TWM676955U - Antenna structure - Google Patents
Antenna structureInfo
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- TWM676955U TWM676955U TW114206093U TW114206093U TWM676955U TW M676955 U TWM676955 U TW M676955U TW 114206093 U TW114206093 U TW 114206093U TW 114206093 U TW114206093 U TW 114206093U TW M676955 U TWM676955 U TW M676955U
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Abstract
Description
本新型創作涉及一種天線結構,特別是一種可縮小體積的天線結構。 This invention relates to an antenna structure, and more particularly to a miniaturized antenna structure.
手機及手錶等通訊產品裝置中存在對鐳射直接成型(Laser Direct structuring,LDS)天線的需求。鐳射直接成型天線一般用於射頻傳輸(Radio Frequency transmission,RF transmission)。 There is a demand for laser direct structuring (LDS) antennas in communication products and devices such as mobile phones and watches. LDS antennas are generally used for radio frequency (RF) transmission.
以圖1和圖2為示例,圖1示出了一種先前技術的天線結構(為方便說明,後文統稱為第一天線結構100)的剖面示意圖,圖2示出了另一種先前技術的天線結構(為方便說明,後文統稱為第二天線結構200)的剖面示意圖。參見圖1,示出了先前技術的第一天線結構100的剖面示意圖。第一天線結構100包括:第一外殼110以及位於第一外殼110上的第一鐳射天線圖案111。第一鐳射天線圖案111通過鐳射直接成型技術形成在第一外殼110的內表面。第一外殼110內部設置有第一天線基板130,以及位於第一天線基板130上方的彈片120。參見圖2,示出了先前技術的第二天線結構200的剖面示意圖。第二天線結構200包括:第二外殼210以及位於第二外殼210上的第二鐳射天線圖案211。第二鐳射天線圖案211通過鐳射直接成型技術形成在第二外殼210的外表面。第二外殼210內部設 置有電路板250,以及位於電路板250上方的第二天線基板240,第二天線基板240上設置有彈針220。位於第二天線基板240上的內部模封層230將彈針220包圍。圖3示出了又一種先前技術的天線結構(為方便說明,後文統稱為第三天線結構300)的三維示意圖。圖3示出了第三天線結構300的第三外殼310上設置的第三鐳射天線圖案311。參見圖1和圖2,一般而言,傳統鐳射直接成型天線結構會將天線圖案(例如第一鐳射天線圖案111和第二鐳射天線圖案211)設計在外殼或中框,使用彈片和彈針(例如圖1和圖2示出的彈片120或彈針220)與天線圖案進行連接以傳遞訊號,然而由於彈片和彈針的尺寸較大而無法實現產品的微小化,並且訊號匯出後會受到彈片和彈針尺寸的局限,進一步阻礙了實現產品的微小化。 Referring to Figures 1 and 2, Figure 1 shows a cross-sectional schematic view of a prior art antenna structure (hereinafter referred to as the first antenna structure 100 for ease of explanation), and Figure 2 shows a cross-sectional schematic view of another prior art antenna structure (hereinafter referred to as the second antenna structure 200 for ease of explanation). Referring to Figure 1, a cross-sectional schematic view of the prior art first antenna structure 100 is shown. The first antenna structure 100 includes: a first housing 110 and a first laser antenna pattern 111 located on the first housing 110. The first laser antenna pattern 111 is formed on the inner surface of the first housing 110 by laser direct forming technology. A first antenna substrate 130 is disposed inside the first housing 110, and a spring clip 120 is located above the first antenna substrate 130. Referring to Figure 2, a cross-sectional schematic diagram of the prior art second antenna structure 200 is shown. The second antenna structure 200 includes a second housing 210 and a second laser antenna pattern 211 located on the second housing 210. The second laser antenna pattern 211 is formed on the outer surface of the second housing 210 by laser direct molding technology. A circuit board 250 is disposed inside the second housing 210, and a second antenna substrate 240 is located above the circuit board 250. A spring pin 220 is disposed on the second antenna substrate 240. An internal molding layer 230 on the second antenna substrate 240 surrounds the spring pin 220. Figure 3 shows a three-dimensional schematic diagram of yet another prior art antenna structure (hereinafter referred to as the third antenna structure 300 for ease of explanation). Figure 3 shows a third laser antenna pattern 311 disposed on the third housing 310 of the third antenna structure 300. Referring to Figures 1 and 2, conventional laser-direct molding antenna structures typically design antenna patterns (e.g., first laser antenna pattern 111 and second laser antenna pattern 211) on the housing or mid-frame, using springs and pins (e.g., spring 120 or pin 220 shown in Figures 1 and 2) to connect to the antenna patterns for signal transmission. However, due to the large size of the springs and pins, miniaturization of the product is not possible, and the signal transmission is limited by the size of the springs and pins, further hindering product miniaturization.
針對以上問題,本新型創作提出一種天線結構,以至少利用第一天線圖案和第二天線圖案之間的耦合傳輸訊號,縮小天線結構的體積。 To address the above problems, this invention proposes an antenna structure that utilizes at least the coupling between the first and second antenna patterns to transmit signals, thereby reducing the size of the antenna structure.
本新型創作的技術手段是這樣實現的,根據本新型創作的一個實施例,提供了一種天線結構,包括:一內封裝體,包括一鐳射直接成型層以及設置在該鐳射直接成型層上的一第一天線圖案,該第一天線圖案具有一第一環狀耦合部;一外殼,覆蓋於該內封裝體上,包括一第二天線圖案,該第二天線圖案具有一第二環狀耦合部,該第一環狀耦合部在垂直方向上重疊該第二環狀耦合部。 The technical means of this invention are implemented as follows: According to one embodiment of this invention, an antenna structure is provided, comprising: an inner package including a laser direct molding layer and a first antenna pattern disposed on the laser direct molding layer, the first antenna pattern having a first annular coupling portion; and an outer shell covering the inner package, including a second antenna pattern, the second antenna pattern having a second annular coupling portion, the first annular coupling portion overlapping the second annular coupling portion in the vertical direction.
在一些實施例中,該內封裝體包括一模封層,該模封層凹陷定義出一凹部。 In some embodiments, the inner package includes a molded sealing layer that recesses to define a recess.
在一些實施例中,該第一天線圖案設置在該凹部,並且延伸至該模封層的頂面的上方。 In some embodiments, the antenna pattern is positioned within the recess and extends above the top surface of the molding layer.
在一些實施例中,該第一環狀耦合部設置在該凹部之外。 In some embodiments, the first annular coupling portion is disposed outside the recess.
在一些實施例中,在俯視時,該第一環狀耦合部的面積調控該天線結構的阻抗。 In some embodiments, the area of the first annular coupling portion, when viewed from above, controls the impedance of the antenna structure.
在一些實施例中,該第二天線圖案的面積大於該第一天線圖案的面積。 In some embodiments, the area of the second line pattern is larger than the area of the first line pattern.
在一些實施例中,該外殼將該內封裝體包裹在內。 In some embodiments, the outer shell encloses the inner package.
在一些實施例中,該外殼與該內封裝體定義出一間隙,並且該外殼與該內封裝體被該間隙間隔開。 In some embodiments, a gap is defined between the outer casing and the inner package, and the outer casing and the inner package are separated by the gap.
在一些實施例中,該第二天線圖案設置於該外殼朝向該內封裝體的內表面。 In some embodiments, the second antenna pattern is disposed on the inner surface of the housing facing the inner package.
在一些實施例中,該內封裝體還包括一基板,該基板承載該模封層。 In some embodiments, the inner package further includes a substrate that supports the molding layer.
在一些實施例中,該鐳射直接成型層設置於該模封層上。 In some embodiments, the laser direct molding layer is disposed on the mold sealing layer.
在一些實施例中,天線結構還包括一印刷電路板,該印刷電路板承載該內封裝體並且設置於該外殼內。 In some embodiments, the antenna structure also includes a printed circuit board that carries the inner package and is disposed within the housing.
在一些實施例中,該鐳射直接成型層限定一腔體,該腔體延伸進入該凹部中。 In some embodiments, the laser-formed layer defines a cavity that extends into the recess.
在一些實施例中,該第一天線圖案自該腔體內延伸至該鐳射直接成型層朝向該第二天線圖案的上表面。 In some embodiments, the first antenna pattern extends from within the cavity to the upper surface of the laser-formed layer facing the second antenna pattern.
在一些實施例中,天線結構還包括複數個阻抗匹配元件,該些阻抗匹配元件設置在位於該腔體內的第一天線圖案上。 In some embodiments, the antenna structure also includes a plurality of impedance matching elements disposed on the first antenna pattern located within the cavity.
在一些實施例中,該間隙中填充有空氣。 In some embodiments, the gap is filled with air.
在一些實施例中,在俯視視角,該第一環狀耦合部所環繞的區域大小和該第二環狀耦合部所環繞的區域大小調控該天線結構的電感大小。 In some embodiments, from a top-down view, the size of the area enclosed by the first annular coupling portion and the size of the area enclosed by the second annular coupling portion control the inductance of the antenna structure.
在一些實施例中,在該第一天線圖案在該鐳射直接成型層上的延伸面處,該第一天線圖案在垂直於該第一天線圖案的延伸方向上具有第一寬度,以及在該第二天線圖案在該外殼上的延伸面處,該第二天線圖案在垂直於該第二天線圖案的延伸方向上具有第二寬度,其中,該第一寬度和該第二寬度調控該天線結構的電容大小。 In some embodiments, at the extension surface of the first antenna pattern on the laser-formed layer, the first antenna pattern has a first width in a direction perpendicular to its extension, and at the extension surface of the second antenna pattern on the housing, the second antenna pattern has a second width in a direction perpendicular to its extension, wherein the first width and the second width control the capacitance of the antenna structure.
在一些實施例中,該第一寬度與該第二寬度相同或不同。 In some embodiments, the first width may be the same as or different from the second width.
本新型創作的另一些實施例提供了一種天線結構,包括:一內封裝體,包括一鐳射直接成型層以及設置在該鐳射直接成型層上的一第一天線圖案,該第一天線圖案具有一第一環狀耦合部;一外殼,覆蓋於該內封裝體上,包括一第二天線圖案,該第二天線圖案具有一第二環狀耦合部,該第一環狀耦合部與該第二環狀耦合部彼此耦合並被該外殼包圍。 Other embodiments of this invention provide an antenna structure comprising: an inner package including a laser direct molding layer and a first antenna pattern disposed on the laser direct molding layer, the first antenna pattern having a first annular coupling portion; and an outer shell covering the inner package, including a second antenna pattern having a second annular coupling portion, the first annular coupling portion and the second annular coupling portion being coupled to each other and surrounded by the outer shell.
藉由本新型創作的上述技術手段,至少利用第一天線圖案和第二天線圖案之間的耦合傳輸訊號,縮小天線結構的體積。 By employing the aforementioned technical means of this novel invention, the size of the antenna structure is reduced by at least utilizing the coupling signal transmission between the first and second antenna patterns.
100:第一天線結構 100: First Skyline Structure
110:第一外殼 110: First outer shell
111:第一鐳射天線圖案 111: First Laser Antenna Pattern
120:彈片 120: Shrapnel
130:第一天線基板 130: First antenna substrate
200:第二天線結構 200: Second Linear Structure
210:第二外殼 210: Second outer shell
211:第二鐳射天線圖案 211: Second Radar Antenna Pattern
220:彈針 220: Spear
230:內部模封層 230: Internal mold sealing layer
240:第二天線基板 240: Second antenna substrate
250:電路板 250: Circuit Board
300:第三天線結構 300: Third antenna structure
310:第三外殼 310: Third outer shell
311:第三鐳射天線圖案 311: Third Radar Antenna Pattern
400:天線結構 400: Antenna Structure
401:內封裝體 401: Inner Package
410:鐳射直接成型層 410: Laser Direct Molding Layer
411:第一天線圖案 411: First Line Pattern
412:第一環狀耦合部 412: First annular coupling section
413:腔體 413: Cavity
420:外殼 420: Shell
421:第二天線圖案 421: Second Line Pattern
422:第二環狀耦合部 422: Second annular coupling section
430:印刷電路板 430: Printed Circuit Board
440:模封層 440: Mold Encapsulation
441:凹部 441: concave part
450:基板 450:Substrate
451:焊盤 451: Solder pad
452:焊料凸塊 452: Solder bump
453:電子元件 453: Electronic Components
454:天線底座 454: Antenna Base
456:外部連接件 456: External Connectors
460:間隙 460: Gap
470:阻抗匹配元件 470: Impedance matching element
801-814:步驟 801-814: Steps
901-919:步驟 901-919: Steps
1000:工藝流程 1000: Process Flow
A:區域 A: Region
為了更清楚地說明本新型創作實施例或現有技術中的技術手段,下面將對實施例中所需要使用的圖式作簡單地介紹,顯而易見地,下面描述中 的圖式僅僅是本新型創作的一些實施例,對於本領域通常知識者而言,在不付出創造性勞動的前提下,還可以根據這些圖式獲得其他的圖式。 To more clearly illustrate the technical means in the embodiments of this invention or the prior art, the drawings used in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this invention. For those skilled in the art, other drawings can be obtained from these drawings without any creative effort.
圖1示出了一種先前技術的天線結構的剖面示意圖。 Figure 1 shows a schematic cross-sectional view of a prior art antenna structure.
圖2示出了另一種先前技術的天線結構的剖面示意圖。 Figure 2 shows a cross-sectional schematic diagram of another prior art antenna structure.
圖3示出了又一種先前技術的天線結構的三維示意圖。 Figure 3 shows a three-dimensional schematic diagram of another prior art antenna structure.
圖4示出了根據本新型創作一些實施例的天線結構的剖面示意圖。 Figure 4 shows a schematic cross-sectional view of an antenna structure according to some embodiments of the present invention.
圖5示出了圖4中A區域的放大示意圖。 Figure 5 shows a magnified schematic diagram of region A in Figure 4.
圖6A示出了根據本新型創作的一些實施例的天線結構的剖面示意圖。 Figure 6A shows a schematic cross-sectional view of an antenna structure according to some embodiments of the present invention.
圖6B示出了根據本新型創作的一些實施例的天線結構的剖面示意圖。 Figure 6B shows a schematic cross-sectional view of an antenna structure according to some embodiments of the present invention.
圖7是本新型創作實施例的天線結構的S-參數曲線圖。 Figure 7 is an S-parameter curve of the antenna structure of this novel embodiment.
圖8示出了根據本新型創作一些實施例的工藝流程。 Figure 8 illustrates the process flow of some embodiments according to this invention.
圖8A至8E示出了流程示意圖。 Figures 8A to 8E show schematic flowcharts.
圖9示出了根據本新型創作另一些實施例的工藝流程。 Figure 9 illustrates the process flow of some other embodiments according to this invention.
圖9A至9F示出了流程示意圖。 Figures 9A to 9F show schematic flowcharts.
下面將結合本新型創作實施例中的圖式,對本新型創作實施例中的技術手段進行清楚、完整地描述,顯然,所描述的實施例僅僅是本新型創作一部分實施例,而不是全部的實施例。基於本新型創作中的實施例,本領域通常知識者所獲得的所有其他實施例,都屬於本新型創作的申請專利範圍之內。 The technical means of this invention will be clearly and completely described below with reference to the drawings in the embodiments of this invention. Obviously, the described embodiments are only a part of the embodiments of this invention, not all of them. All other embodiments obtained by those skilled in the art based on the embodiments of this invention fall within the scope of the patent application for this invention.
下列公開提供了許多用於實現所提供主題的不同特徵的不同實施例或實例。下面將描述元件和佈置的特定實例以簡化本新型創作。當然這些僅僅是實例並不旨在限定本新型創作。例如,在以下描述中,在第二部件上方或上形成第一部件可以包括第一部件和第二部件直接接觸的實施例,也可以包括在第一部件和第二部件之間形成額外的部件使得第一部件和第二部件可以不直接接觸的實施例。而且,本新型創作在各個實例中可重複參考數字和/或字母。這種重複僅是為了簡明和清楚,其自身並不表示所論述的各個實施例和/或配置之間的關係。 The following disclosure provides numerous embodiments or examples for implementing different features of the provided subject matter. Specific examples of elements and arrangements will be described below to simplify the invention. These are merely examples and are not intended to limit the invention. For example, in the following description, forming a first component above or on a second component may include embodiments where the first and second components are in direct contact, or embodiments where an additional component is formed between the first and second components such that the first and second components are not in direct contact. Furthermore, references to numbers and/or letters may be repeated in various embodiments. This repetition is for simplicity and clarity only and does not in itself indicate a relationship between the various embodiments and/or configurations discussed.
另外,在不衝突的情況下,本新型創作中的實施例及實施例中的特徵可以相互組合。下面將參考圖式並結合實施例來詳細說明本新型創作。 Furthermore, without conflict, the embodiments and features of this invention can be combined with each other. The invention will now be described in detail with reference to the drawings and embodiments.
圖4示出了根據本新型創作一些實施例的天線結構400的剖面示意圖。圖5示出了圖4中A區域的放大示意圖。參見圖4和圖5,本新型創作的實施例提供一種天線結構400,該天線結構400包括:一內封裝體401,包括一鐳射直接成型層410以及設置在該鐳射直接成型層410上的一第一天線圖案411,該第一天線圖案411具有一第一環狀耦合部412;一外殼420,覆蓋於該內封裝體401上,包括一第二天線圖案421,該第二天線圖案421具有一第二環狀耦合部422,該第一環狀耦合部412在垂直方向上重疊該第二環狀耦合部422。可以理解,第一天線圖案411可以是鐳射直接成型於鐳射直接成型層410上的圖案;相應地,第二天線圖案421也可以是鐳射直接成型於外殼420上的圖案。本新型創作的天線結構400通過將設置於外殼420內部的第一天線圖案411與位於外殼420上的第二天線圖案421耦合,使得天線圖案的輻射特性與電性表現可以不受封裝尺寸的限制,至少利用了第一天線圖案411和第二天線圖案421之間的耦合傳輸訊號,縮 小了天線結構400的體積。通過設置第一環狀耦合部412在垂直方向上重疊該第二環狀耦合部422使得輻射能量得以上下耦合。並且因此得以方便地控制天線結構400的阻抗,將在之後詳細敘述。 Figure 4 shows a cross-sectional schematic view of an antenna structure 400 according to some embodiments of the present invention. Figure 5 shows an enlarged schematic view of region A in Figure 4. Referring to Figures 4 and 5, embodiments of the present invention provide an antenna structure 400 comprising: an inner package 401 including a laser direct molding layer 410 and a first antenna pattern 411 disposed on the laser direct molding layer 410, the first antenna pattern 411 having a first annular coupling portion 412; and an outer shell 420 covering the inner package 401, including a second antenna pattern 421, the second antenna pattern 421 having a second annular coupling portion 422, the first annular coupling portion 412 overlapping the second annular coupling portion 422 in the vertical direction. It is understood that the first antenna pattern 411 can be a pattern laser-formed directly onto the laser-formed layer 410; correspondingly, the second antenna pattern 421 can also be a pattern laser-formed directly onto the housing 420. The antenna structure 400 of this invention couples the first antenna pattern 411 disposed inside the housing 420 with the second antenna pattern 421 located on the housing 420, allowing the radiation characteristics and electrical performance of the antenna patterns to be unrestricted by the package size. This reduces the volume of the antenna structure 400 by utilizing the coupling between the first antenna pattern 411 and the second antenna pattern 421 to transmit signals. By providing a first annular coupling portion 412 that overlaps the second annular coupling portion 422 in the vertical direction, radiated energy can be coupled vertically. This allows for convenient control of the impedance of the antenna structure 400, which will be described in detail later.
繼續參見圖4和圖5,外殼420可以將該內封裝體401包裹在內,為方便理解,在圖4中以虛線例示出了外殼420的內輪廓。實際上,第二天線圖案421可以設置在外殼420朝向內封裝體401的內表面上,當然,也可以設置在外殼420遠離內封裝體401的外表面上。在一些實施例中,該內封裝體401包括一模封層440,該模封層440凹陷定義出一凹部441。可以理解,該凹部441容納位於該模封層440上方的鐳射直接成型層410的一部分。第一天線圖案411可以設置在該凹部441,並且可以進一步從該凹部441中延伸至模封層440的頂面的上方。並且,第一環狀耦合部412可以設置在該凹部441之外。如前所述的,由於第一環狀耦合部412和第二環狀耦合部422彼此重疊並且均構造為環狀結構,可以通過改變在俯視時第一環狀耦合部412的面積來調控該天線結構400的阻抗,並且,也可以通過改變在俯視時第二環狀耦合部422的面積來調控該天線結構400的阻抗。在一些實施例中,在俯視視角,該第一環狀耦合部412所環繞的區域大小和該第二環狀耦合部422所環繞的區域大小可以調控該天線結構400的電感大小;並且在該第一天線圖案411在該鐳射直接成型層410上的延伸面處,該第一天線圖案411在垂直於該第一天線圖案411的延伸方向上具有第一寬度,以及在該第二天線圖案421在該外殼420上的延伸面處,該第二天線圖案421在垂直於該第二天線圖案421的延伸方向上具有第二寬度,其中,該第一寬度和該第二寬度可以調控該天線結構400的電容大小。該第一寬度與該第二寬度可以相同或不同。在一些實施例中,該第二天線圖案421的面積大於該第一天線圖案411的面積。該外殼 420可以與該內封裝體401定義出一間隙460,並且該外殼420與該內封裝體401被該間隙460間隔開。該間隙460中可以填充有空氣,用以充當第一天線圖案411與第二天線圖案421之間的訊號傳輸的介質。內封裝體401還可以包括一基板(Substrate)450,該基板450承載該模封層440。鐳射直接成型層410可以設置於模封層440上。並且如前述,鐳射直接成型層410的一部分進入模封層440的凹部441。在一些實施例中,天線結構400還包括一印刷電路板430(Printed Circuit Board),該印刷電路板430承載該內封裝體401並且設置於該外殼420內。該鐳射直接成型層410可以限定一腔體413,該腔體413延伸進入該凹部441中。該第一天線圖案411可以自該腔體413內延伸至該鐳射直接成型層410朝向該第二天線圖案421的上表面。天線結構400還可以包括複數個阻抗匹配元件470,該些阻抗匹配元件470設置在位於該腔體413內的第一天線圖案411上。 Referring again to Figures 4 and 5, the outer casing 420 can enclose the inner package 401. For clarity, the inner contour of the outer casing 420 is illustrated with dashed lines in Figure 4. In practice, the second antenna pattern 421 can be disposed on the inner surface of the outer casing 420 facing the inner package 401, or on the outer surface of the outer casing 420 away from the inner package 401. In some embodiments, the inner package 401 includes a molding seal 440 that recesses to define a recess 441. It is understood that the recess 441 accommodates a portion of the laser direct-forming layer 410 located above the molding seal 440. The first antenna pattern 411 can be disposed in the recess 441 and can further extend from the recess 441 to above the top surface of the molding layer 440. Furthermore, the first annular coupling portion 412 can be disposed outside the recess 441. As previously described, since the first annular coupling portion 412 and the second annular coupling portion 422 overlap each other and are both constructed as annular structures, the impedance of the antenna structure 400 can be adjusted by changing the area of the first annular coupling portion 412 in a top view, and the impedance of the antenna structure 400 can also be adjusted by changing the area of the second annular coupling portion 422 in a top view. In some embodiments, from a top-down view, the size of the area enclosed by the first annular coupling portion 412 and the size of the area enclosed by the second annular coupling portion 422 can adjust the inductance of the antenna structure 400; and at the extension surface of the first antenna pattern 411 on the laser direct molding layer 410, the first antenna pattern 411 has a first width perpendicular to the extension direction of the first antenna pattern 411, and at the extension surface of the second antenna pattern 421 on the housing 420, the second antenna pattern 421 has a second width perpendicular to the extension direction of the second antenna pattern 421, wherein the first width and the second width can adjust the capacitance of the antenna structure 400. The first width and the second width can be the same or different. In some embodiments, the area of the second antenna pattern 421 is larger than the area of the first antenna pattern 411. The housing 420 may define a gap 460 with the inner package 401, and the housing 420 and the inner package 401 are separated by the gap 460. The gap 460 may be filled with air to serve as a medium for signal transmission between the first antenna pattern 411 and the second antenna pattern 421. The inner package 401 may also include a substrate 450 that supports the molding layer 440. A laser direct molding layer 410 may be disposed on the molding layer 440. And as mentioned above, a portion of the laser direct molding layer 410 extends into a recess 441 of the molding layer 440. In some embodiments, the antenna structure 400 further includes a printed circuit board 430 that carries the inner package 401 and is disposed within the housing 420. The laser-formed layer 410 may define a cavity 413 extending into the recess 441. The first antenna pattern 411 may extend from within the cavity 413 to the upper surface of the laser-formed layer 410 facing the second antenna pattern 421. The antenna structure 400 may also include a plurality of impedance matching elements 470 disposed on the first antenna pattern 411 located within the cavity 413.
本新型創作還提供一種天線結構400,可以參見圖4和圖5來理解。天線結構400包括:一內封裝體401,包括一鐳射直接成型層410以及設置在該鐳射直接成型層410上的一第一天線圖案411,該第一天線圖案411具有一第一環狀耦合部412;一外殼420,覆蓋於該內封裝體401上,包括一第二天線圖案421,該第二天線圖案421具有一第二環狀耦合部422,該第一環狀耦合部412與該第二環狀耦合部422彼此耦合並被該外殼420包圍。 This invention also provides an antenna structure 400, which can be understood with reference to Figures 4 and 5. The antenna structure 400 includes: an inner package 401, including a laser direct molding layer 410 and a first antenna pattern 411 disposed on the laser direct molding layer 410, the first antenna pattern 411 having a first annular coupling portion 412; and an outer shell 420, covering the inner package 401, including a second antenna pattern 421, the second antenna pattern 421 having a second annular coupling portion 422, the first annular coupling portion 412 and the second annular coupling portion 422 being coupled to each other and surrounded by the outer shell 420.
圖6A示出了根據本新型創作的一些實施例的天線結構400的剖面示意圖。鐳射直接成型層410可以覆蓋在模封層440的上表面和側面上。第二天線圖案421與第一天線圖案411的寬度也可以不一致。 Figure 6A shows a schematic cross-sectional view of an antenna structure 400 according to some embodiments of the present invention. A laser-formed layer 410 may cover the upper surface and side surfaces of the molding layer 440. The widths of the second antenna pattern 421 and the first antenna pattern 411 may also be different.
圖6B示出了根據本新型創作的一些實施例的天線結構400的剖面示意圖。在一些實施例中,模封層440也可以將鐳射直接成型層410上的第一天 線圖案411覆蓋。實際上,根據本新型創作的一些實施例的天線結構400作為耦合天線(coupling antenna)結構,無論是圖6A示出的第一天線圖案411相比於模封層440暴露,亦或是圖6B所示出的第一天線圖案411被模封層440覆蓋,都不影響設計。參見圖4、圖5以及圖6A。在一些實施例中,印刷電路板430的尺寸為40x40x1mm,即為長40mm,寬40mm,厚度1mm,內封裝體401的封裝尺寸(Package size)為7x7x1mm,即為長40mm,寬40mm,厚度1mm。在一些實施例中,基板450的材料為高介電常數材料(High-k dielectric materials),並且在2.4GHz頻率下,材料的介電常數為6.5,在2.5GHz頻率下,材料的損耗因子為0.002。在一些實施例中,模封層440的材料為高介電常數材料,並且在2.4GHz頻率下,材料的介電常數為6.5,在2.5GHz頻率下,材料的損耗因子為0.002。在一些實施例中,天線結構400的天線效率(Ant Eff)為25%@2.45GHz,也即是在2.45GHz頻率下,輻射效率為25%;天線結構400的峰值增益(Peak Gain)為-2.2dBi@2.45GHz,也即是在2.45GHz頻率下,峰值增益可以達到-2.2dBi。 Figure 6B shows a cross-sectional schematic view of an antenna structure 400 according to some embodiments of the present invention. In some embodiments, the molding layer 440 may also cover the first antenna pattern 411 on the laser direct molding layer 410. In fact, the antenna structure 400 according to some embodiments of the present invention is a coupling antenna structure, and it does not affect the design whether the first antenna pattern 411 shown in Figure 6A is exposed relative to the molding layer 440 or whether the first antenna pattern 411 shown in Figure 6B is covered by the molding layer 440. See Figures 4, 5 and 6A. In some embodiments, the printed circuit board 430 has dimensions of 40x40x1mm (length 40mm, width 40mm, thickness 1mm), and the inner package 401 has package dimensions of 7x7x1mm (length 40mm, width 40mm, thickness 1mm). In some embodiments, the substrate 450 is made of high-k dielectric materials, with a dielectric constant of 6.5 at 2.4GHz and a loss factor of 0.002 at 2.5GHz. In some embodiments, the molding layer 440 is made of high-k dielectric materials, with a dielectric constant of 6.5 at 2.4GHz and a loss factor of 0.002 at 2.5GHz. In some embodiments, the antenna structure 400 has an antenna efficiency of 25% at 2.45 GHz, meaning it has a radiative efficiency of 25% at 2.45 GHz; and a peak gain of -2.2 dBi at 2.45 GHz, meaning it achieves a peak gain of -2.2 dBi at 2.45 GHz.
圖7是本新型創作實施例的天線結構400的S-參數曲線圖。其中橫坐標為頻率,縱坐標為天線增益,當天線結構400的天線增益小於例如-10dB時,天線增益即可得到改善。 Figure 7 is an S-parameter curve of the antenna structure 400 of this novel embodiment. The horizontal axis represents frequency, and the vertical axis represents antenna gain. When the antenna gain of the antenna structure 400 is less than, for example, -10 dB, the antenna gain can be improved.
圖8示出了根據本新型創作一些實施例的工藝流程1000。並且可以參照圖8A,圖8B,圖8C,圖8D以及圖8E示出的流程示意圖來理解,圖8A至8E中示出的結構旨在理解本新型創作的工藝流程1000。具體地,參見圖8和圖8A,在步驟801中,引入基板450(或框架),該基板450上可以設置形成有焊盤451。在步驟802中,在基板450上印刷焊料,從而形成焊料凸塊452。在步驟803中,通過表面貼裝技術(SMT)將諸如被動元件的電子元件453通過焊料凸塊452安裝 在基板450上。在步驟804中,參見圖8B,將天線底座454(可以理解為天線底座454包括有第一天線圖案411的鐳射直接成型層410,例如參見圖6A示出了有第一天線圖案411的鐳射直接成型層410)通過表面貼裝技術安裝至基板450,連接至基板450上的焊盤451。在步驟805中,對圖8B所示的結構進行回流。在回流之後,進行步驟806中的焊劑清潔,採用本領域常用的方法。在步驟807中,通過引線接合(WB)形成打線。在步驟808中,參見圖8C,通過模製工藝形成模封層440,之後,進行步驟809中的研磨。在步驟810中,通過激光標記的鑽孔工藝在基板450下方形成相應的開孔。在步驟811中,在相應的開孔中通過焊球接合放置(SBBP)工藝形成外部連接件456,如圖8D所示。之後,如圖8E所示,在步驟812中,通過鋸切工藝對所形成的結構進行鋸切G。進一步,可以再將所形成的結構裝配在形成有第二天線圖案421的外殼420內,從而形成相應的天線結構400(參見例如圖4、圖5以及圖6A中所示出的有第二天線圖案421的外殼420,以及天線結構400)。在步驟813中,通近最終外觀目驗(Final Visual Inspection,FVI)測試所形成的天線結構400(參見例如圖4、圖5以及圖6A中所示出的天線結構400)。最後,在步驟814中,通過裝載、運輸(Shipping)工藝來對所得的天線結構400(參見例如圖4、圖5以及圖6A中所示出的天線結構400)進行進一步使用。 Figure 8 illustrates a process flow 1000 according to some embodiments of the present invention. The process flow diagrams shown in Figures 8A, 8B, 8C, 8D, and 8E are provided for understanding the structure of the process flow 1000 of the present invention. Specifically, referring to Figures 8 and 8A, in step 801, a substrate 450 (or frame) is introduced, on which solder pads 451 may be formed. In step 802, solder is printed on the substrate 450, thereby forming solder bumps 452. In step 803, electronic components 453, such as passive components, are mounted on the substrate 450 via the solder bumps 452 using surface mount technology (SMT). In step 804, referring to FIG. 8B, the antenna base 454 (which can be understood as including a laser direct-formed layer 410 with a first antenna pattern 411, for example, as shown in FIG. 6A) is mounted to the substrate 450 using surface mount technology and connected to the solder pads 451 on the substrate 450. In step 805, the structure shown in FIG. 8B is reflowed. After reflow, flux cleaning in step 806 is performed using methods commonly used in the art. In step 807, wire bonding is formed by wire bonding (WB). In step 808, referring to FIG. 8C, a molding seal layer 440 is formed by a molding process, followed by grinding in step 809. In step 810, corresponding openings are formed under the substrate 450 using a laser-marked drilling process. In step 811, external connectors 456 are formed in the corresponding openings using a solder ball bonding placement (SBBP) process, as shown in FIG8D. Subsequently, as shown in FIG8E, in step 812, the formed structure is sawed G using a sawing process. Furthermore, the formed structure can be assembled into a housing 420 having a second antenna pattern 421, thereby forming a corresponding antenna structure 400 (see, for example, the housing 420 with the second antenna pattern 421 and the antenna structure 400 shown in FIG4, 5, and 6A). In step 813, the antenna structure 400 formed by the near-Final Visual Inspection (FVI) test is examined (see, for example, the antenna structure 400 shown in Figures 4, 5, and 6A). Finally, in step 814, the resulting antenna structure 400 (see, for example, the antenna structure 400 shown in Figures 4, 5, and 6A) is further used through a loading and transport process.
圖9示出了根據本新型創作另一些實施例的工藝流程1000。並且可以參照圖9A,圖9B,圖9C,圖9D,圖9E以及圖9F示出的流程示意圖來理解,圖9A至圖9F中示出的結構旨在理解本新型創作的工藝流程1000。具體地,參見圖9和圖9A,在步驟901中,引入基板450,該基板450上形成有焊盤451。在步驟902中,在基板450上印刷焊料,從而形成焊料凸塊452。在步驟903中,通過表面貼 裝技術將諸如被動元件的電子元件453通過焊料凸塊452安裝在基板450上。在步驟904中,對圖9A所示的結構進行回流。在步驟905中,對回流後的結構進行焊劑清潔(對整條半成品)。在步驟906中,參見圖9B,引入天線底座454(可以理解為天線底座454包括有第一天線圖案411的鐳射直接成型層410,例如參見圖6A示出了有第一天線圖案411的鐳射直接成型層410)。在步驟907中,將圖9A所示的結構通過表面貼裝技術翻轉安裝至天線底座454(即,整條上件)。之後,在步驟908以及步驟909中,對以上所得的結構進行回流和焊劑清潔。在步驟910中,通過引線接合(WB)形成打線。在步驟911中,參見圖9B,通過模製工藝形成模封層440(在該實施例中,含有第一天線圖案411的天線底座454用作下模,可以理解為天線底座454包括有第一天線圖案411的鐳射直接成型層410,例如參見圖6A示出了有第一天線圖案411的鐳射直接成型層410),之後,在步驟912中,進行產品材料控制(PMC)。在步驟913中,通過帶研磨工藝去除部分模封層440,直至形成期望厚度的模封層440,如圖9C所示。接下來,參見圖9D以及在步驟914和步驟915中,分別通過激光燒蝕工藝和激光掩蔽工藝在模封層440中形成開口。之後,參見圖9E並且在步驟916中,通過焊球接合放置(SBBP)工藝在開口中形成外部連接件456(諸如焊料球,在本實施例中,為後植球工藝)。之後,在步驟917中,通過鋸切工藝對圖9E所形成的結構進行鋸切G,從而形成圖9F所示的結構。進一步,可以再將所形成的結構裝配在形成有第二天線圖案421的外殼420內,從而形成相應的天線結構400(參見例如圖4、圖5以及圖6A中所示出的有第二天線圖案421的外殼420,以及天線結構400)。在步驟918中,最終外觀目驗(Final Visual Inspection,FVI)測試所形成的天線結構400(參見例如圖4、 圖5以及圖6A中所示出的天線結構400)。最後,在步驟919中,通過裝載、運輸(Shipping)工藝來對所得的結構進行進一步使用。 Figure 9 illustrates a process flow 1000 according to some other embodiments of the present invention. The process flow diagrams shown in Figures 9A, 9B, 9C, 9D, 9E, and 9F are provided for understanding the structure of the present invention's process flow 1000. Specifically, referring to Figures 9 and 9A, in step 901, a substrate 450 is introduced, on which solder pads 451 are formed. In step 902, solder is printed on the substrate 450, thereby forming solder bumps 452. In step 903, electronic components 453, such as passive components, are mounted on the substrate 450 via the solder bumps 452 using surface mount technology. In step 904, the structure shown in Figure 9A is reflowed. In step 905, the reflowed structure is flux-cleaned (for the entire semi-finished product). In step 906, referring to FIG. 9B, the antenna base 454 is introduced (which can be understood as the antenna base 454 including a laser direct-formed layer 410 with the first antenna pattern 411, for example, as shown in FIG. 6A). In step 907, the structure shown in FIG. 9A is flipped and mounted onto the antenna base 454 (i.e., the entire upper part) using surface mount technology. Then, in steps 908 and 909, the structure obtained above is reflowed and flux-cleaned. In step 910, wire bonding is formed by wire bonding (WB). In step 911, referring to FIG. 9B, a molding seal layer 440 is formed by a molding process (in this embodiment, an antenna base 454 containing the first antenna pattern 411 is used as the lower mold; it can be understood that the antenna base 454 includes a laser direct-formed layer 410 with the first antenna pattern 411, for example, a laser direct-formed layer 410 with the first antenna pattern 411 is shown in FIG. 6A). Then, in step 912, product material control (PMC) is performed. In step 913, a portion of the molding seal layer 440 is removed by a grinding process until a molding seal layer 440 of the desired thickness is formed, as shown in FIG. 9C. Next, referring to FIG. 9D and in steps 914 and 915, an opening is formed in the mold sealing layer 440 by laser ablation and laser masking processes, respectively. Then, referring to FIG. 9E and in step 916, an external connector 456 (such as solder balls, in this embodiment, a post-balling process) is formed in the opening by a solder ball bonding placement (SBBP) process. Then, in step 917, the structure formed in FIG. 9E is sawed G by a sawing process to form the structure shown in FIG. 9F. Furthermore, the formed structure can be assembled within a housing 420 having the second antenna pattern 421, thereby forming a corresponding antenna structure 400 (see, for example, the housing 420 with the second antenna pattern 421 and the antenna structure 400 shown in Figures 4, 5, and 6A). In step 918, the formed antenna structure 400 undergoes a final visual inspection (FVI) test (see, for example, the antenna structure 400 shown in Figures 4, 5, and 6A). Finally, in step 919, the obtained structure is further used through a loading and shipping process.
以上所述僅為本新型創作的較佳實施例而已,並不用以限制本新型創作,凡在本新型創作的精神和原則之內,所作的任何修改、等同替換、改進等,均應包含在本新型創作的申請專利範圍之內。 The above description is merely a preferred embodiment of this invention and is not intended to limit the scope of this invention. Any modifications, equivalent substitutions, or improvements made within the spirit and principles of this invention should be included within the scope of the patent application.
410:鐳射直接成型層 410: Laser Direct Molding Layer
411:第一天線圖案 411: First Line Pattern
412:第一環狀耦合部 412: First annular coupling section
413:腔體 413: Cavity
421:第二天線圖案 421: Second Line Pattern
422:第二環狀耦合部 422: Second annular coupling section
440:模封層 440: Mold Encapsulation
441:凹部 441: concave part
450:基板 450:Substrate
470:阻抗匹配元件 470: Impedance matching element
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| TW114206093U TWM676955U (en) | 2025-06-13 | 2025-06-13 | Antenna structure |
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| TW114206093U TWM676955U (en) | 2025-06-13 | 2025-06-13 | Antenna structure |
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