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JPS6030188B2 - Electrostatic induction voltage extraction device for power transmission lines - Google Patents
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JPS6030188B2 - Electrostatic induction voltage extraction device for power transmission lines - Google Patents

Electrostatic induction voltage extraction device for power transmission lines

Info

Publication number
JPS6030188B2
JPS6030188B2 JP58177061A JP17706183A JPS6030188B2 JP S6030188 B2 JPS6030188 B2 JP S6030188B2 JP 58177061 A JP58177061 A JP 58177061A JP 17706183 A JP17706183 A JP 17706183A JP S6030188 B2 JPS6030188 B2 JP S6030188B2
Authority
JP
Japan
Prior art keywords
power transmission
transmission line
conductive wire
electrostatic induction
voltage
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.)
Expired
Application number
JP58177061A
Other languages
Japanese (ja)
Other versions
JPS5983537A (en
Inventor
桂吉 月岡
貞夫 高橋
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.)
Sankosha Co Ltd
Original Assignee
Sankosha 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
Priority to JP48071800A priority Critical patent/JPS593090B2/en
Application filed by Sankosha Co Ltd filed Critical Sankosha Co Ltd
Priority to JP58177061A priority patent/JPS6030188B2/en
Publication of JPS5983537A publication Critical patent/JPS5983537A/en
Publication of JPS6030188B2 publication Critical patent/JPS6030188B2/en
Expired legal-status Critical Current

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  • Supply And Distribution Of Alternating Current (AREA)
  • Suspension Of Electric Lines Or Cables (AREA)

Description

【発明の詳細な説明】 本発明は必要かつ十分な電圧を容易に得ることのできる
送電線の静電譲導電圧取出装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an electrostatic transfer voltage extraction device for a power transmission line that can easily obtain a necessary and sufficient voltage.

現在、定められた地域内における一定以上の高さの送電
線鉄塔には、航空障害灯を設置することが航空法で定め
られている。
Currently, the Civil Aviation Law requires that aircraft obstruction lights be installed on power transmission line towers of a certain height or higher within designated areas.

しかしながら、従来は、専ら100ボルトの配電線を絶
縁トランスを介して引込み点灯しているために、山上、
および原野においては、配電線が近辺に設けられておら
ず、その点灯には困難な場合が多かった。そこで、従来
においては架空送電線に沿って線状導体を配置し、これ
を架空送電線に絶縁物と介して支持させ、線状導体に静
電誘導により誘起される電圧を取出して、ネオン放電管
を点灯させるようにした方式のものが提案されているが
、これらの方視は理論上可能であっても実用上の実施は
全く不能に等しいものである。なぜならば、線状導体を
送電線に沿わせて支持するものであるため、送電線には
線状導体の全重量を支えるに十分な強度および風圧に耐
える強度が必要となり、通常と異なる強轍な送電線を架
設ちなければならない。また、航空障害灯として、2〜
4個のネオン管を線状導体に誘起される静電誘導電圧に
より点灯させるようにするには数百メータの導体長さが
必要であり、したがって上述の方式を既設の送電線に取
付けることは実際上不可能に等しく、実用的な面に即し
ないのである。
However, in the past, the 100-volt distribution line was exclusively connected through an isolation transformer to turn on the light, so the
In the wild areas, there are no power distribution lines nearby, and it is often difficult to turn on the lights. Therefore, in the past, a linear conductor was placed along the overhead power transmission line, supported by the overhead power transmission line via an insulator, and the voltage induced by electrostatic induction in the linear conductor was extracted, causing neon discharge. Systems have been proposed in which the tube is turned on, but even if these directions are possible in theory, they are completely impossible to implement in practice. This is because the wire conductors are supported along the power transmission line, so the power transmission line needs to be strong enough to support the entire weight of the wire conductor and withstand wind pressure. Transmission lines must be constructed. It can also be used as an aircraft obstruction light.
In order to light four neon tubes using electrostatic induction voltage induced in a linear conductor, a conductor length of several hundred meters is required, so it is not possible to install the above method on an existing power transmission line. This is practically impossible and is not practical.

本発明は上記のような点に鑑みなされたもので、その目
的としるところは、送電線鉄塔の一ないし数スパン間に
送電線に沿ってアースとは絶縁された導電線を張設し、
この導電線に誘起される送電線からの静電誘導電圧をト
ランスを介して取出し負荷の駆動に必要な安定した電力
を得るようにした送電線の静電誘導電圧取出装置を提供
するにある。
The present invention was made in view of the above points, and its purpose is to install a conductive wire insulated from the ground along the power transmission line between one or several spans of power transmission towers,
It is an object of the present invention to provide an electrostatically induced voltage extracting device for a power transmission line, which extracts the electrostatically induced voltage from the power transmission line through a transformer to obtain stable power necessary for driving a load.

以下本発明の実施例について述べる。Examples of the present invention will be described below.

本発明においては、従来のような航空障害灯点灯のため
の配電線の有無に何等拘泥されることなく所期の目5的
を達成できるものである。すなわち、送電線鉄塔の一な
し、し数スパン間にアースより浮かした導電線を張架し
て〜 これに送電線からの静電誘導電圧を生ぜしめ「こ
れをトランス〜ネオン管を経てアースに接続し点灯する
ようにしてものである。そして以上の主旨において試作
した放電管はLI仇側めのガラス管「数のを「直径数1
仇舷のスパイラル状に巻いて4・形化し.たもので、ネ
オンガスを封入し、数10のAを通電したときに、数1
0カンデラが得られたものである。航空法によれば、該
障害灯は、ioカンデラ以上(昭和43手度制定の航空
障害灯仕様書では40カンデラ以上)であることを制定
されているのでト充分、満足する結果が得られたもので
ある。また光源は、塔頂上部と中間部に取り付けるよう
に定められているが、中間部はへ周囲のどの方向からで
も見える必要があるので、合計3個の放電管を必要とす
る。
In the present invention, the desired objective 5 can be achieved without being constrained in any way by the presence or absence of a power distribution line for lighting the aircraft obstacle lights as in the conventional case. In other words, there is no transmission line tower, and a conductive wire suspended above the ground is strung between several spans. This generates an electrostatic induced voltage from the transmission line, which is connected to the ground through a transformer and a neon tube. The discharge tube that was prototyped with the above idea in mind was a glass tube with a diameter of several 1 for the LI side.
Roll it into a spiral shape on the side of the ship to form 4. When filled with neon gas and energized by several tens of A, the result is several 1
0 candela was obtained. According to the Civil Aviation Law, the obstruction light must have a rating of io candela or higher (40 candela or higher according to the aviation obstruction light specifications established in 1968), so we were able to obtain satisfactory results. It is something. The light sources are designed to be installed at the top and middle of the tower, but the middle part needs to be visible from any direction around the tower, so a total of three discharge tubes are required.

よって「 3個の放電管を直列にして「 この回路に数
10mAを流すためには「数1肌Vの送電線の場合に約
数100の(500の以上)の長さ蔓こわたる1本の導
電管を絶縁し、これと送電線との間の静電容量を利用す
るが、この長さは、送電線の標準スパンに略一致するの
で都合がよいものであるが、送電線の標準スパンで所要
の電流がとれない場合には、複数スパン間の静電誘導電
圧を得るようにすればよいものである以上のことを第1
図おつび第2図について説明すると、1,2は送電鉄塔
で「 この鉄塔19 2の上部に取付けたアーム3,3
の一端間にはグランドワイヤ4が送電線5に沿って架設
され、さらにアーム3,3の他端間には碍子6,6を介
して送電線7が張設されている。
Therefore, in order to flow several tens of mA through this circuit by connecting three discharge tubes in series, one tube with a length of approximately several hundred (500 or more) is required for a power transmission line of several volts. This length is convenient because it approximately corresponds to the standard span of a power transmission line, but the length is convenient because it approximately corresponds to the standard span of a power transmission line. If the required current cannot be obtained across a span, it is sufficient to obtain the electrostatic induced voltage between multiple spans.
To explain Figure 1 and Figure 2, 1 and 2 are power transmission towers.
A ground wire 4 is installed along a power transmission line 5 between one end, and a power transmission line 7 is extended between the other ends of the arms 3, 3 via insulators 6, 6.

この送電線7は導電線5に沿って張設されるものであり
トさらに導電線?は一対の鉄塔間に限らず、必要長さを
得るためには2つ以上の鉄塔にまたがって張設される。
また、ァ−スから絶縁された上記導電線7と鉄塔蔓間に
は第2図に示す如くトランス8の−次側巻線8aが接続
され、その二次側巻線8bには負荷、すなわち鉄塔1の
頂上部に設置した航空障害灯9および鉄塔1の中間部に
設置した航空障害灯10,11が直列に接続されている
。この場合「航空障害灯がネオン管であるのでチョーク
コイルあるし、は限流開抵抗が直列に接続される。した
がって、送電線に送電がなされれば、絶縁された導電線
7と送電線5間に第1図の如く静電容量Cが生じること
により、この結果導電線7に譲超された静電誘導電圧は
トランス81こより降圧または昇圧され、その二次側電
圧がリード線12を通して各障害灯9〜1 貫に印加さ
れ「各障害灯を所定の明るさに点灯させる。
This power transmission line 7 is stretched along the conductive wire 5, and is also a conductive wire? is not limited to between a pair of steel towers, but may be stretched across two or more steel towers in order to obtain the required length.
Further, as shown in FIG. 2, a secondary winding 8a of a transformer 8 is connected between the conductive wire 7, which is insulated from the ground, and the steel tower, and a load, i.e., a secondary winding 8b, is connected to the secondary winding 8b. An aviation obstruction light 9 installed at the top of the steel tower 1 and aviation obstruction lights 10 and 11 installed at the middle of the tower 1 are connected in series. In this case, since the aviation obstacle lights are neon tubes, there is a choke coil, and a current limiting resistor is connected in series. Therefore, if power is transmitted to the power transmission line, the insulated conductive wire 7 As a result of the capacitance C generated between them as shown in FIG. A voltage is applied to 9 to 1 obstacle lights to turn on each obstacle light at a predetermined brightness.

この実施例において、送電電圧が低く、かつアースから
浮かせた導電線了の長さ(500の以上)が長い場合、
発生電圧は低いが〜送電線とアースより浮かせた導電線
7間の静電容量Cが大きいので(電流が大きい「数10
のA)、電力は充分あり、したがってトランス8‘こよ
り昇圧すれば、3〜4個のネオン管を安定に点灯するの
に十分な電圧(i7KV)が得られることになる。
In this example, when the transmission voltage is low and the length of the conductive wire suspended from the ground is long (500 mm or more),
Although the generated voltage is low, the capacitance C between the power transmission line and the conductive wire 7 suspended above the ground is large (several 10
A) There is enough power, so if the voltage is stepped up from the transformer 8', a voltage (i7KV) sufficient to stably light 3 to 4 neon tubes will be obtained.

また、上記と逆に送電電圧が高く、かつアースから浮か
せた導電線7の長さが短い場合、Cが小さいので、ネオ
ン管の点灯に必要な電流(数10のA)が得られなくな
るが、発生電圧をトランス8で降圧すれば「点灯に必要
な電流(数10のA)が確保されることになる。
Conversely, if the power transmission voltage is high and the length of the conductive wire 7 suspended from the ground is short, C will be small and the current required to light the neon tube (several tens of amperes) will not be obtained. If the generated voltage is stepped down by the transformer 8, the current (several tens of amperes) required for lighting will be secured.

なお、鉄塔間に張設される導電線7は図示しない避雷装
置を介してアースされることは勿論である。
Incidentally, the conductive wire 7 stretched between the steel towers is of course grounded via a lightning arrester (not shown).

以上のように本発明においては「送電線鉄塔の一ないし
数スパン間に送電線に沿ってアースとは絶縁された導電
線を張設し、この導電線に誘起される送電線からの静電
議導電圧をトランスを介して取出し負荷の駆動に供する
ようにしたので、航空障害灯などの負荷の駆動に必要な
電圧、電流を安定に供給することができ、良好なネオン
管点灯が可能となると共に、静電譲導電圧の取出し‘こ
必要な導電線の長さが長くなってもその支持が容易とな
り、さらに配電線の設置不能な地域でも簡便にかつ安全
に電源を供給することができる。
As described above, in the present invention, a conductive wire insulated from the ground is stretched along the power transmission line between one or several spans of the transmission line tower, and static electricity from the power transmission line induced in the conductive wire is Since the conduction voltage is taken out through a transformer and used to drive the load, it is possible to stably supply the voltage and current necessary to drive loads such as aircraft obstruction lights, and it is possible to achieve good neon tube lighting. At the same time, even if the length of the conductive wire required to take out the electrostatic transfer voltage becomes longer, it becomes easier to support it, and it is also possible to easily and safely supply power even in areas where it is impossible to install distribution lines. can.

なお、上述の実施例においては「航空障害灯について説
明したが、本発明は、特に該障害灯に拘泥されず、種々
の装置に利用できることは自明である。
Although the above-mentioned embodiments have been described with reference to aviation obstacle lights, it is obvious that the present invention is not limited to these obstacle lights and can be applied to various devices.

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

第1図は本発明にかかる送電線の静電誘導電圧取出装置
の一例を示す概要図、第2図はその一部の詳細を示す図
である。 1,2….・・送電線鉄塔、3・・…・アース、4・・
・・・・グランドワイヤ、5・・・・・・送電線、6・
・・・・・碍子、7・・・・・・導電線、8・・・…ト
ランス、9,10,1 1・・・…航空障害灯、C・・
・・・・静電容量。 第「図 第2図
FIG. 1 is a schematic diagram showing an example of an electrostatic induction voltage extraction device for a power transmission line according to the present invention, and FIG. 2 is a diagram showing details of a part thereof. 1, 2…. ...Power line tower, 3...Earth, 4...
... Ground wire, 5 ... Power transmission line, 6.
... Insulator, 7 ... Conductive wire, 8 ... Transformer, 9, 10, 1 1 ... Aviation obstruction light, C ...
...Capacitance. Figure 2

Claims (1)

【特許請求の範囲】[Claims] 1 送電線鉄塔の一ないし数スパン間に架設送電線に沿
つて1本の導電線をアースから絶縁して張設し、この導
電線に上記送電線との間の静電容量を通して静電誘導電
圧を発生させると共に、上記導電線とアース間に負荷電
力を安定に供給するためのトランスの一次側巻線を接続
し、かつ上記トランスの二次側巻線には航空障害灯など
の負荷を接続したことを特徴とする送電線の静電誘導電
圧取出装置。
1. A conductive wire is insulated from the ground and stretched along the installed power transmission line between one or several spans of the transmission line tower, and electrostatic induction is caused by passing the capacitance between this conductive wire and the above power transmission line. In addition to generating voltage, the primary winding of a transformer is connected between the conductive wire and the ground to stably supply load power, and the secondary winding of the transformer is connected to a load such as an aircraft obstruction light. An electrostatic induction voltage extraction device for a power transmission line, characterized in that:
JP58177061A 1973-06-27 1983-09-27 Electrostatic induction voltage extraction device for power transmission lines Expired JPS6030188B2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP48071800A JPS593090B2 (en) 1973-06-27 1973-06-27 The method of using the electric current and the electric pressure that were thoroughly examined in accordance with the electric current sensor
JP58177061A JPS6030188B2 (en) 1973-06-27 1983-09-27 Electrostatic induction voltage extraction device for power transmission lines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP48071800A JPS593090B2 (en) 1973-06-27 1973-06-27 The method of using the electric current and the electric pressure that were thoroughly examined in accordance with the electric current sensor
JP58177061A JPS6030188B2 (en) 1973-06-27 1983-09-27 Electrostatic induction voltage extraction device for power transmission lines

Publications (2)

Publication Number Publication Date
JPS5983537A JPS5983537A (en) 1984-05-15
JPS6030188B2 true JPS6030188B2 (en) 1985-07-15

Family

ID=52285767

Family Applications (2)

Application Number Title Priority Date Filing Date
JP48071800A Expired JPS593090B2 (en) 1973-06-27 1973-06-27 The method of using the electric current and the electric pressure that were thoroughly examined in accordance with the electric current sensor
JP58177061A Expired JPS6030188B2 (en) 1973-06-27 1983-09-27 Electrostatic induction voltage extraction device for power transmission lines

Family Applications Before (1)

Application Number Title Priority Date Filing Date
JP48071800A Expired JPS593090B2 (en) 1973-06-27 1973-06-27 The method of using the electric current and the electric pressure that were thoroughly examined in accordance with the electric current sensor

Country Status (1)

Country Link
JP (2) JPS593090B2 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52132482U (en) * 1976-04-05 1977-10-07
CA1060946A (en) * 1978-04-26 1979-08-21 Hydro-Quebec Stroboscopie beacons fed by a capacitive source___
JPS5923171B2 (en) * 1978-08-12 1984-05-31 株式会社昭電 Transmission line power supply equipment
JPS5831739U (en) * 1981-08-21 1983-03-02 株式会社サンコ−シャ Power transmission equipment that uses overhead ground wires
JPS5857245U (en) * 1981-10-12 1983-04-18 株式会社サンコ−シャ Load circuit using electrostatic induction power supply
JPS6257812A (en) * 1985-09-04 1987-03-13 Honda Motor Co Ltd cutting tools
JPH052248Y2 (en) * 1985-09-04 1993-01-20
JPS6246521U (en) * 1985-09-05 1987-03-20
JPH02114419U (en) * 1989-02-28 1990-09-13
JPH0720047U (en) * 1993-09-10 1995-04-07 古河電気工業株式会社 Power supply
JP6346712B2 (en) * 2015-08-21 2018-06-20 大電株式会社 Power supply
US10387298B2 (en) 2017-04-04 2019-08-20 Hailo Technologies Ltd Artificial neural network incorporating emphasis and focus techniques

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS438427Y1 (en) * 1966-01-13 1968-04-15
JPS4320029Y1 (en) * 1966-07-08 1968-08-22

Also Published As

Publication number Publication date
JPS593090B2 (en) 1984-01-23
JPS5020294A (en) 1975-03-04
JPS5983537A (en) 1984-05-15

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