The present invention generally relates to cellular communications and, more particularly, to base station antennas for cellular communications systems
Cellular communications systems are well known in the art. In a typical cellular communications system, a geographic area is divided into a series of regions that are referred to as “cells,” and each cell is served by a base station. The base station may include baseband equipment, radios and base station antennas that are configured to provide two-way radio frequency (“RF”) communications with subscribers that are positioned throughout the cell. Typically, a base station antenna includes a plurality of phase-controlled arrays of radiating elements, with the radiating elements arranged in one or more vertically-extending columns that are often referred to as “linear arrays.” Each linear array generates an antenna beam or, if the linear array is formed using dual-polarized radiating elements, forms an antenna beam at each of two orthogonal polarizations. Base station antennas further include a radome, which refers to an outer housing that encloses and protects the radiating elements. At least a front surface of the radome is typically designed to be transparent to RF signals within the operating frequency bands of the linear arrays of radiating elements.
As demand for cellular service has grown, cellular operators have upgraded their networks to increase capacity and to support new generations of cellular service. Most recently, base station antennas are being deployed that support so-called fifth generation or “5G” cellular service. When these new services are introduced, the existing services typically must be maintained to support legacy mobile devices. Accordingly, many base station antennas that support fourth generation (“4G”) and 5G service include many different arrays of radiating elements that support cellular service in different operating frequency bands. As the number of arrays of radiating elements included in a base station is increased, the size of the base station antenna also typically increases.
Base station antennas are often mounted on tall antenna towers, and may be subject to very high wind levels. The term “wind load” refers to the forces that wind exerts on a structure, such as a base station antenna. As the size of a base station antenna increases, the amount of wind loading also generally increases. The base station antenna, its mounting hardware, and even the antenna tower must be designed to withstand anticipated amounts of wind loading, and hence larger base station antennas may require the use of more rigid radomes and/or sturdier mounting brackets, and may limit the number of base station antennas that can be mounted on an antenna tower (or, alternatively, require structural reinforcement of the tower).
Pursuant to embodiments of the present invention, base station antennas are provided that include a backplane having a planar reflector, a radiating element mounted to extend forwardly from the planar reflector, the radiating element including a dipole that comprises an inner dipole arm and an outer dipole arm, and a radome having a front wall, a side wall and a curved front transition wall that connects the front wall to the side wall. A distal end of the outer dipole arm is closer to the planar reflector than is a base of the outer dipole arm, and an overlap portion of the outer dipole arm overlaps the curved front transition wall, Additionally, a largest minimum distance between any point on a front surface of the overlap portion of the outer dipole arm and the radome is less than twice a smallest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome.
In some embodiments, the overlap portion of the outer dipole arm may be at least half a length of the outer dipole arm.
In some embodiments, the curved front transition wall may have a radius of curvature of at least 50 mm or a radius of curvature of at least 75 mm.
In some embodiments, the radiating element may be configured to operate in at least a portion of the 617-960 MHz frequency band.
In some embodiments, the largest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome may be less than 1.5 times the smallest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome.
In some embodiments, the largest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome may be less than 1.25 times the smallest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome.
In some embodiments, the outer dipole arm may include at least two bends along a longitudinal axis of the outer dipole arm that divide the outer dipole arm into a plurality of longitudinally-extending sections that are angled with respect to each other. In some embodiments, distances between centers of each longitudinally-extending section and respective closest points on the radome may vary by less than 25%.
Pursuant to further embodiments of the present invention, base station antennas are provided that include a backplane having a reflector, a radiating element mounted to extend forwardly from the reflector, the radiating element including an inner dipole arm and an outer dipole arm, and a radome that has a front wall that is positioned in front of the radiating element. The outer dipole arm includes at least two bends along a longitudinal axis of the outer dipole arm that divide the outer dipole arm into a plurality of longitudinally-extending sections that are angled with respect to the reflector and with respect to each other, where distances between centers of each longitudinally-extending section and respective closest points on the radome vary by less than 50%.
In some embodiments, the distances between the centers of each longitudinally-extending section and the respective closest points on the radome may vary by less than 25%.
In some embodiments, the radome may further include a side wall and a curved front transition wall that connects the front wall to the side wall, and the curved transition wall may have a radius of curvature of at least 50 mm.
In some embodiments, the radome may further include a side wall and a curved front transition wall that connects the front wall to the side wall, and the curved transition wall may have a radius of curvature of at least 90 mm.
In some embodiments, the radiating element may be configured to operate in at least a portion of the 617-960 MHz frequency band.
In some embodiments, the radome may further include a side wall and a curved front transition wall that connects the front wall to the side wall, and an overlap portion of the outer dipole arm overlaps the curved front transition wall may be at least half a length of the outer dipole arm.
In some embodiments, a largest minimum distance between any point on a front surface of the overlap portion of the outer dipole arm and the radome may be less than 1.5 times a smallest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome.
Pursuant to further embodiments of the present invention, base station antennas are provided that include a reflector, a radome having a front wall, a side wall and a curved front transition wall that connects the front wall to the side wall, the curved front transition wall having a radius of curvature of at least 50 mm, and a radiating element mounted to extend forwardly from the reflector, the radiating element including an inner dipole arm and an outer dipole arm. An overlap portion of the outer dipole arm overlaps the curved front transition wall, and a largest minimum distance between any point on a front surface of the overlap portion of the outer dipole arm and the radome is less than 1.5 times a minimum distance between the front wall of the radome and the front surface of the outer dipole arm.
In some embodiments, the curved front transition wall may have a radius of curvature of at least 90 mm.
In some embodiments, the radiating element may be configured to operate in at least a portion of the 617-960 MHz frequency band.
In some embodiments, the largest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome may be less than 1.5 times a smallest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome.
Pursuant to additional embodiments of the present invention, base station antennas are provided that include a backplane having a planar reflector, a radome having a front wall, a side wall and a curved front transition wall that connects the front wall to the side wall, the curved front transition wall of the radome having a radius of curvature of at least 75 mm, and a radiating element mounted to extend forwardly from the reflector, the radiating element including an inner dipole arm and an outer dipole arm. A distal end of the outer dipole arm is closer to the planar reflector than is a base of the outer dipole arm.
In some embodiments, a minimum distance between each point on a front surface of the outer dipole arm and the radome may vary by less than 50% or by less than 25%.
In some embodiments, the curved front transition wall may have a radius of curvature of at least 90 mm.
In some embodiments, the radiating element may be configured to operate in at least a portion of the 617-960 MHz frequency band.
In some embodiments, an overlap portion of the outer dipole arm overlaps the curved front transition wall, and a largest minimum distance between any point on a front surface of the overlap portion of the outer dipole arm and the radome may be less than 1.5 times a smallest minimum distance between any point on the front surface of the overlap portion of the outer dipole arm and the radome.
In some embodiments, the outer dipole arm may include at least two bends along a longitudinal axis of the outer dipole arm that divide the outer dipole arm into a plurality of longitudinally-extending sections that are angled with respect to each other. In some embodiments, distances between centers of each longitudinally-extending section and respective closest points on the radome may vary by less than 25%.
In some embodiments, at least half a length of the outer dipole arm may overlap the curved front transition wall.
Two part reference numerals may be used to refer to elements that are duplicated in the base station antennas according to embodiments of the present invention. Herein, the full reference numeral (e.g., linear array 130-2) may be used to refer to a specific instance of such an element, while the first part of the reference numeral (e.g., the linear arrays 130) may be used to refer to the elements collectively.
It will be appreciated that when base station antennas are mounted for use, the radiating elements typically extend forwardly from a reflector. For convenience, many of the figures, however, depict the radiating elements and/or base station antenna rotated 90° from this configuration. The text herein describes these figures using directional references that are consistent with the orientation of the base station antennas when mounted for use as opposed to how they are shown in some of the figures.
Traditionally, the radiating elements of a base station antenna and the housing of the antenna are designed independently of each other. In particular, the radiating elements will be designed based on desired RF performance characteristics for the antenna, and the housing, including the radome, is designed separately based, for example, on a known width for the reflector of the antenna and other considerations. The radome typically has a front wall and side walls, and most (but not all) radomes further include a back wall so that the radome may be formed as an open tube that surrounds and protects an antenna assembly of the base station antenna. The “corners” where the front wall meets each side wall and where the back wall meets each side wall are typically implemented as curved transition walls in order to reduce the wind loading on the antenna. In a typical antenna design, the radius of curvature of the curved front transition walls may be about 30-35 mm.
As mentioned above, the curved front transition walls 66 typically have a relatively small radii of curvature. This ensures that there is room for the linear arrays 30 of radiating elements 40 to be spaced sufficiently far apart to have good isolation and also ensures that the radiating elements 40 will fit within the radome 60 with sufficient clearance so that the radiating elements 40 will not be damaged when the radome 60 flexes during handling or under wind loading. However, the conventional design process often results in empty space along the front sides of the antenna 1, which is indicated by reference numeral 70 in
Pursuant to embodiments of the present invention, the design process for the radiating elements and the antenna housing may be performed as a combined process so that the “outer” dipole arms of the radiating elements 40 (i.e., the dipole arms that extend close to the side walls of the radome 60) conform, at least to an extent, to the shape of the curved front transition walls of the radome 60. This can be accomplished, for example, by bending at least a portion of each outer dipole arm rearwardly into the space 70 shown in
In some embodiments, base station antennas are provided that include a planar reflector, a radiating element mounted to extend forwardly from the planar reflector, and a radome. The radiating element may include a dipole that has an inner dipole arm and an outer dipole arm. The radome has a front wall, a side wall and a curved front transition wall that connects the front wall to the side wall. The outer dipole arm is bent so that a distal end of the outer dipole arm is closer to the planar reflector than is a base of the outer dipole arm. An overlap portion of the outer dipole arm “overlaps” the curved front transition wall. As discussed herein with reference to
In further embodiments, base station antennas are provided that have a planar reflector, a radiating element that includes an inner dipole arm and an outer dipole arm mounted to extend forwardly from the reflector, and a radome that has a front wall that is positioned in front of the radiating element. The outer dipole arm includes at least two bends along a longitudinal axis of the outer dipole arm that divide the outer dipole arm into a plurality of longitudinally-extending sections that are angled with respect to the reflector and with respect to each other, where distances between centers of each longitudinally-extending section and respective closest points on the radome vary by less than 50%.
In yet additional embodiments, base station antennas are provided that include a reflector, a radiating element that includes an inner dipole arm and an outer dipole arm mounted to extend forwardly from the reflector, and a radome having a front wall, a side wall and a curved front transition wall that connects the front wall to the side wall. The curved front transition wall may have a radius of curvature of at least 50 mm. An overlap portion of the outer dipole arm overlaps the curved front transition wall. Moreover, a largest minimum distance between any point on a front surface of the overlap portion of the outer dipole arm and the radome is less than 1.5 times a minimum distance between the front wall of the radome and the front surface of the outer dipole arm.
According to still further embodiments, base station antennas are provided that include a backplane having a planar reflector, a radome having a front wall, a side wall and a curved front transition wall that connects the front wall to the side wall, the curved front transition wall of the radome having a radius of curvature of at least 75 mm, and a radiating element mounted to extend forwardly from the reflector, the radiating element including an inner dipole arm and an outer dipole arm.
Example base station antennas according to embodiments of the present invention will now be discussed in greater detail with reference to
As shown in
Since the outer dipole arms 148 are bent rearwardly, they do not extend as far into the front corner regions of the radome 160 as do the outer dipole arms of the radiating elements 40 of the conventional base station antenna 1. Consequently, the curved front transition walls 166 of radome 160 may have larger radii of curvature as compared to the corresponding curved front transition walls 66 of radome 60 of the conventional base station antenna 1. The additional curvature in the walls of radome 166 may significantly improve the wind loading performance of base station antenna 100 as compared to conventional base station antenna 1. In example embodiments, the radius of curvature may be extended from about 30 mm in the conventional antenna 1 to 50 mm, 60 mm, 70 mm, 80 mm, 90 mm 100 mm or more in base station antenna 100. By forming the front corner walls of the radome 160 to have larger radii of curvature the wind loading performance of the antenna 100 may be improved considerably. Moreover, since the radome 160 may be designed in conjunction with the radiating elements 140, the radome 160 may be made to generally conform to the shape of the outer dipole arms (and vice versa) so that a maximum improvement in wind loading performance may be achieved. In some embodiments of the present invention, the curved front transition wall may not have a constant radius of curvature. In such embodiments, the radius of curvature of the curved front transition wall is considered to be the radius of curvature of a representative line Lrep on the curved front transition wall of the radome. The representative line Lrep is a line that is defined by three planes P1 through P3, where plane P1 is a plane that is parallel to the reflector that intersects the forward most point of the front wall of the radome, plane P2 is a plane that is perpendicular to plane P1 that intersects the leftward (or rightward) most point on the left (or right) side wall of the radome, and plane P3 is a plane that extends at an angle of 45° from the line defined by the intersection of planes P1 and P2. The line Lrep is normal to plane P3. Planes P1-P3 and Lrep are shown in
Typically, performance parameters will be established for the linear arrays 130 of radiating elements 140 in terms of antenna pattern size (e.g., azimuth and elevation beamwidths), antenna pattern shape (e.g., gain roll off, sidelobe and grating lobe levels), return loss, cross-polarization performance, and various other performance parameters. The radiating elements 140 may be designed to meet these performance parameters. Bending the dipole arms 146, 148 rearwardly may, in many cases, act to improve some performance parameters (e.g., cross-polarization performance) while degrading other performance parameters (e.g., impedance match/return loss, which impacts the operating bandwidth of the linear array 130). As part of the design process, the extent to which the outer dipole arms 148 are bent rearwardly (through one or more bends in each outer dipole arm 148) may be varied to ensure that the linear arrays 130 meet the minimum performance requirements. In some cases, a maximum amount of bending may be applied (i.e., the extent to which the outer dipole arms 148 are bent rearwardly is increased until a performance parameter is barely achieved) so that the radius of curvature of the curved front transition walls 166 may be increased as much as possible. In other cases, the designers may weigh the increase in wind loading performance against any decrease in RF performance and select an amount of bend in the outer dipole arms 148 that provides a good tradeoff between the different performance parameters. In still other embodiments, more complex tradeoffs and design changes may be made. For example, while bending the dipole arms 148 rearwardly tends to degrade the return loss performance of the linear arrays 130, increasing the length of the feed stalk 142 (i.e., how far the feed stalk 142 extends in the forward direction) may act to counter the degradation in return loss performance. Thus, in some cases, it may be advantageous to lengthen the feed stalks 142 (which increases the depth of the antenna 100, which degrades wind loading performance in certain directions) in order to allow increased bending of the outer dipole arms 148 in order to increase the radius of curvature on each of the curved front transition walls 166 of the radome 160.
As described above, by designing the radiating elements 140 and the radome 160 in parallel, base station antennas may be provided that achieve improved wind loading performance while meeting all RF performance parameters. In essence, compromises between RF performance and wind loading performance may be considered to provide a base station antenna that exhibits overall improved performance. This approach also may act to reduce the amount of wasted empty space in the antenna, and may reduce material costs (since the size of the radome may be reduced).
While
As shown in
The linear arrays 230 may be, for example, linear arrays of radiating elements 240 that are configured to operate in all or part of the 617-960 MHz frequency band. In modern base station antennas, radiating elements that operate in all or part of the 617-960 MHz frequency band are typically referred to as “low-band” radiating elements as this frequency band is typically the lowest frequency range used for cellular communications. The low-band radiating elements are typically the largest radiating elements included in the antenna, since the size of a radiating element is generally inversely proportional to the center frequency of the operating frequency band of the radiating element. Thus, the linear arrays 230 of low-band radiating elements 240 tend to drive the depth of the radome 260 as well as the radius of curvature of the curved front transition walls 266 of the radome 260. Each low-band linear array 230 may have any appropriate number of radiating elements 240 (with the number of radiating elements 240 typically selected to achieve a desired elevation beamwidth for the antenna beams generated by the linear arrays 230). It will also be appreciated that additional linear arrays of radiating elements (not shown) such as mid-band linear arrays formed of radiating elements that operate in all or part of the 1427-2690 MHz frequency band or high-band linear arrays formed of radiating elements that operate in all or part of the 3100-4200 MHz frequency band and/or the 5100-5800 MHz frequency band may also be included in base station antenna 200. These additional linear arrays are omitted from
Referring now to
Each dipole arm 246, 248 may have a generally oval shape and may be formed as a series of widened sections 254 that are connected by narrowed inductive traces 256. This may help make the dipole arms 246, 248 relatively transparent to RF energy within the operating frequency bands of any mid-band and/or high-band linear arrays of radiating elements included in base station antenna 200. In some embodiments, the dipole arms 246, 248 may have the design disclosed in U.S. Pat. No. 10,770,803 (“the '803 patent”), except that the radiating element 240 further includes the primary bends 250 and secondary bends 252 (discussed below) in each dipole arm 246, 248. The disclosure of the '803 patent is incorporated herein by reference as if set forth fully herein.
Each dipole arm 246, 248 also includes a pair of secondary bends 252 where outer portions of selected of the widened segments 254 of the dipole arm 246, 248 are bent at a sharp angle (here about 90°) with respect to a plane P1. The secondary bends 252 act to increase the electrical length of each dipole arm 246, 248 without increasing the “footprint” of the dipole arm 246, 248 (i.e., the perimeter of the dipole arm 246, 248 when the radiating element 240 is viewed from the front). This allows the overall physical length of each dipole arm 246, 248 to be reduced, which may also allow for increasing the radius of curvature of each of the curved front transition walls 266 or, alternatively, reducing the overall width of the base station antenna 200, both of which may improve the wind loading performance of the antenna 200. Herein, a primary bend in a dipole refers to a bend that angles the distal end of the dipole arm rearwardly from a plane defined by the bases of the dipole arms that is parallel to the reflector of the base station antenna.
Referring again to
As shown in
The radiating elements 340 comprise −45°/+45° cross-dipole radiating elements. Each radiating element 340 includes a pair of dipole radiators, and each dipole radiator includes an inner dipole arm 346 and an outer dipole arm 348. Only one inner dipole arm 346 and one outer dipole arm 348 are visible in the views of
It will be appreciated that a wide variety of different dipole arm designs may be used that allow for increasing the radius of curvature of each curved front transition wall of the radome of a base station antenna.
In some embodiments, radiating elements may be used that have dipole arms with a primary bend that is a large angle. For example,
As shown in
As shown in
The base station antennas according to embodiments of the present invention may more efficiently utilize the space inside the radome, which may allow for increasing the radius of curvature of the curved forward transition walls of the radome, which may improve the wind loading performance of the antenna.
Referring to
Referring to
Referring to
Referring to
The base station antennas according to embodiments of the present invention may provide improved performance as compared to comparable conventional base station antennas.
It will be appreciated that the present specification only describes a few example embodiments of the present invention and that the techniques described herein have applicability beyond the example embodiments described above.
Embodiments of the present invention have been described above with reference to the accompanying drawings, in which embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. Like numbers refer to like elements throughout.
It will be understood that, although the terms first, second, etc. may be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element, without departing from the scope of the present invention. As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items.
It will be understood that when an element is referred to as being “on” another element, it can be directly on the other element or intervening elements may also be present. In contrast, when an element is referred to as being “directly on” another element, there are no intervening elements present. It will also be understood that when an element is referred to as being “connected” or “coupled” to another element, it can be directly connected or coupled to the other element or intervening elements may be present. In contrast, when an element is referred to as being “directly connected” or “directly coupled” to another element, there are no intervening elements present. Other words used to describe the relationship between elements should be interpreted in a like fashion (i.e., “between” versus “directly between”, “adjacent” versus “directly adjacent”, etc.).
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” “comprising,” “includes” and/or “including” when used herein, specify the presence of stated features, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, operations, elements, components, and/or groups thereof.
Aspects and elements of all of the embodiments disclosed above can be combined in any way and/or combination with aspects or elements of other embodiments to provide a plurality of additional embodiments.
The present application claims priority under 35 U.S.C. § 119 to U.S. Provisional Application Ser. No. 63/191,492, filed May 21, 2021, the entire content of which is incorporated herein by reference as if set forth in its entirety.
Number | Date | Country | |
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63191492 | May 2021 | US |