JPS5841696B2 - Titanium sakuhoshiki - Google Patents
Titanium sakuhoshikiInfo
- Publication number
- JPS5841696B2 JPS5841696B2 JP50006101A JP610175A JPS5841696B2 JP S5841696 B2 JPS5841696 B2 JP S5841696B2 JP 50006101 A JP50006101 A JP 50006101A JP 610175 A JP610175 A JP 610175A JP S5841696 B2 JPS5841696 B2 JP S5841696B2
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- Japan
- Prior art keywords
- signal
- frequency
- pilot
- transmission line
- pilot signal
- 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.)
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- Monitoring And Testing Of Transmission In General (AREA)
Description
【発明の詳細な説明】
本発明は複数個の中継器および線路を多数縦続接続して
構成する伝送路の障害位置探索方式に関するものである
。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for locating a fault in a transmission line configured by cascading a plurality of repeaters and lines.
従来知られている障害位置探索方式の例を第1図および
第2図に示す。Examples of conventionally known fault location searching methods are shown in FIGS. 1 and 2.
第1図は抵抗監視方式と称されるもので、1は伝送路、
2,2′は監視用介在対、3は被監視中継器、4はそれ
ぞれ中継器毎に割り当てられた抵抗、5はパイロット検
出回路、6は開閉器である。Figure 1 shows what is called a resistance monitoring system, where 1 is a transmission line,
2 and 2' are monitoring intervening pairs, 3 is a monitored repeater, 4 is a resistor assigned to each repeater, 5 is a pilot detection circuit, and 6 is a switch.
パイロット検出回路5の出力によりパイロット信号レベ
ルの異常時に閉じる開閉器6が閉じるように構成されて
いる。The output of the pilot detection circuit 5 causes a switch 6 to close when the pilot signal level is abnormal.
ここに、パイロット信号とは伝送周波数帯域の中の1周
波を選び、伝送路の監視制御のために使用する信号をい
う。Here, the pilot signal refers to a signal that selects one frequency within the transmission frequency band and is used for monitoring and controlling the transmission path.
いまかりに、1個の中継器3の障害によりパイロット信
号レベルが異常になればその位置から先の中継点の開閉
器6が閉じる。If the pilot signal level suddenly becomes abnormal due to a failure in one repeater 3, the switch 6 at the relay point beyond that position is closed.
端局から介在対2,2′間の抵抗値をMIIQすれば、
その抵抗値により障害位置を知ることができる。If we MIIQ the resistance value between the terminal station and the intervening pair 2, 2', we get
The location of the fault can be determined by its resistance value.
第2図は同じ〈従来のS■倍信号用いる方式で、図中1
は往路、1′は復路の伝送路、3,3′は被監視中継器
、7はそれぞれの通過周波数帯域を有するSVF波器で
ある。Figure 2 shows the same method (conventional method using S■ times signal), 1 in the figure.
1 is an outbound transmission line, 1' is a return transmission line, 3 and 3' are monitored repeaters, and 7 is an SVF waveform having its respective pass frequency band.
ここに、SV信号とは伝送路の伝送可能周波数帯域の一
部に設けられた監視周波数帯域から、各中継器毎に異な
る周波数を割当て、障害位置探索を行なうための信号を
いう。Here, the SV signal refers to a signal for searching for a fault location by assigning a different frequency to each repeater from a monitoring frequency band provided in a part of the transmittable frequency band of the transmission path.
またSVP波器とはこれに使用される割当てられた周波
数のE波器である。Further, the SVP wave device is an E wave device with an assigned frequency used for this purpose.
f1〜f3はS■倍信号周波数を示す。f1 to f3 indicate S■ times the signal frequency.
いま端局から人ないしはDに周波数f1〜f3を一部レ
ベルで伝送路1あるいは1′に送出し、BないしはCに
てその到着レベルを測定スれば異常個所の探索が可能で
ある。Now, if the terminal station transmits frequencies f1 to f3 at some levels to a person or D to the transmission line 1 or 1', and measures the arrival level at B or C, it is possible to search for an abnormal location.
これらはいずれもよく知られた従来の伝送路障害位置探
索方式であるが、第1図の方式の場合、パイロット信号
周波数は通常伝送周波数帯域の高周波端に選ばれるので
パイロット信号レベルの異常監視では、伝送周波数帯域
内の高周波における障害には有用であっても、低周波に
おける障害に対しては位置探索が不可能になる欠点があ
った。All of these are well-known conventional transmission path fault location methods, but in the case of the method shown in Figure 1, the pilot signal frequency is usually selected at the high frequency end of the transmission frequency band, so it is not possible to monitor abnormalities in the pilot signal level. Although it is useful for failures at high frequencies within the transmission frequency band, it has the disadvantage that position searching becomes impossible for failures at low frequencies.
また監視用として信号線以外に1対だけ余分の線路を必
要とする欠点があった。Another drawback is that it requires an extra pair of lines in addition to the signal lines for monitoring purposes.
第2図の場合も通常SV信号周波数は伝送信号に影響を
与えないよう、伝送周波数帯域の低周波側の一周波が選
ばれるため、高域側の監視ができない第1図の場合と同
様な問題があった。In the case of Fig. 2, the SV signal frequency is normally selected as one frequency on the low frequency side of the transmission frequency band so as not to affect the transmission signal, so it is similar to the case of Fig. 1 that the high frequency side cannot be monitored. There was a problem.
このことは広帯域伝送路の場合特に不都合である。This is particularly disadvantageous in the case of broadband transmission lines.
たとえば第2図の例で帯域幅が大きいビデオ信号のベー
スバンド伝送を行なう場合など、各中継器の高周波利得
の異常や線路の高周波特性不良により画質の劣化が生じ
ているにもかかわらず、低周波のSV倍信号は異常が認
められないような障害が起きると、この方式による監視
局からの障害場所の探索は不可能である。For example, in the case of baseband transmission of a video signal with a large bandwidth in the example shown in Figure 2, even though the image quality has deteriorated due to an abnormality in the high frequency gain of each repeater or poor high frequency characteristics of the line, the If a fault occurs in which no abnormality is recognized in the SV multiplied frequency signal, it is impossible to search for the fault location from the monitoring station using this method.
すなわちこれら従来の方式を単一に用いたのでは、各中
継器毎に、単一周波で障害監視を行なっているので、S
■信号周波数あるいはパイロット周波数以外の帯域にお
ける障害が発生すると、その位置探索は不可能であると
いう欠点があった。In other words, when these conventional methods are used alone, fault monitoring is performed using a single frequency for each repeater, so S
■If a fault occurs in a band other than the signal frequency or pilot frequency, there is a drawback that it is impossible to locate the fault.
本発明による障害位置探索方式は、このような従来の方
式の欠点を改良した障害位置探索方式を提供することを
目的とする。The object of the fault location search method according to the present invention is to provide a fault location search method that improves on the drawbacks of the conventional methods.
本発明の方式はパイロット信号レベルの異常を検出し、
これよりsvp波器への回路を開閉させて、線香位置の
探索を行なうことを特徴とする。The method of the present invention detects an abnormality in the pilot signal level,
The feature is that the circuit to the svp wave device is opened and closed from this, and the incense stick position is searched.
すなわち本発明は、複数の中継器および線路が交互に縦
続接続されて構成された伝送路の伝送可能周波数帯域に
、パイロット信号およびSV倍信号伝送する有線伝送路
の障害位置探索方式において、前記伝送可能周波数帯域
の低周波領域および高周波領域のうちのいずれか一方の
領域に前記パイロット信号を伝送し他方の領域に前記各
中継器毎に周波数を割当てたS■信号を伝送するように
周波数配置され、前記Sv信号用の帰線と、前記伝送路
とこの帰線との間に接続された前記S■信号を抽出する
SVP波器と、前記伝送路に接続され前記パイロット信
号の異状を検出するパイロット検出器と、この検出器の
検出出力に応答して前記svP波器の信号通路を開閉す
る手段とを備え、前記伝送路に送出された前記SV倍信
号前記帰線にて監視することを特徴とする。That is, the present invention provides a fault location search method for a wired transmission line in which a pilot signal and an SV double signal are transmitted in a transmittable frequency band of a transmission line configured by alternately cascading a plurality of repeaters and lines. Frequency arrangement is such that the pilot signal is transmitted to one of the low frequency region and the high frequency region of the available frequency band, and the S signal to which a frequency is assigned to each repeater is transmitted to the other region. , a return line for the Sv signal, an SVP waver connected between the transmission line and the return line for extracting the S■ signal, and a SVP waveform connected to the transmission line for detecting abnormalities in the pilot signal. comprising a pilot detector and a means for opening and closing the signal path of the svp wave device in response to the detection output of this detector, and monitoring the SV multiplied signal sent to the transmission path on the return line. Features.
また、端局もしくは中継器でパイロット信号レベルを人
為的に変化させ、強制的にSVp波器回路を開閉するこ
とのできる手段を備えたことを特徴とする。Further, the present invention is characterized in that it includes a means for artificially changing the pilot signal level at a terminal station or a repeater to forcibly open and close the SVp waveter circuit.
以下、本発明を図面により詳しく説明する。Hereinafter, the present invention will be explained in detail with reference to the drawings.
第3図は本発明の実施例である。FIG. 3 shows an embodiment of the invention.
図中1,1′は伝送路、3,3′は中継器、5,5′は
パイロット検出回路、6は開閉器、7はSVP波器であ
る。In the figure, 1 and 1' are transmission lines, 3 and 3' are repeaters, 5 and 5' are pilot detection circuits, 6 is a switch, and 7 is an SVP wave device.
伝送路1,1′には中継器3,3′が多数縦続接続され
、広帯域伝送を行なうよう構成されている。A large number of repeaters 3, 3' are connected in cascade to the transmission lines 1, 1', and are configured to perform broadband transmission.
各中継点では中継器3の出力は開閉器6およびS’M波
器7を介して中継器3′の入力と結合され、開閉器6は
中継器3,3′の出力に結合されたパイロット検出器5
,5′のレベル異常出力により動作するよう構成されて
いる。At each relay point, the output of the repeater 3 is coupled to the input of the repeater 3' via a switch 6 and an S'M wave unit 7, and the switch 6 is connected to the pilot terminal coupled to the output of the repeaters 3 and 3'. Detector 5
, 5'.
ここでは伝送路1と1′が相互にS■信号用の帰線とな
る。Here, the transmission lines 1 and 1' mutually serve as return lines for the S■ signal.
第3図の構成で、開閉器6をパイロット信号レベルが正
常な場合には閉じ、異常の場合に開くように設定し、S
v信号周波数を伝送帯域内の低周波側に、パイロット周
波数を高周波側に選ぶものとする。In the configuration shown in Fig. 3, the switch 6 is set to close when the pilot signal level is normal and open when it is abnormal, and
It is assumed that the v signal frequency is selected on the low frequency side within the transmission band, and the pilot frequency is selected on the high frequency side.
かりに中継器3の1個がその高周波部分の伝送特性に劣
化をきたして障害となり、低周波側で見る限りは正常で
あるとすれば、障害点以降のパイロット信号レベルが異
常となり開閉器6が開となる。If one of the repeaters 3 deteriorates in the transmission characteristics of its high frequency part and becomes a fault, and if it is normal as far as the low frequency side is concerned, then the pilot signal level after the fault point becomes abnormal and the switch 6 It becomes open.
端局よりDKSV信号f1〜f3を送出し、Cにてf1
〜f3のレベルを観測すると、障害位置の探索が可能と
なる。DKSV signals f1 to f3 are sent from the terminal station, and f1 is sent at C.
By observing the level of ~f3, it becomes possible to search for the location of the fault.
また逆に低周波部分の伝送特性が劣化して、パイロット
信号ノベルは正常であるときには第2図で述べた従来の
場合と同じ方法で障害位置の探索が可能となる。Conversely, when the transmission characteristics of the low frequency portion deteriorate and the pilot signal signal is normal, it becomes possible to search for the fault location using the same method as in the conventional case described in FIG.
このように本発明の方式によれば、伝送周波数帯域の低
周波側あるいは高周波側の部分的な障害に対しても、余
分な監視用介在対を必要とせずに障害位置探索が可能と
なり、はぼ伝送路が形成する全周波数帯域の障害に対し
て障害探索が有効に行なわれる利点がある。As described above, according to the method of the present invention, even if there is a partial fault on the low frequency side or the high frequency side of the transmission frequency band, the fault location can be searched without requiring an extra monitoring intervening pair. This method has the advantage that fault searching can be performed effectively for faults in all frequency bands formed by the transmission path.
第4図に本発明を実施した別の例を示す。FIG. 4 shows another example of implementing the present invention.
これはパイロット信号が正常時にはS’M波器の回路を
開いておき、異常時に閉じるよう構成されたものである
。This is configured to keep the S'M wave device circuit open when the pilot signal is normal and close it when the pilot signal is abnormal.
各開閉器6,6はパイロット信号レベルが正常な場合は
開き、異常な場合は閉じるようパイロット検出器5,5
ノにより制御される。Each switch 6,6 opens when the pilot signal level is normal, and closes when the pilot signal level is abnormal.
Controlled by
各部の符号およびその動作は第3図のものと同一である
。The symbols of each part and their operations are the same as those in FIG. 3.
このような方式では、パイロット信号レベルが異常の場
合には、SVP波器回路が自動的に入るので第2図に説
明した従来方式と同じ方法で位置探索を行なうことがで
きる。In such a system, when the pilot signal level is abnormal, the SVP waveform circuit is automatically entered, so that the position search can be performed in the same manner as the conventional system described in FIG.
運用中にSV信号周波数帯のみが異常になったような場
合には、端局または中間の中継器のところで、パイロッ
ト信号の送出を弱める等人為的に異常レベルとすること
により、強制的に全ての開閉器6,6を閉じれば、第2
図に述べた従来の方式と全く同じことになる。If only the SV signal frequency band becomes abnormal during operation, all signals can be forcibly removed by artificially setting the pilot signal to an abnormal level by weakening the pilot signal transmission at the terminal station or intermediate repeater. If the switches 6, 6 are closed, the second
This is exactly the same as the conventional method shown in the figure.
ここで、このようにパイロット信号の正常時に回路が開
いているものは、伝送路が正常な時にSVP波器が伝送
路と接続されているものと比較゛し、SVf’波器回路
には、伝送信号に影響を与えないよう通過周波数帯域で
の出入力インピーダンス、阻止周波数帯域での減衰量な
ど厳しい特性が要求されることがない。Here, a circuit in which the circuit is open when the pilot signal is normal is compared with a circuit in which the SVP wave device is connected to the transmission path when the transmission path is normal, and the SVf' wave device circuit has the following characteristics. Strict characteristics such as input and output impedance in the pass frequency band and attenuation in the stop frequency band are not required so as not to affect the transmitted signal.
従ってSvP波器回路の特性は、それほど厳しくない簡
単なものを使用することのできる利点もある。Therefore, there is an advantage that the characteristics of the SvP waveform circuit can be simple and not so strict.
第5図は本発明を実施した別の例で複数システムの監視
を同時に行なう場合に応用したものである。FIG. 5 shows another example of implementing the present invention, which is applied to the case where a plurality of systems are monitored simultaneously.
図中1はそれぞれ伝送路、8は共通の監視用伝送線でS
v信号用の帰線、3は被監視中継器、5はパイロット検
出器、6は開閉器、Tはsv信号周波数f1.f2それ
ぞれの通過域をもつSVF波器である。In the figure, 1 is each transmission line, and 8 is a common monitoring transmission line.
3 is the monitored repeater, 5 is the pilot detector, 6 is the switch, T is the sv signal frequency f1. It is an SVF waveformer with a passband for f2.
第5図の構成のものは複数システムの監視に、各中継点
毎に1個のSVP波器を共用することができ、方式構成
が経済的になる利点がある。The configuration shown in FIG. 5 has the advantage that one SVP transducer can be shared for each relay point for monitoring a plurality of systems, making the system configuration economical.
以上述べたように、本発明の方式では信号線以外の監視
用介在対線を必要とせず、簡単な構成で伝送周波数帯域
の全帯域にわたって有効に障害位置探索が行なうことが
できる優れた効果がある。As described above, the method of the present invention does not require any intervening pair of monitoring wires other than the signal line, and has the excellent effect of effectively performing fault location search over the entire transmission frequency band with a simple configuration. be.
なお、上記説明で述べたパイロット信号を高周波に、S
V信号を低周波に配置することは本発明の範囲を限定す
るものでなく、周波数配置は方式適用に際して任意に選
ぶことができることは云うまでもない。In addition, the pilot signal mentioned in the above explanation is converted to a high frequency, S
It goes without saying that placing the V signal at a low frequency does not limit the scope of the present invention, and the frequency placement can be arbitrarily selected depending on the application of the system.
また、本発明の方式はパイロット信号レベルによる自動
利得制御方式等、他の方式と同時時・・くイロット信号
を共用して使用することも可能である。Further, the method of the present invention can be used simultaneously with other methods, such as an automatic gain control method based on the pilot signal level, by sharing the pilot signal.
第1図および第2図は従来例の方式構成図。
第3図は本発明実施例の構成図。
第4図は本発明の別の実施例を示す構成図。
第5図は本発明の別の実施例を示す構成図。
1.1′・・・・・・伝送路、2,2′・・・・・・介
在線、3,3′・・・・・・中継器、4・・・・・・抵
抗器、5・・・・・・パイロット検出器、6・・・・・
・開閉器、7・・・・・・SVP波器、8・・・・・・
監視用伝送線。FIG. 1 and FIG. 2 are system configuration diagrams of a conventional example. FIG. 3 is a configuration diagram of an embodiment of the present invention. FIG. 4 is a configuration diagram showing another embodiment of the present invention. FIG. 5 is a configuration diagram showing another embodiment of the present invention. 1.1'...Transmission line, 2,2'...Intervening line, 3,3'...Relayer, 4...Resistor, 5 ...Pilot detector, 6...
・Switch, 7...SVP wave device, 8...
Monitoring transmission line.
Claims (1)
成された伝送路の伝送可能周波数帯域に、パイロット信
号およびSv倍信号伝送する有線伝送路の障害位置探索
方式において、前記伝送可能周波数帯域の低周波領域お
よび高周波領域のうちのいずれか一方の領域に前記パイ
ロット信号を伝送し他方の領域に前記各中継器毎に周波
数を割当てたS■倍信号伝送するように周波数配置され
、前記SV信号用の帰線と、前記伝送路とこの帰線との
間に接続された前記Sv倍信号抽出するS■沢波器と、
前記伝送路に接続され前記パイロット信号の異状を検出
するパイロット検出器と、この検出器の検出出力に応答
して前記SVF波器の信号通路を開閉する手段とを備え
、前記伝送路に送出された前記S■倍信号前記帰線にて
監視することを特徴とする有線伝送路の障害位置探索方
式。 2、特許請求の範囲第1項記載の方式において、端局も
しくは中継器にパイロット信号のレベルを人為的に変化
することのできる手段を備えたことを特徴とする有線伝
送路の障害位置探索方式。[Claims] 1. In a fault location search method for a wired transmission line that transmits a pilot signal and an Sv multiplied signal in the transmission frequency band of a transmission line configured by alternately cascading a plurality of repeaters and lines, The frequency is set such that the pilot signal is transmitted in one of the low frequency region and the high frequency region of the transmittable frequency band, and the S ■ times signal, which is assigned a frequency for each repeater, is transmitted in the other region. an S waveformer for extracting the Sv multiplied signal, which is arranged and connected between the return line for the SV signal and the transmission line and the return line;
a pilot detector connected to the transmission path to detect an abnormality in the pilot signal; and means for opening and closing a signal path of the SVF waver in response to a detection output of the detector; A system for locating a fault in a wired transmission line, characterized in that said S■ times signal is monitored on said return line. 2. A method for locating a fault in a wired transmission line according to claim 1, characterized in that the terminal station or repeater is provided with means for artificially changing the level of the pilot signal. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP50006101A JPS5841696B2 (en) | 1975-01-13 | 1975-01-13 | Titanium sakuhoshiki |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP50006101A JPS5841696B2 (en) | 1975-01-13 | 1975-01-13 | Titanium sakuhoshiki |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5180708A JPS5180708A (en) | 1976-07-14 |
| JPS5841696B2 true JPS5841696B2 (en) | 1983-09-13 |
Family
ID=11629097
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP50006101A Expired JPS5841696B2 (en) | 1975-01-13 | 1975-01-13 | Titanium sakuhoshiki |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5841696B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4491968A (en) * | 1983-04-07 | 1985-01-01 | Comsonics, Inc. | Status monitor |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5157212A (en) * | 1974-11-15 | 1976-05-19 | Hitachi Ltd |
-
1975
- 1975-01-13 JP JP50006101A patent/JPS5841696B2/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5180708A (en) | 1976-07-14 |
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