JPH01190146A - Transmission system - Google Patents

Transmission system

Info

Publication number
JPH01190146A
JPH01190146A JP63015042A JP1504288A JPH01190146A JP H01190146 A JPH01190146 A JP H01190146A JP 63015042 A JP63015042 A JP 63015042A JP 1504288 A JP1504288 A JP 1504288A JP H01190146 A JPH01190146 A JP H01190146A
Authority
JP
Japan
Prior art keywords
optical
transmission system
transmission
wired
space
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
JP63015042A
Other languages
Japanese (ja)
Inventor
Teruhito Nakamura
中村 照仁
Yuji Hara
原 勇二
Kiyoyuki Sawamura
沢村 清幸
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.)
Panasonic Electric Works Co Ltd
Original Assignee
Matsushita Electric Works 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 Matsushita Electric Works Ltd filed Critical Matsushita Electric Works Ltd
Priority to JP63015042A priority Critical patent/JPH01190146A/en
Publication of JPH01190146A publication Critical patent/JPH01190146A/en
Pending legal-status Critical Current

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  • Small-Scale Networks (AREA)
  • Selective Calling Equipment (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Optical Communication System (AREA)

Abstract

PURPOSE:To eliminate the need for wiring between the ceiling and ground by providing a satellite space transmission unit having an optical transmission section and an optical reception section in a transmission system having a LAN and a terminal space transmission unit respectively to the ceiling and ground. CONSTITUTION:A transmission line l0 is connected to the ceiling B and a terminal set 211 such as a presonal computer is connected to transmission lines l1, l2 on the ground A in the transmission system of LAN. Plural satellite space transmission units 101 are connected to the line l0 is and the terminal space transmission unit. 111 is connected to lines l1, l2. Each space transmission unit consists of the optical transmission section and the optical reception section converting the optical pulse into a transmission signal and the ceiling and ground are sent by optical communication. Thus, the wire between the ceiling and ground is not required.

Description

【発明の詳細な説明】 〔産業上の利用分野] 本発明はパーソナルフンピユータ等を利用してLANを
構成する伝送システムに関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a transmission system that configures a LAN using personal computer computers and the like.

[従来の技術1 従来、パーソナルコンピュータを端末機として使用した
LANでは有線伝送系を用いるため伝送ラインの配線を
近傍の端末機間においては床配線や机上配線で行い、少
し離れたパーソナルコンピュータ間や別のフロアへの配
線は天井への立ち上げ、立ち下げを行って配線する天井
配線等により実現している。
[Prior art 1] Traditionally, LANs that use personal computers as terminals use wired transmission systems, so the transmission lines are wired between nearby terminals using floor wiring or desktop wiring, and between personal computers that are a little apart or Wiring to another floor is accomplished by using ceiling wiring, etc., which involves wiring up and down to the ceiling.

[発明が解決しようとする課題〕 上述のような従来例では非常に配線工事への手間がかか
る上に美観的にも問題があった。
[Problems to be Solved by the Invention] In the conventional example as described above, wiring work is extremely time-consuming and aesthetically problematic.

本発明は上述の問題点に鑑みて為されたもので、地上側
の床或いは机上と天井との間の立ち上げ配線、立ち下げ
配線を無くして配線工事の手間を省き、且つ美観を損な
わない伝送システムを提供することを目的とし、更には
1台のサテライト用空間伝送ユニットと複数のターミナ
ル用空間伝送ユニットとの間でデータ伝送が行え、且つ
端末機の増設に討して容易に対応できる伝送システムを
提供することを目的とし、また更に光送受イε方向を自
在に設定できる伝送システムを提供することを目的とす
る。
The present invention has been made in view of the above-mentioned problems, and eliminates the need for rising and falling wiring between the floor or desk top and ceiling on the ground side, thereby saving the labor of wiring work and not impairing the aesthetic appearance. The purpose is to provide a transmission system that can perform data transmission between one satellite space transmission unit and multiple terminal space transmission units, and can easily accommodate the addition of terminals. It is an object of the present invention to provide a transmission system, and a further object of the present invention is to provide a transmission system in which the ε direction of optical transmission and reception can be freely set.

[課題を解決しようとする課題] 本発明は天井側に配設した有線伝送系の伝送ラインから
の伝送信号を光パルス信号に変換して送出する光送信部
と、光’j!W!J伝送系からの元パルス信号を受信し
て有線伝送系の伝送信号に復調して有線伝送系に送出す
る光受信部と、これら光送信部及び光受信部と有線伝送
系の伝送ラインとの間を電気的に接続するインターフェ
ース手段とからなるサテライト用空間伝送ユニットを天
井側に設けてあり、地上側に配設した有線伝送系の伝送
ラインからの伝送信号を光パルス信号に変換して送出す
る光送信部と、光空間伝送系からの光パルス信号を受信
して有線伝送系の伝送信号に復調して有線伝送系に送出
する先受M部と、これら光送信部及び光受信部と有線伝
送系の伝送フィンとの間を電気的に接続するインターフ
ェース手段とからなるターミナル用空間伝送ユニットを
地上側に設はサテライト用空間伝送ユニットとターミナ
ル用空間伝送ユニットとを1討1で対応させである。
[Problems to be Solved] The present invention provides an optical transmitter that converts a transmission signal from a transmission line of a wired transmission system installed on the ceiling side into an optical pulse signal and sends it out, and an optical 'j! W! An optical receiving section that receives the original pulse signal from the J transmission system, demodulates it into a transmission signal of the wired transmission system, and sends it to the wired transmission system, and a connection between these optical transmitting section and optical receiving section and the transmission line of the wired transmission system. A space transmission unit for satellites is installed on the ceiling and consists of an interface means for electrically connecting between an optical transmitting section that receives an optical pulse signal from an optical space transmission system, demodulates it into a transmission signal of a wired transmission system, and sends it to the wired transmission system; A terminal space transmission unit consisting of an interface means for electrically connecting with the transmission fin of the wired transmission system is installed on the ground side, and the satellite space transmission unit and the terminal space transmission unit are matched in one unit. It is.

サテライト用空間伝送ユニットには上記光送信部と、光
受信部と、インターフェース手段とを持つ回路ユニット
部を複数設け、各回路ユニット部サテライト用空間伝送
ユニット内の上記各回路ユニット部とターミナル用空間
伝送ユニットとを1討1で対応させてもよい。
The satellite spatial transmission unit is provided with a plurality of circuit unit sections each having the above-mentioned optical transmitting section, optical receiving section, and interface means, and each circuit unit section and the above-mentioned circuit unit section in the satellite spatial transmission unit and a terminal space are provided. It is also possible to have one correspondence with one transmission unit.

又各回路ユニット部の先受M部及び光送信部の光送受信
方向を設定するホーン状の光送受信方向設定治具をユニ
ット本体に回動自在に設けてもよい。
Further, a horn-shaped optical transmission/reception direction setting jig for setting the optical transmission/reception direction of the pre-receiving M part and the optical transmitting part of each circuit unit part may be rotatably provided in the unit body.

[作用] 而して端末機と端末機との間で半二重による双方向伝送
を行う場合には、一方の端末機からの送信信号は地上側
の伝送ラインによりターミナル用空間伝送ユニットに伝
えられて更にこのターミナル用空間伝送ユニットにより
光パルス信号に変換され、また更に光空間伝送によって
対応する天井側のサテライト用空間伝送ユニットへ伝え
られ、この空間伝送ユニットにより更に天井側の有線伝
送系の信号に変換されて天井に配設された伝送ラインを
通して別の空間伝送ユニットに送られ、この空間伝送ユ
ニットにより光パルス信号に再び変換されて、対応する
地上側のターミナル用空間伝送ユニットへ伝えられ、再
度地上側の有線伝送系の信号に変換されて対応する端末
機に取り込まれる。この端末機から他方の端末機への送
信は上述の経路とは逆の経路で行なわれる。
[Operation] When half-duplex bidirectional transmission is performed between terminals, the transmission signal from one terminal is transmitted to the terminal space transmission unit via the transmission line on the ground side. This signal is further converted into an optical pulse signal by this terminal space transmission unit, and is further transmitted to the corresponding satellite space transmission unit on the ceiling side by optical space transmission. It is converted into a signal and sent to another spatial transmission unit through a transmission line installed on the ceiling, and this spatial transmission unit converts it back into an optical pulse signal and transmits it to the corresponding terminal spatial transmission unit on the ground side. , it is converted again to a signal for the wired transmission system on the ground side, and then taken in by the corresponding terminal. Transmission from this terminal to the other terminal is performed via a route opposite to the above-mentioned route.

そして回路ユニット部をサテライト用空間伝送ユニット
に設けている場合には地上側のターミナル用空間伝送ユ
ニットとの対応は回路ユニット部の光送信部、光受信部
が行い、また光送受信方向の設定はホーン状の光送受信
方向設定治具を用いで行うと良い。
When the circuit unit is installed in the satellite space transmission unit, the optical transmitter and optical receiver of the circuit unit handle the correspondence with the terminal space transmission unit on the ground side, and the optical transmission and reception directions are set. It is best to use a horn-shaped optical transmission/reception direction setting jig.

[実施例] 以下本発明を実施例により説明する。[Example] The present invention will be explained below with reference to Examples.

第1図は実施例の全体的な構成を示し、天井B側には伝
送ラインI0を配設しである。地上A側では各伝送ライ
ン1..(12・・・にバーンナルコンピュータのよう
な端末機2,1・・・を接続しである。そして伝送ライ
ン10には複数のサテライト用空間伝送ユニット1゜1
・・・を接続し、また各伝送ライン12・・・には上記
サテライト用空間伝送ユニット1゜1・・・に対応する
ターミナル用空間伝送ユニット11、・・・を接続しで
ある。
FIG. 1 shows the overall configuration of the embodiment, in which a transmission line I0 is arranged on the ceiling B side. On the ground A side, each transmission line 1. .. (Terminals 2, 1, etc., such as burner computers, are connected to
. . . and each transmission line 12 . . . is connected to a terminal space transmission unit 11, .

第2図、第3図は本実施例の全体構成を更に模式化した
図面である。
FIGS. 2 and 3 are drawings further schematically showing the overall configuration of this embodiment.

第4図はサテライト用又はターミナル用の空間伝送ユニ
ット1の回路構成を示しており、空間伝送ユニット1に
は光パルス信号にNZRI信号のような伝送信号を変換
して送信させる光送信部3と、受信した光パルス信号を
伝送信号に復調する先受M部4とを備えるとともに、こ
れら光送信部3及び光受信部4と伝送ラインlとの間の
電気的インターフェース手段として伝送ラインlを介し
て伝送されてくるNZRI信号からなる伝送信号を光送
信部3へ通過或いは、遮断させるための受信デートを構
成する例えばR8−422用のラインレシーバ5と、受
信復調した伝送信号を伝送ラインlへ通過、或いは連断
させる送信デートを構成する例えばR8−422用のラ
イントライバ6と、これらラインレシーバ5と、ライン
トライバ6をオンオフ制御するドライバ/レシーバ切り
替え回路7と、切り替えのために送信信号の検出と、受
信信号の検出とを夫々行う送信信号検出回路8と、受信
信号検出回路9とを備えている。尚端末機2.・・・に
は伝送信号を取り込むラインレシーバ(図示せず)と、
伝送信号を送出するライントライバ(図示せず)と、信
号処理を行う信号処理回路(図示せず)とを備えている
Figure 4 shows the circuit configuration of the space transmission unit 1 for satellites or terminals. , and a pre-receiving M section 4 that demodulates the received optical pulse signal into a transmission signal. For example, a line receiver 5 for R8-422 constitutes a reception date for passing or blocking a transmission signal consisting of an NZRI signal transmitted to the optical transmitter 3, and a transmission signal received and demodulated is sent to the transmission line l. For example, a line driver 6 for R8-422 that constitutes a transmission date to pass or connect, a driver/receiver switching circuit 7 that controls on/off the line driver 6, and a transmission date for switching. It includes a transmitted signal detection circuit 8 and a received signal detection circuit 9 that detect signals and detect received signals, respectively. Terminal 2. ... includes a line receiver (not shown) that receives the transmission signal, and
It includes a line driver (not shown) that sends out transmission signals and a signal processing circuit (not shown) that performs signal processing.

而して第3図に示すように例えば端末機27.から伝送
信号が送信されるとその送信信号は地上側の伝送ライン
11によりターミナル用空間伝送ユニット1,1に伝え
られるとともに伝送ライン11に接続しである端末機2
+2,2+3へ伝えられる。ターミナル用空間伝送ユニ
ット1□では送信信号が送信信号検出回路8で検出され
、ドライバ/レシーバ切り替え回路7はこの検出に基づ
いて送信信号を取り込み光送信部3により光パルス信号
に変換し、光空間伝送によって対応する天井側のサテラ
イト用空間伝送ユニット1゜1へ送信する。
As shown in FIG. 3, for example, the terminal 27. When a transmission signal is transmitted from the terminal, the transmission signal is transmitted to the terminal space transmission unit 1, 1 through the transmission line 11 on the ground side, and is also transmitted to the terminal 2 which is connected to the transmission line 11.
It is transmitted to +2, 2+3. In the terminal space transmission unit 1□, the transmission signal is detected by the transmission signal detection circuit 8, and the driver/receiver switching circuit 7 takes in the transmission signal based on this detection, converts it into an optical pulse signal by the optical transmitter 3, and transmits it to the optical space. The data is transmitted to the corresponding satellite spatial transmission unit 1°1 on the ceiling side.

ここでデータ伝送は半二重で行なわれるので、光受信部
4で光パルス信号を受信した空間伝送ユニット1゜1で
は受信信号が光受信部4で復調され、この復調された信
号は受信信号検出回路9の検出出力によるドライバ/レ
シーバ切り替え回路7の働きでラインレシーバ6へ送り
込まれ、伝送ライン10上に送出される。天井Bに配設
された伝送ラインr0を通して送られてきた伝送信号を
取り込んだ別のターミナル用空間伝送ユニット1゜2,
1゜。
Since the data transmission is performed in half-duplex mode, the received signal is demodulated by the optical receiver 4 in the spatial transmission unit 1゜1 which receives the optical pulse signal at the optical receiver 4, and this demodulated signal is converted into the received signal. The detection output of the detection circuit 9 is used by the driver/receiver switching circuit 7 to send the signal to the line receiver 6 and onto the transmission line 10 . Another terminal space transmission unit 1゜2, which takes in the transmission signal sent through the transmission line r0 installed on the ceiling B.
1°.

は空間伝送ユニット111と同様に動作して光パルス信
号に伝送信号を再V変換して、対応する地上A側のター
ミナル用空間伝送ユニット1□ljl:11へ伝える。
operates in the same manner as the space transmission unit 111, re-converts the transmission signal into an optical pulse signal, and transmits it to the corresponding terminal space transmission unit 1□ljl:11 on the ground A side.

各ターミナル用空間伝送ユニツ)12.。Spatial transmission unit for each terminal)12. .

1.1はサテライト用空間伝送ユニット1゜1と同様に
働いて、再度有線伝送系の伝送信号に変換し、各伝送ラ
インI12・・・を通じで各端末機2□1・・・に送る
のである。つまり送信されたデータは全端末機に伝送さ
れることになる。
1.1 works in the same way as the satellite spatial transmission unit 1゜1, converts it again into a transmission signal for the wired transmission system, and sends it to each terminal 2□1... through each transmission line I12... be. In other words, the transmitted data will be transmitted to all terminals.

ここでドライバ/レシーバ切り替え回路7の働きで送受
M信号の切り替えが行なわれるため、有線伝送系と光空
間伝送系とが混在していても正常にシステムが動作する
ことになる。
Since the driver/receiver switching circuit 7 switches between the transmitted and received M signals, the system can operate normally even if the wired transmission system and the optical space transmission system coexist.

第5図は別の実施例を示しており、この実施例では工事
の手間、及びコストの面から先受M部4、光送信部3及
びインターフェース手段とからなる回路ユニット部11
Lt 1 b、 1 cの3組をサテライト用空間伝送
ユニット1゜に設けて、複数のターミナル用空間伝送ユ
ニツ)1.、.1□1113+に対応させたものである
。第6図(a)は3組の回路ユニット部1 at l 
b、 1 cをユニット本体に収納配置した配置例を示
している。勿W!#&6図(b)に示すように4組の回
路ユニット部1 a、 1 b、 1 et 1 dヲ
ユニット本体に収納配置しても良く、回路ユニット部の
個数は実施例に特に限定されない。
FIG. 5 shows another embodiment, in which a circuit unit section 11 consisting of a pre-receiving M section 4, an optical transmitting section 3, and an interface means is used in order to reduce construction time and cost.
Three sets of Lt 1 b and 1 c are provided in the satellite space transmission unit 1° to create a plurality of terminal space transmission units)1. ,. This corresponds to 1□1113+. FIG. 6(a) shows three sets of circuit units 1 at l.
An example of the arrangement in which the units b and 1c are housed in the unit body is shown. Of course! # & 6 As shown in FIG. 6(b), four sets of circuit units 1a, 1b, 1 et 1d may be housed and arranged in the unit body, and the number of circuit units is not particularly limited to the embodiment.

ここで回路ユニット部の収納部を各収納個数に対応して
予め準備しておけば、サテライト用空間伝送ユニット1
の回路ユニット部の収納個数の変更が即座に行え、ター
ミナルの増設時にも容易に対応することができる。
Here, if the storage areas of the circuit unit section are prepared in advance according to the number of storage units, the satellite space transmission unit 1
The number of stored circuit units can be changed instantly, and it is easy to accommodate the addition of terminals.

また天井B側の有線伝送系の伝送ライン10を省略すれ
ば1個のみでも各ターミナル用空間伝送ユニットに対す
る信号中継機としてできる。
Furthermore, if the transmission line 10 of the wired transmission system on the ceiling B side is omitted, even one can serve as a signal repeater for each terminal space transmission unit.

第5図実施例ではサテライト用空間伝送ユニット1゜は
単純にユニット本体の下面を各回路ユニット部111.
1 b、 1 cに合わせて分割しただけであるから送
受信方向の向きは固定されるため、向きの調整はターミ
ナル側で行うようにしであるがターミナル側からの光パ
ルス信号同士が重なりあってデータエラーの発生する恐
れがあるため、第7図に示す実施例では各回路ユニット
部1a、  lb、  ICに対応してホーン状の光送
受信方向股定治其10a、10b、10cを回動自在に
空間伝送ユニット1゜のユニット本体に収設し、送受信
方向を自由に設定できるようにしである。
In the embodiment shown in FIG. 5, the satellite space transmission unit 1° simply connects the bottom surface of the unit body to each circuit unit portion 111.
Since the direction of transmission and reception is fixed because it is only divided according to 1b and 1c, the direction should be adjusted on the terminal side, but the optical pulse signals from the terminal side overlap each other and the data is distorted. To prevent errors from occurring, in the embodiment shown in FIG. 7, horn-shaped optical transmitting/receiving direction fixing devices 10a, 10b, and 10c are made rotatable in correspondence with each circuit unit section 1a, lb, and IC. It is housed in the unit body of the spatial transmission unit 1°, and the transmission and reception directions can be freely set.

[発明の効果] 本発明は天井側に配設した有線伝送系の伝送ラインから
の伝送信号を光パルス信号に変換して送出する光送信部
と、光空間伝送系からの光パルス信号を受信して有線伝
送系の伝送信号に復調して有線伝送系に送出する光受信
部と、これら光送信部及び光受信部と有線伝送系の伝送
ラインとの間を電気的に接続するインターフェース手段
とからなるサテライト用空間伝送ユニットを天井側に設
け、地上側に配設した有線伝送系の伝送ラインからの伝
送信号を光パルス信号に変換して送出する光送信部と、
光空間伝送系からの光パルス信号を受信して有線伝送系
の伝送信号に復調して有線伝送系に送出する光受信部と
、これら光送信部属1光受信部と有線伝送系の伝送ライ
ンとの間を電気的に接続するインターフェース手段とか
らなるターミナル用空間伝送ユニットを地上側に設け、
サテライト用空間伝送ユニットとターミナル用空間伝送
ユニットとを1討1で対応させて半二重通信を行うよう
にさせであるから、従来のように地上側から天井へ伝送
ラインを立ち上がり配線したり、逆に立ち下がり配線し
たりする必要が無く、そのため配線工事の簡便化が図れ
、その上配線による美観上の問題も解決できるという効
果がある。
[Effects of the Invention] The present invention includes an optical transmitter that converts a transmission signal from a transmission line of a wired transmission system installed on the ceiling side into an optical pulse signal and sends it out, and an optical transmitter that receives an optical pulse signal from an optical space transmission system. an optical receiver that demodulates the signal into a transmission signal of the wired transmission system and sends it to the wired transmission system; and an interface means that electrically connects the optical transmitter and the optical receiver to the transmission line of the wired transmission system. an optical transmitter that converts a transmission signal from a transmission line of a wired transmission system arranged on the ground side into an optical pulse signal and sends it out;
An optical receiver that receives an optical pulse signal from an optical space transmission system, demodulates it into a transmission signal for a wired transmission system, and sends it to the wired transmission system; A terminal space transmission unit consisting of an interface means for electrically connecting between the terminals is provided on the ground side,
Since the space transmission unit for the satellite and the space transmission unit for the terminal are made to correspond in one unit to perform half-duplex communication, it is not necessary to run the transmission line from the ground side to the ceiling as in the past. On the other hand, there is no need for falling wiring, which simplifies the wiring work and also solves aesthetic problems caused by the wiring.

更に天井側に配設した有線伝送系の伝送ラインからの伝
送信号を光パルス信号に変換して送出する光送信部と、
光空間伝送系からの光パルス信号を受信して有線伝送系
の伝送信号に復調して有線伝送系に送出する光受信部と
、これら光送信部及び光受信部と有線伝送系の伝送ライ
ンとの間を電気的に接続するインターフェース手段とか
らなる回路ユニット部を複数備えたサテライト用空間伝
送ユニットを天井側に設けることにより、1台のサテラ
イト用空間伝送ユニットで複数のターミナル用空間伝送
ユニットに対応させることができるから、施工性の向上
とともにコストの低減が図れ、またターミナル増設にも
容易に対応できるという効果がある。
Furthermore, an optical transmitter that converts a transmission signal from a transmission line of a wired transmission system arranged on the ceiling side into an optical pulse signal and sends it out;
An optical receiver that receives an optical pulse signal from an optical space transmission system, demodulates it into a transmission signal of a wired transmission system, and sends it to the wired transmission system, and these optical transmitter and receiver, and a transmission line of the wired transmission system. By installing a space transmission unit for satellites on the ceiling side that is equipped with multiple circuit units consisting of interface means for electrically connecting between Since it can be adapted, it is possible to improve workability and reduce costs, and it also has the effect of easily responding to the expansion of terminals.

また各回路ユニット部の光受信部及び光透M部の光送受
信方向を設定するホーン状の光送受信方向設定治具をユ
ニット本体に回動自在に設けたサテライト用空間伝送ユ
ニットを天井側に設ければ、光送受信方向を自由に設定
できるから光空間伝送系のデータエラーの発生が少ない
適正な方向に光送受信方向を定めることができ、ターミ
ナル増設への対応のより一屑の簡便化が図れるという効
果がある。
In addition, a space transmission unit for satellite is installed on the ceiling side, in which a horn-shaped light transmission/reception direction setting jig is rotatably mounted on the unit body to set the light transmission/reception direction of the light receiving section and the light transmitting M section of each circuit unit. If you do so, you can freely set the direction of optical transmission and reception, so you can set the direction of optical transmission and reception in an appropriate direction that reduces the occurrence of data errors in the optical space transmission system, making it even easier to accommodate the expansion of terminals. There is an effect.

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

#41図は本発明の一実施例の配置例図、第2図、第3
図は同上の模式化した構成図、第4図は同上使用の空間
伝送ユニットの回路構成図、第5図は本発明の別の実施
例の構成図、$6図(、)(b)は同上の空間伝送ユニ
ットの回路ユニット部の配置構成説明図、第7図は本発
明の他の実施例の構成図である。 1゜1・・・サテライト用空間伝送ユニット、I I+
・・・ターミナル用空間伝送ユニット、1 lit 1
 b、 1 c・・・回路ユニット部、10a、10b
、10c・・・光送受信方向設定治具、21.・・・端
末機、3・・・光送信部、4・・・光受信部、i o 
、1 l−12−13・・・伝送ラインである。 代理人 弁理士 石 1)長 七 第3図 Jo 第4図 第5図 Jo 第6図 (a)            (b) ゛第7図
#41 is a layout example diagram of one embodiment of the present invention, Figures 2 and 3
The figure is a schematic block diagram of the same as above, Figure 4 is a circuit block diagram of the space transmission unit used in the above, Figure 5 is a block diagram of another embodiment of the present invention, and Figure 6 (,) (b) is a block diagram of another embodiment of the present invention. FIG. 7, which is an explanatory diagram of the arrangement and configuration of the circuit unit section of the space transmission unit same as above, is a configuration diagram of another embodiment of the present invention. 1゜1...Satellite space transmission unit, I I+
...Space transmission unit for terminal, 1 lit 1
b, 1 c... circuit unit section, 10a, 10b
, 10c... Optical transmission/reception direction setting jig, 21. ...terminal device, 3...optical transmitter, 4...optical receiver, i o
, 1 l-12-13...transmission line. Agent Patent Attorney Ishi 1) Chief 7 Figure 3 Jo Figure 4 Figure 5 Jo Figure 6 (a) (b) ゛Figure 7

Claims (3)

【特許請求の範囲】[Claims] (1)端末機を複数台接続してデータ伝送を行う有線伝
送系の一部に、光空間伝送系を用いた伝送システムにお
いて、天井側に配設した有線伝送系の伝送ラインからの
伝送信号を光パルス信号に変換して送出する光送信部と
、光空間伝送系からの光パルス信号を受信して有線伝送
系の伝送信号に復調して有線伝送系に送出する光受信部
と、これら光送信部及び光受信部と有線伝送系の伝送ラ
インとの間を電気的に接続するインターフェース手段と
からなるサテライト用空間伝送ユニットを天井側に設け
、地上側に配設した有線伝送系の伝送ラインからの伝送
信号を光パルス信号に変換して送出する光送信部と、光
空間伝送系からの光パルス信号を受信して有線伝送系の
伝送信号に復調して有線伝送系に送出する光受信部と、
これら光送信部及び光受信部と有線伝送系の伝送ライン
との間を電気的に接続するインターフェース手段とから
なるターミナル用空間伝送ユニットを地上側に設け、サ
テライト用空間伝送ユニットとターミナル用空間伝送ユ
ニットとを1対1で対応させて半二重通信を行うように
して成ることを特徴とする伝送システム。
(1) In a transmission system that uses an optical space transmission system as part of a wired transmission system that connects multiple terminals and transmits data, the transmission signal from the transmission line of the wired transmission system installed on the ceiling side. an optical transmitter that converts the optical pulse signal into an optical pulse signal and sends it out; an optical receiver that receives the optical pulse signal from the optical space transmission system, demodulates it into a transmission signal for the wired transmission system, and sends it to the wired transmission system; A satellite space transmission unit consisting of an optical transmitter and an interface means for electrically connecting the optical receiver and the transmission line of the wired transmission system is installed on the ceiling side, and the wired transmission system is installed on the ground side. An optical transmitter that converts the transmission signal from the line into an optical pulse signal and sends it out, and an optical transmitter that receives the optical pulse signal from the optical space transmission system, demodulates it into a transmission signal for the wired transmission system, and sends it out to the wired transmission system. a receiving section;
A terminal spatial transmission unit consisting of an interface means for electrically connecting these optical transmitting parts and optical receiving parts to the transmission line of the wired transmission system is provided on the ground side, and the satellite spatial transmission unit and the terminal spatial transmission unit are provided on the ground side. A transmission system characterized in that the transmission system is configured to perform half-duplex communication by providing one-to-one correspondence between units.
(2)端末機を複数台接続してデータ伝送を行う有線伝
送系の一部に、光空間伝送系を用いた伝送システムにお
いて、天井側に配設した有線伝送系の伝送ラインからの
伝送信号を光パルス信号に変換して送出する光送信部と
、光空間伝送系からの光パルス信号を受信して有線伝送
系の伝送信号に復調して有線伝送系に送出する光受信部
と、これら光送信部及び光受信部と有線伝送系の伝送ラ
インとの間を電気的に接続するインターフェース手段と
からなる回路ユニット部を複数備えたサテライト用空間
伝送ユニットを天井側に設け、地上側に配設した有線伝
送系の伝送ラインからの伝送信号を光パルス信号に変換
して送出する光送信部と、光空間伝送系からの光パルス
信号を受信して有線伝送系の伝送信号に復調して有線伝
送系に送出する光受信部と、これら光送信部及び光受信
部と有線伝送系の伝送ラインとの間を電気的に接続する
インターフェース手段とからなるターミナル用空間伝送
ユニットを地上側に設け、サテライト用空間伝送ユニッ
ト内の上記各回路ユニット部とターミナル用空間伝送ユ
ニットとを1対1で対応させて半二重通信を行うように
して成ることを特徴とする伝送システム。
(2) In a transmission system that uses an optical space transmission system as part of the wired transmission system that connects multiple terminals and transmits data, the transmission signal from the transmission line of the wired transmission system installed on the ceiling side. an optical transmitter that converts the optical pulse signal into an optical pulse signal and sends it out; an optical receiver that receives the optical pulse signal from the optical space transmission system, demodulates it into a transmission signal for the wired transmission system, and sends it to the wired transmission system; A space transmission unit for a satellite is provided on the ceiling side, and is equipped with a plurality of circuit unit sections each consisting of an interface means for electrically connecting between an optical transmitting section, an optical receiving section, and a transmission line of a wired transmission system, and is arranged on the ground side. An optical transmitter that converts the transmission signal from the transmission line of the wired transmission system installed into an optical pulse signal and sends it out, and an optical transmitter that receives the optical pulse signal from the optical space transmission system and demodulates it into the transmission signal of the wired transmission system. A space transmission unit for a terminal is provided on the ground side, which consists of an optical receiver that sends out data to the wired transmission system, and an interface means that electrically connects these optical transmitters and optical receivers to the transmission line of the wired transmission system. A transmission system characterized in that each of the circuit units in the satellite space transmission unit and the terminal space transmission unit are made to correspond one-to-one to perform half-duplex communication.
(3)端末機を複数台接続してデータ伝送を行う有線伝
送系の一部に、光空間伝送系を用いた伝送システムにお
いて、天井側に配設した有線伝送系の伝送ラインからの
伝送信号を光パルス信号に変換して送出する光送信部と
、光空間伝送系からの光パルス信号を受信して有線伝送
系の伝送信号に復調して有線伝送系に送出する光受信部
と、これら光送信部及び光受信部と有線伝送系の伝送ラ
インとの間を電気的に接続するインターフェース手段と
からなる回路ユニット部を複数備えるとともに各回路ユ
ニット部の光受信部及び光送信部の光送受信方向を設定
するホーン状の光送受信方向設定治具をユニット本体に
回動自在に設けたサテライト用空間伝送ユニットを天井
側に設け、地上側に配設した有線伝送系の伝送ラインか
らの伝送信号を光パルス信号に変換して送出する光送信
部と、光空間伝送系からの光パルス信号を受信して有線
伝送系の伝送信号に復調して有線伝送系に送出する光受
信部と、これら光送信部及び光受信部と有線伝送系の伝
送ラインとの間を電気的に接続するインターフェース手
段とからなるターミナル用空間伝送ユニットを地上側に
設け、サテライト用空間伝送ユニット内の上記各回路ユ
ニット部とターミナル用空間伝送ユニットとを1対1で
対応させて半二重通信を行うようにして成ることを特徴
とする伝送システム。
(3) In a transmission system that uses an optical space transmission system as part of a wired transmission system that connects multiple terminals and transmits data, the transmission signal from the transmission line of the wired transmission system installed on the ceiling side. an optical transmitter that converts the optical pulse signal into an optical pulse signal and sends it out; an optical receiver that receives the optical pulse signal from the optical space transmission system, demodulates it into a transmission signal for the wired transmission system, and sends it to the wired transmission system; It is equipped with a plurality of circuit unit sections consisting of an optical transmitting section and an interface means for electrically connecting the optical receiving section and the transmission line of the wired transmission system, and the optical transmitting and receiving section of the optical receiving section and the optical transmitting section of each circuit unit section. A space transmission unit for satellite is installed on the ceiling side with a horn-shaped optical transmission/reception direction setting jig that is rotatably attached to the unit body, and the transmission signal is transmitted from the transmission line of the wired transmission system installed on the ground side. an optical transmitter that converts the optical pulse signal into an optical pulse signal and sends it out; an optical receiver that receives the optical pulse signal from the optical space transmission system, demodulates it into a transmission signal for the wired transmission system, and sends it to the wired transmission system; A terminal space transmission unit consisting of an optical transmitter, an interface means for electrically connecting the optical receiver and the transmission line of the wired transmission system is provided on the ground side, and each of the above-mentioned circuit units in the satellite space transmission unit is provided on the ground side. A transmission system characterized in that a terminal space transmission unit and a terminal space transmission unit are in one-to-one correspondence to perform half-duplex communication.
JP63015042A 1988-01-26 1988-01-26 Transmission system Pending JPH01190146A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63015042A JPH01190146A (en) 1988-01-26 1988-01-26 Transmission system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63015042A JPH01190146A (en) 1988-01-26 1988-01-26 Transmission system

Publications (1)

Publication Number Publication Date
JPH01190146A true JPH01190146A (en) 1989-07-31

Family

ID=11877781

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63015042A Pending JPH01190146A (en) 1988-01-26 1988-01-26 Transmission system

Country Status (1)

Country Link
JP (1) JPH01190146A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5786921A (en) * 1994-08-15 1998-07-28 Actisys Corporation Infrared communication device for multistandard operations
US6099608A (en) * 1998-07-30 2000-08-08 3M Innovative Properties Company Rotating filtration cartridge and blower for HVAC applications
US6099609A (en) * 1998-07-30 2000-08-08 3M Innovative Properties Company Moving sorbent filter device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5786921A (en) * 1994-08-15 1998-07-28 Actisys Corporation Infrared communication device for multistandard operations
US6099608A (en) * 1998-07-30 2000-08-08 3M Innovative Properties Company Rotating filtration cartridge and blower for HVAC applications
US6099609A (en) * 1998-07-30 2000-08-08 3M Innovative Properties Company Moving sorbent filter device

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