CN111864390A - Co-constructed Antenna Module - Google Patents

Abstract

The present invention discloses a co-constructed antenna module, which includes a carrier, a first patch antenna group, a second patch antenna group, a first dipole antenna group and a second dipole antenna group. The carrier includes a first bearing surface, a second bearing surface and a surrounding side. The first patch antenna group is at least arranged on one of the first bearing surface and the second bearing surface. The second patch antenna group is at least arranged on one of the first bearing surface and the second bearing surface. The first dipole antenna group and the second dipole antenna group are arranged in the carrier. The first dipole antenna group is closer to the surrounding side than the first patch antenna group or the second patch antenna group, and the second dipole antenna group is closer to the surrounding side than the first patch antenna group or the second patch antenna group. The frequencies of the patch antenna groups can be different, the frequencies of the dipole antenna groups can be different, and both the patch antenna group and the dipole antenna group can be applied to the millimeter wave frequency band. Thereby, the present invention achieves the effect of improving the radiation efficiency of the antenna.

Description

Co-constructed Antenna Module

technical field

The present invention relates to an antenna module, in particular to a co-structured antenna module.

Background technique

First, with the development of communication technology, various electronic products using wireless communication technology have been born, such as mobile phones, wireless Internet access devices, personal digital assistants, and so on. Consumers' requirements for the performance, design and size of these wireless communication devices are also increasing.

Next, although the prior art discloses the structure of a patch antenna (Patch Antenna) and a dipole antenna (Dipole Antenna), however, most of the antenna structures in the prior art can only provide a single frequency, and the radiation efficiency thereof is not obvious.

SUMMARY OF THE INVENTION

The technical problem to be solved by the present invention is to provide a co-structured antenna module aiming at the shortcomings of the prior art.

In order to solve the above technical problems, one of the technical solutions adopted by the present invention is to provide a co-constructed antenna module, which includes: a carrier, a first patch antenna group, a second patch antenna group, a a first dipole antenna group and a second dipole antenna group. The carrier includes a first bearing surface, a second bearing surface opposite to the first bearing surface, and a surrounding side edge connected between the first bearing surface and the second bearing surface. The first patch antenna group includes a plurality of first patch antennas arranged on the carrier, and a plurality of the first patch antennas are arranged at least in the first bearing surface and the second bearing surface one of them. The second patch antenna group includes a plurality of second patch antennas arranged on the carrier, and a plurality of the second patch antennas are arranged at least in the first bearing surface and the second bearing surface one of them. The first group of dipole antennas is disposed in the carrier. The second dipole antenna group is disposed in the carrier. Wherein, the first dipole antenna group is closer to the surrounding side than the first patch antenna group or the second patch antenna group, and the second dipole antenna group is closer to the surrounding side than the first patch antenna group or the second patch antenna group. A patch antenna group or the second patch antenna group is closer to the surrounding side.

Further, the first patch antenna group has a first operating frequency band, the second patch antenna group has a second operating frequency band, the first dipole antenna group has a third operating frequency band, and the The second dipole antenna group has a fourth operating frequency band; wherein the frequency of the first operating frequency band is less than the frequency of the second operating frequency band, and the frequency of the third operating frequency band is less than the frequency of the fourth operating frequency band .

Further, the first dipole antenna group includes a plurality of first dipole antennas and a plurality of second dipole antennas, and the second dipole antenna group includes a plurality of third dipole antennas and a plurality of fourth dipole antennas. A pole antenna; wherein the surrounding side is rectangular, and the surrounding side includes a first side, a second side connected to the first side, and a second side connected to the second side The third side of the edge and a fourth side connected between the third side and the first side.

Further, a plurality of the first dipole antennas are arranged along the first side, a plurality of the second dipole antennas are arranged along the second side, and a plurality of the third dipole antennas are arranged along the second side. The pole antennas are arranged along the third side, and a plurality of the fourth dipole antennas are arranged along the fourth side.

Further, a plurality of the first dipole antennas are arranged along the first side, a plurality of the second dipole antennas are arranged along the third side, and a plurality of the third dipoles are arranged. The pole antennas are arranged along the second side, and a plurality of the fourth dipole antennas are arranged along the fourth side.

Further, the first dipole antenna group further includes a plurality of fifth dipole antennas, the second dipole antenna group further includes a plurality of sixth dipole antennas, wherein a plurality of the first dipole antennas are arranged along the first side, a plurality of the second dipole antennas are arranged along the second side, and a plurality of the fifth dipole antennas are arranged along the fourth side , a plurality of the third dipole antennas are arranged along the third side, a plurality of the fourth dipole antennas are arranged along the fourth side, and a plurality of the sixth dipole antennas arranged along the second side.

Further, each of the first patch antennas includes a first radiator and a first feed pin connected to the first radiator, and each of the second patch antennas includes a second radiator body and a second feeding pin connected to the second radiator.

Further, the carrier is a low temperature co-fired ceramic substrate.

Further, the first dipole antenna group and the second dipole antenna group are located on the same layer.

Further, the first dipole antenna group and the second dipole antenna group are located on different layers.

One of the beneficial effects of the present invention is that the co-constructed antenna module provided by the present invention can be disposed at least in the first bearing surface and the second bearing surface through "a plurality of the first patch antennas. one of”, “a plurality of the second patch antennas are arranged on at least one of the first bearing surface and the second bearing surface”, and “the first dipole antenna group is relatively The first patch antenna group or the second patch antenna group is closer to the surrounding side, and the second dipole antenna group is closer than the first patch antenna group or the second patch The antenna group is closer to the surrounding side" technical solution to improve the radiation efficiency of the antenna.

To further understand the features and technical content of the present invention, please refer to the following detailed description and accompanying drawings of the present invention. However, the accompanying drawings are only for reference and description, and are not intended to limit the present invention.

Description of drawings

FIG. 1 is a three-dimensional schematic diagram of a co-configured antenna module according to a first embodiment of the present invention.

FIG. 2 is another schematic perspective view of the co-configured antenna module according to the first embodiment of the present invention.

FIG. 3 is a schematic top view of the co-configured antenna module according to the first embodiment of the present invention.

FIG. 4 is a schematic side view of the co-configured antenna module according to the first embodiment of the present invention.

FIG. 5 is a schematic perspective view of the first patch antenna of the co-configured antenna module according to the first embodiment of the present invention.

FIG. 6 is a schematic perspective view of the second patch antenna of the co-configured antenna module according to the first embodiment of the present invention.

FIG. 7 is a three-dimensional schematic diagram of a co-configured antenna module according to a second embodiment of the present invention.

FIG. 8 is another three-dimensional schematic diagram of the co-configured antenna module according to the second embodiment of the present invention.

FIG. 9 is a schematic top view of a co-constructed antenna module according to a second embodiment of the present invention.

FIG. 10 is a schematic side view of a co-configured antenna module according to a second embodiment of the present invention.

FIG. 11 is a three-dimensional schematic diagram of a co-configured antenna module according to a third embodiment of the present invention.

FIG. 12 is a schematic top view of a co-configured antenna module according to a third embodiment of the present invention.

FIG. 13 is a schematic side view of a co-configured antenna module according to a third embodiment of the present invention.

Detailed ways

The following is a description of the implementation of the "co-structured antenna module" disclosed in the present invention through specific specific embodiments, and those skilled in the art can understand the advantages and effects of the present invention from the content disclosed in this specification. The present invention can be implemented or applied through other different specific embodiments, and various details in this specification can also be modified and changed based on different viewpoints and applications without departing from the concept of the present invention. In addition, the drawings of the present invention are merely schematic illustrations, and are not drawn according to the actual size, and are stated in advance. The following embodiments will further describe the related technical contents of the present invention in detail, but the disclosed contents are not intended to limit the protection scope of the present invention.

It should be understood that, although the terms "first", "second", "third" and the like may be used herein to describe various elements, these elements should not be limited by these terms. These terms are primarily used to distinguish one element from another. In addition, the term "or", as used herein, should include any one or a combination of more of the associated listed items, as the case may be.

first embodiment

First, referring to FIG. 1 to FIG. 3 , FIG. 1 and FIG. 2 are respectively three-dimensional schematic diagrams of the co-configuration antenna module according to the first embodiment of the present invention, and FIG. 3 is a schematic diagram of the co-configuration antenna module according to the first embodiment of the present invention. Top view schematic. The first embodiment of the present invention provides a co-configured antenna module U, which includes: a carrier 1 , a first patch antenna group 2 , a second patch antenna group 3 , a first dipole antenna group 4 , and A second dipole antenna group 5 . Preferably, the carrier 1 can be a multilayer low temperature co-fired ceramics (Low Temperature Co-fired Ceramics, LTCC), in addition, in other embodiments, the carrier 1 can be a low dielectric constant and low loss PCB board, such as but Not limited to multi-layer epoxy glass fiber substrate (FR-4). Thereby, the co-structured antenna module U provided by the present invention can utilize the low-temperature co-fired ceramic technology to combine the first patch antenna group 2 , the second patch antenna group 3 , the first dipole antenna group 4 and the second dipole antenna group The antenna group 5 is co-constructed in the carrier 1 formed by the multilayer low temperature co-fired ceramic substrate. In other words, the first patch antenna group 2 , the second patch antenna group 3 , the first dipole antenna group 4 and the second dipole antenna group 5 can form an integrated co-fired ceramic antenna.

Next, please refer to FIG. 1 and FIG. 2 again, the carrier 1 may include a first bearing surface 11 , a second bearing surface 12 opposite to the first bearing surface 11 , and a second bearing surface 12 connected to the first bearing surface 11 and the second bearing surface 11 . Surrounding sides 13 between the bearing surfaces 12 . The first patch antenna group 2 may include a plurality of first patch antennas 20 (Patch Antenna) disposed on the carrier 1, and the plurality of first patch antennas 20 are disposed at least on the first bearing surface 11 and the second bearing surface 12 one of them. The second patch antenna group 3 may include a plurality of second patch antennas 30 (Patch Antenna) disposed on the carrier 1 , and the plurality of second patch antennas 30 are disposed at least on the first bearing surface 11 and the second bearing surface 12 one of them. Further, according to the first embodiment of the present invention, a plurality of first patch antennas 20 can be disposed on the first carrying surface 11 , and a plurality of second patch antennas 30 can be disposed on the first carrying surface 11 , however, the present invention is not limited to this. Therefore, since the first patch antenna 20 and the second patch antenna 30 in the first embodiment are both disposed on the first bearing surface 11 , the first patch antenna 20 and the second patch antenna 30 are The resulting radiation pattern may be in the Z direction.

Next, please refer to FIG. 4 , and please refer to FIG. 3 again. FIG. 4 is a schematic side view of the co-structured antenna module according to the first embodiment of the present invention. The first dipole antenna group 4 may be provided in the carrier 1 , and the second dipole antenna group 5 may be provided in the carrier 1 . For example, when the carrier 1 is a multi-layer low-temperature co-fired ceramic substrate, the first dipole antenna group 4 and the second dipole antenna group 5 can be disposed on one layer of the multi-layer low-temperature co-fired ceramic substrate. Further, the first dipole antenna group 4 and the second dipole antenna group 5 may be located on the same layer of low temperature co-fired ceramic substrate, or the first dipole antenna group 4 and the second dipole antenna group 5 may be located on different layer on the low temperature co-fired ceramic substrate, the present invention is not limited to this. It should be noted that, in the embodiment shown in FIG. 4 , the first dipole antenna group 4 and the second dipole antenna group 5 may be located on the same layer of the low-temperature co-fired ceramic substrate.

Based on the above, for example, the first dipole antenna group 4 may include a plurality of first dipole antennas 41 (Dipole Antenna) and a plurality of second dipole antennas 42 (Dipole Antenna), and the second dipole antenna group 5 may include A plurality of third dipole antennas 51 (Dipole Antenna) and a plurality of fourth dipole antennas 52 (Dipole Antenna). A plurality of first dipole antennas 41 , a plurality of second dipole antennas 42 , a plurality of third dipole antennas 51 and a plurality of fourth dipole antennas 52 may be disposed adjacent to the surrounding side 13 of the carrier 1 . Further, the first patch antenna group 2 has a first operating frequency band, the second patch antenna group 3 has a second operating frequency band, the first dipole antenna group 4 has a third operating frequency band, and the second dipole antenna group 4 has a third operating frequency band. Antenna group 5 has a fourth operating frequency band. Further, the frequency of the first operating frequency band may be lower than the frequency of the second operating frequency band, and the frequency of the third operating frequency band may be lower than the frequency of the fourth operating frequency band. In addition, for example, the first operating frequency band may be a millimeter wave low frequency, the second operating frequency band may be a millimeter wave high frequency, the third operating frequency band may be a millimeter wave low frequency, and the fourth operating frequency band may be a millimeter wave high frequency. For example, according to the present invention, the first patch antenna group 2 can have a first operating frequency band with a frequency of 28 GHz, the second patch antenna group 3 can have a second operating frequency band with a frequency of 39 GHz, and the first The dipole antenna group 4 may have a third operating frequency band with a frequency of 28 GHz, and the second dipole antenna group 5 may have a fourth operating frequency band with a frequency of 39 GHz, but the invention is not limited thereto. Thereby, the patch antenna and the dipole antenna provided by the present invention can be respectively applicable to two different operating frequency bands.

Next, please refer to FIG. 3 again, according to the present invention, the first dipole antenna group 4 is closer to the surrounding side 13 than the first patch antenna group 2 or the second patch antenna group 3, and the second The dipole antenna group 5 is closer to the surrounding side 13 than the first patch antenna group 2 or the second patch antenna group 3 . In addition, the vertical projection of the first patch antenna group 2 on the second bearing surface 12 of the carrier 1 can form a first projection area, and the vertical projection of the second patch antenna group 3 on the second bearing surface 12 of the carrier 1 A second projection area can be formed, the vertical projection of the first dipole antenna group 4 on the second bearing surface 12 of the carrier 1 can form a third projection area, and the second dipole antenna group 5 can be formed on the second bearing surface of the carrier 1. The vertical projection on the surface 12 can form a fourth projection area. For example, the first projection area and the third projection area and/or the fourth projection area do not overlap each other, and the second projection area and the third projection area and/or the fourth projection area do not overlap each other, but the present invention does not This is limited.

Based on the above, please refer to FIG. 3 again. For example, the surrounding side 13 of the carrier 1 may be rectangular, and the surrounding side 13 may include a first side 131 , a The second side 132 , a third side 133 connected to the second side 132 , and a fourth side 134 connected between the third side 133 and the first side 131 . According to the first embodiment of the present invention, a plurality of first dipole antennas 41 can be arranged along the first side 131, a plurality of second dipole antennas 42 can be arranged along the second side 132, a plurality of The third dipole antennas 51 may be arranged along the third side 133 , and the plurality of fourth dipole antennas 52 may be arranged along the fourth side 134 .

Therefore, according to the first embodiment of the present invention, the radiation pattern in the Z direction can be generated by the first patch antenna group 2 and the second patch antenna group 3, and the radiation pattern in the Z direction can be generated by the first dipole antenna 41 and the second dipole antenna 41. The pole antenna 42 generates radiation patterns in the X direction and the Y direction respectively, and the third dipole antenna 51 and the fourth dipole antenna 52 can respectively generate radiation patterns in the negative X direction and the negative Y direction.

Next, please refer to FIG. 5 , which is a schematic perspective view of the first patch antenna of the co-configuration antenna module according to the first embodiment of the present invention. The first patch antenna 20 may include a first radiator 201 and a first feeding pin 202 connected to the first radiator 201 , so as to use the first feeding pin 202 to feed a signal to the first radiator 201 . However, it should be noted that in the embodiment shown in FIG. 5 , the first patch antenna 20 may include a first radiator 201 and two first feeding pins 202 connected to the first radiator 201 , and the present invention does not It is limited by the signal feeding method of the first radiator 201 .

Next, please refer to FIG. 6 , which is a schematic perspective view of the second patch antenna of the co-configuration antenna module according to the first embodiment of the present invention. The second patch antenna 30 may include a second radiator and a second feed pin 302 connected to the second radiator 301 , so as to feed a signal to the second radiator 301 through the second feed pin 302 . However, it should be noted that in the embodiment shown in FIG. 6 , the second patch antenna 30 may include a second radiator 301 and two second feed pins 302 connected to the second radiator 301 . It is limited by the signal feeding method of the second radiator 301 .

Second Embodiment

First, please refer to FIG. 7 to FIG. 9 . FIG. 7 and FIG. 8 are respectively three-dimensional schematic diagrams of the co-configuration antenna module according to the second embodiment of the present invention, and FIG. 9 is the co-configuration antenna module according to the second embodiment of the present invention. Schematic top view of . The second embodiment of the present invention provides a co-constructed antenna module U. It can be seen from the comparison of FIGS. 7 to 9 with FIGS. 1 to 3 that the biggest difference between the second embodiment of the present invention and the first embodiment is that the second embodiment The configuration positions of the first patch antenna group 2 , the second patch antenna group 3 , the first dipole antenna group 4 and/or the second dipole antenna group 5 of the co-configured antenna module U provided by the embodiment are different. In addition, it should be noted that other structures of the co-constructed antenna module U provided by the second embodiment are similar to those of the foregoing embodiments, and are not described herein again.

Based on the above, please refer to FIG. 9 again. According to the second embodiment of the present invention, a plurality of first patch antennas 20 can be arranged on the first bearing surface 11 , and a plurality of second patch antennas 30 can be arranged On the second bearing surface 12, however, the present invention is not limited to this. Therefore, since the first patch antenna 20 in the second embodiment is disposed on the first carrying surface 11 and the second patch antenna 30 is disposed on the second carrying surface 12, the first patch antenna The radiation pattern generated by 20 and the second patch antenna 30 can be in the Z direction. In addition, according to the second embodiment of the present invention, a plurality of first dipole antennas 41 can be arranged along the first side 131 , and a plurality of second dipole antennas 42 can be arranged along the third side 133 , The plurality of third dipole antennas 51 may be arranged along the second side 132 , and the plurality of fourth dipole antennas 52 may be arranged along the fourth side 134 .

Therefore, according to the second embodiment of the present invention, the radiation pattern in the Z direction can be generated by the first patch antenna group 2 and the second patch antenna group 3, and the radiation pattern in the Z direction can be generated by the first dipole antenna 41 and the second dipole antenna The pole antenna 42 generates radiation patterns in the X direction and the negative X direction respectively, and can generate radiation patterns in the Y direction and the negative Y direction respectively through the third dipole antenna 51 and the fourth dipole antenna 52 .

Next, please refer to FIG. 10 . FIG. 10 is a schematic side view of the co-structured antenna module according to the second embodiment of the present invention. Further, in the embodiment shown in FIG. 10 , the first dipole antenna group 4 and the second dipole antenna group 5 may be located on the same layer of the low-temperature co-fired ceramic substrate, but the present invention is not limited thereto.

Third Embodiment

First, please refer to FIG. 11 and FIG. 12 . FIG. 11 is a three-dimensional schematic diagram of a co-configured antenna module according to a third embodiment of the present invention, and FIG. 12 is a top schematic view of the co-configured antenna module according to the third embodiment of the present invention. The third embodiment of the present invention provides a co-constructed antenna module U. It can be seen from the comparison of FIGS. 11 and 12 with FIGS. 1 to 3 that the biggest difference between the third embodiment of the present invention and the first embodiment is that: the third embodiment The configuration positions of the first patch antenna group 2 , the second patch antenna group 3 , the first dipole antenna group 4 and/or the second dipole antenna group 5 of the co-configured antenna module U provided by the embodiment are different. In addition, it should be noted that other structures of the co-configured antenna module U provided by the third embodiment are similar to those of the foregoing embodiments, and are not described herein again. In addition, according to the third embodiment of the present invention, the first dipole antenna group 4 may further include a plurality of fifth dipole antennas 43 , and the second dipole antenna group 5 may further include a plurality of sixth dipole antennas 53.

12, according to the third embodiment of the present invention, a plurality of first dipole antennas 41 can be arranged along the first side 131, and a plurality of second dipole antennas 42 can be arranged along the The plurality of fifth dipole antennas 43 may be arranged along the fourth side 134, the plurality of third dipole antennas 51 may be arranged along the third side 133, and the plurality of The four dipole antennas 52 may be arranged along the fourth side 134 , and the plurality of sixth dipole antennas 53 may be arranged along the second side 132 . In other words, by disposing the fifth dipole antenna 43 and the sixth dipole antenna 53 , the radiation field directions of the first dipole antenna group 4 and the second dipole antenna group 5 can be increased.

Therefore, according to the third embodiment of the present invention, the radiation pattern in the Z direction can be generated by the first patch antenna group 2 and the second patch antenna group 3, and the radiation pattern in the Z direction can be generated by the first dipole antenna 41 and the second dipole antenna The pole antenna 42 and the fifth dipole antenna 43 respectively generate radiation patterns in the X direction, the Y direction and the negative Y direction, and can be transmitted through the third dipole antenna 51, the fourth dipole antenna 52 and the sixth dipole antenna 53 respectively. Radiation patterns in the negative X, Y and negative Y directions are generated.

Next, please refer to FIG. 13 . FIG. 13 is a schematic side view of a co-structured antenna module according to a third embodiment of the present invention. Further, in the embodiment of FIG. 13 , the first dipole antenna group 4 and the second dipole antenna group 5 may be located on different layers of low-temperature co-fired ceramic substrates, but the invention is not limited thereto.

Beneficial Effects of Embodiments

One of the beneficial effects of the present invention is that in the co-constructed antenna module U provided by the present invention, the plurality of first patch antennas 20 can be disposed on at least one of the first bearing surface 11 and the second bearing surface 12 through "a plurality of first patch antennas 20". one of”, “a plurality of second patch antennas 30 are disposed on at least one of the first bearing surface 11 and the second bearing surface 12”, and “the first dipole antenna group 4 is higher than the first patch antenna group 2 Or the second patch antenna group 3 is closer to the surrounding side 13, and the second dipole antenna group 5 is closer to the surrounding side 13" than the first patch antenna group 2 or the second patch antenna group 3. solution to improve the radiation efficiency of the co-structured antenna module U.

Further, the first patch antenna group 2 , the second patch antenna group 3 , the first dipole antenna group 4 and the second dipole antenna can be formed by using the low temperature co-fired ceramic technology by using the carrier 1 as a low-temperature co-fired ceramic substrate. The antenna group 5 is co-constructed in the carrier 1 formed by the multilayer low temperature co-fired ceramic substrate. Thereby, the first patch antenna group 2 , the second patch antenna group 3 , the first dipole antenna group 4 and the second dipole antenna group 5 can form an integrated co-fired ceramic antenna. At the same time, the co-constructed antenna module U can co-construct the millimeter-wave low-frequency and millimeter-wave high-frequency antennas under the same structure, and is suitable for occasions in different frequency bands.

The content disclosed above is only a preferred feasible embodiment of the present invention, and is not intended to limit the protection scope of the claims of the present invention. Therefore, any equivalent technical changes made by using the contents of the description and the accompanying drawings of the present invention are included in the present invention. within the scope of protection of the claims of the invention.

Claims (10)

1. A co-configured antenna module, the co-configured antenna module comprising:

the carrier comprises a first bearing surface, a second bearing surface opposite to the first bearing surface and a surrounding side edge connected between the first bearing surface and the second bearing surface;

a first patch antenna group, wherein the first patch antenna group comprises a plurality of first patch antennas arranged on the carrier, and the plurality of first patch antennas are arranged on at least one of the first bearing surface and the second bearing surface;

a second patch antenna group, the second patch antenna group including a plurality of second patch antennas disposed on the carrier, the plurality of second patch antennas being disposed on at least one of the first carrying surface and the second carrying surface;

a first set of dipole antennas disposed in the carrier; and

A second set of dipole antennas disposed in the carrier;

wherein the first dipole antenna group is closer to the surrounding side than the first patch antenna group or the second patch antenna group, and the second dipole antenna group is closer to the surrounding side than the first patch antenna group or the second patch antenna group.

2. The co-constructed antenna module of claim 1, wherein the first patch antenna set has a first operating frequency band, the second patch antenna set has a second operating frequency band, the first dipole antenna set has a third operating frequency band, and the second dipole antenna set has a fourth operating frequency band; wherein the frequencies of the first operating frequency band are less than the frequencies of the second operating frequency band, and the frequencies of the third operating frequency band are less than the frequencies of the fourth operating frequency band.

3. The co-constructed antenna module of claim 1, wherein the first set of dipole antennas comprises a first plurality of dipole antennas and a second plurality of dipole antennas, the second set of dipole antennas comprises a third plurality of dipole antennas and a fourth plurality of dipole antennas; wherein, it is the rectangle form to encircle the side, just it includes a first side, a connection in to encircle the side the second side of first side, a connection in the third side of second side and a connection in the third side with fourth side between the first side.

4. The antenna module of claim 3, wherein a plurality of the first dipoles are arranged along the first side, a plurality of the second dipoles are arranged along the second side, a plurality of the third dipoles are arranged along the third side, and a plurality of the fourth dipoles are arranged along the fourth side.

5. The co-configured antenna module as recited in claim 3, wherein a plurality of the first dipoles are arranged along the first side, a plurality of the second dipoles are arranged along the third side, a plurality of the third dipoles are arranged along the second side, and a plurality of the fourth dipoles are arranged along the fourth side.

6. The co-configured antenna module of claim 3, wherein the first dipole antenna group further comprises a plurality of fifth dipole antennas, wherein the second dipole antenna group further comprises a plurality of sixth dipole antennas, wherein the plurality of first dipole antennas are arranged along the first side edge, the plurality of second dipole antennas are arranged along the second side edge, the plurality of fifth dipole antennas are arranged along the fourth side edge, the plurality of third dipole antennas are arranged along the third side edge, the plurality of fourth dipole antennas are arranged along the fourth side edge, and the plurality of sixth dipole antennas are arranged along the second side edge.

7. The antenna module of claim 1, wherein each of the first patch antennas comprises a first radiator and a first feeding pin connected to the first radiator, and each of the second patch antennas comprises a second radiator and a second feeding pin connected to the second radiator.

8. The co-constructed antenna module of claim 1, wherein the carrier is a low temperature co-fired ceramic substrate.

9. The co-configured antenna module of claim 1, wherein the first set of dipole antennas is located on the same layer as the second set of dipole antennas.

10. The co-constructed antenna module of claim 1, wherein the first and second dipole antenna groups are located on different layers.

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