JPH0263202A - Antenna equipment - Google Patents

Antenna equipment

Info

Publication number
JPH0263202A
JPH0263202A JP21415688A JP21415688A JPH0263202A JP H0263202 A JPH0263202 A JP H0263202A JP 21415688 A JP21415688 A JP 21415688A JP 21415688 A JP21415688 A JP 21415688A JP H0263202 A JPH0263202 A JP H0263202A
Authority
JP
Japan
Prior art keywords
radiation
reflecting mirror
frequency
elements
satellite
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.)
Pending
Application number
JP21415688A
Other languages
Japanese (ja)
Inventor
Kazuyoshi Takebayashi
竹林 和芳
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP21415688A priority Critical patent/JPH0263202A/en
Publication of JPH0263202A publication Critical patent/JPH0263202A/en
Pending legal-status Critical Current

Links

Landscapes

  • Aerials With Secondary Devices (AREA)

Abstract

PURPOSE:To use two or more frequencies simultaneously by providing many radiation elements on one reflecting mirror surface and utilizing it also as a radiation face. CONSTITUTION:A radio wave of a transmission signal from a transmitter 61 whose frequency is fHT is sent to a radiation feeding part 4a and fed to many radiator elements 3 fitted to a reflecting mirror 1. Then the phases of lots of the radiation elements 3 are synthesized to radiate a radio wave to a satellite in front of the antenna system. Moreover, a reception signal of a frequency fHR from the satellite is fed to lots of the radiation elements 3 fitted to the reflection mirror 1 in a reverse path, the phases are synthesized and led to the radiation feeding part 4a and sent to a receiver 7a. The reflecting mirror surface has a reflecting face and a radiation face and separate radiation feeding parts 4a, 4b are added respectively and the reflecting mirror surface is used by using two frequencies or more at the same time.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、衛星通信に使用するアンテナ装置に関する
ものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to an antenna device used for satellite communication.

〔従来の技術〕[Conventional technology]

第5図は従来のアンテナ装置を示す構成図であり、1は
反射鏡1.2は反射鏡2.4は上記反射鏡lと反射鏡2
の光学的中心におかれた2つ以上の周波数を共用する放
射給電部である。5は反射鏡2を支持する支持柱である
。6aは周波数rMyの送信装置、6bは周波数rt、
tの送信装置、7aは周波数fallの受信装置、7b
は周波数fLlの受信装置である。
FIG. 5 is a configuration diagram showing a conventional antenna device, in which 1 is a reflecting mirror 1. 2 is a reflecting mirror 2.4 is the reflecting mirror 1 and the reflecting mirror 2.
It is a radiant feeding unit that shares two or more frequencies located at the optical center of the 5 is a support column that supports the reflecting mirror 2. 6a is a transmitter with frequency rMy, 6b is frequency rt,
t transmitting device, 7a a receiving device of frequency fall, 7b
is a receiving device of frequency fLl.

次に動作について説明する。Next, the operation will be explained.

周波数fHTの送信装置6aからの送信信号の電波は放
射給電部4を通り放射され、反射鏡2で反射され、さら
に反射鏡lで反射されて衛星へと放射される。また周波
数f4の送信装置6bからの送信信号の電波は、上記と
同様に放射給電部4を通り放射され、反射鏡2で反射さ
れ、さらに反射鏡1で反射されて衛星へと放射される。
The radio wave of the transmission signal from the transmitting device 6a having the frequency fHT is radiated through the radiation feed section 4, reflected by the reflecting mirror 2, further reflected by the reflecting mirror 1, and radiated to the satellite. Similarly to the above, the radio wave of the transmission signal from the transmitting device 6b having the frequency f4 is radiated through the radiation feeder 4, reflected by the reflecting mirror 2, further reflected by the reflecting mirror 1, and radiated to the satellite.

次に衛星から入射した周波数romの受信信号の電波は
反射鏡1で反射され、さらに反射鏡2で反射され、放射
給電部4へと導かれ、受信装置7aへと導かれる。また
、周波数fLRの受信信号の電波は、上記と同様に反射
鏡1で反射され、さらに反射鏡2で反射されて放射給電
部4へと導かれ、受信装置7bへと導かれる。
Next, the radio wave of the received signal of the frequency ROM incident from the satellite is reflected by the reflecting mirror 1, further reflected by the reflecting mirror 2, guided to the radiation feeding section 4, and then guided to the receiving device 7a. Further, the radio wave of the received signal having the frequency fLR is reflected by the reflecting mirror 1 in the same manner as described above, further reflected by the reflecting mirror 2, and guided to the radiation feeding section 4, and then guided to the receiving device 7b.

上記の様に放射給電部4は2つ以上の周波数の送信信号
および受信信号の電波が通るように、構成されている。
As described above, the radiation feeding section 4 is configured so that radio waves of transmission signals and reception signals of two or more frequencies pass therethrough.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

従来のアンテナ装置は以上のように構成されていたので
、放射給電部4に2つ以上の周波数を通すことが必要と
なり、放射給電部4の中心となる円形導波管において、
高い方の周波数で不要な高次モードの電波を発生するこ
とになり、その不要な高次モードの電波の発生を抑える
ために、高次モード抑圧用のフィルターを入れるために
構造が複雑になり、また、使用できる周波数の範囲が狭
くなるなどの問題点があった。
Since the conventional antenna device is configured as described above, it is necessary to pass two or more frequencies through the radiation feeding section 4, and in the circular waveguide that is the center of the radiation feeding section 4,
Unnecessary high-order mode radio waves are generated at higher frequencies, and in order to suppress the generation of unnecessary high-order mode radio waves, the structure becomes complicated because a filter for suppressing the high-order mode is inserted. In addition, there were other problems such as a narrower frequency range that could be used.

この発明は上記の様な問題点を解消するためになされた
もので、各々独自に周波数の異なった放射給電部を構成
することにより、不要な高次モードの電波の発生をなく
し、かつ、2つ以上の周波数を同時に使用できるアンテ
ナ装置を得ることを目的としている。
This invention was made to solve the above-mentioned problems, and by configuring radiation feeding sections each having a different frequency, it eliminates the generation of unnecessary higher-order mode radio waves, and The purpose of this invention is to obtain an antenna device that can use two or more frequencies simultaneously.

〔課題を解決するための手段〕[Means to solve the problem]

この発明に係るアンテナ装置は少なくとも1枚以上の反
射鏡面の内の1枚の反射鏡面に反射面として使用する周
波数と異なる周波数の多数の放射素子を設けてこれを放
射面としても構成するようにし、該反射面と放射面とに
各々別々の放射給電部を付加することにより、該反射鏡
面を反射面及び放射面として2つ以上の周波数で使用で
きるようにしたものである。
In the antenna device according to the present invention, one of the at least one reflecting mirror surface is provided with a large number of radiating elements having a frequency different from that used as a reflecting surface, so that this also serves as a radiating surface. By adding separate radiation feeding parts to the reflecting surface and the emitting surface, the reflecting mirror surface can be used as a reflecting surface and a emitting surface at two or more frequencies.

〔作用〕[Effect]

この発明におけるアンテナ装置では、1枚の反射鏡面が
反射面と放射面を持ち、各々に別々の放射給電部を付加
するようにしたから、同時に2つ以上の周波数を用いて
使用することができる。
In the antenna device of this invention, one reflective mirror surface has a reflective surface and a radiation surface, and a separate radiation feeding section is added to each surface, so it can be used at the same time using two or more frequencies. .

〔実施例〕〔Example〕

以下、この発明の一実施例を図について説明する。 An embodiment of the present invention will be described below with reference to the drawings.

第1図において、■は反射鏡1.2は反射鏡2.3は反
射鏡1に取り付けられた多数の放射素子、4bは反射鏡
1を反射面として使用する周波数の放射給電部、4aは
反射鏡1を放射面として使用する周波数の放射給電部で
ある。5aおよび6bは各々の放射給電部4aおよび4
bに送信信号を送る、送信装置であり、7aおよび7b
は各々放射給電部4aおよび4bにより分波された衛星
からの受信信号を処理する受信装置である。
In Fig. 1, ■ is a reflector 1.2 is a reflector 2.3 is a large number of radiating elements attached to the reflector 1, 4b is a frequency radiation feeder that uses the reflector 1 as a reflecting surface, and 4a is a This is a frequency radiation feeding section that uses the reflecting mirror 1 as a radiation surface. 5a and 6b are the respective radiant feeders 4a and 4
a transmitting device that sends a transmission signal to 7a and 7b;
are receiving devices that process received signals from satellites separated by the radiation feeding units 4a and 4b, respectively.

次に動作について説明する。Next, the operation will be explained.

周波数「、アの送信装置6aからの送信信号の電波は、
放射給電部4aへ伝送され、反射鏡1に取り付けられた
多数の放射素子3に給電される。ここで、多数の放射素
子3の位相を合成することにより、アンテナ装置の前面
の衛星へと放射することができる。また、衛星からの周
波数f□の受信信号は上記とは逆の経路で反射鏡1に取
り付けられた多数の放射素子3で給電し、その位相を合
成して、放射給電部4aへ導かれ、さらに受信装置7a
へと伝送される。
The frequency of the radio wave of the transmission signal from the transmitting device 6a is
The power is transmitted to the radiation power feeding section 4a, and is fed to a large number of radiation elements 3 attached to the reflecting mirror 1. Here, by combining the phases of a large number of radiating elements 3, it is possible to radiate to the satellite in front of the antenna device. In addition, the received signal of frequency f□ from the satellite is fed by a large number of radiating elements 3 attached to the reflector 1 in the opposite path to the above, the phases are synthesized, and the signal is guided to the radiating feeding section 4a. Furthermore, the receiving device 7a
transmitted to.

次に周波数fLアの送信装置6bからの送信信号の電波
は、専用に作られた放射給電部4bに伝送されて放射し
反射鏡2で反射され、さらに反射鏡11に取り付けられ
た多数の放射素子3で影響されることなく反射鏡1で反
射されて衛星へと放射される。また、衛星からの周波数
fLIIの受信信号は上記とは逆の経路で、反射鏡1に
取り付けられた放射素子3で影響されることなく、反射
鏡1で反射し、さらに反射鏡2で反射し、放射給電部4
bへと導かれ、受信装置7bへと伝送される。
Next, the radio waves of the transmission signal from the transmitting device 6b having the frequency fL-a are transmitted to the radiation feeding part 4b made exclusively for the purpose, are radiated, are reflected by the reflecting mirror 2, and are further transmitted to the radiation feeding section 4b, which is made exclusively for the purpose, and are reflected by the reflecting mirror 2. The light is reflected by the reflector 1 and radiated to the satellite without being affected by the element 3. In addition, the received signal of frequency fLII from the satellite is reflected by the reflector 1 and further reflected by the reflector 2 without being affected by the radiating element 3 attached to the reflector 1, in the opposite path to the above. , radiation feed section 4
b and is transmitted to the receiving device 7b.

ここで、反射鏡1を反射板として使用する周波数fLl
と反射鏡1に取り付けられた多数の放射素子3により反
射Fi1を放射板として使用する周波数fNTおよびf
ilの関係は rHtおよびf。>fLTおよびfLjlとすることに
よりこれを実現できる。
Here, the frequency fLl at which the reflector 1 is used as a reflector is
and the frequencies fNT and f when the reflection Fi1 is used as a radiation plate by a large number of radiation elements 3 attached to the reflection mirror 1.
The relationship of il is rHt and f. This can be achieved by setting >fLT and fLjl.

なお、上記実施例では、反射鏡1面に多数の放射素子3
を設けたが、反射鏡2面に多数の放射素子を設けても良
い。
In the above embodiment, a large number of radiating elements 3 are provided on one surface of the reflecting mirror.
However, a large number of radiating elements may be provided on two surfaces of the reflecting mirror.

また、上記実施例における多数の放射素子のより詳細な
構成の例としては第3,4図の構成が考えられる。
Moreover, the configurations shown in FIGS. 3 and 4 can be considered as examples of more detailed configurations of the large number of radiating elements in the above embodiment.

即ち、第3図は放射面を構成する放射素子として導波管
形スロット素子を用いた例を示し、これは第3図の様に
反射tR1面に多数の導波管8を平行に並べ、その導波
管8の管壁に電波を放射する穴10を設け、その放射さ
せる穴10の反対面にその多数の導波管8の電波を結合
孔9を介して合成する導波管11を設けた構成としたも
のであり、上記実施例の効果を得ることができる。
That is, FIG. 3 shows an example in which a waveguide slot element is used as a radiation element constituting a radiation surface, and as shown in FIG. 3, a number of waveguides 8 are arranged in parallel on the reflection tR1 surface, A hole 10 for radiating radio waves is provided in the wall of the waveguide 8, and a waveguide 11 is provided on the opposite surface of the hole 10 for radiating radio waves, which combines the radio waves of the multiple waveguides 8 via a coupling hole 9. Therefore, the effects of the above embodiments can be obtained.

また第4図は放射面を構成する放射素子としてマイクロ
ストリップ素子を用いた例を示し、これは第4図に示す
様に反射鏡1面に、誘電体板13の両面に金属板12を
設けたプリント基板を用い、その金属板12表面には放
射穴10′を設け、その放射穴10′の裏面に誘電体板
13を介して結合線路14と合成回路15とを設けた構
成としたものであり、上記実施例の効果を得ることがで
きる。
Furthermore, FIG. 4 shows an example in which a microstrip element is used as a radiating element constituting a radiating surface. As shown in FIG. A radiation hole 10' is provided on the surface of the metal plate 12, and a coupling line 14 and a composite circuit 15 are provided on the back surface of the radiation hole 10' via a dielectric plate 13. Therefore, the effects of the above embodiment can be obtained.

〔発明の効果〕〔Effect of the invention〕

以上のように、この発明によれば、1枚の反射鏡面に多
数の放射素子を設けてこれを放射面としても構成するよ
うにしたので、該反射鏡面を反射面及び放射面として2
つ以上の周波数で使用でき、しかもその反射面及び放射
面を各々独自に周波数の異なった放射給電部により構成
することができるため、各々の放射給電部を小さくする
ことができる効果がある。
As described above, according to the present invention, a single reflective mirror surface is provided with a large number of radiating elements so that it can also be configured as a radiation surface, so that the reflective mirror surface can be used as both a reflective surface and a radiation surface.
Since it can be used at more than one frequency, and its reflecting surface and emitting surface can each be configured with a radiant feeding section having a different frequency, each radiating feeding section can be made smaller.

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

第1図はこの発明の一実施例によるアンテナ装置の概略
図、第2図はこの発明の他の実施例の概略図、第3図、
第4図は各々この発明の放射素子の例を示す概略図、第
5図は従来のアンテナ装置を示す概略図である。 1は反射@1.2は反射鏡2.3は放射素子、4は放射
給電部、5は反射鏡支持柱、6は送信装置、7は受信装
置、8は導波管、9は結合穴、lO,10”は放射穴、
11は合成用導波管、12は金属板、13は誘電体板、
14は結合線路、15は合成回路である。 なお図中同一符号は同−又は相当部分を示す。
FIG. 1 is a schematic diagram of an antenna device according to one embodiment of the present invention, FIG. 2 is a schematic diagram of another embodiment of the present invention, and FIG.
FIG. 4 is a schematic diagram showing an example of a radiating element of the present invention, and FIG. 5 is a schematic diagram showing a conventional antenna device. 1 is reflection @1. 2 is a reflector 2. 3 is a radiating element, 4 is a radiation feeder, 5 is a reflector support column, 6 is a transmitter, 7 is a receiver, 8 is a waveguide, 9 is a coupling hole , lO,10” is a radiation hole,
11 is a waveguide for synthesis, 12 is a metal plate, 13 is a dielectric plate,
14 is a coupling line, and 15 is a composite circuit. Note that the same reference numerals in the figures indicate the same or equivalent parts.

Claims (1)

【特許請求の範囲】[Claims] (1)少なくとも1枚以上の反射鏡面をもつアンテナ装
置において、 そのうちの1枚の反射鏡面に、反射面として使用する周
波数と異なる周波数の放射素子を設け、反射鏡面を反射
面及び放射面として、2つ以上の周波数で使用するよう
にしたことを特徴とするアンテナ装置。
(1) In an antenna device having at least one reflective mirror surface, one of the reflective mirror surfaces is provided with a radiating element having a frequency different from the frequency used as the reflective surface, and the reflective mirror surface is used as a reflective surface and a radiation surface. An antenna device characterized in that it is used at two or more frequencies.
JP21415688A 1988-08-29 1988-08-29 Antenna equipment Pending JPH0263202A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21415688A JPH0263202A (en) 1988-08-29 1988-08-29 Antenna equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21415688A JPH0263202A (en) 1988-08-29 1988-08-29 Antenna equipment

Publications (1)

Publication Number Publication Date
JPH0263202A true JPH0263202A (en) 1990-03-02

Family

ID=16651155

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21415688A Pending JPH0263202A (en) 1988-08-29 1988-08-29 Antenna equipment

Country Status (1)

Country Link
JP (1) JPH0263202A (en)

Similar Documents

Publication Publication Date Title
US5130718A (en) Multiple dichroic surface cassegrain reflector
EP0812029B1 (en) Plural frequency antenna feed
US6243049B1 (en) Multi-pattern antenna having independently controllable antenna pattern characteristics
JP2598541B2 (en) Light beam forming device for high frequency antenna array
US4342036A (en) Multiple frequency band, multiple beam microwave antenna system
US5543809A (en) Reflectarray antenna for communication satellite frequency re-use applications
EP0390350B1 (en) Low cross-polarization radiator of circularly polarized radiation
US3810185A (en) Dual polarized cylindrical reflector antenna system
US4821046A (en) Dual band feed system
US5805116A (en) Two-feed full duplex transmitter/receiver for ultra small-aperture satellite communications terminal
JP2839274B2 (en) Antenna system
US4525719A (en) Dual-band antenna system of a beam waveguide type
JPH0936656A (en) Distribution / synthesis device and antenna device
NO316419B1 (en) Compact grounded microbead degree radio using integrated monolith microbead degree circuits
GB796915A (en) Improvements in or relating to aerial systems
JPH0263202A (en) Antenna equipment
US12525714B2 (en) Cavity-backed antenna having controllable beam width
US20060050004A1 (en) Integrated feed horn device
JPH05175933A (en) Indoor communication system
JPH07226618A (en) Right-handed circularly polarized antenna
JPS61178682A (en) Transmitting and receiving apparatus
US2983918A (en) Bilateral transmission system
JP2000349535A (en) Primary radiator
US3444559A (en) Phased array multibeam formation antenna system
JPS58188940A (en) Multiple-branch antenna device