JPH0629714A - Helical antenna for satellite communication - Google Patents

Helical antenna for satellite communication

Info

Publication number
JPH0629714A
JPH0629714A JP17853992A JP17853992A JPH0629714A JP H0629714 A JPH0629714 A JP H0629714A JP 17853992 A JP17853992 A JP 17853992A JP 17853992 A JP17853992 A JP 17853992A JP H0629714 A JPH0629714 A JP H0629714A
Authority
JP
Japan
Prior art keywords
rod
shaped base
satellite communication
winding
support members
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
JP17853992A
Other languages
Japanese (ja)
Other versions
JP3317522B2 (en
Inventor
Yoshimi Egashira
良水 江頭
Moriyoshi Kawasaki
守良 河崎
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.)
Harada Industry Co Ltd
Original Assignee
Harada Industry 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 Harada Industry Co Ltd filed Critical Harada Industry Co Ltd
Priority to JP17853992A priority Critical patent/JP3317522B2/en
Publication of JPH0629714A publication Critical patent/JPH0629714A/en
Application granted granted Critical
Publication of JP3317522B2 publication Critical patent/JP3317522B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE:To provide a helical antenna for satellite communication having high quality around which helical coils different by winding directions, pitches, and modes are wound with the spool of the same type and which eliminates the influence of the dielectric forming the spool upon the antenna characteristics and is produced with the less man-hour in winding and a low cost and does not generate bending parts or the like in helical coils. CONSTITUTION:First and second groove groups 13a and 13b are formed in the symmetrical positions of respective front end edge parts of first and second supporting members 12a and 12b facing each other in the positions different by 180 deg. out of first to fourth supporting members 12a to 12d, which are provided on the outer peripheral surface of a bar-shaped base body 11 so that they are present on two planes which include the central axis of the bar-shaped base body 11 and are intersected orthogonally with each other, with a prescribed pitch, and third and fourth groove groups 13c and 13d are formed in the symmetrical positions of respective front end edge parts of third and fourth supporting members 12c and 12d facing each other in positions, which are shifted from first and second supporting members by 90 deg. and are different by 90 deg., with a prescribed pitch in the states shifted from first and second groove groups by 1/2 pitch.

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、筒状または柱状をなす
絶縁部材からなる巻き枠に、導線を螺旋状に巻回してな
る衛星通信用ヘリカルアンテナに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a helical antenna for satellite communication in which a conductor is spirally wound around a winding frame made of a cylindrical or columnar insulating member.

【0002】[0002]

【従来の技術】従来のこの種の衛星通信用ヘリカルアン
テナとしては、誘電体からなる肉厚寸法の比較的大きな
円筒状の巻き枠の外周面に螺旋状の溝を形成し、この螺
旋状の溝の中に導線を巻き込んでヘリカルコイルとした
ものがある。
2. Description of the Related Art As a conventional helical antenna for satellite communication of this kind, a spiral groove is formed on the outer peripheral surface of a cylindrical winding frame made of a dielectric material and having a relatively large wall thickness. There is a helical coil in which a conductor wire is wound in the groove.

【0003】また実開平3ー32811号に開示されて
いるように、円筒の外周面に複数の矩形状リブを放射状
に設け、これらの各リブの端縁部に螺旋素子挿通用の貫
通穴を設け、これらの貫通穴に予めコイル状に成形した
螺旋素子(ヘリカルコイル)を、その端部から順次ねじ
込むことによって取り付けたヘリカルアンテナが知られ
ている。
Further, as disclosed in Japanese Utility Model Laid-Open No. 3-32811, a plurality of rectangular ribs are radially provided on the outer peripheral surface of a cylinder, and through holes for inserting a spiral element are formed at the end portions of these ribs. A helical antenna is known in which a spiral element (helical coil) which is provided in these through-holes and which is formed in a coil shape in advance is sequentially screwed in from its end portion.

【0004】[0004]

【発明が解決しようとする課題】前者は巻き枠の外周面
に形成した螺旋状の溝により、ヘリカルコイルの巻線ピ
ッチが特定されるため、同じ型式の巻き枠を用いて異な
るピッチのヘリカルコイルを巻装することは不可能であ
る。勿論、異なる巻き方向のヘリカルコイルを巻装する
ことも不可能である。またヘリカルコイルが、所定誘電
率を有する誘電体からなる巻き枠内に埋没した状態で巻
装されるため、上記誘電体の誘電率がアンテナ特性に対
し少なからず影響を与える。
In the former case, since the winding pitch of the helical coil is specified by the spiral groove formed on the outer peripheral surface of the winding frame, the helical coil of the same type is used and the helical coil of different pitch is used. It is impossible to wind up. Of course, it is impossible to wind helical coils in different winding directions. Further, since the helical coil is wound in a winding frame made of a dielectric having a predetermined permittivity, the helical permittivity of the dielectric has a considerable influence on the antenna characteristics.

【0005】また後者は矩形状リブの端縁部に形成した
螺旋素子挿通用の貫通穴に対し、予めコイル状に成形し
た螺旋素子(ヘリカルコイル)を、その端部から順次ね
じ込むことによって取り付けるものであるため、巻線工
数が非常に大きく、コスト高になる欠点を有している。
また貫通穴に対する螺旋素子(ヘリカルコイル)の挿通
のさせ方如何によっては、ヘリカルコイルに部分的な屈
曲部ないし歪みが発生する。このため完成後のヘリカル
コイルの態様に大きなバラツキが生じ、品質を低下させ
るおそれがある。
In the latter case, a spiral element (helical coil) formed in a coil shape in advance is attached to a through hole for inserting a spiral element formed at an end portion of a rectangular rib by sequentially screwing the spiral element from the end portion. Therefore, there is a drawback that the number of winding steps is very large and the cost is high.
Further, depending on how the spiral element (helical coil) is inserted into the through hole, a partial bending portion or distortion is generated in the helical coil. For this reason, there is a possibility that a large variation will occur in the form of the helical coil after completion and the quality will be deteriorated.

【0006】そこで本発明は、同じ型式の巻き枠を用い
て、異なる巻き方向およびピッチおよび態様を有するヘ
リカルコイルを巻装することが可能である上、巻き枠を
形成している誘電体によるアンテナ特性への影響が殆ど
無く、巻線の作業性が著しく良く、巻線工数が少なくて
済み、低コストで製作可能である上、ヘリカルコイルに
部分的な屈曲部ないし歪みを発生させずに済み、高品質
な衛星通信用ヘリカルアンテナを提供することを目的と
する。
Therefore, the present invention is capable of winding helical coils having different winding directions, pitches, and modes using the same type of reel, and further, the antenna made of a dielectric material forming the reel. There is almost no effect on the characteristics, the workability of the winding is remarkably good, the number of winding steps is small, it can be manufactured at low cost, and there is no need for partial bending or distortion of the helical coil. , To provide a high quality helical antenna for satellite communication.

【0007】[0007]

【課題を解決するための手段】上記の課題を解決し目的
を達成するために、本発明では次のような手段を講じ
た。すなわち、巻き枠に導線を螺旋状に巻回してなる衛
星通信用ヘリカルアンテナにおいて、筒状または柱状を
なす棒状基体の中心軸を含みかつ互いに直交する二平面
内にそれぞれが存在するように、上記棒状基体の外周面
の4個所に矩形板状をなす第1〜第4の支持部材を放射
状に突設し、これら第1〜第4の支持部材のうち互いに
180°異なる角度位置で相対向する第1,第2の支持
部材における各先端縁部の対称な位置に、導線係入用の
第1,第2の溝群を所定ピッチで形成し、前記第1,第
2の支持部材とは90°ずれた位置において互いに18
0°異なる角度位置で相対向する第3,第4の支持部材
における各先端縁部の対称な位置に、所定ピッチで且つ
前記第1,第2の溝群とは1/2ピッチ分ずれた状態に
導線係入用の第3,第4の溝群を形成してなる巻き枠を
備えるようにした。
[Means for Solving the Problems] In order to solve the above problems and achieve the object, the present invention takes the following means. That is, in a helical antenna for satellite communication in which a lead wire is spirally wound around a winding frame, the helical antenna for satellite communication includes the central axis of a rod-shaped base having a tubular shape or a columnar shape, and is present in two planes orthogonal to each other. Rectangular plate-shaped first to fourth support members are radially provided at four locations on the outer peripheral surface of the rod-shaped substrate, and the first to fourth support members are opposed to each other at angular positions different from each other by 180 °. The first and second support members are provided with first and second groove groups for engaging the lead wire at a predetermined pitch at symmetrical positions of the respective tip edge portions of the first and second support members. 18 at a position offset by 90 °
The tip edges of the third and fourth support members facing each other at an angle position different by 0 ° are symmetrically displaced from each other by a predetermined pitch and by a 1/2 pitch from the first and second groove groups. In this state, a winding frame formed by forming third and fourth groove groups for engaging the conducting wire is provided.

【0008】なお巻き枠としては、筒状または柱状をな
す複数の棒状基体の隣接する端面どうしが、軸回り方向
の特定角度位置で互いに連結可能な如く設けられている
ことが好ましい。さらに巻き枠としては、筒状または柱
状をなす棒状基体と、矩形板状をなす第1〜第4の支持
部材とが別体に形成され、上記棒状基体の外周に対し
て、上記第1〜第4の支持部材が着脱自在に設けられて
いることが好ましい。
It is preferable that the winding frame is provided so that adjacent end faces of a plurality of rod-shaped bases having a cylindrical or columnar shape can be connected to each other at a specific angular position in the axial direction. Further, as the winding frame, a cylindrical or columnar rod-shaped base body and rectangular plate-shaped first to fourth support members are separately formed, and the first to fourth support members are formed on the outer circumference of the rod-shaped base body. It is preferable that the fourth support member is detachably provided.

【0009】[0009]

【作用】上記手段を講じた結果、次のような作用が生じ
る。
As a result of taking the above-mentioned means, the following effects occur.

【0010】(1) 支持部材の各先端縁部にそれぞれ設け
られている導線係入用の各溝群は、右軸回り方向および
左軸回り方向のいずれの方向にみても、隣接する支持部
材間では、ヘリカルコイルの螺旋形状に対応するよう
に、順次1/2ピッチづつずれた状態を呈している。こ
のためヘリカルコイルの巻き方を、右巻きあるいは左巻
きに特定されずに済み、同じ型式の巻き枠を用いて、異
なる巻き方向のヘリカルコイルを任意に巻装することが
可能となる。
(1) The guide wire engaging groove groups provided at the respective leading edge portions of the supporting member are adjacent to each other in both the right axis direction and the left axis direction. In the interval, the helical coils are in a state of being sequentially displaced by 1/2 pitch so as to correspond to the spiral shape of the helical coil. Therefore, the winding method of the helical coil is not limited to right-handed winding or left-handed winding, and it is possible to arbitrarily wind helical coils in different winding directions using the same type of winding frame.

【0011】(2) 導線を巻き付ける際、導線係入用の各
溝群におけるどの溝に巻き付けるかは、所期の目的に応
じて任意に選択し得る事項である。したがって、導線巻
き付け時に選択使用する溝の選択状況の如何によって
は、巻線ピッチ等を適宜変更することが可能となる。こ
のため同じ型式の巻き枠を用いて、ヘリカルコイルを異
なるピッチに巻装することも、また異なる態様で巻装す
ることも可能である。
(2) When winding the conductor wire, which groove in each groove group for inserting the conductor wire is a matter which can be arbitrarily selected according to the intended purpose. Therefore, the winding pitch and the like can be appropriately changed depending on how the groove is selectively used when winding the conductor wire. For this reason, it is possible to wind the helical coils at different pitches, or to wind them in different modes, using the same type of reel.

【0012】(3) ヘリカルコイルは矩形板状をなす支持
部材の各先端縁部により支持されており、棒状基体の外
周面からは所定距離だけ離間した状態に保持されてい
る。このため、棒状基体を形成している誘電体の誘電率
がアンテナ特性に与える影響を殆ど無くすことができ
る。
(3) The helical coil is supported by each tip edge portion of a support member having a rectangular plate shape, and is held in a state of being separated from the outer peripheral surface of the rod-shaped base body by a predetermined distance. Therefore, the influence of the dielectric constant of the dielectric material forming the rod-shaped base on the antenna characteristics can be almost eliminated.

【0013】(4) 支持部材の各先端縁部に設けられてい
る各溝群に対して導線を押し込むようにして巻き付け操
作するだけで、ヘリカルコイルの巻装が可能なので、例
えば矩形状リブの端縁部に形成した貫通穴に対し、螺旋
素子(ヘリカルコイル)を、その端部から順次ねじ込む
ことによってヘリカルコイルの巻装を行なう如く構成さ
れた従来のものに比べると、巻線の作業性が著しく良
く、巻線工数を大幅に減少させ得る。また巻き付け作業
の際、導線に無理な外力を与えずに済むので、形成され
るヘリカルコイルに部分的な屈曲部ないし歪みを発生さ
せずに済む。したがって完成後のヘリカルコイルの品質
を向上でき、高品質な衛星通信用ヘリカルアンテナを得
ることができる。
(4) The helical coil can be wound by simply winding the conductor wire into each groove group provided at each tip edge portion of the support member, and thus, for example, a rectangular rib. The workability of the winding is better than that of the conventional one, in which the helical element (helical coil) is sequentially screwed into the through hole formed in the end edge portion to wind the helical coil. Is remarkably good, and the winding man-hour can be greatly reduced. Further, since it is not necessary to apply an unreasonable external force to the conducting wire during the winding operation, it is not necessary to generate a partial bending portion or distortion in the formed helical coil. Therefore, the quality of the helical coil after completion can be improved, and a high quality helical antenna for satellite communication can be obtained.

【0014】[0014]

【実施例】図1は本発明の第1実施例に係る衛星通信用
ヘリカルアンテナの概略的構成を示す斜視図である。図
2の(a)(b)および図3の(a)(b)は同実施例
に係る衛星通信用ヘリカルアンテナの巻き枠およびヘリ
カルコイルの要部構成を示す正面図および端面図であ
る。
1 is a perspective view showing a schematic structure of a helical antenna for satellite communication according to a first embodiment of the present invention. FIGS. 2A and 2B and FIGS. 3A and 3B are a front view and an end view showing a main configuration of a winding frame and a helical coil of the satellite communication helical antenna according to the embodiment.

【0015】図1に示すように、この衛星通信用ヘリカ
ルアンテナは、絶縁材料からなる巻き枠10に、導線を
螺旋状に巻回してヘリカルコイル20と成したものであ
る。ヘリカルコイル20はアンテナ先端部に存在してい
る給電部30を中心に第1,第2のコイル21,22が
所謂多重巻き状態に巻装されている。給電部30は、巻
き枠10の筒状をなす棒状基体11の中心部を貫通して
いる同軸ケーブル40の先端部と接続されている。同軸
ケーブル40の巻き枠10の底部側へ導出された基端部
には、同軸ケーブルコネクタ50が取り付けてある。衛
星通信用ヘリカルアンテナは、使用時においてはその外
周を二点鎖線で示すカバー60で覆われる。
As shown in FIG. 1, the helical antenna for satellite communication comprises a winding frame 10 made of an insulating material and a helical coil 20 formed by spirally winding a conductive wire. In the helical coil 20, first and second coils 21 and 22 are wound in a so-called multiple winding state around a power feeding section 30 existing at the tip of the antenna. The power feeding unit 30 is connected to a tip end portion of a coaxial cable 40 that passes through a central portion of the cylindrical rod-shaped base body 11 of the winding frame 10. A coaxial cable connector 50 is attached to a base end portion of the coaxial cable 40 which is led to the bottom side of the winding frame 10. When used, the helical antenna for satellite communication is covered with a cover 60 shown by an alternate long and two short dashes line on the outer periphery thereof.

【0016】図2の(a)(b)および図3の(a)
(b)に示すように、巻き枠10は筒状をなす棒状基体
11と、この棒状基体11の外周に設けた矩形板状をな
す第1〜第4の支持部材12a〜12dと、この支持部
材12a〜12dの各先端縁部に設けた導線係入用の溝
群13a〜13dとからなっている。棒状基体11およ
び第1〜第4の支持部材12a〜12dは、本実施例に
おいては絶縁材料にて一体成形されている。
2 (a) and 2 (b) and FIG. 3 (a).
As shown in (b), the winding frame 10 includes a cylindrical rod-shaped base body 11, rectangular plate-shaped first to fourth support members 12a to 12d provided on the outer periphery of the rod-shaped base body 11, and the support. Each of the members 12a to 12d is provided with a groove group 13a to 13d for engaging a conductor, which is provided at each tip edge portion. In this embodiment, the rod-shaped base 11 and the first to fourth support members 12a to 12d are integrally formed of an insulating material.

【0017】第1〜第4の支持部材12a〜12dは、
棒状基体11の中心軸を含みかつ互いに直交する二平面
内にそれぞれが存在するように、上記棒状基体11の外
周面の4個所に放射状(十字状)に突設されている。こ
れら第1〜第4の支持部材12a〜12dのうち、互い
に180°異なる角度位置で相対向する第1,第2の支
持部材12a,12bにおける各先端縁部の対称な位置
には、導線係入用の第1,第2の溝群13a,13bが
所定ピッチPで形成されている。第1,第2の支持部材
とは90°ずれた位置において、互いに180°異なる
角度位置で相対向する第3,第4の支持部材12c,1
2dにおける各先端縁部の対称な位置には、所定ピッチ
Pで且つ前記第1,第2の溝群13a,13bとは1/
2ピッチ分ずれた状態に、導線係入用の第3,第4の溝
群13c,13dが形成されている。この様に構成され
た本実施例においては次のような作用効果を奏する。
The first to fourth support members 12a to 12d are
Radial (cross-shaped) projections are provided at four locations on the outer peripheral surface of the rod-shaped substrate 11 so that they respectively exist in two planes that include the central axis of the rod-shaped substrate 11 and are orthogonal to each other. Among the first to fourth support members 12a to 12d, the wire guides are arranged at symmetrical positions of the respective leading edge portions of the first and second support members 12a and 12b facing each other at angular positions different from each other by 180 °. The required first and second groove groups 13a and 13b are formed at a predetermined pitch P. Third and fourth support members 12c, 1 facing each other at an angle position different from each other by 180 ° at a position shifted from the first and second support members by 90 °.
At a symmetrical position of each tip edge portion in 2d, at a predetermined pitch P and 1 / second with the first and second groove groups 13a and 13b.
The third and fourth groove groups 13c and 13d for engaging the conducting wire are formed in a state of being displaced by two pitches. In this embodiment having such a configuration, the following operational effects are obtained.

【0018】支持部材12a〜12dの各先端縁部にそ
れぞれ設けられている導線係入用の各溝群13a〜13
dは、右軸回り方向および左軸回り方向のいずれの方向
にみても、隣接する支持部材すなわち12aー12c、
12cー12b、12bー12d、12dー12aの各
相互間では、ヘリカルコイル20の螺旋形状に対応する
ように、順次1/2ピッチづつずれた状態を呈してい
る。このためヘリカルコイル20は、その巻き方を右巻
き或いは左巻きに特定されずに済み、図2に示すような
右巻きコイル20Aとして巻装することも、或いは図3
に示すような左巻きコイル20Bとして巻装することも
可能となる。したがって同じ型式の巻き枠10を用い
て、異なる巻き方向のヘリカルコイル20A,20Bを
任意に巻装することが可能となる。
Each of the groove groups 13a to 13 for engaging the conducting wire, which are provided at the respective leading edge portions of the supporting members 12a to 12d.
d is an adjacent support member, that is, 12a-12c, when viewed in either the right-hand axis direction or the left-axis direction.
12c-12b, 12b-12d, and 12d-12a are sequentially shifted by 1/2 pitch so as to correspond to the helical shape of the helical coil 20. Therefore, the helical coil 20 need not be specified as a right-handed or left-handed winding, and may be wound as a right-handed coil 20A as shown in FIG.
It is also possible to wind as a left-handed coil 20B as shown in FIG. Therefore, it is possible to arbitrarily wind the helical coils 20A and 20B in different winding directions by using the winding frame 10 of the same type.

【0019】導線係入用の各溝群13a〜13dに対し
て導線を巻き付ける際に、各溝群13a〜13dにおけ
るどの溝に巻き付けるかは、所期の目的に応じて任意に
選択し得る事項である。したがって、導線巻き付け時に
おいて選択使用する溝の選択状況の如何によっては、巻
線ピッチ等を適宜変更することが可能である。このため
同じ型式の巻き枠10を用いてヘリカルコイル20を異
なるピッチ(例えば2P,3P…)に巻装することも、
また異なる態様(例えば1Pと2Pとを混在させる等)
で巻装することも可能である。
When winding the conductor wire around each of the groove groups 13a to 13d for engaging the conductor wire, which groove in each of the groove groups 13a to 13d is to be wound can be arbitrarily selected according to the intended purpose. Is. Therefore, the winding pitch and the like can be appropriately changed depending on the selection situation of the groove that is selectively used when winding the conductor wire. Therefore, it is possible to wind the helical coils 20 at different pitches (for example, 2P, 3P ...) Using the same type of reel 10.
In addition, a different mode (for example, 1P and 2P are mixed)
It is also possible to wind up.

【0020】ヘリカルコイル20は矩形板状をなす支持
部材12a〜12dの各先端縁部により支持されてお
り、棒状基体11の外周面からは所定距離Lだけ離間し
た状態に保持されている。このため、棒状基体11を形
成している誘電体の誘電率がたとえ大きくても、上記誘
電体がアンテナ特性に与える影響を殆ど無くすことがで
きる。
The helical coil 20 is supported by the tip edges of the supporting members 12a to 12d each having a rectangular plate shape, and is held at a distance L from the outer peripheral surface of the rod-shaped base 11. Therefore, even if the dielectric constant of the rod-shaped substrate 11 is large, the influence of the dielectric on the antenna characteristics can be almost eliminated.

【0021】支持部材12a〜12dの各先端縁部に設
けられている各溝群13a〜13dに対して導線を押し
込むようにして巻き付け操作するだけで、ヘリカルコイ
ル20の巻装が可能である。したがって例えば矩形状リ
ブの端縁部に形成した貫通穴に対し、螺旋素子(ヘリカ
ルコイル)を、その端部から順次ねじ込むことによって
ヘリカルコイルの巻装を行なう如く構成された従来のも
のに比べると、作業性が著しく優れており、巻線工数を
大幅に削減することができる。また巻き付け作業の際、
導線を単に各溝群13a〜13dの各溝内に挿入するだ
けで良いので、大きな外力が導線に無理な形で加わるお
それがない。このため形成されるヘリカルコイルに部分
的な屈曲部ないし歪みを発生させずに済む。したがって
完成後のヘリカルコイルの品質を向上でき、高品質なヘ
リカルアンテナを得ることができる。
The helical coil 20 can be wound by simply winding the conductor wire into the groove groups 13a to 13d provided on the respective leading edge portions of the support members 12a to 12d by pushing the conductor wire. Therefore, for example, in comparison with a conventional one configured to wind a helical coil by sequentially screwing a spiral element (helical coil) into the through hole formed in the edge portion of the rectangular rib from the end portion, The workability is remarkably excellent, and the number of winding steps can be significantly reduced. Also, during the winding work,
Since it suffices to simply insert the conductor wire into each groove of each groove group 13a to 13d, there is no fear that a large external force is applied to the conductor wire in an unreasonable manner. Therefore, it is not necessary to generate a partial bend or distortion in the formed helical coil. Therefore, the quality of the helical coil after completion can be improved, and a high quality helical antenna can be obtained.

【0022】図4は本発明の第2実施例に係る衛星通信
用ヘリカルアンテナの巻き枠の要部構成を示す図であ
る。図4に示すように、この巻き枠は長尺な単一枠体か
らなる巻き枠ではなく、軸方向に沿って多分割した複数
個(本実施例では2個)の分割枠体70(図4の(a)
(b)に示すもの),80(図4の(c)(d)に示す
もの)からなっている。そしてこれらの分割体70,8
0は、隣接する棒状基体71と81との端面どうしが、
軸回り方向の特定角度位置で互いに連結可能な如く設け
られたものである。すなわち一方の分割枠体70の棒状
基体71の端面には一対の凸部73,74が対向配設さ
れており、他方の分割枠体80の棒状基体81の端面に
は一対の凹部83,84が対向配設されている。上記凸
部73,74と凹部83,84とを差し込み操作するこ
とにより両者は互いに係合し合い、分割枠体70,80
どうしを連結し得るものとなっている。
FIG. 4 is a view showing the structure of the essential parts of the reel of the helical antenna for satellite communication according to the second embodiment of the present invention. As shown in FIG. 4, this winding frame is not a long single frame body, but a plurality of (two in this embodiment) divided frame bodies 70 (two in this embodiment) divided in the axial direction. 4 (a)
(Shown in (b)) and 80 (shown in (c) and (d) of FIG. 4). And these divided bodies 70, 8
0 means that the end faces of the adjacent rod-shaped bases 71 and 81 are
It is provided so as to be connectable to each other at a specific angular position in the axial direction. That is, a pair of convex portions 73, 74 are arranged opposite to each other on the end surface of the rod-shaped base body 71 of the one divided frame body 70, and a pair of concave portions 83, 84 are formed on the end surface of the rod-shaped base body 81 of the other divided frame body 80. Are opposed to each other. By inserting and operating the convex portions 73, 74 and the concave portions 83, 84, the two are engaged with each other, and the divided frame bodies 70, 80
It is possible to connect each other.

【0023】この様に構成された第2実施例によれば、
第1実施例と同様の作用効果を奏する上、分割枠体7
0,80としたことによる短尺化により、巻き枠の成形
が容易化する。その結果、成形歪みのない高品質な巻き
枠が容易に得られる利点を有する。
According to the second embodiment constructed as described above,
In addition to achieving the same effects as the first embodiment, the dividing frame 7
Since the length is reduced to 0.80, the reel can be easily formed. As a result, there is an advantage that a high quality reel without molding distortion can be easily obtained.

【0024】図5は本発明の第3実施例に係る衛星通信
用ヘリカルアンテナの巻き枠の要部構成を示す図であ
る。図5に示すように、この巻き枠90は筒状をなす棒
状基体91と、矩形板状をなす第1〜第4の支持部材
(図では第1の支持部材92aのみを図示)とが別体に
形成されおり、上記棒状基体91の外周に対して、上記
第1〜第4の支持部材が着脱自在に取り付け得るものと
なっている。すなわち棒状基体91の外周には、結合透
孔群95a,95b〜が設けられており、第1の支持部
材92aには挿着突起群94aが設けられている。同様
に図示はしてないが第2〜第4の支持部材にも挿着突起
群が設けられている。かくして第1の支持部材92a
を、矢印で示すように棒状基体91の外周に対して接近
させ、挿着突起群94aの尖端を結合透孔群95aに当
てがって押し込み操作すると、挿着突起群94aが弾性
変形しながら結合透孔群95aの内部へ挿入される。こ
の挿入が終了したところで挿着突起群94aは自らの弾
性により復元するので、挿着突起群94aの爪部が結合
透孔群95aの内面縁部で引っ掛かり、第1の支持部材
92aは抜け止めを係止された状態で挿着される。同様
に図示してない第2〜第4の支持部材についても挿着が
なされる。
FIG. 5 is a diagram showing a main structure of a reel of a helical antenna for satellite communication according to a third embodiment of the present invention. As shown in FIG. 5, the winding frame 90 includes a cylindrical rod-shaped base 91 and rectangular plate-shaped first to fourth support members (only the first support member 92a is shown in the figure). It is formed in a body, and the first to fourth support members can be detachably attached to the outer periphery of the rod-shaped base 91. That is, the coupling through-hole groups 95a and 95b are provided on the outer periphery of the rod-shaped base 91, and the insertion projection group 94a is provided on the first support member 92a. Similarly, although not shown, the second to fourth support members are also provided with insertion protrusion groups. Thus, the first support member 92a
Is approached to the outer periphery of the rod-shaped base 91 as indicated by the arrow, and the tip of the insertion projection group 94a is applied to the coupling through hole group 95a and pushed in, the insertion projection group 94a elastically deforms. It is inserted into the combination through hole group 95a. When this insertion is completed, the insertion projection group 94a is restored by its own elasticity, so that the claws of the insertion projection group 94a are caught at the inner surface edge of the coupling through hole group 95a, and the first support member 92a is prevented from coming off. Is inserted in a locked state. Similarly, the second to fourth support members (not shown) are also attached.

【0025】このように構成された第3実施例によれ
ば、第1実施例と同様の作用効果を奏する上、巻き枠成
形用の「型」の構造が単純化されるため、製造コストを
大幅に低減することができる。しかも種類(主として溝
群93aのピッチPの大きさ)が異なる支持部材92a
等を、適宜選択して棒状基体91に挿着できる利点を有
する。なお支持部材92a等は、挿着突起群94a等を
その弾性係止力に逆らって結合透孔群95a等から強引
に引き抜けば、棒状基体91から比較的簡単に離脱させ
得る。なお本発明は上記各実施例に限定されるものでは
なく、本発明の要旨を逸脱しない範囲で種々変形実施可
能であるのは勿論である。
According to the third embodiment thus constituted, the same operational effect as that of the first embodiment is obtained, and the structure of the "mold" for forming the reel is simplified, so that the manufacturing cost is reduced. It can be significantly reduced. Moreover, the supporting members 92a of different types (mainly the size of the pitch P of the groove group 93a) are different.
And the like can be appropriately selected and inserted into the rod-shaped substrate 91. The support member 92a and the like can be relatively easily detached from the rod-shaped base 91 by forcibly pulling out the insertion projection group 94a and the like from the coupling through hole group 95a and the like against the elastic locking force. The present invention is not limited to the above-mentioned embodiments, and it goes without saying that various modifications can be made without departing from the gist of the present invention.

【0026】[0026]

【発明の効果】本発明によれば、巻き枠の各支持部材に
おける各先端縁部に、導線係入用の各溝群が、右軸回り
方向および左軸回り方向のいずれの方向にみても、隣接
する支持部材間では、順次1/2ピッチづつずれた状態
を呈する如く設けられ、これらの溝群に対して導線が螺
旋状に巻き付けられる如く構成されているので、同じ型
式の巻き枠を用いて、異なる巻き方向,異なるピッチ,
および異なる態様を有するヘリカルコイルを巻装するこ
とが可能である上、巻き枠を形成している誘電体による
アンテナ特性への影響が殆ど無く、また巻線の作業性が
著しく良く、巻線工数が少なくて済み、低コストで製作
可能である上、ヘリカルコイルに部分的な屈曲部ないし
歪みを発生させずに済み、高品質な衛星通信用ヘリカル
アンテナを提供できる。
According to the present invention, each of the groove groups for engaging the conducting wire is formed at each of the front edge portions of each of the supporting members of the reel regardless of the direction of the right axis or the direction of the left axis. , The adjacent support members are provided so as to be sequentially displaced by 1/2 pitch, and the conductor wire is wound around these groove groups in a spiral shape. With different winding direction, different pitch,
In addition, it is possible to wind a helical coil having a different form, there is almost no influence on the antenna characteristics due to the dielectric material forming the winding frame, and the workability of the winding is extremely good, and the number of winding steps is large. It is possible to provide a high-quality helical antenna for satellite communication, which can be manufactured at a low cost and does not require partial bending or distortion in the helical coil.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の一実施例に係る衛星通信用ヘリカルア
ンテナの概略的構成を示す斜視図。
FIG. 1 is a perspective view showing a schematic configuration of a helical antenna for satellite communication according to an embodiment of the present invention.

【図2】同実施例に係る衛星通信用ヘリカルアンテナの
巻き枠および右巻きヘリカルコイルの要部構成を示す正
面図および端面図。
2A and 2B are a front view and an end view showing a main configuration of a winding frame and a right-handed helical coil of a satellite communication helical antenna according to the embodiment.

【図3】同実施例に係る衛星通信用ヘリカルアンテナの
巻き枠および左巻きヘリカルコイルの要部構成を示す正
面図および端面図。
3A and 3B are a front view and an end view showing a main configuration of a reel and a left-handed helical coil of the satellite antenna for satellite communication according to the embodiment.

【図4】本発明の第2実施例に係る衛星通信用ヘリカル
アンテナの巻き枠の要部構成を示す図。
FIG. 4 is a diagram showing a main configuration of a reel of a helical antenna for satellite communication according to a second embodiment of the present invention.

【図5】本発明の第3実施例に係る衛星通信用ヘリカル
アンテナの巻き枠の要部構成を示す図。
FIG. 5 is a view showing a main configuration of a reel of a helical antenna for satellite communication according to a third embodiment of the present invention.

【符号の説明】[Explanation of symbols]

10…巻き枠、11…棒状基体、12a〜12d…支持
部材、13a〜13d…導体係入用の溝群、20…ヘリ
カルコイル、21,22…第1,第2のコイル、20A
…右巻きコイル、20B…左巻きコイル、30…給電
部、40…同軸ケーブル、50…同軸ケーブルコネク
タ、60…カバー。
DESCRIPTION OF SYMBOLS 10 ... Reel, 11 ... Rod-shaped base, 12a-12d ... Support member, 13a-13d ... Groove group for conductor insertion, 20 ... Helical coil, 21, 22 ... 1st, 2nd coil, 20A
... right-handed coil, 20B ... left-handed coil, 30 ... feeding part, 40 ... coaxial cable, 50 ... coaxial cable connector, 60 ... cover.

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 巻き枠に導線を螺旋状に巻回してなる衛
星通信用ヘリカルアンテナにおいて、 筒状または柱状をなす棒状基体と、 この棒状基体の中心軸を含みかつ互いに直交する二平面
内にそれぞれが存在するように、上記棒状基体の外周面
の4個所に放射状に突設された矩形板状をなす第1〜第
4の支持部材と、 これら第1〜第4の支持部材のうち、互いに180°異
なる角度位置で相対向する第1,第2の支持部材におけ
る各先端縁部の対称な位置に、所定ピッチで形成された
導線係入用の第1,第2の溝群と、 前記第1,第2の支持部材とは90°ずれた位置におい
て、互いに180°異なる角度位置で相対向する第3,
第4の支持部材における各先端縁部の対称な位置に、所
定ピッチで且つ前記第1,第2の溝群とは1/2ピッチ
分ずれた状態に形成された導線係入用の第3,第4の溝
群と、 からなる巻き枠を備えたことを特徴とする衛星通信用ヘ
リカルアンテナ。
1. A helical antenna for satellite communication in which a conductor is spirally wound around a winding frame, wherein a cylindrical or columnar rod-shaped base and two planes that include the central axis of the rod-shaped base and are orthogonal to each other. Of the first to fourth supporting members, which are rectangular plate-shaped and are radially provided at four positions on the outer peripheral surface of the rod-shaped base so that each of them exists, and among these first to fourth supporting members, First and second groove groups for engaging the conducting wires, which are formed at a predetermined pitch, at symmetrical positions of the respective tip edge portions of the first and second support members facing each other at angular positions different from each other by 180 °, The third and the third support members, which are opposite to each other at an angle position different from each other by 180 °, at a position offset by 90 ° from the first and second support members
A third wire-engaging wire insertion member formed at a symmetrical position of each tip edge portion of the fourth support member at a predetermined pitch and at a pitch displaced from the first and second groove groups by 1/2 pitch. , A helical antenna for satellite communication, characterized in that it has a fourth groove group and a winding frame composed of.
【請求項2】複数の分割枠体における隣接する棒状基体
の端面どうしが、軸回り方向の特定角度位置で互いに連
結可能な如く設けられたことを特徴とする請求項1に記
載の衛星通信用ヘリカルアンテナ。
2. The satellite communication according to claim 1, wherein end faces of adjacent rod-shaped bases in the plurality of divided frame bodies are provided so as to be connectable to each other at a specific angular position in the axial direction. Helical antenna.
【請求項3】 筒状または柱状をなす棒状基体と、矩形
板状をなす第1〜第4の支持部材とが別体に形成され、
上記棒状基体の外周に対して、上記第1〜第4の支持部
材が着脱自在に設けられていることを特徴とする請求項
1に記載の衛星通信用ヘリカルアンテナ。
3. A cylindrical or columnar rod-shaped base body and rectangular plate-shaped first to fourth support members are separately formed,
The helical antenna for satellite communication according to claim 1, wherein the first to fourth support members are detachably provided on the outer periphery of the rod-shaped base.
JP17853992A 1992-07-06 1992-07-06 Helical antenna for satellite communication Expired - Fee Related JP3317522B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17853992A JP3317522B2 (en) 1992-07-06 1992-07-06 Helical antenna for satellite communication

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17853992A JP3317522B2 (en) 1992-07-06 1992-07-06 Helical antenna for satellite communication

Publications (2)

Publication Number Publication Date
JPH0629714A true JPH0629714A (en) 1994-02-04
JP3317522B2 JP3317522B2 (en) 2002-08-26

Family

ID=16050251

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17853992A Expired - Fee Related JP3317522B2 (en) 1992-07-06 1992-07-06 Helical antenna for satellite communication

Country Status (1)

Country Link
JP (1) JP3317522B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002261537A (en) * 2001-02-27 2002-09-13 Mitsumi Electric Co Ltd Helical composite antenna structure
US6486852B1 (en) 2000-01-31 2002-11-26 Mitsubishi Materials Corporation Antenna device and assembly of the antenna device
JP2013507850A (en) * 2009-10-16 2013-03-04 イーエムエス・テクノロジーズ・カナダ,リミテッド Increasing the gain of an array antenna by optimal suspension of segmented linear conductors

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015010917A1 (en) * 2015-08-20 2017-02-23 Diehl Metering Gmbh Antenna device for receiving and / or transmitting radio signals
CN105449334A (en) * 2015-12-15 2016-03-30 成都迅德科技有限公司 Base station antenna

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6486852B1 (en) 2000-01-31 2002-11-26 Mitsubishi Materials Corporation Antenna device and assembly of the antenna device
JP2002261537A (en) * 2001-02-27 2002-09-13 Mitsumi Electric Co Ltd Helical composite antenna structure
JP4539798B2 (en) * 2001-02-27 2010-09-08 ミツミ電機株式会社 Helical composite antenna structure
JP2013507850A (en) * 2009-10-16 2013-03-04 イーエムエス・テクノロジーズ・カナダ,リミテッド Increasing the gain of an array antenna by optimal suspension of segmented linear conductors
US9054425B2 (en) 2009-10-16 2015-06-09 Ems Technologies Canada, Ltd. Spherical perturbation of an array antenna
US9118118B2 (en) 2009-10-16 2015-08-25 Ems Technologies Canada, Ltd. Increased gain in an array antenna through optimal suspension of piece-wise linear conductors
US9362625B2 (en) 2009-10-16 2016-06-07 Ems Technologies Canada, Ltd. Optimal loading for increased gain in an array antenna

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