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TWI849763B - Antenna module - Google Patents

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Publication number
TWI849763B
TWI849763B TW112106357A TW112106357A TWI849763B TW I849763 B TWI849763 B TW I849763B TW 112106357 A TW112106357 A TW 112106357A TW 112106357 A TW112106357 A TW 112106357A TW I849763 B TWI849763 B TW I849763B
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Taiwan
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section
inductor
antenna module
inductive
coupling
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TW112106357A
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Chinese (zh)
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TW202435504A (en
Inventor
曾冠學
江正雄
楊振坤
蔡可峻
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微星科技股份有限公司
大陸商恩斯邁電子(深圳)有限公司
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Priority to TW112106357A priority Critical patent/TWI849763B/en
Priority to CN202310433161.9A priority patent/CN118539138A/en
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Publication of TWI849763B publication Critical patent/TWI849763B/en
Publication of TW202435504A publication Critical patent/TW202435504A/en

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/48Earthing means; Earth screens; Counterpoises
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/50Structural association of antennas with earthing switches, lead-in devices or lightning protectors

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  • Support Of Aerials (AREA)

Abstract

An antenna module includes a ground plane, a first radiation section, a second radiation section, and an inductive circuit. The first radiation section includes a first coupling section. The second radiation includes a second coupling section. The first coupling section and the second coupling section are adjacent to each other and separated by a first coupling gap. The inductive circuit includes a first inductive unit and a second inductive unit. The first inductive unit provides a first inductive path between the first radiation section and a feed source. The second inductive unit provides a second inductive path between the second radiation section and the ground plane. The first inductive path is adjacent to and not connected to the second inductive path.

Description

天線模組Antenna Module

本發明是關於通訊技術,尤其是關於天線模組。The present invention relates to communication technology, and more particularly to an antenna module.

現今各式電子裝置體積逐漸縮小,因此電子裝置內的天線的體積也需要縮小。一般會將天線高度降低以縮小天線的體積,例如將天線高度降低為小於5mm(毫米)。此類型的天線也稱為低姿態(low profile)天線。然而,天線高度與天線特性之間呈正相關。具體來說,當天線高度降低時,天線的輻射元件將更接近於接地元件而產生電容效應,致使天線的阻抗呈電容性。如此,天線的頻寬將縮減且呈現較差的天線特性。Nowadays, the size of various electronic devices is gradually shrinking, so the size of the antenna in the electronic device also needs to be reduced. Generally, the height of the antenna is reduced to reduce the size of the antenna, for example, the height of the antenna is reduced to less than 5mm (millimeter). This type of antenna is also called a low profile antenna. However, there is a positive correlation between the antenna height and the antenna characteristics. Specifically, when the antenna height is reduced, the radiation element of the antenna will be closer to the ground element and produce a capacitive effect, causing the impedance of the antenna to be capacitive. In this way, the bandwidth of the antenna will be reduced and the antenna characteristics will be poor.

鑒於上述,本發明提供一種天線模組。天線模組包含接地部、第一輻射段、第二輻射段及電感電路。第一輻射段包括第一耦合區段。第二輻射段包括第二耦合區段。第一耦合區段與第二耦合區段相鄰且間隔第一耦合間隙。電感電路包含第一電感單元及第二電感單元。第一電感單元提供介於第一輻射段及饋入源之間的第一電感性路徑,第二電感單元提供介於第二輻射段及接地部之間的第二電感性路徑,且第一電感性路徑與第二電感性路徑相鄰且不相接。In view of the above, the present invention provides an antenna module. The antenna module includes a ground portion, a first radiation segment, a second radiation segment and an inductor circuit. The first radiation segment includes a first coupling segment. The second radiation segment includes a second coupling segment. The first coupling segment and the second coupling segment are adjacent to each other and separated by a first coupling gap. The inductor circuit includes a first inductor unit and a second inductor unit. The first inductor unit provides a first inductive path between the first radiation segment and the feed source, and the second inductor unit provides a second inductive path between the second radiation segment and the ground portion, and the first inductive path and the second inductive path are adjacent to each other and are not connected.

綜上所述,依據一些實施例,透過電感電路,本發明可以在天線高度被降低(即低姿態)的同時消除第一輻射段與接地部之間的電容效應及消除第二輻射段與接地部之間的電容效應,以改善天線模組的頻寬及天線特性。In summary, according to some embodiments, the present invention can reduce the height of the antenna (i.e., low posture) by using an inductor circuit while eliminating the capacitance effect between the first radiation segment and the ground portion and eliminating the capacitance effect between the second radiation segment and the ground portion, so as to improve the bandwidth and antenna characteristics of the antenna module.

在本文中,平行可以是指數理中的真實平行或是大致平行。In this article, parallel can refer to true parallelism or approximate parallelism in mathematics.

參照圖1,係為本發明之天線模組10之第一實施例之立體示意圖。天線模組10包含接地部20、第一輻射段30、第二輻射段40及電感電路50。接地部20與主機板的參考地端(圖未示)連接,以獲得參考地。第一輻射段30及第二輻射段40用以發送(激發)及接收無線訊號(電磁波)。電感電路50連接於接地部20、第一輻射段30、第二輻射段40及饋入源FD之間。電感電路50用以提供兩個電感性路徑。第一電感性路徑介於饋入源FD與第一輻射段30之間,以消除第一輻射段30與接地部20之間的電容效應;第二電感性路徑介於第二輻射段40與接地部20之間,以消除第二輻射段40與接地部20之間的電容效應。此兩電感性路徑相鄰且不相接以產生互感,藉以進一步消除第一輻射段30與第二輻射段40之間的第一耦合間隙CG1與接地部20之間的電容效應。透過前述電容效應的消除來改善天線模組10的頻寬及天線特性。Referring to FIG. 1 , it is a three-dimensional schematic diagram of the first embodiment of the antenna module 10 of the present invention. The antenna module 10 includes a ground portion 20, a first radiation segment 30, a second radiation segment 40 and an inductor circuit 50. The ground portion 20 is connected to a reference ground terminal (not shown) of a motherboard to obtain a reference ground. The first radiation segment 30 and the second radiation segment 40 are used to send (excite) and receive wireless signals (electromagnetic waves). The inductor circuit 50 is connected between the ground portion 20, the first radiation segment 30, the second radiation segment 40 and a feed source FD. The inductor circuit 50 is used to provide two inductive paths. The first inductive path is between the feed source FD and the first radiation section 30 to eliminate the capacitive effect between the first radiation section 30 and the ground portion 20; the second inductive path is between the second radiation section 40 and the ground portion 20 to eliminate the capacitive effect between the second radiation section 40 and the ground portion 20. The two inductive paths are adjacent to each other but not connected to generate mutual inductance, so as to further eliminate the capacitive effect between the first coupling gap CG1 between the first radiation section 30 and the second radiation section 40 and the ground portion 20. The bandwidth and antenna characteristics of the antenna module 10 are improved by eliminating the aforementioned capacitive effect.

第一輻射段30包含第一耦合區段31。第二輻射段40包含第二耦合區段41。第一耦合區段31與第二耦合區段41相鄰且間隔第一耦合間隙CG1。饋入源FD經由電感電路50的第一電感性路徑連接第一輻射段30,使第一耦合區段31激發第一共振頻帶。藉由第一耦合間隙CG1,能量從第一耦合區段31耦合至第二耦合區段41,並經過電感電路50的第二電感性路徑、接地部20及參考地端以形成迴路,從而使第一耦合間隙CG1及第二耦合區段41分別激發第二共振頻帶及第三共振頻帶。第一共振頻帶可以是高頻帶,例如6吉赫茲(GHz)至7GHz之間。第二共振頻帶可以是中頻帶,例如5GHz至6GHz之間。第三共振頻帶可以是低頻帶,例如2GHz至3GHz之間。The first radiation section 30 includes a first coupling section 31. The second radiation section 40 includes a second coupling section 41. The first coupling section 31 and the second coupling section 41 are adjacent to each other and separated by a first coupling gap CG1. The feed source FD is connected to the first radiation section 30 via a first inductive path of the inductive circuit 50, so that the first coupling section 31 excites a first resonance frequency band. Through the first coupling gap CG1, energy is coupled from the first coupling section 31 to the second coupling section 41, and passes through the second inductive path of the inductive circuit 50, the grounding portion 20 and the reference ground to form a loop, so that the first coupling gap CG1 and the second coupling section 41 excite a second resonance frequency band and a third resonance frequency band respectively. The first resonance frequency band may be a high frequency band, for example, between 6 GHz and 7 GHz. The second resonance frequency band may be a middle frequency band, for example, between 5 GHz and 6 GHz. The third resonance frequency band may be a low frequency band, for example, between 2 GHz and 3 GHz.

參照圖1及2。圖2係為本發明之電感電路50之第一實施例之立體示意圖。電感電路50包含用以實現前述第一電感性路徑的第一電感單元51及用以實現前述第二電感性路徑的第二電感單元52。第一電感單元51連接於第一輻射段30及饋入源FD之間。第二電感單元52連接於第二輻射段40及接地部20之間。具體來說,第一電感單元51的一端(即第一端E1)連接饋入源FD,第一電感單元51的相對於第一端E1的第二端E2連接第一輻射段30的第一耦合區段31。第二電感單元52的一端(即第三端E3)連接接地部20,第二電感單元52的相對於第三端E3的第四端E4連接第二輻射段40的第二耦合區段41。第一電感單元51用以提供第一自感,以消除第一耦合區段31與接地部20之間的電容效應。第二電感單元52用以提供第二自感,以消除第二耦合區段41與接地部20之間的電容效應。第一電感單元51與第二電感單元52相互耦合以產生互感,以消除第一耦合間隙CG1與接地部20之間的電容效應。如此,在天線高度被降低(即低姿態,例如第一耦合區段31與接地部20之間的距離及第二耦合區段41與接地部20之間的距離皆是小於5mm)下,天線模組10仍能具有良好的頻寬及天線特性。Refer to Figures 1 and 2. Figure 2 is a three-dimensional schematic diagram of the first embodiment of the inductor circuit 50 of the present invention. The inductor circuit 50 includes a first inductor unit 51 for realizing the aforementioned first inductive path and a second inductor unit 52 for realizing the aforementioned second inductive path. The first inductor unit 51 is connected between the first radiation section 30 and the feed source FD. The second inductor unit 52 is connected between the second radiation section 40 and the ground portion 20. Specifically, one end (i.e., the first end E1) of the first inductor unit 51 is connected to the feed source FD, and the second end E2 of the first inductor unit 51 relative to the first end E1 is connected to the first coupling section 31 of the first radiation section 30. One end (i.e., the third end E3) of the second inductor unit 52 is connected to the ground portion 20, and a fourth end E4 of the second inductor unit 52, which is opposite to the third end E3, is connected to the second coupling section 41 of the second radiation section 40. The first inductor unit 51 is used to provide a first self-inductance to eliminate the capacitive effect between the first coupling section 31 and the ground portion 20. The second inductor unit 52 is used to provide a second self-inductance to eliminate the capacitive effect between the second coupling section 41 and the ground portion 20. The first inductor unit 51 and the second inductor unit 52 are coupled to each other to generate mutual inductance to eliminate the capacitive effect between the first coupling gap CG1 and the ground portion 20. Thus, when the antenna height is lowered (ie, in a low posture, for example, the distance between the first coupling section 31 and the ground portion 20 and the distance between the second coupling section 41 and the ground portion 20 are both less than 5 mm), the antenna module 10 can still have good bandwidth and antenna characteristics.

在一些實施例中,第一自感及第二自感的電感值可以分別在0.1奈亨利(nH)至10nH之間。第一電感單元51及第二電感單元52之間的互感的電感值可以在0.1nH至5nH之間。在一示範例中,在天線模組10激發第一共振頻段(例如6.5GHz)時,第一自感的電感值可為2.23nH,第二自感的電感值可為1.8nH,互感的電感值可為0.62nH。在天線模組10激發第二共振頻段(例如5.5GHz)時,第一自感的電感值可為2.28nH,第二自感的電感值可為1.85nH,互感的電感值可為0.62nH。在天線模組10激發第三共振頻段(例如2.45GHz)時,第一自感的電感值可為2.59nH,第二自感的電感值可為2.12nH,互感的電感值可為0.66nH。In some embodiments, the inductance values of the first self-inductance and the second self-inductance may be between 0.1 nanohenry (nH) and 10nH, respectively. The inductance value of the mutual inductance between the first inductance unit 51 and the second inductance unit 52 may be between 0.1nH and 5nH. In an exemplary embodiment, when the antenna module 10 excites the first resonant frequency band (e.g., 6.5GHz), the inductance value of the first self-inductance may be 2.23nH, the inductance value of the second self-inductance may be 1.8nH, and the inductance value of the mutual inductance may be 0.62nH. When the antenna module 10 excites the second resonant frequency band (e.g., 5.5GHz), the inductance value of the first self-inductance may be 2.28nH, the inductance value of the second self-inductance may be 1.85nH, and the inductance value of the mutual inductance may be 0.62nH. When the antenna module 10 excites the third resonance frequency band (eg, 2.45 GHz), the inductance value of the first self-inductance may be 2.59 nH, the inductance value of the second self-inductance may be 2.12 nH, and the inductance value of the mutual inductance may be 0.66 nH.

參照圖1及圖3。圖3係為本發明之天線模組10之第二實施例之立體示意圖。在一些實施例中,天線模組10還包含基板60。接地部20、第一輻射段30、第二輻射段40及電感電路50位於基板60的同一表面(例如頂表面)。在一些實施例中,第一輻射段30的第一耦合區段31具有兩區段,第一耦合區段31的第一區段是從電感電路50的第二端E2朝遠離接地部20的方向延伸一段長度,第一耦合區段31的第二區段是接續第一耦合區段31的第一區段的末端以沿著平行於接地部20之邊緣延伸一段長度。第二輻射段40的第二耦合區段41具有兩區段,第二耦合區段41的第一區段是從電感電路50的第四端E4朝遠離接地部20的方向延伸一段長度,第二耦合區段41的第二區段是接續第二耦合區段41的第一區段的末端以大致沿著平行於接地部20之邊緣延伸一段長度。也就是說,第一耦合區段31的第二區段平行於第二耦合區段41的第二區段。在一些實施例中,第一耦合區段31的第二區段所延伸的長度係短於第二耦合區段41的第二區段所延伸的長度。如圖1所示,在一些實施例中,第二輻射段40位於第一輻射段30的外側(以接地部20的觀點),亦即第一輻射段30位於第二輻射段40及接地部20之間。在一些實施例中,接地部20具有短路端21,以供電感電路50的第三端E3連接。在一些實施例中,如圖1所示,第一耦合間隙CG1為等寬結構。但本發明並不限於此,在另一些實施例中,如圖3所示,第一耦合間隙CG1為不等寬結構。例如,第一耦合間隙CG1包含第一區域CG1A_1及第二區域CG1A_2,第一區域CG1A_1鄰近於第一耦合區段31的第二區段的末端及第二耦合區段41的第二區段的末端,第二區域CG1A_2鄰近於電感電路50。第一區域CG1A_1的寬度小於第二區域CG1A_2。在一些實施例中,第一耦合區段31與第二耦合區段41大致呈平行直線,但不應以此為限。Refer to FIG. 1 and FIG. 3. FIG. 3 is a three-dimensional schematic diagram of the second embodiment of the antenna module 10 of the present invention. In some embodiments, the antenna module 10 further includes a substrate 60. The ground portion 20, the first radiation section 30, the second radiation section 40 and the inductor circuit 50 are located on the same surface (e.g., the top surface) of the substrate 60. In some embodiments, the first coupling section 31 of the first radiation section 30 has two sections, the first section of the first coupling section 31 extends from the second end E2 of the inductor circuit 50 in a direction away from the ground portion 20 for a length, and the second section of the first coupling section 31 is connected to the end of the first section of the first coupling section 31 to extend along an edge parallel to the ground portion 20 for a length. The second coupling section 41 of the second radiation section 40 has two sections. The first section of the second coupling section 41 extends from the fourth end E4 of the inductor circuit 50 to a distance away from the ground portion 20. The second section of the second coupling section 41 continues the end of the first section of the second coupling section 41 and extends along a distance substantially parallel to the edge of the ground portion 20. In other words, the second section of the first coupling section 31 is parallel to the second section of the second coupling section 41. In some embodiments, the length of the second section of the first coupling section 31 is shorter than the length of the second section of the second coupling section 41. As shown in FIG. 1 , in some embodiments, the second radiation section 40 is located outside the first radiation section 30 (from the perspective of the ground portion 20), that is, the first radiation section 30 is located between the second radiation section 40 and the ground portion 20. In some embodiments, the grounding portion 20 has a short-circuit end 21 for connecting to the third end E3 of the inductor circuit 50. In some embodiments, as shown in FIG. 1 , the first coupling gap CG1 is an equal-width structure. However, the present invention is not limited thereto. In other embodiments, as shown in FIG. 3 , the first coupling gap CG1 is an unequal-width structure. For example, the first coupling gap CG1 includes a first region CG1A_1 and a second region CG1A_2, the first region CG1A_1 is adjacent to the end of the second segment of the first coupling segment 31 and the end of the second segment of the second coupling segment 41, and the second region CG1A_2 is adjacent to the inductor circuit 50. The width of the first region CG1A_1 is smaller than that of the second region CG1A_2. In some embodiments, the first coupling segment 31 and the second coupling segment 41 are substantially parallel straight lines, but should not be limited thereto.

參照圖2及圖4。圖4係為本發明之電感電路50之第一實施例之側視示意圖。在電感電路50之第一實施例中,第一電感單元51包含第一線圈CL1,第二電感單元52包含第二線圈CL2。第一線圈CL1提供第一自感,第二線圈CL2提供第二自感。第一線圈CL1具有至少一第一線圈匝,第二線圈CL2具有至少一第二線圈匝。於此繪示二個第一線圈匝CL1N_1、CL1N_2及二個第二線圈匝CL2N_1、CL2N_2,但本發明並不限於此,第一線圈匝及第二線圈匝的數量可以依據設計需求做調整。相鄰的第一線圈匝與第二線圈匝間具有匝間距GN,以使第一線圈CL1及第二線圈CL2可以相互耦合而產生互感。如圖4所示,第一線圈匝CL1N_2相鄰於第二線圈匝CL2N_1,且彼此之間具有匝間距GN。Refer to Figures 2 and 4. Figure 4 is a side view schematic diagram of the first embodiment of the inductor circuit 50 of the present invention. In the first embodiment of the inductor circuit 50, the first inductor unit 51 includes a first coil CL1, and the second inductor unit 52 includes a second coil CL2. The first coil CL1 provides a first self-inductance, and the second coil CL2 provides a second self-inductance. The first coil CL1 has at least one first coil turn, and the second coil CL2 has at least one second coil turn. Two first coil turns CL1N_1, CL1N_2 and two second coil turns CL2N_1, CL2N_2 are shown here, but the present invention is not limited to this. The number of first coil turns and second coil turns can be adjusted according to design requirements. There is a turn spacing GN between adjacent first coil turns and second coil turns, so that the first coil CL1 and the second coil CL2 can be coupled with each other to generate mutual inductance. As shown in FIG. 4 , the first coil turn CL1N_2 is adjacent to the second coil turn CL2N_1 and has a turn-to-turn distance GN therebetween.

參照圖2、圖4及圖5。圖5係為本發明之電感電路50之第二實施例之立體示意圖。如圖2及圖4所示,在電感電路50之第一實施例中,第一線圈CL1及第二線圈CL2係由方線繞設而成。如圖5所示,與電感電路50之第一實施例的差異在於,在電感電路50之第二實施例中,第一線圈CL1及第二線圈CL2係由圓線繞設而成。Refer to FIG. 2, FIG. 4 and FIG. 5. FIG. 5 is a three-dimensional schematic diagram of the second embodiment of the inductor circuit 50 of the present invention. As shown in FIG. 2 and FIG. 4, in the first embodiment of the inductor circuit 50, the first coil CL1 and the second coil CL2 are wound by square wire. As shown in FIG. 5, the difference from the first embodiment of the inductor circuit 50 is that in the second embodiment of the inductor circuit 50, the first coil CL1 and the second coil CL2 are wound by round wire.

參照圖6,係為本發明之電感電路50之第三實施例之立體示意圖。與電感電路50之第二實施例之差異在於,在電感電路50之第三實施例中,第一線圈匝及第二線圈匝彼此交錯排列。例如,每兩個第二線圈匝即夾有一個第一線圈匝。如圖6所示,兩個第二線圈匝CL2N_1、CL2N_2之間夾有一個第一線圈匝CL1N_2。具體來說,第一線圈匝CL1N_1、CL1N_2及第二線圈匝CL2N_1、CL2N_2的排列順序為「第一線圈匝CL1N_1、第二線圈匝CL2N_1、第一線圈匝CL1N_2、第二線圈匝CL2N_2…等」。如此,第一線圈匝CL1N_1與第二線圈匝CL2N_1彼此相鄰且間隔匝間距GN1,第二線圈匝CL2N_1與第一線圈匝CL1N_2彼此相鄰且間隔匝間距GN2,第一線圈匝CL1N_2與第二線圈匝CL2N_2彼此相鄰且間隔匝間距GN3。在一些實施例中,該些第一線圈匝CL1N_1、CL1N_2及該些第二線圈匝CL2N_1、CL2N_2之間的該些匝間距GN1、GN2、GN3可以具有同一尺寸。但本發明並不限於此,在另一些實施例中,該些匝間距GN1、GN2、GN3可以具有不同的尺寸。Referring to FIG. 6 , it is a three-dimensional schematic diagram of the third embodiment of the inductor circuit 50 of the present invention. The difference from the second embodiment of the inductor circuit 50 is that in the third embodiment of the inductor circuit 50, the first coil turns and the second coil turns are arranged alternately with each other. For example, a first coil turn is sandwiched between every two second coil turns. As shown in FIG. 6 , a first coil turn CL1N_2 is sandwiched between two second coil turns CL2N_1 and CL2N_2. Specifically, the arrangement order of the first coil turns CL1N_1 and CL1N_2 and the second coil turns CL2N_1 and CL2N_2 is "first coil turn CL1N_1, second coil turn CL2N_1, first coil turn CL1N_2, second coil turn CL2N_2...etc.". In this way, the first coil turn CL1N_1 and the second coil turn CL2N_1 are adjacent to each other and are separated by a turn distance GN1, the second coil turn CL2N_1 and the first coil turn CL1N_2 are adjacent to each other and are separated by a turn distance GN2, and the first coil turn CL1N_2 and the second coil turn CL2N_2 are adjacent to each other and are separated by a turn distance GN3. In some embodiments, the turn distances GN1, GN2, and GN3 between the first coil turns CL1N_1, CL1N_2 and the second coil turns CL2N_1, CL2N_2 may have the same size. However, the present invention is not limited thereto, and in other embodiments, the turn distances GN1, GN2, and GN3 may have different sizes.

參照圖7,係為本發明之電感電路50之第四實施例之立體示意圖。在一些實施例中,電感電路50還包含密封體53,包覆第一線圈CL1及第二線圈CL2。雖然圖2、圖4至圖6沒有顯示,然而該等實施例中的電感電路50也可包含包覆第一線圈CL1及第二線圈CL2的密封體53。如圖6所示,在電感電路50之第三實施例中,第一線圈CL1及第二線圈CL2係由圓線繞設而成。如圖7所示,與電感電路50之第三實施例的差異在於,在電感電路50之第四實施例中,第一線圈CL1及第二線圈CL2係由方線繞設而成。在一些實施例中,密封體53可以是由絕緣材質形成,例如FR4玻璃纖維、陶瓷(Ceramic)、鈦酸鍶(SrTiO 3)、氧化鈦(TiO 2)、鈦酸鋇(BaTiO 3)等。 Referring to FIG. 7 , it is a three-dimensional schematic diagram of the fourth embodiment of the inductor circuit 50 of the present invention. In some embodiments, the inductor circuit 50 further includes a sealing body 53 covering the first coil CL1 and the second coil CL2. Although not shown in FIG. 2 , FIG. 4 to FIG. 6 , the inductor circuit 50 in these embodiments may also include a sealing body 53 covering the first coil CL1 and the second coil CL2. As shown in FIG. 6 , in the third embodiment of the inductor circuit 50, the first coil CL1 and the second coil CL2 are wound by round wire. As shown in FIG. 7 , the difference from the third embodiment of the inductor circuit 50 is that in the fourth embodiment of the inductor circuit 50, the first coil CL1 and the second coil CL2 are wound by square wire. In some embodiments, the sealing body 53 may be formed of an insulating material, such as FR4 glass fiber, ceramic, strontium titanate (SrTiO 3 ), titanium oxide (TiO 2 ), barium titanate (BaTiO 3 ), and the like.

在電感電路50之第一實施例、第二實施例、第三實施例及第四實施例中,匝間距GN、GN1、GN2、GN3可以是在0.15mm以下的範圍內,可視需求調整匝間距GN、GN1、GN2、GN3,不應以此為限。在電感電路50之第一實施例、第二實施例、第三實施例及第四實施例中,第一線圈CL1與第二線圈CL2重疊。具體來說,第一線圈CL1與第二線圈CL2具有同一繞設軸心。也就是說,第一線圈CL1與第二線圈CL2基於同一繞設軸心進行卷繞。In the first, second, third and fourth embodiments of the inductor circuit 50, the turn pitches GN, GN1, GN2 and GN3 may be within a range of less than 0.15 mm, and the turn pitches GN, GN1, GN2 and GN3 may be adjusted as required, but should not be limited thereto. In the first, second, third and fourth embodiments of the inductor circuit 50, the first coil CL1 and the second coil CL2 overlap. Specifically, the first coil CL1 and the second coil CL2 have the same winding axis. That is, the first coil CL1 and the second coil CL2 are wound based on the same winding axis.

參照圖8,係為本發明之電感電路50之第五實施例之立體示意圖。與電感電路50之第一實施例之差異在於,在電感電路50之第五實施例中,第一線圈CL1與第二線圈CL2並未重疊或是部分重疊。具體來說,第一線圈CL1所卷繞的繞設軸心C1與第二線圈CL2所卷繞的繞設軸心C2之間具有第一距離R。在一些實施例中,第一距離R是不大於第一線圈CL1的繞設半徑R1及第二線圈CL2的繞設半徑R2之總和,如式1所示。繞設半徑R1是第一線圈CL1的繞設軸心C1至第一線圈CL1的一端(即第一端E1或第二端E2)的距離。繞設半徑R2是第二線圈CL2的繞設軸心C2至第二線圈CL2的一端(即第三端E3或第四端E4)的距離。在一些實施例中,第一線圈CL1的繞設半徑R1及第二線圈CL2的繞設半徑R2之總和可以是4mm。在一些實施例中,第一線圈CL1及第二線圈CL2相鄰的一端之間(即第一端E1及第四端E4之間)具有第二距離GV。在一些實施例中,第二距離GV是在1.5mm以下的範圍內,如式2所示。Referring to FIG8 , it is a three-dimensional schematic diagram of the fifth embodiment of the inductor circuit 50 of the present invention. The difference from the first embodiment of the inductor circuit 50 is that in the fifth embodiment of the inductor circuit 50, the first coil CL1 and the second coil CL2 do not overlap or partially overlap. Specifically, there is a first distance R between the winding axis C1 around which the first coil CL1 is wound and the winding axis C2 around which the second coil CL2 is wound. In some embodiments, the first distance R is not greater than the sum of the winding radius R1 of the first coil CL1 and the winding radius R2 of the second coil CL2, as shown in Formula 1. The winding radius R1 is the distance from the winding axis C1 of the first coil CL1 to one end of the first coil CL1 (i.e., the first end E1 or the second end E2). The winding radius R2 is the distance from the winding axis C2 of the second coil CL2 to one end of the second coil CL2 (i.e., the third end E3 or the fourth end E4). In some embodiments, the sum of the winding radius R1 of the first coil CL1 and the winding radius R2 of the second coil CL2 may be 4 mm. In some embodiments, there is a second distance GV between adjacent ends of the first coil CL1 and the second coil CL2 (i.e., between the first end E1 and the fourth end E4). In some embodiments, the second distance GV is within a range of less than 1.5 mm, as shown in Formula 2.

……………………………………(式1) ……………………………………(Formula 1)

…………………………………(式2) …… ...

參照圖9,係為本發明之電感電路50之第六實施例之立體示意圖。在電感電路50之第六實施例中,電感電路50的第一電感單元51包含第一電感性線段ML1。電感電路50的第二電感單元52包含第二電感性線段ML2。第一電感性線段ML1提供第一自感,第二電感性線段ML2提供第二自感。第一電感性線段ML1與第二電感性線段ML2之間具有線間距g,以使第一電感性線段ML1及第二電感性線段ML2可以相互耦合而產生互感。第一電感性線段ML1的兩端分別是第一端E1及第二端E2。第二電感性線段ML2的兩端分別是第三端E3及第四端E4。在一些實施例中,第一電感性線段ML1與第二電感性線段ML2之間的線間距g可以是在3mm以下的範圍內。Referring to FIG. 9 , it is a three-dimensional schematic diagram of the sixth embodiment of the inductor circuit 50 of the present invention. In the sixth embodiment of the inductor circuit 50, the first inductor unit 51 of the inductor circuit 50 includes a first inductor segment ML1. The second inductor unit 52 of the inductor circuit 50 includes a second inductor segment ML2. The first inductor segment ML1 provides a first self-inductance, and the second inductor segment ML2 provides a second self-inductance. There is a line spacing g between the first inductor segment ML1 and the second inductor segment ML2, so that the first inductor segment ML1 and the second inductor segment ML2 can be coupled to each other to generate mutual inductance. The two ends of the first inductor segment ML1 are the first end E1 and the second end E2. The two ends of the second inductor segment ML2 are the third end E3 and the fourth end E4. In some embodiments, the line spacing g between the first inductive line segment ML1 and the second inductive line segment ML2 may be in a range of less than 3 mm.

在電感電路50之第六實施例中,第一電感性線段ML1及第二電感性線段ML2為位於基板54的同一表面上的導電層。導電層的材質可以是具有導電特性的碳纖維、金屬或合金,例如:金、銀、銅、鎳、鈀合金等。在一些實施例中,第一電感性線段ML1及第二電感性線段ML2是透過乾蝕刻或濕蝕刻等方式對鋪設於基板54的表面上的導電層圖案化而形成。在一些實施例中,第一電感性線段ML1及第二電感性線段ML2大致呈直線狀且相互平行。亦即,第一電感性線段ML1及第二電感性線段ML2的導電層的分布形狀可以分別大致呈直線形且相互平行。In the sixth embodiment of the inductor circuit 50, the first inductor segment ML1 and the second inductor segment ML2 are conductive layers located on the same surface of the substrate 54. The material of the conductive layer can be carbon fiber, metal or alloy with conductive properties, such as gold, silver, copper, nickel, palladium alloy, etc. In some embodiments, the first inductor segment ML1 and the second inductor segment ML2 are formed by patterning the conductive layer laid on the surface of the substrate 54 by dry etching or wet etching. In some embodiments, the first inductor segment ML1 and the second inductor segment ML2 are substantially straight and parallel to each other. That is, the distribution shapes of the conductive layers of the first inductor segment ML1 and the second inductor segment ML2 can be substantially straight and parallel to each other.

參照圖10及圖11。圖10係為本發明之電感電路50之第七實施例之立體示意圖。圖11係為本發明之電感電路50之第七實施例之側視剖面示意圖。與電感電路50之第六實施例之差異在於,在電感電路50之第七實施例中,第一電感性線段ML1及第二電感性線段ML2分別位於基板54的相對二平面。如此,第一電感性線段ML1與第二電感性線段ML2之間的線間距g是基板54的頂表面及底表面之間的距離(即,基板54的厚度)。在一些實施例中,第一電感性線段ML1及第二電感性線段ML2的走線路徑非為直線狀,例如分別呈凹形及凸形。第一電感性線段ML1及第二電感性線段ML2分別具有一重疊區段,該二重疊區段彼此相對,以相互耦合產生互感。Refer to FIG. 10 and FIG. 11. FIG. 10 is a three-dimensional schematic diagram of the seventh embodiment of the inductor circuit 50 of the present invention. FIG. 11 is a side cross-sectional schematic diagram of the seventh embodiment of the inductor circuit 50 of the present invention. The difference from the sixth embodiment of the inductor circuit 50 is that in the seventh embodiment of the inductor circuit 50, the first inductor line segment ML1 and the second inductor line segment ML2 are respectively located in two opposite planes of the substrate 54. In this way, the line spacing g between the first inductor line segment ML1 and the second inductor line segment ML2 is the distance between the top surface and the bottom surface of the substrate 54 (i.e., the thickness of the substrate 54). In some embodiments, the routing paths of the first inductor line segment ML1 and the second inductor line segment ML2 are not straight lines, for example, they are concave and convex, respectively. The first inductive line segment ML1 and the second inductive line segment ML2 each have an overlapping section, and the two overlapping sections are opposite to each other to couple with each other to generate mutual inductance.

如圖10及圖11所示,在一些實施例中,第一電感單元51還包含第一電感器I1。第二電感單元52還包含第二電感器I2。第一電感器I1連接第一電感性線段ML1。第二電感器I2連接第二電感性線段ML2。第一電感器I1及第二電感器I2是電感器組件。如此,可增添額外的電感值,以加強第一電感單元51的第一自感、第二電感單元52的第二自感,從而滿足天線模組10為了消除電容效應所需的電感量。在一些實施例中,第一電感器I1及第二電感器I2位於基板54的同一側。在一些實施例中,第一電感器I1及第二電感器I2和第一電感性線段ML1位於基板54的同一側;在另一些實施例中,第一電感器I1及第二電感器I2和第二電感性線段ML2位於基板54的同一側(圖未示)。如圖10及圖11所示,係示意第一電感器I1及第二電感器I2和第一電感性線段ML1位於基板54的同一側之例,第一電感器I1的接腳直接連接第一電感性線段ML1,第二電感器I2的接腳經由通過基板54的導線WR間接連接第二電感性線段ML2。As shown in FIG. 10 and FIG. 11 , in some embodiments, the first inductor unit 51 further includes a first inductor I1. The second inductor unit 52 further includes a second inductor I2. The first inductor I1 is connected to the first inductance line segment ML1. The second inductor I2 is connected to the second inductance line segment ML2. The first inductor I1 and the second inductor I2 are inductor components. In this way, an additional inductance value can be added to enhance the first self-inductance of the first inductor unit 51 and the second self-inductance of the second inductor unit 52, thereby satisfying the inductance required by the antenna module 10 to eliminate the capacitive effect. In some embodiments, the first inductor I1 and the second inductor I2 are located on the same side of the substrate 54. In some embodiments, the first inductor I1, the second inductor I2 and the first inductive line segment ML1 are located on the same side of the substrate 54; in other embodiments, the first inductor I1, the second inductor I2 and the second inductive line segment ML2 are located on the same side of the substrate 54 (not shown). As shown in FIG10 and FIG11, the first inductor I1, the second inductor I2 and the first inductive line segment ML1 are located on the same side of the substrate 54, and the pin of the first inductor I1 is directly connected to the first inductive line segment ML1, and the pin of the second inductor I2 is indirectly connected to the second inductive line segment ML2 via the wire WR passing through the substrate 54.

在一些實施例中,第一電感器I1及第二電感器I2位於基板54的相對兩側(即第一側與第二側)。例如,第一電感器I1與第一電感性線段ML1位於基板54的同一側(第一側),且第一電感器I1直接連接第一電感性線段ML1;第二電感器I2與第二電感性線段ML2位於基板54的同一側(第二側),且第二電感器I2直接連接第二電感性線段ML2。In some embodiments, the first inductor I1 and the second inductor I2 are located on opposite sides (i.e., the first side and the second side) of the substrate 54. For example, the first inductor I1 and the first inductive line segment ML1 are located on the same side (the first side) of the substrate 54, and the first inductor I1 is directly connected to the first inductive line segment ML1; the second inductor I2 and the second inductive line segment ML2 are located on the same side (the second side) of the substrate 54, and the second inductor I2 is directly connected to the second inductive line segment ML2.

在一些實施例中,第一自感及第二自感的電感值係可以透過前述第一線圈CL1、第二線圈CL2、第一電感性線段ML1及第二電感性線段ML2的長度、寬度及磁導率(permeability)與第一電感器I1及第二電感器I2的電感值來決定。在一些實施例中,磁導率可以是小於40倍的真空磁導率,其中真空磁導率為4π×10 -7H/m(亨利每米)。在一些實施例中,第一電感單元51及第二電感單元52之間的互感係可以透過前述第一線圈CL1與第二線圈CL2之間的重疊的區域尺寸、匝間距GN、GN1、GN2、GN3、第二距離GV及線間距g來決定。 In some embodiments, the inductance of the first self-inductance and the second self-inductance can be determined by the length, width and permeability of the first coil CL1, the second coil CL2, the first inductive line segment ML1 and the second inductive line segment ML2 and the inductance of the first inductor I1 and the second inductor I2. In some embodiments, the permeability can be less than 40 times the vacuum permeability, where the vacuum permeability is 4π× 10-7 H/m (henry per meter). In some embodiments, the mutual inductance between the first inductance unit 51 and the second inductance unit 52 can be determined by the size of the overlapping area between the first coil CL1 and the second coil CL2, the turn spacing GN, GN1, GN2, GN3, the second distance GV and the line spacing g.

參照圖12,係為本發明之天線模組10之第三實施例之立體示意圖。與天線模組10之第一實施例之差異在於,在天線模組10之第三實施例中,第一輻射段30還包含第一分支段32,第二輻射段40還包含第二分支段42。第一分支段32連接第一耦合區段31。第二分支段42連接第二耦合區段41。第一分支段32及第二分支段42用以分別激發不同於第一共振頻帶、第二共振頻帶及第三共振頻帶的其他共振頻帶。如此,可以提升天線模組10所支援的頻寬多樣性。在一些實施例中,第一分支段32具有兩區段,第一分支段32的第一區段是從第一耦合區段31的第二區段的中間處向接地部20延伸一段長度,第一分支段32的第二區段是接續第一分支段32的第一區段的末端以大致沿著平行於第一耦合區段31的第二區段延伸一段長度。也就是說,第一分支段32的第二區段平行於第一耦合區段31的第二區段。第一分支段32位於第一耦合區段31的內側(以接地部20的觀點),亦即第一分支段32位於第一耦合區段31及接地部20之間。在一些實施例中,第一分支段32的第二區段係短於第一耦合區段31的第二區段。在一些實施例中,第二分支段42是從第二耦合區段41的第一區段與第二區段之間的交界處大致沿著平行於接地部20之邊緣朝遠離第二耦合區段41的第二區段的方向延伸一段長度。Referring to FIG. 12 , it is a three-dimensional schematic diagram of the third embodiment of the antenna module 10 of the present invention. The difference from the first embodiment of the antenna module 10 is that in the third embodiment of the antenna module 10, the first radiation section 30 further includes a first branch section 32, and the second radiation section 40 further includes a second branch section 42. The first branch section 32 is connected to the first coupling section 31. The second branch section 42 is connected to the second coupling section 41. The first branch section 32 and the second branch section 42 are used to respectively excite other resonance frequency bands different from the first resonance frequency band, the second resonance frequency band, and the third resonance frequency band. In this way, the bandwidth diversity supported by the antenna module 10 can be improved. In some embodiments, the first branch segment 32 has two sections, the first section of the first branch segment 32 extends from the middle of the second section of the first coupling segment 31 to the grounding portion 20 for a certain length, and the second section of the first branch segment 32 continues from the end of the first section of the first branch segment 32 to extend for a certain length along the second section substantially parallel to the first coupling segment 31. In other words, the second section of the first branch segment 32 is parallel to the second section of the first coupling segment 31. The first branch segment 32 is located at the inner side of the first coupling segment 31 (from the perspective of the grounding portion 20), that is, the first branch segment 32 is located between the first coupling segment 31 and the grounding portion 20. In some embodiments, the second section of the first branch segment 32 is shorter than the second section of the first coupling segment 31. In some embodiments, the second branch segment 42 extends from the boundary between the first segment and the second segment of the second coupling segment 41 to a length substantially along an edge parallel to the ground portion 20 in a direction away from the second segment of the second coupling segment 41 .

在一些實施例中,天線模組10還包含寄生段70。寄生段70連接接地部20。寄生段70與第一輻射段30及第二輻射段40中之至少一者相鄰且間隔第二耦合間隙CG2(CG2_A、CG2_B)。藉由第二耦合間隙CG2(CG2_A、CG2_B),饋入源FD的能量可以從第一耦合區段31耦合至寄生段70,並經過接地部20及參考地端以形成共振迴路,從而使寄生段70激發不同於第一共振頻帶、第二共振頻帶及第三共振頻帶的其它頻帶,或是使寄生段70協助第一輻射段30及第二輻射段40激發第一共振頻帶、第二共振頻帶及第三共振頻帶。以下將以天線模組10之第四實施例至第七實施例進行寄生段70的說明。In some embodiments, the antenna module 10 further includes a parasitic section 70. The parasitic section 70 is connected to the ground portion 20. The parasitic section 70 is adjacent to at least one of the first radiation section 30 and the second radiation section 40 and is separated by a second coupling gap CG2 (CG2_A, CG2_B). Through the second coupling gap CG2 (CG2_A, CG2_B), the energy of the feed source FD can be coupled from the first coupling section 31 to the parasitic section 70, and pass through the ground portion 20 and the reference ground to form a resonant loop, so that the parasitic section 70 excites other frequency bands different from the first resonant frequency band, the second resonant frequency band, and the third resonant frequency band, or the parasitic section 70 assists the first radiation section 30 and the second radiation section 40 to excite the first resonant frequency band, the second resonant frequency band, and the third resonant frequency band. The parasitic segment 70 will be described below using the fourth to seventh embodiments of the antenna module 10 .

參照圖13,係為本發明之天線模組10之第四實施例之立體示意圖。在天線模組10之第四實施例中,寄生段70從接地部20的短路端21大致沿著平行於第一輻射段30的第一耦合區段31的第二區段延伸一段距離。寄生段70與第一輻射段30相鄰且間隔第二耦合間隙CG2。在一些實施例中,寄生段70與第二耦合區段41的第二區段的末端係延伸至同一軸線。在一些實施例中,寄生段70位於第一輻射段30的內側(以接地部20的觀點),亦即寄生段70位於第一輻射段30及接地部20之間。Referring to FIG. 13 , it is a three-dimensional schematic diagram of the fourth embodiment of the antenna module 10 of the present invention. In the fourth embodiment of the antenna module 10, the parasitic section 70 extends from the short-circuit end 21 of the ground portion 20 to a distance substantially along the second section of the first coupling section 31 parallel to the first radiation section 30. The parasitic section 70 is adjacent to the first radiation section 30 and is separated by a second coupling gap CG2. In some embodiments, the ends of the second section of the parasitic section 70 and the second coupling section 41 extend to the same axis. In some embodiments, the parasitic section 70 is located on the inner side of the first radiation section 30 (from the perspective of the ground portion 20), that is, the parasitic section 70 is located between the first radiation section 30 and the ground portion 20.

參照圖14,係為本發明之天線模組10之第五實施例之立體示意圖。與天線模組10之第四實施例之差異在於,在天線模組10之第五實施例中,寄生段70具有兩區段,寄生段70的第一區段從接地部20朝遠離接地部20的方向延伸一段距離,寄生段70的第二區段是接續寄生段70的第一區段的末端以大致沿著平行於第一輻射段30的第一耦合區段31的第二區段延伸一段距離。寄生段70與第一輻射段30相鄰且間隔第二耦合間隙CG2。亦即,寄生段70的第二區段與第一輻射段30的第一耦合區段31的第二區段相鄰且間隔第二耦合間隙CG2。Referring to FIG. 14 , it is a three-dimensional schematic diagram of the fifth embodiment of the antenna module 10 of the present invention. The difference from the fourth embodiment of the antenna module 10 is that in the fifth embodiment of the antenna module 10, the parasitic section 70 has two sections, the first section of the parasitic section 70 extends a distance from the ground portion 20 in a direction away from the ground portion 20, and the second section of the parasitic section 70 is a second section extending a distance from the end of the first section of the parasitic section 70 to substantially extend along the first coupling section 31 parallel to the first radiation section 30. The parasitic section 70 is adjacent to the first radiation section 30 and is separated by the second coupling gap CG2. That is, the second section of the parasitic section 70 is adjacent to the second section of the first coupling section 31 of the first radiation section 30 and is separated by the second coupling gap CG2.

參照圖15,係為本發明之天線模組10之第六實施例之立體示意圖。與天線模組10之第五實施例之差異在於,在天線模組10之第六實施例中,寄生段70的第二區段是接續寄生段70的第一區段的末端以大致沿著平行於第二輻射段40的第二耦合區段41的第二區段延伸一段距離,且寄生段70的第二區段的末端及第一耦合區段31的第二區段的末端是朝向彼此延伸。寄生段70與第一輻射段30及第二輻射段40相鄰且分別間隔第二耦合間隙CG2_A、CG2_B。具體來說,寄生段70的末端與第一耦合區段31的末端相對且間隔第二耦合間隙CG2_A。寄生段70的第二區段與第二輻射段40的第二耦合區段41的第二區段相鄰且間隔第二耦合間隙CG2_B。其中,第二耦合間隙CG2_A及第二耦合間隙CG2_B可以不相同。在一些實施例中,第二輻射段40是位於寄生段70的外側(以接地部20的觀點)。亦即,寄生段70位於第二輻射段40及接地部20之間。Referring to FIG. 15 , it is a three-dimensional schematic diagram of the sixth embodiment of the antenna module 10 of the present invention. The difference from the fifth embodiment of the antenna module 10 is that in the sixth embodiment of the antenna module 10, the second section of the parasitic section 70 is connected to the end of the first section of the parasitic section 70 to extend a distance substantially along the second section of the second coupling section 41 parallel to the second radiation section 40, and the end of the second section of the parasitic section 70 and the end of the second section of the first coupling section 31 extend toward each other. The parasitic section 70 is adjacent to the first radiation section 30 and the second radiation section 40 and is separated by the second coupling gaps CG2_A and CG2_B, respectively. Specifically, the end of the parasitic section 70 is opposite to the end of the first coupling section 31 and is separated by the second coupling gap CG2_A. The second section of the parasitic section 70 is adjacent to the second section of the second coupling section 41 of the second radiation section 40 and is separated by a second coupling gap CG2_B. The second coupling gap CG2_A and the second coupling gap CG2_B may be different. In some embodiments, the second radiation section 40 is located outside the parasitic section 70 (from the perspective of the ground portion 20). That is, the parasitic section 70 is located between the second radiation section 40 and the ground portion 20.

參照圖16,係為本發明之天線模組10之第七實施例之立體示意圖。與天線模組10之第五實施例之差異在於,在天線模組10之第七實施例中,寄生段70的第二區段是接續寄生段70的第一區段的末端以大致沿著平行於接地部20之邊緣延伸一段距離。寄生段70是位於第一輻射段30及第二輻射段40的外側(以接地部20的觀點)。亦即,第一輻射段30及第二輻射段40位於寄生段70及接地部20之間。寄生段70的第二區段與第二輻射段40的第二耦合區段41的第二區段相鄰且間隔第二耦合間隙CG2。Referring to FIG. 16 , it is a three-dimensional schematic diagram of the seventh embodiment of the antenna module 10 of the present invention. The difference from the fifth embodiment of the antenna module 10 is that in the seventh embodiment of the antenna module 10, the second section of the parasitic section 70 is connected to the end of the first section of the parasitic section 70 to extend a distance substantially along the edge parallel to the ground portion 20. The parasitic section 70 is located on the outer side of the first radiation section 30 and the second radiation section 40 (from the perspective of the ground portion 20). That is, the first radiation section 30 and the second radiation section 40 are located between the parasitic section 70 and the ground portion 20. The second section of the parasitic section 70 is adjacent to the second section of the second coupling section 41 of the second radiation section 40 and is separated by a second coupling gap CG2.

在一些實施例中,第一輻射段30位於第二輻射段40的外側(以接地部20的觀點)。亦即,第二輻射段40位於第一輻射段30及接地部20之間。以下將以天線模組10之第八實施例至第十二實施例進行說明。In some embodiments, the first radiation section 30 is located outside the second radiation section 40 (from the perspective of the ground portion 20). That is, the second radiation section 40 is located between the first radiation section 30 and the ground portion 20. The eighth to twelfth embodiments of the antenna module 10 are described below.

參照圖17,係為本發明之天線模組10之第八實施例之立體示意圖。與天線模組10之第一實施例之差異在於,在天線模組10之第八實施例中,第一輻射段30位於第二輻射段40的外側(以接地部20的觀點)。第二輻射段40的第二耦合區段41大致沿著平行於接地部20之邊緣延伸一段長度。也就是說,第一耦合區段31的第二區段平行於第二耦合區段41。第一耦合區段31的第二區段所延伸的長度係短於第二耦合區段41的延伸長度。Referring to FIG. 17 , it is a three-dimensional schematic diagram of the eighth embodiment of the antenna module 10 of the present invention. The difference from the first embodiment of the antenna module 10 is that in the eighth embodiment of the antenna module 10, the first radiation section 30 is located outside the second radiation section 40 (from the perspective of the ground portion 20). The second coupling section 41 of the second radiation section 40 extends along a length substantially parallel to the edge of the ground portion 20. In other words, the second section of the first coupling section 31 is parallel to the second coupling section 41. The length of the second section of the first coupling section 31 is shorter than the extension length of the second coupling section 41.

參照圖18,係為本發明之天線模組10之第九實施例之立體示意圖。與天線模組10之第八實施例之差異在於,在天線模組10之第九實施例中,第一輻射段30還包含連接第一耦合區段31的第一分支段32,第二輻射段40還包含連接第二耦合區段41的第二分支段42。舉例來說,第二分支段42具有兩區段,第二分支段42的第一區段是從第二耦合區段41的中間處向接地部20延伸一段長度,第二分支段42的第二區段是接續第二分支段42的第一區段的末端以大致沿著平行於第二耦合區段41延伸一段長度。也就是說,第二分支段42的第二區段平行於第二耦合區段41。第二分支段42位於第二耦合區段41的內側(以接地部20的觀點),亦即第二分支段42位於第二耦合區段41及接地部20之間。在一些實施例中,第二分支段42的第二區段係短於第二耦合區段41。第一分支段32是從第一耦合區段31的第一區段與第二區段之間的交界處大致沿著平行於接地部20之邊緣朝遠離第一耦合區段31的第二區段的方向延伸一段長度。Referring to FIG. 18 , it is a three-dimensional schematic diagram of the ninth embodiment of the antenna module 10 of the present invention. The difference from the eighth embodiment of the antenna module 10 is that in the ninth embodiment of the antenna module 10, the first radiation section 30 further includes a first branch section 32 connected to the first coupling section 31, and the second radiation section 40 further includes a second branch section 42 connected to the second coupling section 41. For example, the second branch section 42 has two sections, the first section of the second branch section 42 extends from the middle of the second coupling section 41 to the ground portion 20 for a length, and the second section of the second branch section 42 continues from the end of the first section of the second branch section 42 to extend for a length substantially parallel to the second coupling section 41. That is, the second section of the second branch section 42 is parallel to the second coupling section 41. The second branch segment 42 is located inside the second coupling segment 41 (from the perspective of the grounding portion 20), that is, the second branch segment 42 is located between the second coupling segment 41 and the grounding portion 20. In some embodiments, the second segment of the second branch segment 42 is shorter than the second coupling segment 41. The first branch segment 32 extends from the boundary between the first segment and the second segment of the first coupling segment 31 substantially along the edge parallel to the grounding portion 20 toward the direction away from the second segment of the first coupling segment 31.

參照圖19,係為本發明之天線模組10之第十實施例之立體示意圖。與天線模組10之第八實施例之差異在於,在天線模組10之第十實施例中,天線模組10還包含連接接地部20的寄生段70。舉例來說,寄生段70從接地部20的短路端21大致沿著平行於接地部20之邊緣延伸一段距離。寄生段70與第一輻射段30相鄰且間隔第二耦合間隙CG2。亦即,寄生段70與第一輻射段30的第一耦合區段31的第二區段相鄰且間隔第二耦合間隙CG2。在一些實施例中,寄生段70所延伸的距離可以長於第一耦合區段31的第二區段但短於第二耦合區段41。寄生段70位於第一輻射段30及第二輻射段40的外側(以接地部20的觀點)。亦即,第一輻射段30及第二輻射段40位於寄生段70及接地部20之間。Refer to Figure 19, which is a three-dimensional schematic diagram of the tenth embodiment of the antenna module 10 of the present invention. The difference from the eighth embodiment of the antenna module 10 is that in the tenth embodiment of the antenna module 10, the antenna module 10 further includes a parasitic section 70 connected to the ground portion 20. For example, the parasitic section 70 extends a distance from the short-circuit end 21 of the ground portion 20 approximately along the edge parallel to the ground portion 20. The parasitic section 70 is adjacent to the first radiation section 30 and is separated by the second coupling gap CG2. That is, the parasitic section 70 is adjacent to the second section of the first coupling section 31 of the first radiation section 30 and is separated by the second coupling gap CG2. In some embodiments, the distance extended by the parasitic section 70 may be longer than the second section of the first coupling section 31 but shorter than the second coupling section 41. The parasitic section 70 is located outside the first radiation section 30 and the second radiation section 40 (from the perspective of the ground portion 20 ). That is, the first radiation section 30 and the second radiation section 40 are located between the parasitic section 70 and the ground portion 20 .

參照圖20,係為本發明之天線模組10之第十一實施例之立體示意圖。與天線模組10之第十實施例之差異在於,在天線模組10之第十一實施例中,寄生段70具有兩區段,寄生段70的第一區段從接地部20朝遠離接地部20的方向延伸一段距離,寄生段70的第二區段是接續寄生段70的第一區段的末端以大致沿著平行於接地部20之邊緣延伸一段距離。寄生段70與第一輻射段30及第二輻射段40相鄰且分別間隔第二耦合間隙CG2_A、CG2_B。亦即,寄生段70的第一區段與第二耦合區段41的末端相鄰且間隔第二耦合間隙CG2_B,寄生段70的第二區段與第一耦合區段31的第二區段相鄰且間隔第二耦合間隙CG2_A。其中,第二耦合間隙CG2_A及第二耦合間隙CG2_B可以不相同。Referring to FIG. 20 , it is a three-dimensional schematic diagram of the eleventh embodiment of the antenna module 10 of the present invention. The difference from the tenth embodiment of the antenna module 10 is that in the eleventh embodiment of the antenna module 10, the parasitic section 70 has two sections, the first section of the parasitic section 70 extends a distance from the ground portion 20 in a direction away from the ground portion 20, and the second section of the parasitic section 70 is connected to the end of the first section of the parasitic section 70 and extends a distance substantially along the edge parallel to the ground portion 20. The parasitic section 70 is adjacent to the first radiation section 30 and the second radiation section 40 and is separated by second coupling gaps CG2_A and CG2_B, respectively. That is, the first section of the parasitic section 70 is adjacent to the end of the second coupling section 41 and separated by the second coupling gap CG2_B, and the second section of the parasitic section 70 is adjacent to the second section of the first coupling section 31 and separated by the second coupling gap CG2_A. The second coupling gap CG2_A and the second coupling gap CG2_B may be different.

參照圖21,係為本發明之天線模組10之第十二實施例之立體示意圖。與天線模組10之第十一實施例之差異在於,在天線模組10之第十二實施例中,寄生段70的第二區段是接續寄生段70的第一區段的末端以大致沿著平行於第二耦合區段41延伸一段距離。寄生段70是位於第二輻射段40的內側(以接地部20的觀點)。亦即,寄生段70位於第二輻射段40及接地部20之間。Referring to FIG. 21 , it is a three-dimensional schematic diagram of the twelfth embodiment of the antenna module 10 of the present invention. The difference from the eleventh embodiment of the antenna module 10 is that in the twelfth embodiment of the antenna module 10, the second section of the parasitic section 70 is connected to the end of the first section of the parasitic section 70 to extend a distance substantially parallel to the second coupling section 41. The parasitic section 70 is located on the inner side of the second radiation section 40 (from the perspective of the ground portion 20). That is, the parasitic section 70 is located between the second radiation section 40 and the ground portion 20.

參照圖22,係為本發明之天線模組10之第十三實施例之立體示意圖。與天線模組10之第一實施例之差異在於,在天線模組10之第十三實施例中,接地部20連接有電感器I3作為短路端21,以供電感電路50的第三端E3連接。電感器I3可以是電感器組件。在一些實施例中,電感器I3的電感值可為小於2nH。Referring to FIG. 22 , it is a three-dimensional schematic diagram of the thirteenth embodiment of the antenna module 10 of the present invention. The difference from the first embodiment of the antenna module 10 is that in the thirteenth embodiment of the antenna module 10, the ground portion 20 is connected to an inductor I3 as a short-circuit end 21 for connection to the third end E3 of the inductor circuit 50. The inductor I3 may be an inductor assembly. In some embodiments, the inductance value of the inductor I3 may be less than 2nH.

在一些實施例中,前述接地部20、第一輻射段30、第二輻射段40及寄生段70係由導電材質構成。導電材質具體可以是基板60的表面上的導電層。例如,前述接地部20、第一輻射段30、第二輻射段40及寄生段70是透過乾蝕刻或濕蝕刻等方式對鋪設於基板60的導電層圖案化而形成。In some embodiments, the grounding portion 20, the first radiation section 30, the second radiation section 40 and the parasitic section 70 are made of a conductive material. The conductive material may be a conductive layer on the surface of the substrate 60. For example, the grounding portion 20, the first radiation section 30, the second radiation section 40 and the parasitic section 70 are formed by patterning the conductive layer disposed on the substrate 60 by dry etching or wet etching.

在一些實施中,饋入源FD透過同軸纜線(具體來說其內部芯線與編織線)連接主機板的無線通訊模組。如此,無線通訊模組可以透過天線模組10進行無線訊號的傳輸。無線通訊模組可以是具有無線通訊認證(Wi-Fi)、藍芽等無線傳輸功能的無線通訊電路。In some implementations, the feed source FD is connected to the wireless communication module of the motherboard via a coaxial cable (specifically, its internal core wire and braided wire). In this way, the wireless communication module can transmit wireless signals via the antenna module 10. The wireless communication module can be a wireless communication circuit with wireless communication authentication (Wi-Fi), Bluetooth, etc. wireless transmission functions.

參照圖23至圖25。圖23係為本發明之第一比較例之天線模組10_PA之立體示意圖。圖24係為本發明之第二比較例之天線模組10_PA之立體示意圖。圖25係為本發明之第三比較例之天線模組10_PA之立體示意圖。在第一比較例中,天線高度是較高的,即第二耦合區段41_PA與接地部20_PA之間的距離大於5mm。在第二比較例中,天線高度是較低的,即第二耦合區段41_PA與接地部20_PA之間的距離小於5mm,也就是說與第一比較例相比,第二比較例之天線模組10_PA是低姿態。與第二比較例之差異在於,在第三比較例中,第一耦合區段31_PA與饋入源FD_PA之間及第二耦合區段41_PA與接地部20_PA之間分別連接有電感器I_PA(即電感器組件)。Refer to Figures 23 to 25. Figure 23 is a three-dimensional schematic diagram of the antenna module 10_PA of the first comparative example of the present invention. Figure 24 is a three-dimensional schematic diagram of the antenna module 10_PA of the second comparative example of the present invention. Figure 25 is a three-dimensional schematic diagram of the antenna module 10_PA of the third comparative example of the present invention. In the first comparative example, the antenna height is relatively high, that is, the distance between the second coupling section 41_PA and the ground portion 20_PA is greater than 5 mm. In the second comparative example, the antenna height is relatively low, that is, the distance between the second coupling section 41_PA and the ground portion 20_PA is less than 5 mm, that is, compared with the first comparative example, the antenna module 10_PA of the second comparative example is in a low posture. The difference from the second comparative example is that in the third comparative example, an inductor I_PA (ie, an inductor assembly) is connected between the first coupling section 31_PA and the feeding source FD_PA and between the second coupling section 41_PA and the ground portion 20_PA, respectively.

參照圖26,係為本發明之第一比較例至第三比較例之天線模組10_PA之回波損耗的實驗數據圖。從圖26可見,在第一比較例中,當天線高度較高的情形下,天線模組10_PA具有較佳的回波損耗(如曲線CU1),例如在天線模組10_PA所支援的共振頻帶下,天線模組10_PA的回波損耗小於-6dB(Decibel)。在第二比較例中,當天線高度較低(即低姿態)的情形下,天線模組10_PA具有較差的回波損耗(如曲線CU2),例如在天線模組10_PA所支援的共振頻帶下,天線模組10_PA的回波損耗大於-6dB。也就是說,天線高度與天線特性之間呈正相關。在第三比較例中,由於電感器I_PA可以消除部分的電容效應(例如第一耦合區段31_PA與接地部20_PA之間的電容效應及第二耦合區段41_PA與接地部20_PA之間的電容效應),因此第三比較例的回波損耗(如曲線CU3)較佳於第二比較例的回波損耗。然而,由於天線模組10_PA中仍有其他的電容效應(例如,第一耦合間隙CG1_PA與接地部20_PA之間的電容效應)未被消除,因此第三比較例的回波損耗仍無法具有較佳的回波損耗,且無法趨近於第一比較例的回波損耗。Referring to FIG. 26 , it is an experimental data diagram of the return loss of the antenna module 10_PA of the first to third comparative examples of the present invention. As can be seen from FIG. 26 , in the first comparative example, when the antenna height is higher, the antenna module 10_PA has a better return loss (such as curve CU1), for example, in the resonance frequency band supported by the antenna module 10_PA, the return loss of the antenna module 10_PA is less than -6dB (Decibel). In the second comparative example, when the antenna height is lower (i.e., low posture), the antenna module 10_PA has a worse return loss (such as curve CU2), for example, in the resonance frequency band supported by the antenna module 10_PA, the return loss of the antenna module 10_PA is greater than -6dB. That is to say, there is a positive correlation between the antenna height and the antenna characteristics. In the third comparative example, since the inductor I_PA can eliminate part of the capacitive effect (e.g., the capacitive effect between the first coupling section 31_PA and the ground portion 20_PA and the capacitive effect between the second coupling section 41_PA and the ground portion 20_PA), the return loss of the third comparative example (such as curve CU3) is better than the return loss of the second comparative example. However, since there are still other capacitive effects in the antenna module 10_PA (e.g., the capacitive effect between the first coupling gap CG1_PA and the ground portion 20_PA) that have not been eliminated, the return loss of the third comparative example still cannot have a better return loss and cannot approach the return loss of the first comparative example.

參照圖27,係為本發明之天線模組10之第一實施例及第三實施例之回波損耗的實驗數據圖。曲線CU4為天線模組10之第一實施例之回波損耗。曲線CU5為天線模組10之第三實施例之回波損耗。由於電感電路50可以消除第一輻射段30與接地部20之間的電容效應及消除第二輻射段40與接地部20之間的電容效應(例如,第一耦合區段31與接地部20之間的電容效應、第二耦合區段41與接地部20之間的電容效應及第一耦合間隙CG1與接地部20之間的電容效應),因此天線模組10具有較佳的回波損耗。例如在天線模組10所支援的共振頻帶下,天線模組10的回波損耗小於-6 dB,且可以趨近於第一比較例的回波損耗。Referring to FIG. 27 , it is an experimental data graph of the echo loss of the first embodiment and the third embodiment of the antenna module 10 of the present invention. Curve CU4 is the echo loss of the first embodiment of the antenna module 10. Curve CU5 is the echo loss of the third embodiment of the antenna module 10. Since the inductor circuit 50 can eliminate the capacitive effect between the first radiation section 30 and the ground portion 20 and eliminate the capacitive effect between the second radiation section 40 and the ground portion 20 (for example, the capacitive effect between the first coupling section 31 and the ground portion 20, the capacitive effect between the second coupling section 41 and the ground portion 20, and the capacitive effect between the first coupling gap CG1 and the ground portion 20), the antenna module 10 has better echo loss. For example, in the resonance frequency band supported by the antenna module 10, the echo loss of the antenna module 10 is less than -6 dB and can be close to the echo loss of the first comparative example.

綜上所述,依據一些實施例,透過電感電路,本發明可以在天線高度被降低(即低姿態)的同時消除第一輻射段與接地部之間的電容效應及消除第二輻射段與接地部之間的電容效應,以改善天線模組的頻寬及天線特性。In summary, according to some embodiments, the present invention can reduce the height of the antenna (i.e., low posture) by using an inductor circuit while eliminating the capacitance effect between the first radiation segment and the ground portion and eliminating the capacitance effect between the second radiation segment and the ground portion, so as to improve the bandwidth and antenna characteristics of the antenna module.

10,10_PA:天線模組 20,20_PA:接地部 21:短路端 I3:電感器 30:第一輻射段 31,31_PA:第一耦合區段 32:第一分支段 40:第二輻射段 41,41_PA:第二耦合區段 42:第二分支段 50:電感電路 51:第一電感單元 CL1:第一線圈 CL1N_1,CL1N_2:第一線圈匝 ML1:第一電感性線段 I1:第一電感器 52:第二電感單元 CL2:第二線圈 CL2N_1,CL2N_2:第二線圈匝 ML2:第二電感性線段 I2:第二電感器 53:密封體 54:基板 E1:第一端 E2:第二端 E3:第三端 E4:第四端 GN,GN1,GN2,GN3:匝間距 R:第一距離 R1,R2:繞設半徑 GV:第二距離 g:線間距 WR:導線 C1,C2:繞設軸心 60:基板 70:寄生段 FD,FD_PA:饋入源 CG1,CG1_PA:第一耦合間隙 CG1A_1:第一區域 CG1A_2:第二區域 CG2,CG2_A,CG2_B:第二耦合間隙 I_PA:電感器 CU1,CU2,CU3,CU4,CU5:曲線 10,10_PA: antenna module 20,20_PA: grounding part 21: short circuit end I3: inductor 30: first radiation section 31,31_PA: first coupling section 32: first branch section 40: second radiation section 41,41_PA: second coupling section 42: second branch section 50: inductor circuit 51: first inductor unit CL1: first coil CL1N_1,CL1N_2: first coil turn ML1: first inductive line segment I1: first inductor 52: second inductor unit CL2: second coil CL2N_1,CL2N_2: second coil turn ML2: second inductive line segment I2: second inductor 53: sealing body 54: substrate E1: first end E2: second end E3: third end E4: fourth end GN, GN1, GN2, GN3: turn spacing R: first distance R1, R2: winding radius GV: second distance g: wire spacing WR: conductor C1, C2: winding axis 60: substrate 70: parasitic segment FD, FD_PA: feed source CG1, CG1_PA: first coupling gap CG1A_1: first region CG1A_2: second region CG2, CG2_A, CG2_B: second coupling gap I_PA: inductor CU1, CU2, CU3, CU4, CU5: curve

圖1係為本發明之天線模組之第一實施例之立體示意圖。 圖2係為本發明之電感電路之第一實施例之立體示意圖。 圖3係為本發明之天線模組之第二實施例之立體示意圖。 圖4係為本發明之電感電路之第一實施例之側視示意圖。 圖5係為本發明之電感電路之第二實施例之立體示意圖。 圖6係為本發明之電感電路之第三實施例之立體示意圖。 圖7係為本發明之電感電路之第四實施例之立體示意圖。 圖8係為本發明之電感電路之第五實施例之立體示意圖。 圖9係為本發明之電感電路之第六實施例之立體示意圖。 圖10係為本發明之電感電路之第七實施例之立體示意圖。 圖11係為本發明之電感電路之第七實施例之側視剖面示意圖。 圖12係為本發明之天線模組之第三實施例之立體示意圖。 圖13係為本發明之天線模組之第四實施例之立體示意圖。 圖14係為本發明之天線模組之第五實施例之立體示意圖。 圖15係為本發明之天線模組之第六實施例之立體示意圖。 圖16係為本發明之天線模組之第七實施例之立體示意圖。 圖17係為本發明之天線模組之第八實施例之立體示意圖。 圖18係為本發明之天線模組之第九實施例之立體示意圖。 圖19係為本發明之天線模組之第十實施例之立體示意圖。 圖20係為本發明之天線模組之第十一實施例之立體示意圖。 圖21係為本發明之天線模組之第十二實施例之立體示意圖。 圖22係為本發明之天線模組之第十三實施例之立體示意圖。 圖23係為本發明之第一比較例之天線模組之立體示意圖。 圖24係為本發明之第二比較例之天線模組之立體示意圖。 圖25係為本發明之第三比較例之天線模組之立體示意圖。 圖26係為本發明之第一比較例至第三比較例之天線模組之回波損耗(return loss)的實驗數據圖。 圖27係為本發明之天線模組之第一實施例及第二實施例之回波損耗的實驗數據圖。 FIG. 1 is a three-dimensional schematic diagram of the first embodiment of the antenna module of the present invention. FIG. 2 is a three-dimensional schematic diagram of the first embodiment of the inductor circuit of the present invention. FIG. 3 is a three-dimensional schematic diagram of the second embodiment of the antenna module of the present invention. FIG. 4 is a side view schematic diagram of the first embodiment of the inductor circuit of the present invention. FIG. 5 is a three-dimensional schematic diagram of the second embodiment of the inductor circuit of the present invention. FIG. 6 is a three-dimensional schematic diagram of the third embodiment of the inductor circuit of the present invention. FIG. 7 is a three-dimensional schematic diagram of the fourth embodiment of the inductor circuit of the present invention. FIG. 8 is a three-dimensional schematic diagram of the fifth embodiment of the inductor circuit of the present invention. FIG. 9 is a three-dimensional schematic diagram of the sixth embodiment of the inductor circuit of the present invention. FIG. 10 is a three-dimensional schematic diagram of the seventh embodiment of the inductor circuit of the present invention. FIG. 11 is a side cross-sectional schematic diagram of the seventh embodiment of the inductor circuit of the present invention. FIG. 12 is a three-dimensional schematic diagram of the third embodiment of the antenna module of the present invention. FIG. 13 is a three-dimensional schematic diagram of the fourth embodiment of the antenna module of the present invention. FIG. 14 is a three-dimensional schematic diagram of the fifth embodiment of the antenna module of the present invention. FIG. 15 is a three-dimensional schematic diagram of the sixth embodiment of the antenna module of the present invention. FIG. 16 is a three-dimensional schematic diagram of the seventh embodiment of the antenna module of the present invention. FIG. 17 is a three-dimensional schematic diagram of the eighth embodiment of the antenna module of the present invention. FIG. 18 is a three-dimensional schematic diagram of the ninth embodiment of the antenna module of the present invention. FIG. 19 is a three-dimensional schematic diagram of the tenth embodiment of the antenna module of the present invention. FIG. 20 is a three-dimensional schematic diagram of the eleventh embodiment of the antenna module of the present invention. FIG. 21 is a three-dimensional schematic diagram of the twelfth embodiment of the antenna module of the present invention. FIG. 22 is a three-dimensional schematic diagram of the thirteenth embodiment of the antenna module of the present invention. FIG. 23 is a three-dimensional schematic diagram of the antenna module of the first comparative example of the present invention. FIG. 24 is a three-dimensional schematic diagram of the antenna module of the second comparative example of the present invention. FIG. 25 is a three-dimensional schematic diagram of the antenna module of the third comparative example of the present invention. FIG. 26 is an experimental data diagram of return loss of the antenna modules of the first to third comparative examples of the present invention. Figure 27 is an experimental data diagram of the echo loss of the first embodiment and the second embodiment of the antenna module of the present invention.

10:天線模組 10: Antenna module

20:接地部 20: Grounding part

21:短路端 21: Short circuit end

30:第一輻射段 30: The first radiation segment

31:第一耦合區段 31: First coupling section

40:第二輻射段 40: Second radiation segment

41:第二耦合區段 41: Second coupling section

50:電感電路 50: Inductor circuit

E1:第一端 E1: First end

E2:第二端 E2: Second end

E3:第三端 E3: The third end

E4:第四端 E4: The fourth end

60:基板 60: Substrate

FD:饋入源 FD: Feed source

CG1:第一耦合間隙 CG1: First coupling gap

Claims (10)

一種天線模組,包含:一接地部;一第一輻射段,包括一第一耦合區段;一第二輻射段,包括一第二耦合區段,該第一耦合區段與該第二耦合區段相鄰且間隔一第一耦合間隙;及一電感電路,包含一第一電感單元及一第二電感單元,該第一電感單元提供介於該第一輻射段及一饋入源之間的一第一電感性路徑,該第二電感單元提供介於該第二輻射段及該接地部之間的一第二電感性路徑,且該第一電感性路徑與該第二電感性路徑相鄰且不相接;其中,該第一電感單元包含具有至少一第一線圈匝的一第一線圈,該第二電感單元包含具有至少一第二線圈匝的一第二線圈,且該至少一第一線圈匝與該至少一第二線圈匝之間具有一匝間距。 An antenna module comprises: a ground portion; a first radiation section including a first coupling section; a second radiation section including a second coupling section, wherein the first coupling section and the second coupling section are adjacent to each other and separated by a first coupling gap; and an inductor circuit comprising a first inductor unit and a second inductor unit, wherein the first inductor unit provides a first inductive path between the first radiation section and a feed source, and the second inductor unit provides a first inductive path between the first radiation section and a feed source. The inductive unit provides a second inductive path between the second radiation section and the grounding portion, and the first inductive path is adjacent to and not connected to the second inductive path; wherein the first inductive unit includes a first coil having at least one first coil turn, the second inductive unit includes a second coil having at least one second coil turn, and there is a turn spacing between the at least one first coil turn and the at least one second coil turn. 如請求項1所述之天線模組,其中,該至少一第一線圈匝及該至少一第二線圈匝彼此交錯排列。 The antenna module as described in claim 1, wherein the at least one first coil turn and the at least one second coil turn are arranged alternately with each other. 如請求項1所述之天線模組,其中,該第一電感單元包含一第一電感性線段,該第二電感單元包含一第二電感性線段,且該第一電感性線段及該第二電感性線段之間具有一線間距。 The antenna module as described in claim 1, wherein the first inductor unit includes a first inductive line segment, the second inductive unit includes a second inductive line segment, and there is a line spacing between the first inductive line segment and the second inductive line segment. 如請求項3所述之天線模組,其中,該第一電感性線段及該第二電感性線段位於同一平面。 The antenna module as described in claim 3, wherein the first inductive line segment and the second inductive line segment are located in the same plane. 如請求項4所述之天線模組,其中,該第一電感性線段及該第二電感性線段呈直線狀且相互平行。 The antenna module as described in claim 4, wherein the first inductive line segment and the second inductive line segment are straight lines and parallel to each other. 如請求項3所述之天線模組,其中,該第一電感性線段及該第二電感性線段分別位於相對的二平面。 The antenna module as described in claim 3, wherein the first inductive line segment and the second inductive line segment are located in two opposite planes. 如請求項6所述之天線模組,其中,該第一電感單元更包含一第一電感器,連接該第一電感性線段,該第二電感單元更包含一第二電感器,連接該第二電感性線段。 The antenna module as described in claim 6, wherein the first inductor unit further includes a first inductor connected to the first inductive line segment, and the second inductor unit further includes a second inductor connected to the second inductive line segment. 如請求項1所述之天線模組,其中,該第一輻射段更包含連接於該第一耦合區段的一第一分支段,該第二輻射段更包含連接於該第二耦合區段的一第二分支段。 The antenna module as described in claim 1, wherein the first radiation section further includes a first branch section connected to the first coupling section, and the second radiation section further includes a second branch section connected to the second coupling section. 如請求項1所述之天線模組,更包含一寄生段,連接該接地部,並與該第一輻射段及該第二輻射段中之至少一者相鄰且間隔一第二耦合間隙。 The antenna module as described in claim 1 further includes a parasitic section connected to the ground portion and adjacent to at least one of the first radiation section and the second radiation section and separated by a second coupling gap. 如請求項1所述之天線模組,其中該接地部具有一短路端,該第二電感性路徑介於該第二輻射段及該短路端之間,且該短路端係為一電感器。 The antenna module as described in claim 1, wherein the ground portion has a short-circuit end, the second inductive path is between the second radiation section and the short-circuit end, and the short-circuit end is an inductor.
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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TW201424118A (en) * 2012-12-13 2014-06-16 Acer Inc Mobile device and control method thereof
TW201810798A (en) * 2016-03-11 2018-03-16 宏碁股份有限公司 Communication device with narrow-ground-clearance antenna element
TW202127727A (en) * 2020-01-09 2021-07-16 廣達電腦股份有限公司 Communication device
CN114824836A (en) * 2019-02-27 2022-07-29 华为技术有限公司 Common antenna and electronic device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TW201424118A (en) * 2012-12-13 2014-06-16 Acer Inc Mobile device and control method thereof
TW201810798A (en) * 2016-03-11 2018-03-16 宏碁股份有限公司 Communication device with narrow-ground-clearance antenna element
CN114824836A (en) * 2019-02-27 2022-07-29 华为技术有限公司 Common antenna and electronic device
TW202127727A (en) * 2020-01-09 2021-07-16 廣達電腦股份有限公司 Communication device

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