JPH04281604A - Spiral antenna and array antenna using the spiral antenna - Google Patents

Spiral antenna and array antenna using the spiral antenna

Info

Publication number
JPH04281604A
JPH04281604A JP6882791A JP6882791A JPH04281604A JP H04281604 A JPH04281604 A JP H04281604A JP 6882791 A JP6882791 A JP 6882791A JP 6882791 A JP6882791 A JP 6882791A JP H04281604 A JPH04281604 A JP H04281604A
Authority
JP
Japan
Prior art keywords
conductor
insulating layer
spiral
antenna
radiating element
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP6882791A
Other languages
Japanese (ja)
Other versions
JP3187853B2 (en
Inventor
Hisamatsu Nakano
久松 中野
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NIPPON DENGIYOU KOSAKU KK
Nihon Dengyo Kosaku Co Ltd
Original Assignee
NIPPON DENGIYOU KOSAKU KK
Nihon Dengyo Kosaku Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by NIPPON DENGIYOU KOSAKU KK, Nihon Dengyo Kosaku Co Ltd filed Critical NIPPON DENGIYOU KOSAKU KK
Priority to JP06882791A priority Critical patent/JP3187853B2/en
Publication of JPH04281604A publication Critical patent/JPH04281604A/en
Application granted granted Critical
Publication of JP3187853B2 publication Critical patent/JP3187853B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

PURPOSE:To attain excellent directivity, reflection attenuation characteristic and axial ratio characteristic. CONSTITUTION:A radiation element 7 made of a spiral conductor, and a strip conductor 3 connecting to its end are supported on a same plane and an upper ground conductor 1 and a lower ground conductor 2 are provided to the upper and lower part via an upper insulation layer 4 and a lower insulation layer 5, and an opening 6 is provided to a part corresponding to the radiation element 7 in the upper ground conductor 1. Thus, the array antenna using the spiral antenna as the component is most suited as a satellite broadcast reception antenna employing a circularly polarized wave.

Description

【発明の詳細な説明】[Detailed description of the invention]

【0001】0001

【産業上の利用分野】本発明は、例えば円偏波を用いる
衛星放送受信用アンテナ等に用いられる平面アレ−アン
テナの構成素子アンテナに好適な渦巻きアンテナ及びこ
のアンテナを用いたアレ−アンテナに関するものである
[Field of Industrial Application] The present invention relates to a spiral antenna suitable for a component antenna of a planar array antenna used, for example, in a satellite broadcast receiving antenna using circularly polarized waves, and an array antenna using this antenna. It is.

【0002】0002

【従来の技術】従来の高利得平面アレ−アンテナは、例
えばマイクロストリップパッチアンテナのように、誘電
体基板上に形成された複数個の放射素子及びマイクロス
トリップ伝送線路より成る給電線を同一平面上に配設し
、前記給電線によって前記複数個の放射素子を並列給電
するように構成されている。
2. Description of the Related Art A conventional high-gain planar array antenna, such as a microstrip patch antenna, has a feeder line consisting of a plurality of radiating elements formed on a dielectric substrate and a microstrip transmission line on the same plane. The plurality of radiating elements are arranged in parallel and are configured to be fed in parallel by the feeder line.

【0003】0003

【発明が解決しようとする課題】上記平面アレ−アンテ
ナの給電線として用いられているマイクロストリップ伝
送線路は、開放形線路であるため、線路自体からの放射
損失及び電気的特性の安定性は、線路を構成する絶縁体
の物性に左右され、したがって、この絶縁体の材質を選
択するに当っては、損失及び電気的特性の安定性の両面
に配慮する必要があるため、必ずしも常に損失の十分に
小さい材質を選べるとは限らない。
[Problems to be Solved by the Invention] Since the microstrip transmission line used as the feed line of the planar array antenna is an open line, the radiation loss from the line itself and the stability of the electrical characteristics are It depends on the physical properties of the insulator that makes up the line, and therefore, when selecting the material of this insulator, it is necessary to consider both loss and stability of electrical characteristics. It is not always possible to choose a material that is small.

【0004】電気的特性の安定性を保持するために損失
の十分に小さい絶縁材質を選ぶことができない場合には
、伝送線路における放射損失を補うために、放射素子の
数を増して利得を増加させることが行われているが、放
射素子の増加に伴って給電線路長が長くなり、実効上の
利得増加を得ることができない。
[0004] When it is not possible to select an insulating material with sufficiently low loss to maintain the stability of electrical characteristics, the number of radiating elements is increased to increase the gain in order to compensate for the radiation loss in the transmission line. However, as the number of radiating elements increases, the feed line length increases, making it impossible to obtain an effective gain increase.

【0005】このような問題を解決するために、マイク
ロストリップ伝送線路に較べて構成は複雑であるが、形
状が平面的で、構成上、損失の少ない絶縁体の使用が可
能なトリプレ−ト伝送線路又はサスペンデット伝送線路
を用いて実効上の利得を増加させるように構成したアン
テナが提案されている。
[0005] In order to solve these problems, triple-plate transmission has been proposed, which is more complex than a microstrip transmission line, but has a planar shape and can use insulators with low loss. Antennas have been proposed that are constructed using lines or suspended transmission lines to increase the effective gain.

【0006】トリプレ−ト伝送線路又はサスペンデット
伝送線路は、いずれも二つのア−ス導体間にストリップ
導体が挟まれた構造であるため、これらの伝送線路を放
射素子に結合するに当って、従来は、トリプレ−ト伝送
線路又はサスペンデット伝送線路を構成する二つのア−
ス導体のうち、いずれか一方のア−ス導体面に配設され
た縮退分離素子を有する放射素子を電磁結合により励振
するか、トリプレ−ト伝送線路又はサスペンデット伝送
線路により位相差給電される二つのモノポ−ルアンテナ
を介して放射素子を励振する方法が用いられている。
[0006] Since both the triple-plate transmission line and the suspended transmission line have a structure in which a strip conductor is sandwiched between two ground conductors, it is difficult to couple these transmission lines to a radiating element using conventional is two arcs constituting a triple-plate transmission line or a suspended transmission line.
Among the ground conductors, a radiating element having a degenerate separation element arranged on one of the ground conductor surfaces is excited by electromagnetic coupling, or two A method is used in which a radiating element is excited through two monopole antennas.

【0007】いずれか一方のア−ス導体面に配設された
縮退分離素子を有する放射素子を電磁結合により励振す
る方法は、トリプレ−ト伝送線路又はサスペンデット伝
送線路を構成するストリップ導体と縮退分離素子相互の
位置関係が、所要の位置関係に正確に保たれていないと
特性が劣化することとなるので、ストリップ導体と縮退
分離素子相互の位置関係の精度を高くする必要があり、
その結果、製作コストの上昇を免れることができず、位
相差給電される二つのモノポ−ルアンテナを介して放射
素子を励振する方法においては、部品数が多く、給電系
が複雑となる。
[0007] A method of exciting a radiating element having a degenerate separation element disposed on one of the ground conductor planes by electromagnetic coupling is based on a method of exciting a radiating element having a degenerate separation element disposed on one of the ground conductor surfaces. If the positional relationship between the elements is not accurately maintained at the required positional relationship, the characteristics will deteriorate, so it is necessary to increase the accuracy of the mutual positional relationship between the strip conductor and the degenerate separation element.
As a result, an increase in manufacturing costs cannot be avoided, and the method of exciting a radiating element through two monopole antennas that are fed with phase difference requires a large number of parts and a complicated feeding system.

【0008】[0008]

【課題を解決するための手段】本発明は、上部外部導体
と下部外部導体との間に介在する上部絶縁層及び下部絶
縁層と、前記上部外部導体の一部適宜範囲を除去して形
成した開口部と、この開口部に対応する前記上部絶縁層
と下部絶縁層との間に設けた渦巻き状導体より成る放射
素子と、前記上部絶縁層と下部絶縁層との間に介在させ
ると共に、前記渦巻き状導体より成る放射素子に高周波
的に接続した内部導体とを備えたアンテナを実現するこ
とによって、従来の欠点を除こうとするものである。
[Means for Solving the Problems] The present invention provides an upper insulating layer and a lower insulating layer interposed between an upper outer conductor and a lower outer conductor, and a part of the upper outer conductor formed by removing an appropriate range. a radiating element made of a spiral conductor provided between an opening, the upper insulating layer and the lower insulating layer corresponding to the opening; and a radiating element interposed between the upper insulating layer and the lower insulating layer; The present invention attempts to eliminate the drawbacks of the prior art by realizing an antenna comprising a radiating element made of a spiral conductor and an internal conductor connected at high frequency.

【0009】[0009]

【作用】内部導体から供給される高周波電流は、渦巻き
状導体より成る放射素子の一端から流入し、放射素子の
長さを適当に調整しておくことにより、放射素子上の電
流分布が進行波分布となって円偏波を放射する。
[Operation] The high-frequency current supplied from the internal conductor flows from one end of the radiating element made of a spiral conductor, and by appropriately adjusting the length of the radiating element, the current distribution on the radiating element is created as a traveling wave. It emits circularly polarized waves in a distributed manner.

【0010】0010

【実施例】図1の(a)は、本発明の一実施例を示す平
面図、図1の(b)は、図1の(a)のA−A断面図で
、両図において、1は上部外部導体(以下、上部ア−ス
導体と称する)、2は下部外部導体(以下、下部ア−ス
導体と称する)、3は内部導体(以下、ストリップ導体
と称する)、4は、上部ア−ス導体1とストリップ導体
3間に介在する上部絶縁層、5は、下部ア−ス導体2と
ストリップ導体3間に介在する下部絶縁層で、これらに
よってトリプレ−ト伝送線路が構成される。
[Embodiment] FIG. 1(a) is a plan view showing an embodiment of the present invention, and FIG. 1(b) is a cross-sectional view taken along line AA in FIG. 1(a). is the upper outer conductor (hereinafter referred to as the upper ground conductor), 2 is the lower outer conductor (hereinafter referred to as the lower earth conductor), 3 is the inner conductor (hereinafter referred to as the strip conductor), and 4 is the upper The upper insulating layer 5 interposed between the ground conductor 1 and the strip conductor 3 is a lower insulating layer interposed between the lower ground conductor 2 and the strip conductor 3, and these constitute a triple plate transmission line. .

【0011】6は、上部ア−ス導体1の一部適宜範囲を
除去して形成した開口部で、図には、その輪郭形状を円
形に形成した場合を例示してあるが、任意の輪郭形状に
形成して本発明を実施することができる。
Reference numeral 6 denotes an opening formed by removing a suitable part of the upper ground conductor 1. Although the figure shows an example in which the outline is circular, it can be formed into any arbitrary outline. The present invention can be practiced by forming it into a shape.

【0012】7は放射素子で、開口部6に対応する下部
絶縁層5の表面に付着させた渦巻き状の導体より成り、
その外端を、ストリップ導体3の端部に直接又は容量を
介して高周波的に接続してある。したがって、放射素子
7とストリップ導体3とは、同一平面上に設けられるこ
ととなる。
Reference numeral 7 denotes a radiating element, which is made of a spiral conductor attached to the surface of the lower insulating layer 5 corresponding to the opening 6.
Its outer end is connected to the end of the strip conductor 3 directly or via a capacitor in a high frequency manner. Therefore, the radiating element 7 and the strip conductor 3 are provided on the same plane.

【0013】図には、放射素子7をアルキメデス形渦巻
き状の導体で形成した場合を例示してあるが、等角渦巻
状の導体で形成してもよく、この場合には、渦巻き状導
体の外端をストリップ導体3に接続する他、内端を接続
することも可能である。以下、放射状素子7をアルキメ
デス形渦巻き状の導体で形成した場合について説明する
Although the figure shows an example in which the radiating element 7 is formed of an Archimedean spiral conductor, it may also be formed of an equiangular spiral conductor. In addition to connecting the outer end to the strip conductor 3, it is also possible to connect the inner end. Hereinafter, a case will be described in which the radial element 7 is formed of an Archimedean spiral conductor.

【0014】図には、上部絶縁層4及び下部絶縁層5を
固体より成る絶縁体で形成した場合を例示してあるが、
空気で置き換えてもよく、この場合には、適宜の絶縁体
より成るスペ−サによって、ストリップ導体3及び放射
素子7を所要位置に保持させるように形成する。
The figure shows an example in which the upper insulating layer 4 and the lower insulating layer 5 are formed of solid insulators, but
It may be replaced with air, in which case a spacer made of a suitable insulator is formed to hold the strip conductor 3 and the radiating element 7 in the required position.

【0015】8は遮蔽導体で、ストリップ導体3の端部
が開口部6内に対応する個所に突出したままの状態にし
ておくと、放射素子7からの円偏波放射に悪影響を及ぼ
すこととなるので、ストリップ導体3の突出部分の真上
を覆うように、上部ア−ス導体1と一体に設けてある。 遮蔽導体8を比較的幅の広い導体で形成し、その両側縁
を下方に折り曲げて、開口部6内に対応する個所に突出
しているストリップ導体3の上方のみならず両側方をも
覆うように形成してもよい。なお、放射素子7を等角渦
巻き状の導体で形成した場合には、その外端をストリッ
プ導体3の端部に接続するに当って、ストリップ導体3
の端部を開口部6内に対応する個所まで延長突出させる
ことなく接続することも可能であるから、このような場
合には、遮蔽導体8を設ける必要のないこと勿論である
Reference numeral 8 denotes a shielding conductor, and if the end of the strip conductor 3 is left protruding into the corresponding part of the opening 6, it will adversely affect the circularly polarized radiation from the radiating element 7. Therefore, it is provided integrally with the upper ground conductor 1 so as to cover directly above the protruding portion of the strip conductor 3. The shielding conductor 8 is formed of a relatively wide conductor, and both edges of the shielding conductor 8 are bent downward so as to cover not only the upper part of the strip conductor 3 protruding into the opening 6 but also both sides thereof. may be formed. Note that when the radiating element 7 is formed of a conductor in the form of an equiangular spiral, when connecting its outer end to the end of the strip conductor 3, the strip conductor 3
Since it is also possible to connect the end portions of the conductors without extending and projecting them to the corresponding locations within the opening 6, it is of course unnecessary to provide the shield conductor 8 in such a case.

【0016】上部絶縁層4及び下部絶縁層5を固体で形
成する場合における本発明アンテナを製作するに当って
は、例えばフイルム状の絶縁体の同一表面にプリント印
刷手法等によってストリップ導体3及び放射素子7を形
成する導体を付着させ、その表裏面に誘電体損失の少な
い発泡プラスチック、例えばポリエチレンフォ−ム又は
ウレタンフォ−ム等より成る薄膜を重ねて上部絶縁層4
及び下部絶縁層5を形成し、更に、表面に金属薄膜を付
着させたフイルム状の絶縁体を上部絶縁層4及び下部絶
縁層5の各表面に重ねて上部ア−ス導体1及び下部ア−
ス導体2を形成する。金属薄板にプレス加工又は放電加
工等を施して上部ア−ス導体1、下部ア−ス導体2、ス
トリップ導体3及び放射素子7を形成し、上部絶縁層4
及び下部絶縁層5を形成するフイルム状絶縁体と重ね合
わせるようにしてもよく、このようにして形成する場合
には、機械的な安定性を高めることができる。
When manufacturing the antenna of the present invention in which the upper insulating layer 4 and the lower insulating layer 5 are formed of a solid material, the strip conductor 3 and the radiation are printed on the same surface of a film-like insulator, for example. The conductor forming the element 7 is attached, and a thin film made of foamed plastic with low dielectric loss, such as polyethylene foam or urethane foam, is overlaid on the front and back surfaces to form an upper insulating layer 4.
and a lower insulating layer 5 are formed, and a film-like insulator having a metal thin film adhered to the surface is layered on each surface of the upper insulating layer 4 and the lower insulating layer 5 to form an upper ground conductor 1 and a lower ground conductor 1.
A conductor 2 is formed. An upper ground conductor 1, a lower ground conductor 2, a strip conductor 3, and a radiating element 7 are formed by pressing or electrical discharge machining on a metal thin plate, and an upper insulating layer 4 is formed.
It may also be overlapped with the film-like insulator forming the lower insulating layer 5. When formed in this way, mechanical stability can be improved.

【0017】図には、放射素子7の渦巻き方向を、Z軸
(放射素子7の中心において放射素子7の面に垂直な軸
、なお、後述するY軸はトリプレ−ト伝送線路の長手方
向の軸、X軸はY軸に直角方向の軸とする)の周りに、
放射素子の内端から時計方向に旋回するように形成した
場合を例示してあるが、逆旋回をする渦巻き状の放射素
子を設けるようにしても本発明を実施することができる
In the figure, the spiral direction of the radiating element 7 is indicated by the Z axis (an axis perpendicular to the surface of the radiating element 7 at the center of the radiating element 7; the Y axis, which will be described later, is the longitudinal direction of the triple plate transmission line). around the axis, the X-axis is perpendicular to the Y-axis),
Although a case is illustrated in which the radiating element is formed to rotate clockwise from the inner end, the present invention can also be practiced by providing a spiral radiating element that rotates in the opposite direction.

【0018】開口部6の周壁の延長周面に、リング状の
導体を設け、その上縁を上部ア−ス導体1に接続し、下
縁を下部ア−ス導体2に接続すると共に、リング状の導
体のうち、ストリップ導体3が開口部6内に対応する個
所に導出される部分に孔隙を穿ち、リング状の導体とス
トリップ導体3とが接触することのないように形成して
、ストリップ導体3からの給電を妨げることなく、放射
素子7からの放射電磁波が上部絶縁層4及び下部絶縁層
5内に漏洩伝搬するのを防ぐように構成してもよい。
A ring-shaped conductor is provided on the extended circumferential surface of the peripheral wall of the opening 6, and its upper edge is connected to the upper ground conductor 1 and its lower edge is connected to the lower ground conductor 2. A hole is bored in the part of the conductor in the shape of a ring where the strip conductor 3 is led out to the corresponding part in the opening 6, and the ring-shaped conductor and the strip conductor 3 are formed so as not to come into contact with each other. It may be configured to prevent the electromagnetic waves radiated from the radiating element 7 from leaking and propagating into the upper insulating layer 4 and the lower insulating layer 5 without interfering with power feeding from the conductor 3.

【0019】開口部6の周壁の延長周面に、リング状の
導体を設ける代りに、開口部6の外周部分を形成する上
部ア−ス導体1の部分に、包絡線が開口部6の外周とほ
ぼ同心円を成すように、円周方向に適宜間隔を隔てて適
宜数のスル−ホ−ルを穿つと共に、これらのスル−ホ−
ルを穿った個所に対応する下部ア−ス導体2の部分に同
様のスル−ホ−ルを穿ち、上下の各対応するスル−ホ−
ル相互を棒状又は線状の導体で接続して遮蔽体を形成し
てもよい。
Instead of providing a ring-shaped conductor on the extended peripheral surface of the peripheral wall of the opening 6, an envelope line is formed on the portion of the upper ground conductor 1 forming the outer peripheral portion of the opening 6. An appropriate number of through holes are bored at appropriate intervals in the circumferential direction so as to form approximately concentric circles, and these through holes are
Drill a similar through hole in the part of the lower ground conductor 2 corresponding to the location where the hole was drilled, and connect the upper and lower corresponding through holes.
The shielding body may be formed by connecting the wires with each other with a rod-shaped or wire-shaped conductor.

【0020】開口部6の円周の大きさについては、後述
するように、本発明アンテナを構成素子アンテナとして
アレ−アンテナを構成する場合、アレ−アンテナ全体を
大形化することなく、素子アンテナ相互の間隔を広く保
って、各素子アンテナの給電線の配設の自由度を確保し
ようとするためには、開口部6の円周の大きさをできる
だけ小さくすることが望ましいが、放射素子7から放射
される電磁波が広帯域に亙って減衰することなく開口部
6を通過し得るようにするためには、開口部6の円周を
、放射素子7の最外円周より適宜大となるように定める
ことが望ましい。
Regarding the size of the circumference of the opening 6, as will be described later, when an array antenna is constructed using the antenna of the present invention as a component antenna, the size of the element antenna can be reduced without increasing the size of the entire array antenna. In order to maintain a wide mutual spacing and to ensure flexibility in arranging the feeder lines of each element antenna, it is desirable to make the circumference of the opening 6 as small as possible. In order to allow the electromagnetic waves radiated from the aperture 6 to pass through the aperture 6 without being attenuated over a wide band, the circumference of the aperture 6 should be appropriately larger than the outermost circumference of the radiating element 7. It is desirable to define it as follows.

【0021】渦巻き状放射素子7の長さ及び幅は、トリ
プレ−ト伝送線路によって給電された高周波電流が放射
素子7において進行波分布となって、円偏波を放射し得
るように適宜調整する必要があるが、この調整は、トリ
プレ−ト伝送線路における上部ア−ス導体1及び下部ア
−ス導体2の間隔、上部絶縁層4及び下部絶縁層5を形
成する誘電体の電気的物性及び開口部6の開口の大きさ
等によって左右されるが、放射素子7のほぼ中心から内
端までの距離と、放射素子のほぼ中心から外端までの距
離との和に、円周率πを乗じた長さに等しい円周(以下
、仮想円周と称する)が、近似的に使用周波数のほぼ1
波長(自由空間波長、λ)の整数倍となる仮想円周の範
囲内で調整可能である。
The length and width of the spiral radiating element 7 are appropriately adjusted so that the high frequency current fed by the triple plate transmission line becomes a traveling wave distribution in the radiating element 7 and radiates circularly polarized waves. This adjustment is necessary, but this adjustment depends on the distance between the upper ground conductor 1 and the lower ground conductor 2 in the triple plate transmission line, the electrical properties of the dielectric material forming the upper insulating layer 4 and the lower insulating layer 5, and Although it depends on the size of the aperture 6, etc., the circumference ratio π is calculated as the sum of the distance from the approximate center of the radiating element 7 to the inner end and the distance from the approximate center to the outer end of the radiating element. The circumference equal to the multiplied length (hereinafter referred to as virtual circumference) is approximately 1 of the frequency used.
Adjustment is possible within the range of a virtual circumference that is an integral multiple of the wavelength (free space wavelength, λ).

【0022】本発明アンテナにおいて、例えば、上部絶
縁層4及び下部絶縁層5を形成する誘電体の比誘電率を
1.0 とし、渦巻き状放射素子7の動径関数  γ=
aφ−Δ(aは渦巻き定数、φは渦巻きの始点からの角
度、Δは始点定数)において、 渦巻き定数aが、0.19mm/rad始点定数Δが、
  0.86mm φの範囲が、  6.72π(rad) ≦φ≦10π
(rad)開口部6の半径Rが、8.19mm となるように形成した場合、使用周波数が、11.85
GHzにおける本発明アンテナの指向特性は、図2及び
図3に示すとおりである。
In the antenna of the present invention, for example, assuming that the dielectric constant of the dielectric material forming the upper insulating layer 4 and the lower insulating layer 5 is 1.0, the radial function of the spiral radiating element 7 is γ=
In aφ-Δ (a is the spiral constant, φ is the angle from the starting point of the spiral, and Δ is the starting point constant), the spiral constant a is 0.19 mm/rad, and the starting point constant Δ is,
The range of 0.86mm φ is 6.72π (rad) ≦φ≦10π
(rad) When the radius R of the opening 6 is formed to be 8.19 mm, the operating frequency is 11.85 mm.
The directional characteristics of the antenna of the present invention at GHz are as shown in FIGS. 2 and 3.

【0023】図2は、Z−X面における指向特性で、指
向特性の半値幅(ビ−ム幅)76°、図3は、Z−Y面
における指向特性で、指向特性の半値幅(ビ−ム幅)7
8°である。直交する2平面、すなわち、Z−X面及び
Z−Y面における各半値幅がそれぞれ76°及び78°
で、ほぼ一致しているから、本発明アンテナを素子アン
テナとしてアレ−アンテナを構成するに当って、X方向
及びY方向の素子アンテナ間隔を同一にすることができ
、アレ−アンテナの設計製作が容易である。
FIG. 2 shows the directional characteristic in the Z-X plane, where the half-width (beam width) of the directional characteristic is 76°. FIG. 3 shows the directional characteristic in the Z-Y plane, where the half-width (beam width) of the directional characteristic is 76°. - width) 7
It is 8°. The half widths in two perpendicular planes, that is, the Z-X plane and the Z-Y plane, are 76° and 78°, respectively.
Since they almost match, when configuring an array antenna using the antenna of the present invention as an element antenna, the element antenna spacing in the X direction and Y direction can be made the same, and the design and manufacture of the array antenna can be simplified. It's easy.

【0024】図4は、本発明アンテナにおける反射減衰
量の一例を示す曲線図で、横軸は使用周波数f(GHz
) 、縦軸は反射減衰量RL(dB)である。図5は、
本発明アンテナの軸比の一例を示す曲線図で、横軸は使
用周波数f(GHz) 、縦軸は軸比AR(dB)であ
る。アンテナにおける反射減衰量及び軸比は、円偏波の
電波を如何に効率よく受信し得るかのパラメ−タである
が、図4及び図5から明らかなように、本発明アンテナ
は、反射減衰量及び軸比のいずれにおいても我が国の衛
星放送に使用される周波数帯域11.7GHz ないし
12.0GHz において極めて良好な特性を有する。
FIG. 4 is a curve diagram showing an example of return loss in the antenna of the present invention, and the horizontal axis represents the operating frequency f (GHz
), the vertical axis is the return loss RL (dB). Figure 5 shows
1 is a curve diagram showing an example of the axial ratio of the antenna of the present invention, where the horizontal axis is the operating frequency f (GHz), and the vertical axis is the axial ratio AR (dB). The return loss and axial ratio of an antenna are parameters that determine how efficiently circularly polarized radio waves can be received.As is clear from FIGS. 4 and 5, the antenna of the present invention has a Both in terms of quantity and axial ratio, it has extremely good characteristics in the frequency band of 11.7 GHz to 12.0 GHz used for satellite broadcasting in Japan.

【0025】以上は、放射素子7の仮想円周をほぼ1波
長とした場合について説明したが、仮想円周がほぼ2波
長となるように放射素子の長さを選んだ場合にも放射素
子上の電流分布を進行波分布とすることができ、開口部
6の円周を、ほぼ1波長の2倍に選んだ仮想円周より適
宜大きくすることによって、Z−X面及びZ−Y面にお
いて双方向性の指向特性を持たせることができる。
The above description has been made for the case where the virtual circumference of the radiating element 7 is approximately one wavelength, but even if the length of the radiating element is selected so that the virtual circumference is approximately two wavelengths, the radiating element The current distribution can be made into a traveling wave distribution, and by appropriately making the circumference of the aperture 6 larger than the virtual circumference selected to be approximately twice one wavelength, the current distribution can be made into a traveling wave distribution. It can have bidirectional directional characteristics.

【0026】放射素子7の仮想円周をほぼ1波長の任意
の整数倍に選ぶと共に、仮想円周の大きさに応じて開口
部の大きさを適宜大きくすることによって、円偏波にお
ける指向特性を種々変化させることができる。これらの
指向特性は、1周任意波長の進行波電流が流れるル−プ
アンテナに置き換えることによって、仮想円周の大きさ
と指向特性の関係を容易に判断し得るので、使用目的に
応じて仮想円周の大きさを1波長の何倍とするかを定め
ると共に、開口部の大きさを仮想円周の大きさより適宜
大きくすることによって目的を達することができる。
By selecting the virtual circumference of the radiating element 7 to be an arbitrary integer multiple of approximately one wavelength and appropriately increasing the size of the aperture according to the size of the virtual circumference, the directivity characteristics in circularly polarized waves can be improved. can be varied in various ways. These directional characteristics can be easily determined by replacing the antenna with a loop antenna through which a traveling wave current of an arbitrary wavelength flows for one round, and the relationship between the size of the virtual circumference and the directional characteristics. The purpose can be achieved by determining how many times the size of one wavelength is to be made and by making the size of the aperture appropriately larger than the size of the virtual circumference.

【0027】図6の(a)は、仮想円周がほぼ1波長の
場合の或る時間における進行波電流の最大値を矢印を付
した実線で示し、図6の(b)は、その単一方向性の指
向特性を示し、図7の(a)は、仮想円周がほぼ2波長
の場合の或る時間における進行波電流の最大値を矢印を
付した実線で示し、図7の(b)は、その双方向性の指
向特性を示す。
FIG. 6(a) shows the maximum value of the traveling wave current at a certain time when the virtual circumference is approximately one wavelength, and FIG. 6(b) shows the maximum value of the traveling wave current at a certain time by a solid line with an arrow. Figure 7(a) shows the maximum value of the traveling wave current at a certain time when the virtual circumference is approximately two wavelengths, as a solid line with an arrow. b) shows its bidirectional directional characteristics.

【0028】図8は、上記本発明アンテナを素子アンテ
ナとして構成したアレ−アンテナの一例を示す平面概略
図で、9ないし12は本発明アンテナより成る素子アン
テナで、図には4個の素子アンテナの各中心を同一線上
に一列に配設した場合を例示してあるが、適宜増減して
アレ−アンテナを構成することができる。破線はトリプ
レ−ト伝送線路を構成する内部導体で、各素子アンテナ
を並列的に励振する。素子アンテナを複数個配設した場
合、素子アンテナ相互間の結合等の影響を受けるため、
各素子アンテナにおける渦巻き状導体より成る放射素子
の仮想円周長を適宜調整して最適値を求める必要がある
FIG. 8 is a schematic plan view showing an example of an array antenna in which the antenna of the present invention is constructed as an element antenna. Numerals 9 to 12 are element antennas made of the antenna of the present invention, and the figure shows four element antennas. Although the example is shown in which the centers of the antennas are arranged in a row on the same line, the array antenna can be constructed by increasing or decreasing the number of antennas as appropriate. The broken line is an internal conductor constituting a triplate transmission line, which excites each element antenna in parallel. When multiple element antennas are installed, they are affected by coupling between the element antennas, so
It is necessary to appropriately adjust the virtual circumference length of the radiating element made of the spiral conductor in each element antenna to find an optimum value.

【0029】図9ないし図12は、図8に示したアレ−
アンテナの各種特性を示す図で、各図のデ−タは、図8
における素子アンテナの中心間隔を、使用周波数11.
85GHzにおいて 0.9λに選定した場合のもので
あり、図9及び図10における座標軸は、図8における
素子アンテナ10及び11の中心間隔の中心点から放射
面に垂直な方向をZ軸、素子アンテナの各中心を連ねる
線の方向をX軸、Z軸及びX軸に各直角な方向をY軸と
する。
FIGS. 9 to 12 show the array shown in FIG.
This is a diagram showing various characteristics of the antenna, and the data for each diagram is shown in Figure 8.
The center spacing of the element antennas at the working frequency 11.
The coordinate axes in FIGS. 9 and 10 are the Z-axis in the direction perpendicular to the radiation surface from the center point of the center spacing between the element antennas 10 and 11 in FIG. The direction of the line connecting the centers of is the X-axis, the Z-axis, and the direction perpendicular to the X-axis is the Y-axis.

【0030】図9は、図8に示したアレ−アンテナのZ
−X面における指向特性、図10は、Z−Y面における
指向特性で、Z−X面においては、本発明アンテナ単独
の場合の指向特性における半値幅76°に対して図8に
示したアレ−アンテナにおいては14°と極めて鋭くな
り、高利得化されている。又、広角に対する軸比特性も
本発明アンテナ単独の場合に比し損なわれていない。
FIG. 9 shows the Z angle of the array antenna shown in FIG.
- Directional characteristics in the X plane, FIG. 10 shows the directivity characteristics in the Z-Y plane, and in the Z-X plane, the array shown in FIG. -The antenna is extremely sharp at 14 degrees and has a high gain. Furthermore, the axial ratio characteristics for wide angles are not impaired compared to the case of using only the antenna of the present invention.

【0031】図11は、図8に示したアレ−アンテナに
おける反射減衰量を示す曲線図で、横軸は使用周波数f
(GHz) 、縦軸は反射減衰量RL(dB)である。 図8に示したアレ−アンテナにおいては、周波数ほぼ1
1.55GHzないし12.3GHzに亙って電圧定在
波比(VSWR)が1.5 以下で、良好である。
FIG. 11 is a curve diagram showing the return loss in the array antenna shown in FIG. 8, and the horizontal axis represents the operating frequency f.
(GHz), and the vertical axis is the return loss RL (dB). In the array antenna shown in Fig. 8, the frequency is approximately 1
The voltage standing wave ratio (VSWR) is 1.5 or less from 1.55 GHz to 12.3 GHz, which is good.

【0032】図12は、図8に示したアレ−アンテナに
おけるZ軸方向の軸比特性を示す曲線図で、周波数ほぼ
11.5GHz ないし12.1GHz に亙って3d
b以下の良好な円偏波特性を呈している。
FIG. 12 is a curve diagram showing the axial ratio characteristics in the Z-axis direction of the array antenna shown in FIG.
It exhibits good circular polarization characteristics of less than b.

【0033】図8には、共通の上部ア−ス導体に4個の
開口部を設け、上部絶縁層、下部絶縁層及び下部ア−ス
導体も共通に形成し、各開口部に対応して放射素子を配
設し、共通の上部絶縁層と下部絶縁層との間に、各放射
素子の並列励振用ストリップ導体を配設してアレ−アン
テナを構成した場合を例示したが、各独立に形成した本
発明アンテナを素子アンテナとして同一又はほぼ同一平
面上に配設し、各素子アンテナに給電線を外付けしてア
レ−アンテナを構成してもよい。
In FIG. 8, four openings are provided in a common upper ground conductor, an upper insulating layer, a lower insulating layer, and a lower ground conductor are also formed in common, and a hole is formed corresponding to each opening. An example is shown in which an array antenna is constructed by arranging radiating elements and arranging strip conductors for parallel excitation of each radiating element between a common upper insulating layer and a lower insulating layer. The formed antenna of the present invention may be arranged as element antennas on the same or substantially the same plane, and a feeder line may be externally attached to each element antenna to form an array antenna.

【0034】以上は、給電線をトリプレ−ト伝送線路で
形成した場合について説明したが、サスペンデット伝送
線路で給電線を形成した場合にも全く同様にして本発明
を実施することができる。
Although the above description has been made of the case where the feeder line is formed by a triple-plate transmission line, the present invention can be carried out in exactly the same way even when the feeder line is formed by a suspended transmission line.

【0035】[0035]

【発明の効果】本発明アンテナは、トリプレ−ト伝送線
路又はサスペンデット伝送線路のように、本来損失の少
ない伝送線路を給電線として用い、その一部に簡単な加
工を施すことによって放射素子の取付けが可能なばかり
でなく、放射素子と給電線との結合構造が、従来に比し
遥かに簡潔で、製作が容易であるから製作コストが低く
、又、図2ないし図5に示したように指向特性及び軸比
特性の優れたもので、このアンテナを構成素子とするア
レ−アンテナは、例えば円偏波を用いる衛星放送受信用
アレ−アンテナとして極めて好適である。
[Effects of the Invention] The antenna of the present invention uses a transmission line that inherently has low loss, such as a triple-plate transmission line or a suspended transmission line, as a feed line, and attaches a radiating element by performing simple processing on a part of the transmission line. Not only is this possible, but the coupling structure between the radiating element and the feeder line is much simpler and easier to manufacture than in the past, so the manufacturing cost is low. It has excellent directivity characteristics and axial ratio characteristics, and an array antenna having this antenna as a component is extremely suitable, for example, as an array antenna for receiving satellite broadcasting using circularly polarized waves.

【図面の簡単な説明】[Brief explanation of the drawing]

【図1】(a)は、本発明の一実施例を示す平面図であ
る。 (b)は、本発明の一実施例を示す断面図である。
FIG. 1(a) is a plan view showing an embodiment of the present invention. (b) is a sectional view showing one embodiment of the present invention.

【図2】本発明アンテナの指向特性の一例を示す図であ
る。
FIG. 2 is a diagram showing an example of the directivity characteristics of the antenna of the present invention.

【図3】本発明アンテナの指向特性の一例を示す図であ
る。
FIG. 3 is a diagram showing an example of the directivity characteristics of the antenna of the present invention.

【図4】本発明アンテナの反射減衰特性の一例を示す図
である。
FIG. 4 is a diagram showing an example of return loss characteristics of the antenna of the present invention.

【図5】本発明アンテナの軸比特性の一例を示す図であ
る。
FIG. 5 is a diagram showing an example of the axial ratio characteristic of the antenna of the present invention.

【図6】(a)は、本発明アンテナの動作説明のための
図である。 (b)は、本発明アンテナの指向特性の一例を示す図で
ある。
FIG. 6(a) is a diagram for explaining the operation of the antenna of the present invention. (b) is a diagram showing an example of the directional characteristics of the antenna of the present invention.

【図7】(a)は、本発明アンテナの動作説明のための
図である。 (b)は、本発明アンテナの指向特性の一例を示す図で
ある。
FIG. 7(a) is a diagram for explaining the operation of the antenna of the present invention. (b) is a diagram showing an example of the directional characteristics of the antenna of the present invention.

【図8】本発明アンテナを素子とするアレ−アンテナの
一例を示す図である。
FIG. 8 is a diagram showing an example of an array antenna using the antenna of the present invention as an element.

【図9】本発明アンテナを素子とするアレ−アンテナの
指向特性の一例を示す図である。
FIG. 9 is a diagram showing an example of the directivity characteristics of an array antenna using the antenna of the present invention as an element.

【図10】本発明アンテナを素子とするアレ−アンテナ
の指向特性の一例を示す図である。
FIG. 10 is a diagram showing an example of the directivity characteristics of an array antenna using the antenna of the present invention as an element.

【図11】本発明アンテナを素子とするアレ−アンテナ
の反射減衰特性の一例を示す図である。
FIG. 11 is a diagram showing an example of return loss characteristics of an array antenna using the antenna of the present invention as an element.

【図12】本発明アンテナを素子とするアレ−アンテナ
の軸比特性の一例を示す図である。
FIG. 12 is a diagram showing an example of the axial ratio characteristic of an array antenna using the antenna of the present invention as an element.

【符号の説明】[Explanation of symbols]

1    上部外部導体 2    下部外部導体 3    内部導体 4    上部絶縁層 5    下部絶縁層 6    開口部 7    放射素子 8    遮蔽導体 9    本発明アンテナ 10  本発明アンテナ 11  本発明アンテナ 12  本発明アンテナ 1 Upper outer conductor 2 Lower external conductor 3. Internal conductor 4 Upper insulating layer 5 Lower insulating layer 6 Opening 7 Radiating element 8 Shielded conductor 9. Antenna of the present invention 10 Antenna of the present invention 11 Antenna of the present invention 12 Antenna of the present invention

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】上部外部導体と下部外部導体との間に介在
する上部絶縁層及び下部絶縁層と、前記上部外部導体の
一部適宜範囲を除去して形成した開口部と、この開口部
に対応する前記上部絶縁層と下部絶縁層との間に設けた
渦巻き状導体より成る放射素子と、前記上部絶縁層と下
部絶縁層との間に介在させると共に、前記渦巻き状導体
より成る放射素子に高周波的に接続した内部導体とを備
えたことを特徴とする渦巻きアンテナ。
1. An upper insulating layer and a lower insulating layer interposed between an upper external conductor and a lower external conductor, an opening formed by removing a portion of the upper external conductor, and an opening formed in the opening. A radiating element made of a spiral conductor provided between the corresponding upper insulating layer and lower insulating layer; and a radiating element interposed between the upper insulating layer and the lower insulating layer and made of the spiral conductor. A spiral antenna characterized by comprising an internal conductor connected in a high frequency manner.
【請求項2】渦巻き状導体より成る放射素子のほぼ中心
から渦巻き状導体の巻き始めまでの距離と、渦巻き状導
体より成る放射素子のほぼ中心から渦巻き状導体の巻き
終りまでの距離との和に円周率を乗じた値を、使用電磁
波のほぼ1波長の整数倍に近似させて成る請求項1に記
載の渦巻きアンテナ。
Claim 2: The sum of the distance from approximately the center of a radiating element made of a spiral conductor to the start of winding of the spiral conductor, and the distance from approximately the center of the radiating element comprised of a spiral conductor to the end of winding of the spiral conductor. 2. The spiral antenna according to claim 1, wherein a value obtained by multiplying by a circumference is approximately an integral multiple of one wavelength of the electromagnetic wave used.
【請求項3】内部導体との高周波的接続個所が、渦巻き
状導体より成る放射素子の外端である請求項1に記載の
渦巻きアンテナ。
3. The spiral antenna according to claim 1, wherein the high-frequency connection point with the internal conductor is an outer end of the radiating element made of the spiral conductor.
【請求項4】内部導体の配設個所を除いて、開口部の周
辺に対応する下部外部導体部分と上部外部導体部分間に
電磁的遮蔽体を設けて成る請求項1に記載の渦巻きアン
テナ。
4. The spiral antenna according to claim 1, wherein an electromagnetic shield is provided between the lower outer conductor portion and the upper outer conductor portion corresponding to the periphery of the opening except for the location where the inner conductor is disposed.
【請求項5】上部絶縁層及び下部絶縁層が固体より成る
請求項1に記載の渦巻きアンテナ。
5. The spiral antenna according to claim 1, wherein the upper insulating layer and the lower insulating layer are made of solid material.
【請求項6】上部絶縁層及び下部絶縁層が空気より成り
、渦巻き状導体より成る放射素子及び内部導体を、絶縁
体より成るスペ−サによって所要位置に保持させて成る
請求項1に記載の渦巻きアンテナ。
6. The device according to claim 1, wherein the upper insulating layer and the lower insulating layer are made of air, and the radiating element and the inner conductor made of a spiral conductor are held in a predetermined position by a spacer made of an insulator. spiral antenna.
【請求項7】上部外部導体と下部外部導体との間に介在
する上部絶縁層及び下部絶縁層と、前記上部外部導体の
一部適宜範囲を除去して形成した開口部と、この開口部
に対応する前記上部絶縁層と下部絶縁層との間に設けた
渦巻き状導体より成る放射素子と、前記上部絶縁層と下
部絶縁層との間に介在させると共に、前記渦巻き状導体
より成る放射素子に高周波的に接続した内部導体とを備
えて成る渦巻きアンテナを、同一平面上に適宜数配設し
て成ることを特徴とするアレ−アンテナ。
7. An upper insulating layer and a lower insulating layer interposed between an upper external conductor and a lower external conductor, an opening formed by removing a portion of the upper external conductor, and an opening formed in the opening. A radiating element made of a spiral conductor provided between the corresponding upper insulating layer and lower insulating layer; and a radiating element interposed between the upper insulating layer and the lower insulating layer and made of the spiral conductor. 1. An array antenna comprising an appropriate number of spiral antennas each having a high-frequency connected internal conductor arranged on the same plane.
JP06882791A 1991-03-09 1991-03-09 Spiral antenna and array antenna using this antenna Expired - Fee Related JP3187853B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP06882791A JP3187853B2 (en) 1991-03-09 1991-03-09 Spiral antenna and array antenna using this antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP06882791A JP3187853B2 (en) 1991-03-09 1991-03-09 Spiral antenna and array antenna using this antenna

Publications (2)

Publication Number Publication Date
JPH04281604A true JPH04281604A (en) 1992-10-07
JP3187853B2 JP3187853B2 (en) 2001-07-16

Family

ID=13384931

Family Applications (1)

Application Number Title Priority Date Filing Date
JP06882791A Expired - Fee Related JP3187853B2 (en) 1991-03-09 1991-03-09 Spiral antenna and array antenna using this antenna

Country Status (1)

Country Link
JP (1) JP3187853B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997033341A1 (en) * 1996-03-08 1997-09-12 Nippon Antena Kabushiki Kaisha Single-wire spiral antenna
KR100429410B1 (en) * 2001-08-27 2004-04-29 박익모 Microstrip Spiral Antenna with a Circular Slot on the Ground Plane
DE102021124938A1 (en) 2020-09-28 2022-03-31 Faverights, Inc. SUBSTRATE-TYPE ANTENNA FOR A GLOBAL NAVIGATION-SATELLITE SYSTEM

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997033341A1 (en) * 1996-03-08 1997-09-12 Nippon Antena Kabushiki Kaisha Single-wire spiral antenna
US6018327A (en) * 1996-03-08 2000-01-25 Nippon Antena Kabushiki Kaisha Single-wire spiral antenna
KR100429410B1 (en) * 2001-08-27 2004-04-29 박익모 Microstrip Spiral Antenna with a Circular Slot on the Ground Plane
DE102021124938A1 (en) 2020-09-28 2022-03-31 Faverights, Inc. SUBSTRATE-TYPE ANTENNA FOR A GLOBAL NAVIGATION-SATELLITE SYSTEM
US11581649B2 (en) 2020-09-28 2023-02-14 Nissei Limited Substrate-type antenna for global navigation satellite system

Also Published As

Publication number Publication date
JP3187853B2 (en) 2001-07-16

Similar Documents

Publication Publication Date Title
ES2289826T3 (en) DIELECTRIC RESONATOR ANTENNA WITH CIRCULAR POLARIZATION.
JP3189735B2 (en) Helical antenna
US6414647B1 (en) Slender omni-directional, broad-band, high efficiency, dual-polarized slot/dipole antenna element
EP2917963B1 (en) Dual polarization current loop radiator with integrated balun
US6018327A (en) Single-wire spiral antenna
JP7168752B2 (en) slotted patch antenna
JPH0453322B2 (en)
JPH08195617A (en) Circularly polarized wave loop antenna
US4555708A (en) Dipole ring array antenna for circularly polarized pattern
EP0824766A1 (en) Antenna unit
KR101557291B1 (en) Quadrifilar Helix Antenna
US6121936A (en) Conformable, integrated antenna structure providing multiple radiating apertures
JP3452971B2 (en) Polarization variable antenna
JPH07336133A (en) Antenna device
JP2004048369A (en) Composite antenna
JP2005117493A (en) Frequency sharing omnidirectional antenna and array antenna
JPH04281604A (en) Spiral antenna and array antenna using the spiral antenna
JP2025539368A (en) Slot-fed patch antenna for GNSS applications
JP3304019B2 (en) ARRAY ANTENNA, RECEIVER HAVING THE SAME, AND METHOD OF DETERMINING DIRECTIVITY CHARACTERISTICS IN ARRAY ANTENNA
US5877729A (en) Wide-beam high gain base station communications antenna
JP2591806B2 (en) Microstrip array antenna
JP3341292B2 (en) Dual-polarized radial line slot antenna
JP2606139Y2 (en) Dual frequency antenna device
JP3510961B2 (en) Wide-angle circularly polarized antenna
JPH05267930A (en) Vertical/horizontal polarized wave shared plane antenna

Legal Events

Date Code Title Description
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20010424

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees