The present disclosure relates to an antenna structure and an electronic device, and more particularly to an antenna structure and an electronic device capable of generating an omnidirectional radiation pattern in a specific frequency band.
Electronic products, such as network routers, routers and miniature base stations, use built-in antennas to communicate with the outside world. Built-in antennas are antennas that are embedded in the electronic products. Generally speaking, implanting antennas into products during the design process can make the products more aesthetically pleasing and easy to use. However, the signal strength and stability of the antenna may be restricted by the space inside the product itself. For example, when the housing of the product is made of metal material, the antenna clearance area is reduced, and the space where the antenna can be installed inside the product is limited, which will affect the radiation efficiency of the antenna.
Therefore, how to overcome the above defects through the improvement of structural design has become one of the important issues to be solved in this field.
In one aspect, the present disclosure provides an antenna structure, which includes a first dipole radiating piece, a second dipole radiating piece and a third dipole radiating element. The first dipole radiating element is perpendicular to a plane. The second dipole radiating element is connected to the first dipole radiating element. The third dipole radiating element is connected to the first dipole radiating element and the second dipole radiating element. The first dipole radiating element is configured to generate a first radiation pattern, the second dipole radiation element is configured to generate a second radiation pattern, and the third dipole radiation element is configured to generate a third radiation pattern. The first radiation pattern is omnidirectional radiation on the plane. The polarization direction of the second radiation pattern is orthogonal to the polarization direction of the first radiation pattern, and the polarization direction of the third radiation pattern is orthogonal to the polarization direction of the first radiation pattern.
In another aspect, the present disclosure provides an electronic device, which includes a carrier and an antenna structure. The antenna structure is disposed on the carrier. The antenna structure includes a first dipole radiating element, a second dipole radiating element and a third dipole radiating element. The first dipole radiating element is perpendicular to a plane. The second dipole radiating element is connected to the first dipole radiating element. The third dipole radiating element is connected to the first dipole radiating element and the second dipole radiating element. The first dipole radiating element is configured to generate a first radiation pattern, the second dipole radiation element is configured to generate a second radiation pattern, and the third dipole radiation element is configured to generate a third radiation pattern. The first radiation pattern is omnidirectional radiation on the plane. The polarization direction of the second radiation pattern is orthogonal to the polarization direction of the first radiation pattern, and the polarization direction of the third radiation pattern is orthogonal to the polarization direction of the first radiation pattern.
These and other aspects of the present disclosure will become apparent from the following description of the embodiment taken in conjunction with the following drawings and their captions, although variations and modifications therein may be affected without departing from the spirit and scope of the novel concepts of the disclosure.
The described embodiments may be better understood by reference to the following description and the accompanying drawings, in which:
The present disclosure is more particularly described in the following examples that are intended as illustrative only since numerous modifications and variations therein will be apparent to those skilled in the art. Like numbers in the drawings indicate like components throughout the views. As used in the description herein and throughout the claims that follow, unless the context clearly dictates otherwise, the meaning of “a”, “an”, and “the” includes plural reference, and the meaning of “in” includes “in” and “on”. Titles or subtitles can be used herein for the convenience of a reader, which shall have no influence on the scope of the present disclosure.
The terms used herein generally have their ordinary meanings in the art. In the case of conflict, the present document, including any definitions given herein, will prevail. The same thing can be expressed in more than one way. Alternative language and synonyms can be used for any term(s) discussed herein, and no special significance is to be placed upon whether a term is elaborated or discussed herein. A recital of one or more synonyms does not exclude the use of other synonyms. The use of examples anywhere in this specification including examples of any terms is illustrative only, and in no way limits the scope and meaning of the present disclosure or of any exemplified term. Likewise, the present disclosure is not limited to various embodiments given herein. Numbering terms such as “first”, “second” or “third” can be used to describe various components, signals or the like, which are for distinguishing one component/signal from another one only, and are not intended to, nor should be construed to impose any substantive limitations on the components, signals or the like.
In addition, the term “or”, as used herein, should include any one or a combination of the associated enlisted items, as the case may be. The term “connect” in the context of the present disclosure means there is a physical connection between two elements and is directly or indirectly connected. The term “couple” in the context of the present disclosure means there is no physical connection between two separated elements, and the two elements are instead connected by their electric field energy where the electric field energy generated by the current of one element excites the electric field energy of the other element.
Referring to
In addition, it should be noted that the present disclosure does not limit the number of antenna structures. For example, in the present disclosure, the electronic device D has two antenna structures M1 and M2. A part of the antenna structure M1 is arranged on the first board S1 and the other part is arranged on the second board S2. A part of the antenna structure M2 is arranged on the first board S1 and the other part is arranged on the third board S3. The structural shapes of the two antenna structures M1 and M2 are basically the same, so in the following embodiments, only the antenna structure M1 is used as an example for illustration, and the antenna structure M2 is not described herein.
The antenna structure M1 includes a substrate T and a plurality of radiating elements arranged on the substrate T. The substrate T may be an FR4 substrate, a printed circuit board or a flexible printed circuit board (FPCB), and the present disclosure is not limited thereto. In detail, the antenna structure M1 includes a first dipole radiating element 1, a second dipole radiating element 2 and a third dipole radiating element 3. The second dipole radiating element 2 is connected to the first dipole radiating element 1, and the third dipole radiating element 3 is connected to the first dipole radiating component 1 and the second dipole radiating component 2. The first dipole radiating element 1, the second dipole radiating element 2 and the third dipole radiating element 3 may be metal sheets, metal patterns or other conductive bodies with conductive effects.
The substrate T includes a first substrate T1 and a second substrate T2. The first substrate T1 is arranged on the second plate piece S2, and the second substrate T2 is arranged on the first plate piece S1. The first dipole radiating element 1 is arranged on the first substrate T1, in other words, the first dipole radiating element 1 is perpendicular to the XY plane. However, in other embodiments, the first dipole radiating element 1 may also be perpendicular to other planes, such as a YZ plane or an XZ plane, and the present disclosure is not limited thereto. The configuration of the second dipole radiating element 2 and the third dipole radiating element 3 changes when the first dipole radiating element 1 is arranged in different directions.
Refer to
As shown in
Further, the first dipole radiating element 1 generates a first radiation pattern in the high-frequency range (i.e., the first operating frequency band), the second dipole radiating element 2 generates a second radiation pattern in the mid-frequency range (i.e., the second operating frequency band), and the third dipole radiating element 3 generates a third radiation pattern in the low-frequency range (i.e., the third operating frequency band). For example, when the electronic device D of the present disclosure is placed on a horizontal tabletop, the XY plane of
It should be noted that the antenna structure provided by the present disclosure is not limited to only designs in which the first dipole radiating element 1 is a high-frequency antenna, the second dipole radiating element 2 is a mid-frequency antenna, and the third dipole radiating element 3 is a low-frequency antenna. For example, in another embodiment, the first dipole radiating element 1 may be a high-frequency antenna, the second dipole radiating element 2 may be a low-frequency antenna, and the third dipole radiating element 3 may be a mid-frequency antenna. In other words, as long as the antenna structure includes the vertical polarization design of one of the radiating elements along with the orthogonal polarization design of the other two radiating elements, the radiation patterns generated by each of the radiating elements will not be affected by one another.
Referring to
The antenna structure M1 further includes two inductance elements L, which are connected in series to two third radiating elements 31 and 32 respectively. Each inductance element L is designed and configured on the corresponding low-frequency trace. The distance between each inductance element L and the corresponding connection point is exactly one quarter (¼) of the high-frequency wavelength, and this distance is also equal to the length of each first radiating element 11 and 12. In detail, as shown in
One of the advantages of the antenna structure and electronic device provided by the present disclosure is that the first dipole radiating element, the second dipole radiating element and the third dipole radiating element are connected to each other such that the first dipole radiating element produces an omnidirectional first radiation pattern, and the second and third radiation patterns produced by the second dipole radiating element and the third dipole radiating element are orthogonal to the first radiation pattern. In this way, the first radiation pattern generated by the first dipole radiating element is not affected by the other two dipole radiating elements, and the omnidirectional radiation characteristics can be maintained.
Further, in the conventional technology, the antenna performance may be affected due to the limited internal space of the product. The present disclosure first utilizes the vertical polarization design of the first dipole radiating element 1 to produce the first radiation pattern in the high-frequency range as omnidirectional radiation in the XY plane, and then utilizes the structural design of the second dipole radiating element 2 and the third dipole radiating element 3 to respectively produce the second radiation pattern and the third radiation pattern that are orthogonally polarized to the first radiation pattern. Thus, the first radiation pattern generated by the first dipole radiating element 1 is not affected by the second dipole radiating element 2 and the third dipole radiating element 3, and the omnidirectional radiation characteristics are still retained.
Furthermore, the antenna structure M1 also utilizes two inductance elements L to be connected in series to two third radiating elements 31 and 32 respectively. Each inductance element L is designed and configured to be on the corresponding low-frequency trace. The distance between each inductance element L and the corresponding connection point is exactly one quarter (¼) of the high-frequency wavelength. By virtue of the characteristics of the inductance element L, the interference generated by the low-frequency antenna (third dipole radiating element 3) can be suppressed, so that the radiation pattern of the high-frequency antenna (first dipole radiating element 1) is not affected by the low-frequency antenna (third dipole radiating element 3), and the high-frequency radiation pattern (i.e., the first radiation pattern) is further optimized.
The foregoing description of the exemplary embodiments of the disclosure has been presented only for the purposes of illustration and description and is not intended to be exhaustive or to limit the disclosure to the precise forms disclosed. Many modifications and variations are possible in light of the above teaching.
The embodiments were chosen and described in order to explain the principles of the disclosure and their practical application so as to enable others skilled in the art to utilize the disclosure and various embodiments and with various modifications as are suited to the particular use contemplated. Alternative embodiments will become apparent to those skilled in the art to which the present disclosure pertains without departing from its spirit and scope.
Number | Date | Country | Kind |
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113102510 | Jan 2024 | TW | national |
This application claims the benefit of priority to Taiwan Patent Application No. 113102510, filed on Jan. 23, 2024 and U.S. Provisional Application No. 63/517,384 filed on Aug. 3, 2023. The entire content of the above identified application is incorporated herein by reference. Some references, which may include patents, patent applications and various publications, may be cited and discussed in the description of this disclosure. The citation and/or discussion of such references is provided merely to clarify the description of the present disclosure and is not an admission that any such reference is “prior art” to the disclosure described herein. All references cited and discussed in this specification are incorporated herein by reference in their entireties and to the same extent as if each reference was individually incorporated by reference.
Number | Date | Country | |
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63517384 | Aug 2023 | US |