hollow cavity 01c. An inner conductor 01b is disposed in the hollow cavity 01c, and the inner conductor 01b is suspendedly disposed in the hollow cavity. In a specific connection, radiation baluns 00c of the radiating element <NUM> are electrically connected to the strip line ground plane 01a, and feeding inner cores 00b are electrically connected to the inner conductor 01b.

A surface, of the strip line ground plane 01a, that faces the radiating element <NUM> is used as a reflective surface, and is used to reflect a radiation wave transmitted by the radiating element <NUM>. Therefore, a structure of an antenna system is simplified, and no reflective structure that is used to reflect a radiation wave needs to be disposed independently. In specific disposing, the surface, of the strip line ground plane 01a, that faces the radiating element <NUM> is a flat surface or a convex arc surface, and the strip line ground plane 01a is made by metallic materials.

In addition, the inner conductor 01b provided in an embodiment is of a PCB structure or a metal strip line structure. In this embodiment, as another optional solution, a dielectric combination that can slide against the inner conductor 01b is disposed on the inner conductor 01b. When the dielectric combination slides against the inner conductor 01b, a transmission phase of the inner conductor 01b may be changed, so that an offset of a maximum direction of a radiation pattern of the antenna system is caused, so as to better serve mobile communications.

In addition, the hollow cavity 01c of the strip line <NUM> provided in an embodiment is a hollow cavity 01c with openings at two ends. When the inner conductor 01b is being disposed, the inner conductor 01b may directly penetrate into the hollow cavity 01c through an opening of the hollow cavity 01c, thereby facilitating disposing of the inner conductor 01b and improving entire antenna production efficiency.

For the antenna system provided in this embodiment, the radiating element <NUM> and the strip line <NUM> are covered by a protective cover, and in specific disposing, the protective cover covers the radiating element <NUM> and the strip line <NUM>.

In specific disposing, there may be multiple radiating elements <NUM>, each radiation balun 00c is electrically connected to the strip line ground plane 01a, and each feeding inner core 00b is electrically connected to the inner conductor 01b. Specifically, the multiple radiating elements <NUM> are arranged in a single row, and an orientation of the radiating elements <NUM> that are arranged in a single row is the same as a length direction of the hollow cavity 01c, that is, the multiple radiating elements <NUM> are arranged along the length direction of the hollow cavity 01c to form a row of radiating elements.

As shown in <FIG> and <FIG>, an antenna in an antenna system provided in this embodiment is a dual-polarization antenna, that is, a radiating element <NUM> has radiation arms in two polarization directions, where <FIG> is a schematic diagram of a side cross section of the dual-polarization antenna, and <FIG> is a cross-sectional view of a side structure of the dual-polarization antenna.

In this embodiment, the radiating element <NUM> is a dual-polarization radiating element, and the dual-polarization radiating element includes a radiation arm whose polarization direction is positive <NUM> degrees and a radiation arm whose polarization direction is negative <NUM> degrees. Two inner conductors are disposed in the hollow cavity, the radiation arm whose polarization direction is positive <NUM> degrees is electrically connected to one inner conductor by using a feeding inner core to which the radiation arm whose polarization direction is positive <NUM> degrees is connected, and the radiation arm whose polarization direction is negative <NUM> degrees is electrically connected to the other inner conductor by using a feeding inner core to which the radiation arm whose polarization direction is negative <NUM> degrees is connected.

In a specific connection, the radiation arm whose polarization direction is positive <NUM> degrees is a first polarized radiation arm 00a1, and the radiation arm whose polarization direction is negative <NUM> degrees is a second polarized radiation arm 00a2, where the first polarized radiation arm 00a1 is corresponding to a first feeding inner core 00b1, and the second polarized radiation arm 00a2 is corresponding to a second feeding inner core 00b2. The foregoing radiation arms may be connected, in an electrical coupling manner or a welding manner, to the feeding inner cores corresponding to the radiation arms for feeding. The foregoing radiation balun 00c has a cavity, and the feeding inner cores 00b1 and 00b2 are disposed in the cavity of the radiation balun 00c. A separator is disposed in the hollow cavity of a strip line <NUM>, the separator divides the hollow cavity into two side-by-side cavities, and the two inner conductors are located in the two cavities respectively. The foregoing two cavities are respectively a first hollow cavity 01c1 and a second hollow cavity 01c2. An upper sidewall of the first hollow cavity 01c1 is a first strip line ground plane 01a1, and a first inner conductor 01b1 is disposed in the first hollow cavity 01c1. An upper sidewall of the second hollow cavity 01c2 is a second strip line ground plane 01a2, and a second inner conductor 01b2 is disposed in the second hollow cavity 01c2. For a specific connection manner, reference may be made to a connection manner of the radiating element <NUM> and the strip line <NUM> in Example <NUM>, that is, the first polarized radiation arm 00a1 is fastened on a radiation balun 00c, the radiation balun 00c is electrically connected to the first strip line ground plane 01a1, and the first feeding inner core 00b1 is electrically connected to the first inner conductor 01b1; the second polarized radiation arm 00a2 is fastened on a radiation balun 00c, the radiation balun 00c is electrically connected to the second strip line ground plane 01a2, and the second feeding inner core 00b2 is connected to the second inner conductor 01b2. In addition, in specific disposing, the first strip line ground plane 01a1 and the second strip line ground plane 01a2 may be of an integrated structure.

In this embodiment, the two hollow cavities divided by the separator are arranged side by side. For each hollow cavity, structures of the hollow cavity, an inner conductor 01b, and a strip line ground plane 01a are similar to structures in the foregoing Example <NUM>, and details are not described herein. In addition, when the first strip line ground plane 01a1 and the second strip line ground plane 01a2 are of an integrated structure, a surface, of the strip line ground plane 01a in the integrated structure, that faces the radiating element <NUM> is used as a reflective surface, and a shape of the surface is an arc or a planform.

To facilitate understanding of the antenna system provided in this embodiment, the following describes in detail the antenna system with reference to accompany drawings.

As shown in <FIG> shows a structure of a dual-polarization antenna system according to an embodiment. In <FIG>, radiating elements in the antenna system are arranged in a single row, and the radiating elements are arranged along a length direction of a hollow cavity. The radiating elements included in the antenna system are <NUM>, <NUM>, <NUM>, <NUM>, <NUM>, <NUM>, <NUM>, <NUM>, <NUM>,.

The radiating element <NUM> is used as an example; as shown in <FIG>, the radiating element <NUM> includes a first polarized radiation arm 201a1 and a second polarized radiation arm 201a2. A first feeding inner core 201b1 of the radiating element <NUM> is connected to a first inner conductor 21b1 in a first hollow cavity 21c1 of a strip line <NUM>, and an electrical connection point 201d1 between the first feeding inner core 201b1 and the first inner conductor 21b1 is shown in <FIG>. A second feeding inner core 201b2 of the radiating element <NUM> is connected to a second inner conductor 21b2 in a second hollow cavity 21c2 of the strip line <NUM>, and an electrical connection point 201d2 between the second feeding inner core 201b2 and the second inner conductor 21b2 is shown in <FIG>. In the foregoing specific connection, the feeding inner cores are connected to the inner conductors by means of welding, or the feeding inner cores are fixedly connected to the inner conductors by using a first connecting piece. Preferably, in this embodiment, a connection is established by using a connecting piece; during a specific connection, the connecting piece may be a bolt or a screw. An electrical connection point 201e between the radiation balun and the strip line ground plane is shown in <FIG>. In this embodiment, the radiation balun is electrically connected to the strip line ground plane by using a second connecting piece, where the second connecting piece is a bolt or a screw. Electrical connection points that are not shown in <FIG> may further be 202e,. 20ne, which are respectively and correspondingly used to electrically connect radiation baluns of radiation arms <NUM> to 20n and the strip line ground plane, and structures and connection manners of the electrical connection points are the same as those of the electrical connection point 201e of the radiating element <NUM>.

In this embodiment, a separator is used to isolate the hollow cavity into two independent strip line cavities, so as to ensure that isolation indicators of two polarizations in a mobile communications system are met.

The antenna system shown in <FIG> is an integrated array antenna system, includes a radiation array that includes n radiation arms whose polarization directions are positive or negative <NUM> degrees, and includes two electrically isolated strip lines, that is, two electrically isolated hollow cavities and inner conductors.

To better explain working principles, a signal in one strip line feeds radiation arms 201a1, 202a1, 203a1,. , 20na1 of radiating elements by using an inner conductor, and the radiation arms 201a1, 202a1, 203a1,. , 20na1 of the radiating elements together form a radiator, of the array antenna, whose polarization direction is positive <NUM> degrees.

A signal in the other strip line feeds radiation arms 201a2, 202a2, 203a2,. , 20na2 of the radiating elements by using an inner conductor, and the radiation arms 201a2, 202a2, 203a2,. , 20na2 of the radiating elements together form a radiator, of the array antenna, whose polarization direction is negative <NUM> degrees.

In specific disposing, there are multiple radiating elements, each radiation balun is electrically connected to a strip line ground plane, and each feeding inner core is electrically connected to an inner conductor. Specifically, the multiple radiating elements may be arranged in a single row, or arranged in an array manner, and an orientation of the single row of radiating elements is the same as a length direction of a hollow cavity. When strip lines are arranged in multiple columns, a planar antenna system is formed. Refer to <FIG> and <FIG> together, multiple strip lines may use independent structures, or use an integrated structure. As shown in <FIG>, strip lines in <FIG> use independent structures, that is, strip lines of all columns of radiating elements are independent of each other. As shown in <FIG>, strip lines corresponding to multiple columns of radiating elements in <FIG> are of an integrated structure, that is, strip lines corresponding to all columns of radiating elements are integrally connected.

Claim 1:
An antenna system, comprising:
a dual-polarization radiating element (<NUM>), and a strip line (<NUM>);
the dual-polarization radiating element (<NUM>) comprises: a radiation balun (00c), a first radiation arm (00a1) with a polarization direction of positive <NUM> degrees, a second radiation arm (00a2) with a polarization direction of negative <NUM> degrees, a first feeding inner core (00b1), and a second feeding inner core (00b2), wherein the first radiation arm (00a1) and the second radiation arm (00a2)are fastened on the radiation balun (00c), the first radiation arm (00a1) corresponds to the first feeding inner core (00b1), the second radiation arm (00a2) corresponds to the second feeding inner core (00b2);
the strip line (<NUM>) comprises: a strip line ground plane (01a1,01a2), a hollow cavity (01c), a first inner conductor (Olbl) disposed in the hollow cavity (01c), and a second inner conductor (01b2) disposed in the hollow cavity (01c);
the first radiation arm (00a1) is electrically connected to the first inner conductor (Olbl) by the first feeding inner core (00b1), the second radiation arm (00a2) is electrically connected to the second inner conductor (01b2) by the second feeding inner core (00b2), wherein the balun (00c) has a bottom surface which contacts the strip line ground plane (01a1,01a2), and the bottom surface of the radiation balun (00c) is fastened on the strip line ground plane (01a1, 01a2) by one first connecting piece (201e); wherein
the strip line ground plane (01a1,01a2) comprises a first strip line ground plane (01a1), and a second strip line ground plane (01a2); the hollow cavity (01c) is divided into a first hollow cavity (01c1) and a second hollow cavity (01c2); the first inner conductor (Olbl) is located in the first hollow cavity (01c1), an upper sidewall of the first hollow cavity (01c1) is the first strip line ground plane (01a1); the second inner conductor (01b2) is located in the second hollow cavity (01c2), an upper sidewall of the second hollow cavity (01c2) is the second strip line ground plane (01a2); and wherein
the first connecting piece (201e) is located between the first strip line ground plane (01a1) and the second strip line ground plane (01a2).