TWI525901B - Dipole antenna structure and antenna device - Google Patents

Dipole antenna structure and antenna device Download PDF

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TWI525901B
TWI525901B TW102101995A TW102101995A TWI525901B TW I525901 B TWI525901 B TW I525901B TW 102101995 A TW102101995 A TW 102101995A TW 102101995 A TW102101995 A TW 102101995A TW I525901 B TWI525901 B TW I525901B
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radiating
radiating portion
predetermined direction
shaped
conductor
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TW201431183A (en
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林丁丙
林哲旭
蘇志銘
鄭大福
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佳邦科技股份有限公司
國立台北科技大學
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偶極天線結構及天線裝置 Dipole antenna structure and antenna device

本發明係有關於一種天線結構及天線裝置,尤指一種圓極化的偶極天線結構及內部安裝有偶極天線結構的天線裝置。 The present invention relates to an antenna structure and an antenna device, and more particularly to a circularly polarized dipole antenna structure and an antenna device having a dipole antenna structure mounted therein.

隨著衛星廣播科技的成熟,傳統廣播電台、類比電視以及多媒體服務已不敷使用,由於衛星廣播系統帶動了高資料量、高品質的影音串流服務,因而受到各界所關注。衛星系統從早期的固定式裝置應用逐漸提升至行動影音多媒體的服務,如何完整接收衛星廣播的訊號,天線在這當中扮演了非常重要的角色。 With the maturity of satellite broadcasting technology, traditional radio stations, analog TVs and multimedia services are no longer available. As satellite broadcasting systems have driven high-volume, high-quality audio and video streaming services, they have received attention from all walks of life. The satellite system has gradually increased from the early fixed device application to the mobile audio and video multimedia service, and how to completely receive the satellite broadcast signal, the antenna plays a very important role in this.

由於現今諸多的應用,天線往往需建置於高導電性物體表面或具有金屬之環境,天線易受到金屬屏蔽的效應而使整體的輻射特性改變而呈現不規則的場型變化。對衛星廣播系統應用上較為普及化的歐美國家而言,一顆衛星通常需要涵蓋幅員廣闊的區域,因此衛星廣播系統會規範在特定的仰角範圍內達到一定的天線增益值,此限制對於放置於高導電性物體上之天線有其設計上的困難度,尤其在距離導電性物體較近的低仰角範圍,若天線未經特殊設計增益值會迅速下降而無法達到衛星廣播系統的規範。 Due to many applications today, antennas often need to be placed on the surface of highly conductive objects or have a metal environment. The antenna is susceptible to the effect of metal shielding and the overall radiation characteristics change to exhibit irregular field variations. For European and American countries where satellite broadcasting systems are more popular, a satellite usually needs to cover a wide area, so the satellite broadcasting system will standardize a certain antenna gain value within a certain elevation angle. Antennas on highly conductive objects have difficulty in design, especially in the low elevation range close to the conductive object. If the antenna is not specially designed, the gain value will drop rapidly and the specification of the satellite broadcasting system cannot be achieved.

然而,由於習知使用的天線(例如微帶天線)結構並不理想,例如習知天線設置在高導電性物體上容易影響原有的天線輻射特性,使得輻射場型不易達到均向性。再者,習知圓極化偶極天線的輻射場型,若未經過特殊的設計通常無法達到高增益寬波束圓極化場型的特性(類均向性的 輻射場型)。此外,習知四臂螺旋天線的輻射場型,雖然具備寬波束圓極化的特性,但此類型架構有高度限制以及整體結構變化性少的缺點,因此在設計上會較缺乏彈性。因此,如何藉由結構的設計,來改善天線例如可建置於大型高導性物體上方特性的問題,已成為該項事業人士所欲解決的重要課題。 However, since the structure of the antenna (for example, a microstrip antenna) used in the prior art is not ideal, for example, the conventional antenna is disposed on a highly conductive object, which easily affects the original antenna radiation characteristics, so that the radiation field type is not easy to achieve the uniformity. Furthermore, the radiation pattern of a conventional circularly polarized dipole antenna cannot be characterized by a high gain and wide beam circular polarization field without special design (average-like Radiation field type). In addition, the radiation field type of the conventional four-arm helical antenna has the characteristics of wide beam circular polarization, but this type of architecture has the disadvantages of high limitation and less structural change, and thus is less flexible in design. Therefore, how to improve the characteristics of an antenna such as a large-scale high-conductivity object by the design of the structure has become an important issue that the business person wants to solve.

本發明實施例在於提供一種偶極天線結構及天線裝置,其能夠基於大型高導電性物體上方的設計,而能夠有效地考量金屬對天線場型特性的影響,並藉由在高導電性物體上方置入圓柱形金屬反射面的結構,以達到調節各仰角輻射場型的平均增益值。 Embodiments of the present invention provide a dipole antenna structure and an antenna device capable of effectively considering the influence of a metal on an antenna field characteristic based on a design above a large high-conductivity object, and by using a highly conductive object The structure of the cylindrical metal reflecting surface is placed to achieve an average gain value for adjusting the radiation pattern of each elevation angle.

本發明其中一實施例提供一種設置在導電性本體上的偶極天線結構,包括反射本體、傳輸線、及天線本體。反射本體具有反射表面。傳輸線穿過且設置在反射本體上,傳輸線包括中心導體、包覆中心導體的絕緣體及包覆絕緣體的外層接地導體,中心導體的兩端分別具有饋入端及第一連接端,外層接地導體具有第二連接端。天線本體包括第一輻射單元及第二輻射單元,第一輻射單元電性連接於中心導體的第一連接端、第二輻射單元電性連接於外層接地導體的第二連接端。 One embodiment of the present invention provides a dipole antenna structure disposed on a conductive body, including a reflective body, a transmission line, and an antenna body. The reflective body has a reflective surface. The transmission line passes through and is disposed on the reflective body. The transmission line includes a center conductor, an insulator covering the center conductor, and an outer ground conductor covering the insulator. The two ends of the center conductor respectively have a feeding end and a first connecting end, and the outer grounding conductor has The second connection end. The antenna body includes a first radiating unit and a second radiating unit. The first radiating unit is electrically connected to the first connecting end of the center conductor, and the second radiating unit is electrically connected to the second connecting end of the outer grounding conductor.

本發明另一實施例提供一種天線裝置,包括反射本體、傳輸線、天線本體及天線殼體。反射本體具有反射表面。傳輸線穿過且設置在反射本體上,傳輸線包括中心導體、包覆中心導體的絕緣體及包覆絕緣體的外層接地導體,中心導體的兩端分別具有饋入端及第一連接端 ,外層接地導體具有第二連接端。天線本體包括第一輻射單元及第二輻射單元,第一輻射單元電性連接於中心導體的第一連接端、第二輻射單元電性連接於外層接地導體的第二連接端。此外,反射本體、傳輸線及天線本體設置在天線殼體內。 Another embodiment of the present invention provides an antenna device including a reflective body, a transmission line, an antenna body, and an antenna housing. The reflective body has a reflective surface. The transmission line passes through and is disposed on the reflective body. The transmission line includes a center conductor, an insulator covering the center conductor, and an outer ground conductor covering the insulator. The two ends of the center conductor respectively have a feeding end and a first connecting end. The outer ground conductor has a second connection end. The antenna body includes a first radiating unit and a second radiating unit. The first radiating unit is electrically connected to the first connecting end of the center conductor, and the second radiating unit is electrically connected to the second connecting end of the outer grounding conductor. In addition, the reflective body, the transmission line, and the antenna body are disposed within the antenna housing.

綜上所述,本發明實施例所提供的偶極天線結構及天線裝置,其可透過“反射本體具有反射表面”與“第一輻射單元電性連接於中心導體的第一連接端及第二輻射單元電性連接於外層接地導體的第二連接端”的設計,以使得本發明的偶極天線結構及天線裝置能夠設置在於大型高導性物體上方、改善天線低仰角輻射場型的平均增益值、及降低製造的成本。 In summary, the dipole antenna structure and the antenna device provided by the embodiments of the present invention can transmit the first connecting end and the second end of the first radiating element electrically connected to the center conductor through the “reflecting body having a reflecting surface” and the “first radiating unit” The radiation unit is electrically connected to the second connection end of the outer ground conductor" so that the dipole antenna structure and the antenna device of the present invention can be disposed above the large high-conductivity object to improve the average gain of the antenna low-elevation radiation pattern Value, and reduce the cost of manufacturing.

為使能更進一步瞭解本發明之特徵及技術內容,請參閱以下有關本發明之詳細說明與附圖,然而所附圖式僅提供參考與說明用,並非用來對本發明加以限制者。 For a better understanding of the features and technical aspects of the present invention, reference should be made to the accompanying drawings.

〔第一實施例〕 [First Embodiment]

首先,請同時參閱圖1A至圖1D。由上述圖中可知,本發明第一實施例提供一種設置在一導電性本體W上的偶極天線結構1。於實務上,上述導電性本體W可為汽車的車頂,以作為天線的參考接地面,但本發明不以此為限。 First, please refer to FIG. 1A to FIG. 1D at the same time. As can be seen from the above figures, the first embodiment of the present invention provides a dipole antenna structure 1 disposed on a conductive body W. In practice, the conductive body W may be the roof of an automobile as a reference ground plane of the antenna, but the invention is not limited thereto.

如圖1A及圖1D所示,偶極天線結構1包括:反射本體11、傳輸線12及天線本體13。反射本體11具有反射表面110。更進一步地說,反射本體11可設置在導電性本體W的上方,以形成步階式的接地面架構。舉例來 說,反射本體11可採用圓柱形的對稱結構。換言之,由於圓柱形的對稱結構是平面且均勻的,所以反射波不會因為遇到不連續面的影響而使輻射場型產生不規則性的變化。藉此,本發明可透過調整反射本體11的尺寸、高度或形狀,從而改善輻射場型的均向性,並提升整體的平均增益。於實務上,上述反射本體11的形狀可為圓柱形,反射本體11的材質可為金屬材料例如裸銅。須注意的是,反射本體11的形狀可根據實際需求而改變,例如反射本體11可為梯形結構、雙層的圓柱形結構等對稱性的結構。 As shown in FIGS. 1A and 1D, the dipole antenna structure 1 includes a reflective body 11, a transmission line 12, and an antenna body 13. The reflective body 11 has a reflective surface 110. Furthermore, the reflective body 11 can be disposed above the conductive body W to form a stepped ground plane structure. For example It is said that the reflective body 11 can adopt a cylindrical symmetrical structure. In other words, since the cylindrical symmetrical structure is planar and uniform, the reflected wave does not cause irregularities in the radiation pattern due to the influence of the discontinuous surface. Thereby, the present invention can improve the uniformity of the radiation pattern and improve the overall average gain by adjusting the size, height or shape of the reflective body 11. In practice, the shape of the reflective body 11 may be a cylindrical shape, and the material of the reflective body 11 may be a metal material such as bare copper. It should be noted that the shape of the reflective body 11 may be changed according to actual needs. For example, the reflective body 11 may be a symmetrical structure such as a trapezoidal structure or a double-layered cylindrical structure.

如圖1B及圖1C所示,傳輸線12穿過且設置在該反射本體11上,更進一步地說,傳輸線12是設置在反射本體11的中心點。傳輸線12包括中心導體121、包覆中心導體121的絕緣體122及包覆絕緣體122的外層接地導體123,中心導體121的兩端分別具有饋入端1210及第一連接端1211,外層接地導體123具有第二連接端1231。於實務上,上述傳輸線12可採用半硬質式同軸纜線(semi-rigid coaxial cable)。 As shown in FIGS. 1B and 1C, the transmission line 12 is passed through and disposed on the reflective body 11, and further, the transmission line 12 is disposed at a center point of the reflective body 11. The transmission line 12 includes a central conductor 121, an insulator 122 covering the central conductor 121, and an outer ground conductor 123 covering the insulator 122. The two ends of the central conductor 121 have a feeding end 1210 and a first connecting end 1211, respectively, and the outer grounding conductor 123 has The second connection end 1231. In practice, the transmission line 12 can be a semi-rigid coaxial cable.

如圖1B所示,天線本體13包括第一輻射單元131及第二輻射單元132,第一輻射單元131電性連接於中心導體121的第一連接端1211、第二輻射單元132電性連接於外層接地導體123的第二連接端1231。更進一步地說,由於天線本體13為一具有圓極化特性的交叉式偶極天線結構,所以本發明可透過適當的設計使兩偶極天線(第一輻射單元131及第二輻射單元132)間產生振幅相同、相位相差90度的電流特性,以達到圓極化的 特性。舉例來說,第一輻射單元131包括第一L型輻射部1311及第二L型輻射部1312,第一L型輻射部1311的第一尾端1311b及第二L型輻射部1312的第一頭端1312a分別電性連接於中心導體121的第一連接端1211,第二輻射單元132包括第三L型輻射部1323及第四L型輻射部1324,第三L型輻射部1323的第二尾端1323b及第四L型輻射部1324的第二頭端1324a分別電性連接於外層接地導體123的第二連接端1231。 As shown in FIG. 1B, the antenna unit 13 includes a first radiating unit 131 and a second radiating unit 132. The first radiating unit 131 is electrically connected to the first connecting end 1211 of the center conductor 121, and the second radiating unit 132 is electrically connected to The second connection end 1231 of the outer layer ground conductor 123. Furthermore, since the antenna body 13 is a crossed dipole antenna structure having circular polarization characteristics, the present invention can make the two dipole antennas (the first radiating unit 131 and the second radiating unit 132) through appropriate design. Current characteristics with the same amplitude and phase difference of 90 degrees to achieve circular polarization characteristic. For example, the first radiating unit 131 includes a first L-type radiating portion 1311 and a second L-shaped radiating portion 1312, and the first end 1311b of the first L-shaped radiating portion 1311 and the first portion of the second L-shaped radiating portion 1312 The first end 1312a is electrically connected to the first connecting end 1211 of the center conductor 121, and the second radiating unit 132 includes a third L-shaped radiating portion 1323 and a fourth L-shaped radiating portion 1324, and the second L-shaped radiating portion 1323 is second. The second end 1324a of the tail end 1323b and the fourth L-type radiating portion 1324 is electrically connected to the second connecting end 1231 of the outer layer grounding conductor 123, respectively.

如圖1B所示,並同時依據圖1B中所界定的座標方向。第一L型輻射部1311包括由第一尾端1311b朝第一預定方向(x軸的相反方向)延伸的第一輻射段13111及由第一輻射段13111的末端朝第二預定方向(z軸的方向)延伸且與第一預定方向呈第一預定角度θ1的第二輻射段13112,更進一步地說,第一輻射段13111是平行於反射本體11,而第二輻射段13112是垂直於反射本體11(如圖1D所示)。第一輻射段13111與第二輻射段13112之間的夾角為第一預定角度θ1,例如可為90度。須注意的是,上述第一預定角度θ1可根據實際需求而調整。 As shown in FIG. 1B, and at the same time according to the coordinate direction defined in FIG. 1B. The first L-type radiating portion 1311 includes a first radiating section 1311 extending from the first trailing end 1311b toward the first predetermined direction (the opposite direction of the x-axis) and the end of the first radiating section 1311 toward the second predetermined direction (z-axis) a second radiant section 1312 extending at a first predetermined angle θ 1 from the first predetermined direction, and further, the first radiant section 13111 is parallel to the reflective body 11 and the second radiant section 13112 is perpendicular to Reflecting body 11 (as shown in Figure 1D). The angle between the first radiating section 13111 and the second radiating section 13112 is a first predetermined angle θ 1 , and may be, for example, 90 degrees. It should be noted that the above first predetermined angle θ 1 can be adjusted according to actual needs.

第三L型輻射部1323包括由第二尾端1323b朝向第一預定方向的相反方向延伸的第五輻射段13235及由第五輻射段13235的末端朝向第二預定方向的相反方向(z軸的相反方向)延伸的第六輻射段13236。更進一步地說,第五輻射段13235與第六輻射段13236之間夾角的角度θ3可為90度。第五輻射段13235反向對稱於第一輻射段13111,而第六輻射段13236反向對稱於第二輻射段13112。換言之,由於第一L型輻射部1311與第三 L型輻射部1323為反向對稱式的架構,所以能夠避免在上述輻射段發生電流相消的情況,從而維持天線輻射場強的大小。 The third L-type radiating portion 1323 includes a fifth radiating portion 13235 extending from the second trailing end 1323b in an opposite direction to the first predetermined direction and an opposite direction from the end of the fifth radiating portion 13235 toward the second predetermined direction (z-axis) The sixth radiant section 13236 extends in the opposite direction. Furthermore, the angle θ 3 between the fifth radiating section 13235 and the sixth radiating section 13236 may be 90 degrees. The fifth radiating section 13235 is inversely symmetric with respect to the first radiating section 1311, and the sixth radiating section 13236 is inversely symmetric with respect to the second radiating section 13112. In other words, since the first L-type radiating portion 1311 and the third L-type radiating portion 1323 are of an inverse symmetrical structure, it is possible to avoid the occurrence of current cancellation in the above-described radiant section, thereby maintaining the magnitude of the antenna radiation field strength.

第二L型輻射部1312包括由第一頭端1312a朝第三預定方向(y軸的相反方向)延伸且與第一預定方向呈第二預定角度θ2的第三輻射段13123及由第三輻射段13123的末端朝向第一預定方向的相反方向(x軸的方向)延伸的第四輻射段13124。更進一步地說,第三輻射段13123與第四輻射段13124皆是平行於反射本體11(如圖1D所示)。第三輻射段13123與第一輻射段13111之間的夾角為第二預定角度θ2,例如可為90度,而第三輻射段13123與第四輻射段13124之間的夾角可為90度。須注意的是,上述第二預定角度θ2可根據實際需求而調整。 The second L-type radiating portion 1312 includes a third radiating portion 13123 extending from the first head end 1312a toward the third predetermined direction (opposite direction of the y-axis) and at a second predetermined angle θ 2 with the first predetermined direction, and by the third The end of the radiating section 13123 faces the fourth radiating section 13124 extending in the opposite direction of the first predetermined direction (the direction of the x-axis). Furthermore, the third radiant section 13123 and the fourth radiant section 13124 are both parallel to the reflective body 11 (as shown in FIG. 1D). The angle between the third radiating section 13123 and the first radiating section 13111 is a second predetermined angle θ 2 , which may be, for example, 90 degrees, and the angle between the third radiating section 13123 and the fourth radiating section 13124 may be 90 degrees. It should be noted that the above second predetermined angle θ 2 can be adjusted according to actual needs.

第四L型輻射部1324包括由第二頭端1324a朝向第三預定方向的相反方向(y軸的方向)延伸的第七輻射段13247及由第七輻射段13247的末端朝向第一預定方向延伸的第八輻射段13248。更進一步地說,第七輻射段13247與第八輻射段13248之間的夾角的角度θ4可為90度。第七輻射段13247反向對稱於第三輻射段13123,而第八輻射段13248反向對稱於第四輻射段13124。換言之,由於第二L型輻射部1312與第四L型輻射部1324為反向對稱式的架構,所以能夠避免在上述輻射段發生電流相消的情況,從而維持天線輻射場強的大小。另外,由於第一輻射單元131與第二輻射單元132形成類似卍字型的天線架構,所以能夠提升低仰角方向圓極 化電流的分佈,從而提升低仰角的平均增益值。 The fourth L-type radiating portion 1324 includes a seventh radiating section 13247 extending from the second head end 1324a toward the opposite direction of the third predetermined direction (the direction of the y-axis) and extending from the end of the seventh radiating section 13247 toward the first predetermined direction The eighth radiating section 13248. Furthermore, the angle θ 4 of the angle between the seventh radiating section 13247 and the eighth radiating section 13248 may be 90 degrees. The seventh radiating section 13247 is inversely symmetric with respect to the third radiating section 13123, and the eighth radiating section 13248 is inversely symmetric with respect to the fourth radiating section 13124. In other words, since the second L-type radiating portion 1312 and the fourth L-shaped radiating portion 1324 are of an inverse symmetrical structure, it is possible to avoid the occurrence of current cancellation in the above-described radiant section, thereby maintaining the magnitude of the antenna radiation field strength. In addition, since the first radiating element 131 and the second radiating element 132 form a U-shaped antenna structure, the distribution of the circularly polarized current in the low elevation direction can be improved, thereby increasing the average gain value of the low elevation angle.

此外,由於天線本體13與傳輸線12直接連接會產生漏電流,而使傳輸線12也成為輻射體的一部分。因此天線本體13需要有一抑制電流產生的設計。如圖1B及圖1C所示,舉例來說,天線本體13包括匹配轉換單元133,外層接地導體123的一末端接觸匹配轉換單元133,匹配轉換單元133的其餘部分圍繞外層接地導體123且相距外層接地導體123一預定距離。更進一步地說,本發明透過運用四分之一波長的特性於匹配轉換單元133的末端短路銜接傳輸線12的外層接地導體123,並於匹配轉換單元133的頂端呈現開路阻抗無限大的特性,以阻止高頻電流流向傳輸線12的外層接地導體123。藉此,本發明可透過匹配轉換單元133的設計達到抑制漏電流,以維持天線原有的輻射特性。於實務上,上述匹配轉換單元133可為套筒式巴倫轉換器(balun converter),但本發明不以此為限。 In addition, since the antenna body 13 is directly connected to the transmission line 12, a leakage current is generated, and the transmission line 12 is also a part of the radiator. Therefore, the antenna body 13 needs to have a design that suppresses current generation. As shown in FIG. 1B and FIG. 1C, for example, the antenna body 13 includes a matching conversion unit 133, and one end of the outer ground conductor 123 contacts the matching conversion unit 133, and the remaining portion of the matching conversion unit 133 surrounds the outer ground conductor 123 and is spaced apart from the outer layer. The ground conductor 123 is a predetermined distance. More specifically, the present invention short-circuits the outer ground conductor 123 of the transmission line 12 by matching the end of the matching conversion unit 133 with the characteristics of the quarter-wavelength, and exhibits an infinite impedance of the open circuit impedance at the top end of the matching conversion unit 133. The high frequency current is prevented from flowing to the outer ground conductor 123 of the transmission line 12. Thereby, the present invention can achieve the suppression of leakage current through the design of the matching conversion unit 133 to maintain the original radiation characteristics of the antenna. In practice, the matching conversion unit 133 may be a sleeve balun converter, but the invention is not limited thereto.

如圖2A及圖2B所示,本發明第一實施例所提供的偶極天線結構1,在操作頻率為2170MHz至2200MHz之間所量測到的反射損耗及天線軸比皆可滿足衛星廣播系統S頻段的需求(例如ONDAS衛星廣播系統所規範的反射損耗為-10dB以下而天線軸比為3dB以下)。 As shown in FIG. 2A and FIG. 2B, the dipole antenna structure 1 provided by the first embodiment of the present invention can measure the reflection loss and the antenna axis ratio between the operating frequency of 2170 MHz and 2200 MHz to satisfy the satellite broadcasting system. The demand for the S-band (for example, the reflection loss specified by the ONDAS satellite broadcasting system is -10 dB or less and the antenna axis ratio is 3 dB or less).

如圖2C及圖2D所示,本發明第一實施例所提供的偶極天線結構1,在操作頻率為2185MHz並且在仰角(Elevation Angle,EA)30度至90度之間所量測到的輻射場型具備了類均向性的輻射場型。更進一步地說,仰角角度在30度、45度、60度、75度及90度之間所量測 到的平均增益值皆可滿足衛星廣播系統S頻段的需求(例如ONDAS衛星廣播系統所規範的仰角30度為3dB以上、仰角45度至75度為5dB以上、仰角90度為4dB以上)。換言之,由於偶極天線結構1具備了類均向性的輻射場型,所以可達到穩定的衛星訊號接收的功能,從而符合衛星廣播系統的需求。須注意的是,本發明的偶極天線結構並不侷限於衛星廣播系統,可根據實據需求調整操作頻率以應用於不同頻段的系統。 As shown in FIG. 2C and FIG. 2D, the dipole antenna structure 1 provided by the first embodiment of the present invention is measured at an operating frequency of 2185 MHz and between an elevation angle (EA) of 30 degrees and 90 degrees. The radiation field type has a type-like radiation field type. Furthermore, the elevation angle is measured between 30 degrees, 45 degrees, 60 degrees, 75 degrees and 90 degrees. The average gain value can meet the requirements of the S-band of the satellite broadcasting system (for example, the ONDAS satellite broadcasting system has an elevation angle of 30 degrees or more of 3 dB, an elevation angle of 45 degrees to 75 degrees of 5 dB or more, and an elevation angle of 90 degrees of 4 dB or more). In other words, since the dipole antenna structure 1 has an isotropic radiation field type, a stable satellite signal receiving function can be achieved, thereby meeting the requirements of the satellite broadcasting system. It should be noted that the dipole antenna structure of the present invention is not limited to a satellite broadcasting system, and the operating frequency can be adjusted according to actual data requirements to be applied to systems of different frequency bands.

〔第二實施例〕 [Second embodiment]

首先,請參閱圖3B。由圖3B與圖1B的比較可知,本發明第二實施例與第一實施例的差異在於:在第二實施例中,第一輻射單元131包括第一L型輻射部1311,第一L型輻射部1311的第一轉折處1311c電性連接於該中心導體121的第一連接端1211,第二輻射單元132包括第二L型輻射部1322,第二L型輻射部1322的第二轉折處1322c電性連接於外層接地導體123的第二連接端1231。 First, please refer to Figure 3B. It can be seen from the comparison between FIG. 3B and FIG. 1B that the second embodiment of the present invention differs from the first embodiment in that, in the second embodiment, the first radiating unit 131 includes a first L-shaped radiating portion 1311, and the first L-shaped The first turning point 1311c of the radiating portion 1311 is electrically connected to the first connecting end 1211 of the center conductor 121, the second radiating unit 132 includes the second L-shaped radiating portion 1322, and the second turning portion of the second L-shaped radiating portion 1322 The 1322c is electrically connected to the second connection end 1231 of the outer ground conductor 123.

更進一步地說,如圖3B所示,並同時依據圖3B中所界定的座標方向。第一L型輻射部1311包括由第一轉折處1311c朝第一預定方向(x軸的相反方向)延伸的第一輻射段13111及由第一轉折處1311c朝第二預定方向(y軸的相反方向)延伸且與第一預定方向呈第一預定角度θ1的第二輻射段13112,第二L型輻射部1322包括由該第二轉折處1322c朝向第一預定方向的相反方向(x軸的方向)延伸的第三輻射段13223及由第二轉折處1322c朝向第二預定方向的相反方向(y軸的方向)延伸的 第四輻射段13224。換言之,第一L型輻射部1311與第二L型輻射部1322為反向對稱式的架構。藉此,本發明可透過第一L型輻射部1311及第二L型輻射部1322的設計,以使本發明的偶極天線結構1能提供類均向性的輻射場型。 Further, as shown in FIG. 3B, and at the same time according to the coordinate direction defined in FIG. 3B. The first L-shaped radiating portion 1311 includes a first radiating portion 13111 extending from the first turning portion 1311c toward the first predetermined direction (the opposite direction of the x-axis) and a second predetermined portion (the opposite of the y-axis by the first turning portion 1311c) a second radiant section 1312 extending in a first predetermined angle θ 1 with respect to the first predetermined direction, the second L-shaped radiating portion 1322 including an opposite direction (x-axis) from the second turning point 1322c toward the first predetermined direction The third radiant section 13223 extending in the direction and the fourth radiant section 13224 extending from the second turning point 1322c in the opposite direction to the second predetermined direction (the direction of the y-axis). In other words, the first L-type radiating portion 1311 and the second L-shaped radiating portion 1322 are of an inverse symmetrical structure. Thereby, the present invention can transmit the design of the first L-type radiating portion 1311 and the second L-type radiating portion 1322 so that the dipole antenna structure 1 of the present invention can provide a radiation-like pattern of the homogeneity.

〔第三實施例〕 [Third embodiment]

首先,請參閱圖4B。由圖4B與圖1B的比較可知,本發明第三實施例與第一實施例的差異在於:在第三實施例中,第一輻射單元131包括第一L型輻射部1311及第一筆直型輻射部1315,第一L型輻射部1311的第一頭端1311a及第一筆直型輻射部1315的第一頭端1315a分別電性連接於中心導體121的第一連接端1211,第二輻射單元132包括第二L型輻射部1322及第二筆直型輻射部1325,第二L型輻射部1322的第二頭端1322a及第二筆直型輻射部1325的一第二頭端1325a分別電性連接於該外層接地導體123的該第二連接端1231。換言之,第一L型輻射部1311與第二L型輻射部1322為反向對稱式的架構,而第一筆直型輻射部1315與第二筆直型輻射部1325為反向對稱式的架構。 First, please refer to Figure 4B. 4B and FIG. 1B, the third embodiment of the present invention differs from the first embodiment in that, in the third embodiment, the first radiating unit 131 includes the first L-shaped radiating portion 1311 and the first straight type. The first end 1311a of the first L-shaped radiating portion 1311 and the first end 1315a of the first straight radiating portion 1315 are electrically connected to the first connecting end 1211 of the center conductor 121, and the second radiating unit is respectively connected to the radiating portion 1315. 132 includes a second L-shaped radiating portion 1322 and a second straight-type radiating portion 1325. The second head end 1322a of the second L-shaped radiating portion 1322 and a second head end 1325a of the second straight-type radiating portion 1325 are electrically connected. The second connection end 1231 of the outer ground conductor 123. In other words, the first L-type radiating portion 1311 and the second L-shaped radiating portion 1322 are of an inverse symmetrical structure, and the first straight radiating portion 1315 and the second straight radiating portion 1325 are of an inverse symmetrical structure.

如圖4B所示,並同時依據圖4B中所界定的座標方向。第一L型輻射部1311包括由第一頭端1311a朝第一預定方向(y軸的相反方向)延伸的第一輻射段13111及由第一輻射段13111的末端朝第二預定方向延伸(x軸的方向)且與第一預定方向呈第一預定角度θ1的第二輻射段13112。第二L型輻射部1322包括由第二頭端1322a朝向第一預定方向的相反方向(y軸的方向)延伸的第四 輻射段13224及由第四輻射段13224的末端朝向第二預定方向的相反方向(x軸的相反方向)延伸的第五輻射段13225。換言之,第一輻射段13111是平行於反射本體11,並且第一輻射段13111與第二輻射段13112之間的夾角為第一預定角度θ1,例如可為90度。須注意的是,上述第一預定角度θ1可根據實際需求而調整。 As shown in Figure 4B, and in accordance with the coordinate direction defined in Figure 4B. The first L-type radiating portion 1311 includes a first radiating section 1311 extending from the first head end 1311a toward the first predetermined direction (the opposite direction of the y-axis) and extending from the end of the first radiating section 1311 toward the second predetermined direction (x) The second radiant section 1312 of the direction of the axis and at a first predetermined angle θ 1 with the first predetermined direction. The second L-type radiating portion 1322 includes a fourth radiating portion 13224 extending from the second head end 1322a toward the opposite direction of the first predetermined direction (the direction of the y-axis) and the end of the fourth radiating portion 13224 toward the second predetermined direction A fifth radiant section 13225 extending in the opposite direction (the opposite direction of the x-axis). In other words, the first radiant section 13111 is parallel to the reflective body 11, and the angle between the first radiant section 13111 and the second radiant section 13112 is a first predetermined angle θ 1 , which may be, for example, 90 degrees. It should be noted that the above first predetermined angle θ 1 can be adjusted according to actual needs.

第一筆直型輻射部1315包括由第一頭端1315a朝向第二預定方向的相反方向(x軸的相反方向)延伸且與第一預定方向呈第二預定角度θ2的第三輻射段13153。換言之,第三輻射段13153與第一輻射段13111之間的夾角為第二預定角度θ2,例如可為90度。須注意的是,上述第二預定角度θ2可根據實際需求而調整。此外,第三輻射段13153相對於第一輻射段13111可為稍微向上傾斜的角度例如15度(圖未示)。換言之,第三輻射段13153並非平行於反射本體11。 The first straight type radiating portion 1315 includes a third radiating portion 13153 extending from the first head end 1315a toward the opposite direction of the second predetermined direction (opposite direction of the x-axis) and at a second predetermined angle θ 2 with the first predetermined direction. In other words, the angle between the third radiant section 13153 and the first radiant section 13111 is a second predetermined angle θ 2 , which may be, for example, 90 degrees. It should be noted that the above second predetermined angle θ 2 can be adjusted according to actual needs. Further, the third radiant section 13153 may be slightly inclined upward at an angle of, for example, 15 degrees (not shown) with respect to the first radiant section 13111. In other words, the third radiant section 13153 is not parallel to the reflective body 11.

第二筆直型輻射部1325包括由第二頭端1325a朝向第二預定方向延伸的第六輻射段13256。換言之,第六輻射段13256相對於第四輻射段13224可為稍微向下傾斜的角度例如15度(圖未示)。更進一步地說,雖然第六輻射段13256相較於其它輻射段是更接近於導電性本體W(參考接地面),但仍維持有一段相當大的距離,所以可降低輻射場型受到參考接地面的影響。藉此,本發明的偶極天線結構1能提夠提升輻射場型的對稱性,以及提升整體的平均增益值。 The second straight radiating portion 1325 includes a sixth radiating portion 13256 that extends from the second head end 1325a toward the second predetermined direction. In other words, the sixth radiant section 13256 can be a slightly downwardly inclined angle, such as 15 degrees (not shown), relative to the fourth radiant section 13224. Furthermore, although the sixth radiating section 13256 is closer to the conductive body W (reference ground plane) than the other radiating sections, it still maintains a considerable distance, so that the radiation field can be reduced by reference. The impact of the ground. Thereby, the dipole antenna structure 1 of the present invention can improve the symmetry of the radiation pattern and improve the overall average gain value.

〔第四實施例〕 [Fourth embodiment]

首先,請參閱圖5。由上述圖中可知,本發明第四實施 例提供一種天線裝置2,包括反射本體11、傳輸線12、天線本體13及天線殼體21。舉例來說,上述天線裝置2可設置在汽車的車頂,以作為天線的參考接地面,但本發明不以此為限。 First, please refer to Figure 5. As can be seen from the above figures, the fourth embodiment of the present invention An antenna device 2 is provided, including a reflective body 11, a transmission line 12, an antenna body 13, and an antenna housing 21. For example, the antenna device 2 can be disposed on the roof of the automobile as a reference ground plane of the antenna, but the invention is not limited thereto.

如圖5所示,反射本體11具有反射表面110。傳輸線12穿過且設置在反射本體11上,傳輸線12包括中心導體121、包覆中心導體121的絕緣體122及包覆絕緣體122的外層接地導體123,中心導體121的兩端分別具有饋入端1210及第一連接端1211,外層接地導體123具有第二連接端1231。天線本體13包括第一輻射單元131及第二輻射單元132,第一輻射單元131電性連接於中心導體121的第一連接端1211、第二輻射單元132電性連接於外層接地導體123的第二連接端1231。舉例來說,上述反射本體11、傳輸線12及天線本體13可設置在天線殼體21內。換言之,反射本體11、傳輸線12及天線本體13皆被包覆天線殼體21的內部。藉此,本發明天線裝置2可保持產品整體外觀的完整性與美感度。 As shown in FIG. 5, the reflective body 11 has a reflective surface 110. The transmission line 12 passes through and is disposed on the reflective body 11. The transmission line 12 includes a center conductor 121, an insulator 122 covering the center conductor 121, and an outer ground conductor 123 covering the insulator 122. The two ends of the center conductor 121 respectively have a feeding end 1210. And the first connection end 1211, the outer ground conductor 123 has a second connection end 1231. The antenna body 13 includes a first radiating unit 131 and a second radiating unit 132. The first radiating unit 131 is electrically connected to the first connecting end 1211 of the center conductor 121, and the second radiating unit 132 is electrically connected to the outer grounding conductor 123. Two connection ends 1231. For example, the reflective body 11, the transmission line 12, and the antenna body 13 may be disposed in the antenna housing 21. In other words, the reflective body 11, the transmission line 12, and the antenna body 13 are both covered inside the antenna housing 21. Thereby, the antenna device 2 of the present invention can maintain the integrity and aesthetics of the overall appearance of the product.

〔實施例的可能功效〕 [Possible effects of the examples]

綜上所述,本發明實施例所提供的偶極天線結構及天線裝置,其可透過“反射本體具有反射表面”與“第一輻射單元電性連接於中心導體的第一連接端及第二輻射單元電性連接於外層接地導體的第二連接端”的設計,以使得本發明的偶極天線結構及天線裝置能夠設置在於大型高導性物體上方、改善天線低仰角輻射場型的平均增益值、及降低製造的成本。 In summary, the dipole antenna structure and the antenna device provided by the embodiments of the present invention can transmit the first connecting end and the second end of the first radiating element electrically connected to the center conductor through the “reflecting body having a reflecting surface” and the “first radiating unit” The radiation unit is electrically connected to the second connection end of the outer ground conductor" so that the dipole antenna structure and the antenna device of the present invention can be disposed above the large high-conductivity object to improve the average gain of the antenna low-elevation radiation pattern Value, and reduce the cost of manufacturing.

以上所述僅為本發明之較佳可行實施例,非因此侷限本發明之專利範圍,故舉凡運用本發明說明書及圖式內容所為之等效技術變化,均包含於本發明之範圍內。 The above are only the preferred embodiments of the present invention, and are not intended to limit the scope of the invention, and the equivalents of the invention are included in the scope of the invention.

1‧‧‧偶極天線結構 1‧‧‧ Dipole antenna structure

11‧‧‧反射本體 11‧‧‧Reflecting ontology

110‧‧‧反射表面 110‧‧‧Reflective surface

12‧‧‧傳輸線 12‧‧‧ transmission line

121‧‧‧中心導體 121‧‧‧Center conductor

1210‧‧‧饋入端 1210‧‧‧Feeding end

1211‧‧‧第一連接端 1211‧‧‧First connection

122‧‧‧絕緣體 122‧‧‧Insulator

123‧‧‧外層接地導體 123‧‧‧ outer grounding conductor

1231‧‧‧第二連接端 1231‧‧‧second connection

13‧‧‧天線本體 13‧‧‧Antenna body

131‧‧‧第一輻射單元 131‧‧‧First Radiation Unit

1311‧‧‧第一L型輻射部 1311‧‧‧First L-type Radiation Department

1311a‧‧‧第一頭端 1311a‧‧‧ first head

1311b‧‧‧第一尾端 1311b‧‧‧First end

1311c‧‧‧第一轉折處 1311c‧‧‧First Turning Place

13111‧‧‧第一輻射段 13111‧‧‧First radiant section

13112‧‧‧第二輻射段 13112‧‧‧second radiant section

1312‧‧‧第二L型輻射部 1312‧‧‧Second L-type radiation department

1312a‧‧‧第一頭端 1312a‧‧‧ first head

13123‧‧‧第三輻射段 13123‧‧‧The third radiant section

13124‧‧‧第四輻射段 13124‧‧‧fourth radiant section

1315‧‧‧第一筆直型輻射部 1315‧‧‧The first straight radiation department

1315a‧‧‧第一頭端 1315a‧‧‧ first head

13153‧‧‧第三輻射段 13153‧‧‧The third radiant section

132‧‧‧第二輻射單元 132‧‧‧second radiation unit

1322‧‧‧第二L型輻射部 1322‧‧‧Second L-type radiation department

1322a‧‧‧第二頭端 1322a‧‧‧second head

1322c‧‧‧第二轉折處 1322c‧‧‧second turning point

13223‧‧‧第三輻射段 13223‧‧‧third radiant section

13224‧‧‧第四輻射段 13224‧‧‧fourth radiant section

13225‧‧‧第五輻射段 13225‧‧‧The fifth radiant section

1323‧‧‧第三L型輻射部 1323‧‧‧ Third L-type Radiation Department

1323b‧‧‧第二尾端 1323b‧‧‧second end

13235‧‧‧第五輻射段 13235‧‧‧The fifth radiant section

13236‧‧‧第六輻射段 13236‧‧‧Sixth radiant section

1324‧‧‧第四L型輻射部 1324‧‧‧Fourth L-type Radiation Department

1324a‧‧‧第二頭端 1324a‧‧‧second head

13247‧‧‧第七輻射段 13247‧‧‧ seventh radiant section

13248‧‧‧第八輻射段 13248‧‧‧8th radiant section

1325‧‧‧第二筆直型輻射部 1325‧‧‧Second straight radiation department

1325a‧‧‧第二頭端 1325a‧‧‧second head

13256‧‧‧第六輻射段 13256‧‧‧Sixth radiant section

133‧‧‧匹配轉換單元 133‧‧‧match conversion unit

2‧‧‧天線裝置 2‧‧‧Antenna device

21‧‧‧天線殼體 21‧‧‧Antenna housing

θ1‧‧‧第一預定角度 θ 1 ‧‧‧first predetermined angle

θ2‧‧‧第二預定角度 θ 2 ‧‧‧second predetermined angle

θ3、θ4‧‧‧角度 θ 3 , θ 4 ‧‧‧ angle

W‧‧‧導電性本體 W‧‧‧Electrical ontology

圖1A為本發明第一實施例其中一視角的立體示意圖。 1A is a perspective view of a first embodiment of the present invention.

圖1B為圖1A的A部分的放大示意圖。 Fig. 1B is an enlarged schematic view of a portion A of Fig. 1A.

圖1C為本發明第一實施例另一視角的立體示意圖。 1C is a perspective view of another perspective of the first embodiment of the present invention.

圖1D為本發明第一實施例的側視示意圖。 Figure 1D is a side elevational view of a first embodiment of the present invention.

圖2A為本發明第一實施例在不同頻率下所量測到的反射損耗曲線圖。 2A is a graph showing the reflection loss measured at different frequencies according to the first embodiment of the present invention.

圖2B為本發明第一實施例在不同頻率下所量測到的天線軸比曲線圖。 2B is a graph showing an antenna shaft ratio measured at different frequencies according to the first embodiment of the present invention.

圖2C為本發明第一實施例在不同仰角下所量測到的輻射場型曲線圖。 2C is a graph showing the radiation pattern measured at different elevation angles according to the first embodiment of the present invention.

圖2D為本發明第一實施例在不同仰角下所量測到的右旋圓極化平均增益曲線圖。 2D is a graph showing the right-handed circular polarization average gain measured at different elevation angles according to the first embodiment of the present invention.

圖3A為本發明第二實施例其中一視角的立體示意圖。 3A is a perspective view of a perspective view of a second embodiment of the present invention.

圖3B為圖3A的A部分的放大示意圖。 Fig. 3B is an enlarged schematic view of a portion A of Fig. 3A.

圖4A為本發明第三實施例其中一視角的立體示意圖。 4A is a perspective view of a perspective view of a third embodiment of the present invention.

圖4B為本發明第三實施例另一視角的立體示意圖。 4B is a perspective view of another perspective of the third embodiment of the present invention.

圖5為本發明第四實施例的立體示意圖。 Figure 5 is a perspective view of a fourth embodiment of the present invention.

1‧‧‧偶極天線結構 1‧‧‧ Dipole antenna structure

11‧‧‧反射本體 11‧‧‧Reflecting ontology

110‧‧‧反射表面 110‧‧‧Reflective surface

12‧‧‧傳輸線 12‧‧‧ transmission line

13‧‧‧天線本體 13‧‧‧Antenna body

W‧‧‧導電性本體 W‧‧‧Electrical ontology

Claims (9)

一種偶極天線結構,其設置在一導電性本體上,該偶極天線結構包括:一反射本體,其具有一反射表面;一傳輸線,其穿過且設置在該反射本體上,該傳輸線包括一中心導體、一包覆該中心導體的絕緣體及一包覆該絕緣體的外層接地導體,該中心導體的兩端分別具有一饋入端及一第一連接端,該外層接地導體具有一第二連接端;以及一天線本體,其包括一第一輻射單元及一第二輻射單元,該第一輻射單元電性連接於該中心導體的該第一連接端、該第二輻射單元電性連接於該外層接地導體的該第二連接端。 A dipole antenna structure is disposed on a conductive body, the dipole antenna structure includes: a reflective body having a reflective surface; a transmission line passing through and disposed on the reflective body, the transmission line including a a central conductor, an insulator covering the central conductor, and an outer grounding conductor covering the insulator, the two ends of the central conductor respectively have a feeding end and a first connecting end, and the outer grounding conductor has a second connection And an antenna body including a first radiating unit and a second radiating unit, the first radiating unit is electrically connected to the first connecting end of the center conductor, and the second radiating unit is electrically connected to the first radiating unit The second connection end of the outer ground conductor. 如申請專利範圍第1項所述之偶極天線結構,其中該天線本體包括一匹配轉換部,該外層接地導體的一末端接觸該匹配轉換部,該匹配轉換部的其餘部分圍繞該外層接地導體且相距該外層接地導體一預定距離。 The dipole antenna structure of claim 1, wherein the antenna body comprises a matching conversion portion, an end of the outer ground conductor contacts the matching conversion portion, and the remaining portion of the matching conversion portion surrounds the outer ground conductor And a predetermined distance from the outer ground conductor. 如申請專利範圍第2項所述之偶極天線結構,其中該第一輻射單元包括一第一L型輻射部及一第二L型輻射部,該第一L型輻射部的一第一尾端及該第二L型輻射部的一第一頭端分別電性連接於該中心導體的該第一連接端,該第二輻射單元包括一第三L型輻射部及一第四L型輻射部,該第三L型輻射部的一第二尾端及該第四L型輻射部的一第二頭端分別電性連接於該外層接地導體的該第二連接端。 The dipole antenna structure of claim 2, wherein the first radiating unit comprises a first L-type radiating portion and a second L-shaped radiating portion, and a first tail of the first L-shaped radiating portion The first end of the second L-shaped radiating portion is electrically connected to the first connecting end of the center conductor, and the second radiating unit comprises a third L-shaped radiating portion and a fourth L-shaped radiation a second tail end of the third L-shaped radiating portion and a second end end of the fourth L-shaped radiating portion are electrically connected to the second connecting end of the outer grounding conductor, respectively. 如申請專利範圍第3項所述之偶極天線結構,其中該第 一L型輻射部包括一由該第一尾端朝一第一預定方向延伸的第一輻射段及一由該第一輻射段的末端朝一第二預定方向延伸且與該第一預定方向呈一第一預定角度的第二輻射段,該第二L型輻射部包括一由該第一頭端朝一第三預定方向延伸且與該第一預定方向呈一第二預定角度的第三輻射段及一由該第三輻射段的末端朝向該第一預定方向的相反方向延伸的第四輻射段,該第三L型輻射部包括一由該第二尾端朝向該第一預定方向的相反方向延伸的第五輻射段及一由該第五輻射段的末端朝向該第二預定方向的相反方向延伸的第六輻射段,該第四L型輻射部包括一由該第二頭端朝向該第三預定方向的相反方向延伸的第七輻射段及一由該第七輻射段的末端朝向該第一預定方向延伸的第八輻射段。 The dipole antenna structure as described in claim 3, wherein the An L-shaped radiating portion includes a first radiating section extending from the first trailing end toward a first predetermined direction and a second extending direction from the end of the first radiating section and forming a first predetermined direction a second radiant section of a predetermined angle, the second L-shaped radiating section including a third radiant section extending from the first head end toward a third predetermined direction and at a second predetermined angle to the first predetermined direction a fourth radiating section extending from an end of the third radiating section toward an opposite direction of the first predetermined direction, the third L-shaped radiating section including a second end extending from the second end toward the first predetermined direction a fifth radiant section and a sixth radiant section extending from an end of the fifth radiant section toward the second predetermined direction, the fourth L-shaped radiating section including a second head end facing the third predetermined a seventh radiating section extending in opposite directions of the direction and an eighth radiating section extending from the end of the seventh radiating section toward the first predetermined direction. 如申請專利範圍第2項所述之偶極天線結構,其中該第一輻射單元包括一第一L型輻射部,該第一L型輻射部的一第一轉折處電性連接於該中心導體的該第一連接端,該第二輻射單元包括一第二L型輻射部,該第二L型輻射部的一第二轉折處電性連接於該外層接地導體的該第二連接端。 The dipole antenna structure of claim 2, wherein the first radiating unit comprises a first L-shaped radiating portion, and a first turning portion of the first L-shaped radiating portion is electrically connected to the central conductor The second connecting unit includes a second L-shaped radiating portion, and a second turning portion of the second L-shaped radiating portion is electrically connected to the second connecting end of the outer grounding conductor. 如申請專利範圍第5項所述之偶極天線結構,其中該第一L型輻射部包括一由該第一轉折處朝一第一預定方向延伸的第一輻射段及一由該第一轉折處朝一第二預定方向延伸且與該第一預定方向呈一第一預定角度的第二輻射段,該第二L型輻射部包括一由該第二轉折處朝向該第一預定方向的相反方向延伸的第三輻射段及一由該第二轉折處朝向該第二預定方向的相反方向延伸的第四輻 射段。 The dipole antenna structure of claim 5, wherein the first L-type radiating portion comprises a first radiating portion extending from the first turning portion toward a first predetermined direction and a first turning portion a second radiating section extending toward a second predetermined direction and at a first predetermined angle to the first predetermined direction, the second L-shaped radiating portion including an extension of the second inflection direction opposite to the first predetermined direction a third radiant section and a fourth radii extending from the second turn toward the second predetermined direction Shooting segment. 如申請專利範圍第2項所述之偶極天線結構,其中該第一輻射單元包括一第一L型輻射部及一第一筆直型輻射部,該第一L型輻射部的一第一頭端及該第一直型型輻射部的一第一頭端分別電性連接於該中心導體的該第一連接端,該第二輻射單元包括一第二L型輻射部及一第二筆直型輻射部,該第二L型輻射部的一第二頭端及該第二筆直型輻射部的一第二頭端分別電性連接於該外層接地導體的該第二連接端。 The dipole antenna structure of claim 2, wherein the first radiating unit comprises a first L-shaped radiating portion and a first straight radiating portion, and a first head of the first L-shaped radiating portion The first end of the first straight type radiating portion is electrically connected to the first connecting end of the center conductor, and the second radiating unit comprises a second L-shaped radiating portion and a second straight type The second end of the second L-shaped radiating portion and the second end of the second straight radiating portion are electrically connected to the second connecting end of the outer grounding conductor, respectively. 如申請專利範圍第7項所述之偶極天線結構,其中該第一L型輻射部包括一由該第一頭端朝一第一預定方向延伸的第一輻射段及一由該第一輻射段的末端朝一第二預定方向延伸且與該第一預定方向呈一第一預定角度的第二輻射段,該第一筆直型輻射部包括一由該第一頭端朝向該第二預定方向的相反方向延伸且與該第一預定方向呈一第二預定角度的第三輻射段,該第二L型輻射部包括一由該第二頭端朝向該第一預定方向的相反方向延伸的第四輻射段及一由該第四輻射段的末端朝向該第二預定方向的相反方向延伸的第五輻射段,該第二筆直型輻射部包括一由該第二頭端朝向該第二預定方向延伸的第六輻射段。 The dipole antenna structure of claim 7, wherein the first L-type radiating portion comprises a first radiating portion extending from the first head end toward a first predetermined direction and a first radiating portion a second radiant section extending toward a second predetermined direction and at a first predetermined angle to the first predetermined direction, the first straight radiating portion including a reverse direction from the first head end toward the second predetermined direction a third radiant section extending in a direction and at a second predetermined angle to the first predetermined direction, the second L-shaped radiating portion including a fourth radiation extending from the second head end in an opposite direction to the first predetermined direction a fifth radiant section extending from an end of the fourth radiant section toward an opposite direction of the second predetermined direction, the second straight radiating portion including a second tip end extending toward the second predetermined direction The sixth radiant section. 一種天線裝置,包括:一反射本體,其具有一反射表面;一傳輸線,其穿過且設置在該反射本體上,該傳輸線包括一中心導體、一包覆該中心導體的絕緣體及一包覆該絕緣體的外層接地導體,該中心導體的兩端分別具 有一饋入端及一第一連接端,該外層接地導體具有一第二連接端;一天線本體,其包括一第一輻射單元及一第二輻射單元,該第一輻射單元電性連接於該中心導體的該第一連接端、該第二輻射單元電性連接於該外層接地導體的該第二連接端;以及一天線殼體,其中該反射本體、該傳輸線及該天線本體設置在該天線殼體內。 An antenna device includes: a reflective body having a reflective surface; a transmission line passing through and disposed on the reflective body, the transmission line including a center conductor, an insulator covering the center conductor, and a covering An outer layer grounding conductor of the insulator, the two ends of the center conductor respectively having The first grounding conductor has a second connecting end, and the antenna body includes a first radiating unit and a second radiating unit. The first radiating unit is electrically connected to the antenna. The first connecting end of the center conductor, the second radiating unit is electrically connected to the second connecting end of the outer grounding conductor; and an antenna housing, wherein the reflecting body, the transmission line and the antenna body are disposed on the antenna Inside the housing.
TW102101995A 2013-01-18 2013-01-18 Dipole antenna structure and antenna device TWI525901B (en)

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