CN115810910A - Antenna cover and antenna device - Google Patents

Antenna cover and antenna device Download PDF

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Publication number
CN115810910A
CN115810910A CN202111068308.6A CN202111068308A CN115810910A CN 115810910 A CN115810910 A CN 115810910A CN 202111068308 A CN202111068308 A CN 202111068308A CN 115810910 A CN115810910 A CN 115810910A
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China
Prior art keywords
arc
radome
segment
straight line
antenna
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CN202111068308.6A
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Chinese (zh)
Inventor
杨天勇
张伟
于海军
张戈
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Huawei Technologies Co Ltd
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Huawei Technologies Co Ltd
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Priority to CN202111068308.6A priority Critical patent/CN115810910A/en
Priority to PCT/CN2022/117609 priority patent/WO2023036192A1/en
Priority to EP22866655.8A priority patent/EP4386982A1/en
Publication of CN115810910A publication Critical patent/CN115810910A/en
Pending legal-status Critical Current

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/005Damping of vibrations; Means for reducing wind-induced forces
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/22Supports; Mounting means by structural association with other equipment or articles
    • H01Q1/24Supports; Mounting means by structural association with other equipment or articles with receiving set
    • H01Q1/241Supports; Mounting means by structural association with other equipment or articles with receiving set used in mobile communications, e.g. GSM
    • H01Q1/246Supports; Mounting means by structural association with other equipment or articles with receiving set used in mobile communications, e.g. GSM specially adapted for base stations
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Details Of Aerials (AREA)

Abstract

The application provides an antenna housing and an antenna device. The antenna cover has a space formed therein for accommodating the antenna. At least a part of a cover body of the radome has a cross-sectional shape in a cross section perpendicular to a longitudinal direction of the radome. The sectional shape is formed in a closed shape, the sectional shape includes one straight line segment, and the sectional shape is symmetrical with respect to a reference line that passes through a midpoint of the straight line segment and is perpendicular to the straight line segment. On one side of the datum line, the section shape comprises a plurality of arc line sections connected with one side end of the straight line section, the circle centers corresponding to all the arc line sections are located in the closed shape, and the curvature radiuses of the plurality of arc line sections from one side end become larger in sequence. Thus, the radome of the present application having such a cross-sectional shape can optimize the wind load applied to the radome by the radome against wind from various directions, thereby reducing wind resistance.

Description

Antenna cover and antenna device
Technical Field
The application relates to the field of antennas, in particular to an antenna housing and an antenna device comprising the same.
Background
With the development of the technology, the bearing capacity of the antenna device approaches the limit, and the wind load of the antenna housing of the antenna device becomes a key technical index influencing the product performance of the antenna device, so that the low wind load design of the antenna housing becomes one of the main directions of the industry development. In the prior art radome, means such as additional provision of vortex generators and construction of a radome having a special configuration have been added to achieve a low wind load design of the radome. However, these designs can only achieve optimization of the wind load for a specific wind direction (angle of attack) of the radome.
For example, the radome disclosed in patent document No. DE202018006123U1 can reduce only the wind load in a specific direction, but deteriorates the wind load from the wind in other directions. In patent document US9979079B2, the peak of the wind load is reduced by providing a wire loop on the antenna cover, but this solution is optimized only for the wind load of the side wind of the antenna device, and adversely affects the wind load of the wind from other directions.
Disclosure of Invention
In view of the problems existing in the background art, the present application provides an antenna cover which can greatly optimize the omnidirectional wind load compared with the existing antenna cover. In addition, the application also provides an antenna device comprising the antenna housing, and the antenna device has the same effects as those described above.
Therefore, the following technical scheme is adopted in the application.
In a first aspect, an embodiment of the present application provides a radome characterized in that a space for housing an antenna is formed inside the radome, at least a portion of a cover body of the radome has a cross-sectional shape in a cross-section perpendicular to a length direction of the radome,
the sectional shape is formed in a closed shape including one straight line segment and being symmetrical with respect to a reference line passing through a midpoint of the straight line segment and perpendicular to the straight line segment,
on one side of the datum line, the section shape comprises a plurality of arc line segments connected with one side end of the straight line segment, the circle centers of all the arc line segments are located in the closed shape, and the curvature radiuses of the arc line segments are sequentially increased from the one side end.
Through adopting above-mentioned technical scheme, compare with prior art's antenna house, the antenna house of this application that has above cross sectional shape can optimize the antenna house and exert the wind-load on the antenna house to the wind that comes from all directions to reduce the windage.
In one possible embodiment according to the first aspect, the connecting portion of two adjacent arc segments is formed with a chamfer.
By adopting the technical scheme, smooth connection of the adjacent arc line sections can be realized, so that wind load applied to the antenna housing by the antenna housing to wind from all directions is further optimized, and wind resistance is reduced.
In a possible implementation manner according to the first aspect, on one side of the reference line, the cross-sectional shape includes a first arc segment, a second arc segment and a third arc segment, one end of the first arc segment is connected with one end of the straight line segment, the other end of the first arc segment is connected with one end of the second arc segment, and the other end of the second arc segment is connected with one end of the third arc segment.
Through adopting above-mentioned technical scheme, provide one kind and easily construct the scheme of the antenna house of this application.
In one possible implementation form according to the first aspect, the third arc segment has a length greater than the first arc segment, and the first arc segment has a length greater than the second arc segment.
By adopting the technical scheme, the wind load applied to the antenna housing by the antenna housing to wind from all directions can be further optimized by setting the length relation between different arc line sections.
In one possible implementation manner according to the first aspect, when the midpoint of the straight line segment is the origin of coordinates, the x-axis is along the straight line where the straight line segment is located and the positive direction of the x-axis is toward the one side, the y-axis is along the reference line and the positive direction of the y-axis is toward the third arc line segment,
the first arc line section satisfies the following relational expression: (x-a) 2 +(y-0.6a) 2 =0.36a 2 ,x∈(a,1.6a);
The second arc line section satisfies the following relational expression: (x-0.6 a) 2 +(y-0.7a) 2 =a 2 ,x∈(1.5a,1.6a);
The third arc line segment satisfies the following relation: x is a radical of a fluorine atom 2 +(y-0.4a) 2 =2.78a 2 ,x∈(0,1.5a),
Where a is a dimensionless reference number and is an arbitrary real number.
By adopting the technical scheme, the non-dimensional function relation of the arc line segment is set, so that the optimal section shape of the component is facilitated. But also the cross-sectional shape of the present application can be applied to antennas of different sizes.
In one possible embodiment according to the first aspect, the length of said straight line segment is 2a.
By adopting the technical scheme, the length relation of the straight line sections matched with the circular arc line sections is further limited.
In one possible embodiment according to the first aspect, the radome further comprises a trip wire fixed to the cover body, the trip wire extending along a length direction of the cover body, the trip wire being formed in a configuration protruding from an outer surface of the cover body.
Through adopting above-mentioned technical scheme, can make the air current realize the separation in the antenna housing expectation position through setting up the line of tripping to further optimize the antenna housing and exert the wind-load in the antenna housing to the wind that comes from all directions.
In one possible embodiment according to the first aspect, the radome further includes a trip wire fixed to the radome body, the trip wire extending along a length direction of the radome body, the trip wire being formed in a configuration protruding from an outer surface of the radome body, the trip wire being provided at a midpoint of the third circular arc segment and/or the trip wire being provided at a connection point of the first circular arc segment and the second circular arc segment.
Through adopting above-mentioned technical scheme, can make the air current realize the separation in the antenna housing expectation position through setting up the line of tripping to further optimize the antenna housing and exert the wind-load in the antenna housing to the wind that comes from all directions.
In one possible embodiment according to the first aspect, the length of the trip wire is equal to the length of the cover body.
By adopting the technical scheme, the ability of separating the airflow at the expected position on the antenna cover can be fully exerted by the aid of the tripwire.
In one possible embodiment according to the first aspect, the trip wire is rectangular, trapezoidal or triangular in shape in said cross-section.
Through adopting above-mentioned technical scheme, be favorable to making the tripwire.
In a second aspect, an embodiment of the present application provides an antenna device, where the antenna device includes the antenna cover according to any one of the above technical solutions.
By adopting the above technical scheme, the antenna device including the present application can exert the function of the antenna cover described above.
In a possible embodiment according to the second aspect, the antenna arrangement comprises a plurality of radomes arranged in a circular array.
By adopting the technical scheme, the beneficial arrangement scheme of the antenna housing is provided.
In one possible embodiment according to the second aspect, the antenna arrangement is used for a radio base station antenna arrangement of a communication network.
By adopting the technical scheme, an optional application scene of the antenna housing is provided.
These and other aspects of the present application will be more readily apparent from the following description of the embodiment(s).
Drawings
The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate exemplary embodiments, features, and aspects of the application and, together with the description, serve to explain the principles of the application.
Fig. 1 is a schematic perspective view illustrating a structure of a radome according to an embodiment of the present application.
Fig. 2 is a side view schematically showing the structure of the radome in fig. 1.
Fig. 3 is a cross-sectional view showing a sectional shape of the radome in fig. 1.
Fig. 4A to 4C are schematic views showing a cross-sectional shape of a trip wire of the radome in fig. 1.
Description of the reference numerals
1 cover main body LS straightway ARC1 first ARC ARC2 second ARC ARC3 third ARC ARC4 fourth ARC ARC5 fifth ARC ARC6 sixth ARC ARC2 trip wire
L length direction.
Detailed Description
Various exemplary embodiments, features and aspects of the present application will be described in detail below with reference to the accompanying drawings. In the drawings, like reference numbers can indicate functionally identical or similar elements. While the various aspects of the embodiments are presented in drawings, the drawings are not necessarily drawn to scale unless specifically indicated.
The word "exemplary" is used exclusively herein to mean "serving as an example, embodiment, or illustration. Any embodiment described herein as "exemplary" is not necessarily to be construed as preferred or advantageous over other embodiments.
In addition, in the following detailed description, numerous specific details are set forth in order to provide a better understanding of the present application. It will be understood by those skilled in the art that the present application may be practiced without some of these specific details. In some instances, methods, means, elements well known to those skilled in the art have not been described in detail so as not to obscure the present application.
In the present application, the "longitudinal direction" refers to the longitudinal direction of the radome (cover body), unless otherwise specified.
First, the overall technical concept of the radome according to the present application is explained. According to the radome of this application through the cross-sectional shape that changes the cover main part to further the transition of the air current that obtains according to the experiment is twisted and is set up the line of tripping with the isolated position at the specific position of cover main part, thereby realizes that the radome of this application compares with current radome and has obtained the optimization of qxcomm technology wind-load.
The structure of a radome according to an embodiment of the present application is described below with reference to the accompanying drawings.
As shown in fig. 1 to 3, an antenna cover according to an embodiment of the present application has a long rod structure extending linearly as a whole. The radome includes a radome body 1 and a trip wire 2 fixed to an outer surface of the radome body 1.
As shown in fig. 1 and 3, a space for housing components that realize the antenna function is formed inside the cover main body 1. In the present embodiment, the cover body 1 has a cross section perpendicular to the longitudinal direction L of the radome, and the cross-sectional shape of any portion of the cover body 1 is the same. The cross-sectional shape of the cover main body 1 of the radome is optimized to achieve omnidirectional wind load optimization.
Specifically, as shown in fig. 3, the cross-sectional shape of the cover main body 1 is formed into a closed shape. The cross-sectional shape comprises one straight line segment LS and a plurality of circular ARC segments ARC1 to ARC6. The sectional shape is symmetrical with respect to a reference line passing through a midpoint of the straight line segment LS and perpendicular to the straight line segment LS. On one side of the reference line (the right side in fig. 3), the cross-sectional shape includes a first ARC segment ARC1, a second ARC segment ARC2, and a third ARC segment ARC3 connected to one side end of the straight line segment LS. One end of the first ARC line segment ARC1 is connected with one side end of the straight line segment LS, the other end of the first ARC line segment ARC1 is connected with one end of the second ARC line segment ARC2, and the other end of the second ARC line segment ARC2 is connected with one end of the third ARC line segment ARC3. As described above, the cross-sectional shape of the cross-section of the mask body 1 is symmetrical about the reference line, and on the other side (left side in fig. 3) of the reference line, the cross-sectional shape includes the fourth ARC segment ARC4, the fifth ARC segment ARC5, and the sixth ARC segment ARC6 connected to the other side end of the straight line segment LS. The fourth ARC line segment ARC4 and the first ARC line segment ARC1 are symmetrical about the reference line, the fifth ARC line segment ARC5 and the second ARC line segment ARC2 are symmetrical about the reference line, and the sixth ARC line segment ARC6 and the third ARC line segment ARC3 are symmetrical about the reference line. One end of the fourth ARC line segment ARC4 is connected with the other side end of the straight line segment LS, the other end of the fourth ARC line segment ARC4 is connected with one end of the fifth ARC line segment ARC5, the other end of the fifth ARC line segment ARC5 is connected with one end of the sixth ARC line segment ARC6, and the other end of the sixth ARC line segment ARC6 is connected with the other end of the third ARC line segment ARC3. In fact, the other ends of the sixth ARC segment ARC6 and the third ARC segment ARC3 are coincident and both located on the reference line, and the sixth ARC segment ARC6 and the third ARC segment ARC3 can be regarded as the same ARC segment.
The centers of circles corresponding to all the ARC line segments (the first ARC line segment ARC1 to the sixth ARC line segment ARC 6) are located inside the closed shape. On one side of the datum line, the curvature radiuses of the ARC line segments ARC1 to ARC3 from one side end of the straight line segment LS become larger in sequence, that is, the curvature radius of the first ARC line segment ARC1 is smaller than that of the second ARC line segment ARC2, and the curvature radius of the second ARC line segment ARC2 is smaller than that of the third ARC coil. Further, the length of the third ARC segment ARC3 is greater than the length of the first ARC segment ARC1, and the length of the first ARC segment ARC1 is greater than the length of the second ARC segment ARC 2. On the other side of the reference line, the curvature radii of the ARC segments ARC4 to ARC6 from the other side end of the straight line segment LS become larger in sequence, that is, the curvature radius of the fourth ARC segment ARC4 is smaller than that of the fifth ARC segment ARC5, and the curvature radius of the fifth ARC segment ARC5 is smaller than that of the sixth ARC coil. Further, the length of the sixth ARC segment ARC6 is greater than the length of the fourth ARC segment ARC4, and the length of the fourth ARC segment ARC4 is greater than the length of the fifth ARC segment ARC 5.
Further, except for the connecting position between the third ARC line segment ARC3 and the sixth ARC line segment ARC6, the outer surfaces of the connecting positions of the two adjacent ARC line segments form chamfers, especially fillets, so that a smooth connection mode is adopted between the two adjacent ARC line segments.
In this way, the cover body 1 having the above-described sectional shape is advantageous in optimizing the wind load applied to the radome by the radome against wind from various directions, thereby reducing wind resistance.
In the present embodiment, through experiments, the purpose of optimizing the omnidirectional wind load of the present application can be better achieved when the following relational expression is satisfied for the arc line segment in the cross section of the shroud body 1 of the present application.
When the middle point of the straight line segment LS is the origin of coordinates, the x-axis is along the straight line where the straight line segment LS is located, and the forward direction of the x-axis faces one side of the reference line, the y-axis is along the reference line, and the forward direction of the y-axis faces the third ARC line segment ARC3 and the sixth ARC line segment ARC6,
the three arc segments on one side of the reference line satisfy the following relational expression.
The first ARC segment ARC1 satisfies the following relation: (x-a) 2 +(y-0.6a) 2 =0.36a 2 And x belongs to (a, 1.6 a), and the coordinate of the circle center O1 corresponding to the first ARC line segment ARC1 is (a, 0.6 a).
The second ARC segment ARC2 satisfies the following relation: (x-0.6 a) 2 +(y-0.7a) 2 =a 2 And x belongs to (1.5a, 1.6a), and the coordinate of the circle center O2 corresponding to the second ARC line section ARC2 is (0.6a, 0.7a).
The third ARC segment ARC3 satisfies the following relation: x is the number of 2 +(y-0.4a) 2 =2.78a 2 And x belongs to (0, 1.5a), and the coordinate of the center O3 corresponding to the second ARC line segment ARC2 is (0, 0.4a).
As described above, since the cross-sectional shape of the cover main body 1 in the cross section is symmetrical with respect to the reference line, the three arc segments on the other side of the reference line satisfy the following relational expression.
The fourth ARC segment ARC4 satisfies the following relation: (x + a) 2 +(y-0.6a) 2 =0.36a 2 And x belongs to (-1.6 a, -a), and the coordinate of the center of the circle corresponding to the fourth ARC segment ARC4 is (-a, 0.6 a).
The fifth ARC line segment ARC5 satisfies the following relation: (x +0.6 a) 2 +(y-0.7a) 2 =a 2 And x belongs to (-1.6 a, -1.5 a), and the coordinate of the center of the circle corresponding to the fifth circular ARC segment ARC5 is (-0.6a, 0.7a).
The sixth ARC line segment ARC6 satisfies the following relation: x is the number of 2 +(y-0.4a) 2 =2.78a 2 And x belongs to (-1.5a, 0), the coordinate of the center of the circle corresponding to the sixth ARC line segment ARC6 is (0, 0.4a), and the center of the circle corresponding to the sixth ARC line segment ARC6 and the center of the circle corresponding to the third ARC line segment ARC3 are located at the same coordinate point.
Further, the length of the straight line segment LS is 2a.
In the above relational expression, a is a dimensionless constant and may be an arbitrary real number. By setting the dimensionless functional relationship, the application of the cross-sectional shape of the present application to antennas of different sizes is facilitated.
Further, as shown in fig. 1 and 2, the catch wire 2 extends along the longitudinal direction L of the cover main body 1, and the length of the catch wire 2 is equal to the length of the cover main body 1. The catch wire 2 is formed in a configuration protruding from the outer surface of the cover main body 1. In this embodiment, the trip line 2 is disposed at a midpoint of the third ARC segment ARC3, a midpoint of the sixth ARC segment, a connection between the first ARC segment ARC1 and the second ARC segment ARC2, and a connection between the fourth ARC segment and the fifth ARC segment. The arrangement of the trip wire 2 can separate the airflow formed by wind at a desired position on the antenna housing, so that the wind load applied to the antenna housing by the antenna housing to the wind from all directions is further optimized.
As shown in fig. 4A to 4C, the shape of the trip wire 2 in cross section may be rectangular, trapezoidal (e.g., isosceles trapezoid), or triangular (equilateral triangle). The maximum height of the trip wire 2 protruding from the outer surface of the cover main body 1 may be about 1 mm. That is, when the cross section of the trip wire 2 is rectangular and the long side of the rectangle is connected to the outer surface of the cover main body 1, the length of the short side of the rectangle is about 1 mm. When the cross section of the trip wire 2 is an isosceles trapezoid and the long bottom side of the isosceles trapezoid is connected with the outer surface of the cover main body 1, the height of the isosceles trapezoid is about 1 mm. When the cross section of the trip wire 2 is an equilateral triangle and one side of the equilateral triangle is connected with the outer surface of the cover main body 1, the height of the equilateral triangle is about 1 mm. In addition, other sizes of the cross section of the trip wire 2 may be set as required, for example, when the cross section of the trip wire 2 is an isosceles trapezoid, the size of the long base of the isosceles trapezoid may be 5mm and the size of the short base may be 4mm.
Experiments show that by using a radome with the above cross-sectional dimensions, the wind resistance can be optimized in most directions compared to existing radomes. The data in table 1 below are parameters measured by a wind tunnel test for an existing radome (the sectional shape having a flat configuration) and a radome according to the present application (the sectional shape having a shape as described above, i.e., a mushroom-like shape).
TABLE 1
Figure BDA0003259421640000051
Figure BDA0003259421640000061
In table 1 above, when the windward angle is 0 °, the radome is in the first state in the wind tunnel as follows: the wind direction in the wind tunnel is over against the convex vertex part of the radome according to the present application (that is, the wind direction is towards the part formed by the other end points of the third ARC segment ARC3 and the sixth ARC segment ARC6 of each section of the radome, and the wind direction extends along the reference line); when the windward angle is 180 degrees, the antenna housing is in the following second state in the wind tunnel: the wind direction in the wind tunnel is opposite to the flat plate part of the radome according to the application (namely, the wind direction faces to the part formed by straight line sections LS of all the sections of the radome, and the wind direction extends along a datum line); other angles of attack are angles through which the radome turns from the first state around its central axis towards the second state.
Further, the present application also provides an antenna device, which may be a wireless base station antenna device for a communication network. The antenna device may include one antenna cover or a plurality of antenna covers as described above, depending on the case of the component that performs the antenna function. When the antenna device comprises a plurality of radomes, the radomes are arranged in a circular array, so that the convex part of each radome faces the outer side of the circular array.
The foregoing has outlined exemplary embodiments of the detailed description of the present application and related modifications, as well as additional descriptions that follow.
i. Although it is described in the above embodiments that the antenna device is a radio base station antenna device for a communication network, the present application is not limited thereto. The antenna device according to the present application may be used for other purposes.
it is to be understood that a plurality of trip wires may be provided in parallel with each other at a portion of the radome where the trip wire is provided, and the cross-sectional shape and size of the trip wire are not limited to those illustrated in the above embodiments, but may be adjusted as needed.
While the present application has been described in connection with various embodiments, other variations to the disclosed embodiments can be understood and effected by those skilled in the art in practicing the claimed application, from a review of the drawings, the disclosure, and the appended claims. In the claims, the word "comprising" does not exclude other elements or steps, and the word "a" or "an" does not exclude a plurality. The mere fact that certain measures are recited in mutually different dependent claims does not indicate that a combination of these measures cannot be used to advantage.
Having described embodiments of the present application, the foregoing description is intended to be exemplary, not exhaustive, and not limited to the disclosed embodiments. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments. The terminology used herein is chosen in order to best explain the principles of the embodiments, the practical application, or improvements made to the technology in the marketplace, or to enable others of ordinary skill in the art to understand the embodiments disclosed herein.

Claims (13)

1. A radome characterized in that a space for housing an antenna is formed inside the radome, at least a portion of a cover body of the radome has a cross-sectional shape in a cross-section perpendicular to a longitudinal direction of the radome,
the sectional shape is formed in a closed shape including one straight line segment and being symmetrical with respect to a reference line passing through a midpoint of the straight line segment and perpendicular to the straight line segment,
on one side of the datum line, the cross-sectional shape comprises a plurality of arc line segments connected with one side end of the straight line segment, the circle centers of all the arc line segments are located in the closed shape, and the curvature radiuses of the arc line segments are sequentially increased from the one side end.
2. The radome of claim 1, wherein a chamfer is formed at a connection portion of two adjacent arc segments.
3. The radome of claim 1 or 2, wherein the cross-sectional shape includes a first arc segment, a second arc segment and a third arc segment on one side of the reference line, one end of the first arc segment is connected to one end of the straight segment, the other end of the first arc segment is connected to one end of the second arc segment, and the other end of the second arc segment is connected to one end of the third arc segment.
4. The radome of claim 3, wherein the third arc segment has a length greater than a length of the first arc segment, and wherein the first arc segment has a length greater than a length of the second arc segment.
5. The radome of claim 3, wherein when the midpoint of the straight line segment is the origin of coordinates, the x-axis is along the straight line where the straight line segment is located and the positive direction of the x-axis is toward the one side, the y-axis is along the reference line and the positive direction of the y-axis is toward the third arc line segment,
the first arc line section satisfies the following relational expression: (x-a) 2 +(y-0.6a) 2 =0.36a 2 ,x∈(a,1.6a);
The second arc line section satisfies the following relational expression: (x-0.6 a) 2 +(y-0.7a) 2 =a 2 ,x∈(1.5a,1.6a);
The third arc line segment satisfies the following relation: x is the number of 2 +(y-0.4a) 2 =2.78a 2 ,x∈(0,1.5a),
Where a is a dimensionless reference number and is an arbitrary real number.
6. The radome of claim 5, wherein the straight line segment has a length of 2a.
7. The radome of claim 1 or 2, further comprising a trip wire secured to the shroud body, the trip wire extending along a length of the shroud body, the trip wire being formed in a configuration projecting from an outer surface of the shroud body.
8. The radome of claim 3, further comprising a trip wire fixed to the cover body, the trip wire extending along a length direction of the cover body, the trip wire being formed in a configuration protruding from an outer surface of the cover body, the trip wire being provided at a midpoint of the third circular arc segment and/or the trip wire being provided at a connection point of the first circular arc segment and the second circular arc segment.
9. The radome of claim 8, wherein the length of the trip wire is equal to the length of the radome body.
10. The radome of claim 8, wherein the trip wire is rectangular, trapezoidal, or triangular in shape in the cross-section.
11. An antenna arrangement, characterized in that it comprises a radome according to any one of claims 1-9.
12. The antenna device according to claim 11, characterized in that the antenna device comprises a plurality of radomes arranged in a circular array.
13. The antenna device according to claim 11 or 12, wherein the antenna device is used in a radio base station antenna device of a communication network.
CN202111068308.6A 2021-09-13 2021-09-13 Antenna cover and antenna device Pending CN115810910A (en)

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Application Number Priority Date Filing Date Title
CN202111068308.6A CN115810910A (en) 2021-09-13 2021-09-13 Antenna cover and antenna device
PCT/CN2022/117609 WO2023036192A1 (en) 2021-09-13 2022-09-07 Radome and antenna device
EP22866655.8A EP4386982A1 (en) 2021-09-13 2022-09-07 Radome and antenna device

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US9979079B2 (en) 2015-02-23 2018-05-22 Quintel Technology Limited Apparatus and method to reduce wind load effects on base station antennas
WO2019161818A1 (en) 2018-02-23 2019-08-29 Kathrein Se Antenna housing and structure for antenna housing
CN208272135U (en) * 2018-06-26 2018-12-21 江苏亨鑫科技有限公司 A kind of low windage antenna house
CN208460979U (en) * 2018-08-09 2019-02-01 东莞东石新材料开发有限公司 A kind of dual-component polyurethane high intensity antenna house

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