JPS5983537A - Electrostatic induction pickup device for transmission line - Google Patents

Electrostatic induction pickup device for transmission line

Info

Publication number
JPS5983537A
JPS5983537A JP58177061A JP17706183A JPS5983537A JP S5983537 A JPS5983537 A JP S5983537A JP 58177061 A JP58177061 A JP 58177061A JP 17706183 A JP17706183 A JP 17706183A JP S5983537 A JPS5983537 A JP S5983537A
Authority
JP
Japan
Prior art keywords
transmission line
power transmission
voltage
transformer
conductive wire
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
JP58177061A
Other languages
Japanese (ja)
Other versions
JPS6030188B2 (en
Inventor
月岡 桂吉
高橋 貞夫
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

Links

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

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
送電線の静電誘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 induction 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坑壁法で定め
られている。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。
Currently, the Mine Wall Law requires that aircraft obstruction lights be installed on power transmission line towers of a certain height or higher within designated areas. However, in the past, 100-volt power distribution lines were used to run the lights through isolation transformers, so in mountaintops and wilderness areas, there were no power distribution lines nearby, making it difficult to turn on the lights. There were many.

そこで、従来においては架空送電線に池゛つて線状導体
を配償し、これを架空送電線に絶縁物を介して支持さセ
、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六方式のものが提
案されているが、これらの方式は理論士可能でおっても
実用上の実路1ね全く不能に等しいもの・である。なぜ
ならば、i線状導体を送電線に沿わせて支持するもので
奢るため、送電線には線状導体の全重量を支えるに十分
な分度および風圧に耐える強度が必要となシ、通常と異
なる強靭な送を線を架設しなけれはならない。
Therefore, in the past, a linear conductor was installed on the overhead power transmission line, and this was supported on the overhead power transmission line via an insulator to extract the voltage induced in the linear conductor by electrostatic induction. Six methods have been proposed for lighting neon discharge tubes, but although these methods may be possible in theory, they are completely impossible in practice. This is because the I-wire conductor is supported along the transmission line, so the transmission line must be strong enough to support the entire weight of the wire conductor and strong enough to withstand wind pressure. It is necessary to construct a strong transmission line that is different from the above.

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1誘導電圧によυ点灯させるようにす
るには数Uメータの導体長さが必要で21りシ、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。
In addition, in order to light up 2 to 4 neon tubes as aircraft obstacle lights by static 1 induced voltage induced in a linear conductor, a conductor length of several U meters is required. Therefore, it is practically impossible to attach the above-mentioned method to an existing power transmission line, and it 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
的とするところは、送電線鉄塔の−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 has been made in view of the above points, and its purpose is to stretch a conductive wire insulated from the ground along a power transmission line between one to several spans of a transmission line tower,
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 induced in the conductive line via a transformer and obtains stable power necessary for driving a load.

以下本発明の実施例について述べる。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的を達成できるもので
ある。すなわち、送電線鉄塔の−ないし数スパン間にア
ースより浮かLl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たものである。
Examples of the present invention will be described below. In the present invention, the intended purpose can be achieved without being restricted 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, an Ll conductive wire suspended from the ground is strung between one or several spans of a power transmission line tower, an electrostatic induced voltage is generated from the power transmission line, and this is connected to the ground via a transformer and a neon tube. It is designed to light up.

そして以上の主旨において試作した放電管は、10闘φ
のガラス管、数mを、直径数10闘のスパイラル状に巻
いて小形化したもので、ネオンガスを封入し、数10?
?’lAを通電したときに、数10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、10カンデ
ラ以上(昭和43年度制定の航空障害灯仕様書では40
力ンデラ以上)であることを制定されているので、充分
、満足する結果が得られたものでおる。
The discharge tube prototyped with the above idea in mind was 10 mm in diameter.
A glass tube, several meters long, is made smaller by winding it into a spiral shape with a diameter of several tens of meters, and is filled with neon gas.
? When a current of 'lA was applied, several tens of candelas were obtained. According to the Civil Aviation Law, the obstruction light must be 10 candelas or more (according to the Aviation Obstruction Light Specifications established in 1961, the obstruction light must be 40 candelas or more).
Since it has been established that the power is higher than 100%, the results are quite satisfactory.

また光源は、塔頂上部と中間部に取り付けるように宇め
られているが、中間部は、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。
Furthermore, the light sources are installed at the top and the middle part of the tower, but the middle part needs to be visible from any direction around it, 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Jii
lOfftAを流すためには、数IQKVの送電線の場
合に約数10(11(500f71以−ヒ)の長さにわ
たるグランドワイヤを絶縁し、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
に酪一致するので都合がよいものであるが、送電線の椰
準スパンでPIrW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。
Therefore, three discharge tubes are connected in series and Jii is connected to this circuit.
In order to flow lOfftA, in the case of a power transmission line of several IQKV, insulate the ground wire over a length of about several tens (11 (500f71 or more)) and use the capacitance between this and the power transmission line. However, this length is convenient because it corresponds to the standard span of the transmission line, but if the PIrW current cannot be taken in the palm span of the transmission line, the electrostatic induced voltage between multiple spans All you have to do is get it.

以上のことを第1図および第2図について説明すると、
1.2は送!鉄塔で、この鉄塔1.2の上部にを付けた
アーム3,3の一端間にはグランドワイヤ4が送電線5
に沼って架設され、さらにアーム3,3の他端間にけ碍
子6,6を介して導電線7が張設されている。この導電
線7は送電線5に沿って張設されるものであり、さらに
導電線7は一対の鉄塔間に限らず、必要長さを得るため
に祉2つ以上の鉄塔にまたがって張設される。また、ア
ースから絶縁された上記導を線7と鉄塔1間には第2図
に示す如くトランス・8の一次側巻線8mが接続され、
その二次側巻線8bには負荷、す々わち鉄塔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
あるいは限流閉抵抗が直列に接続される。
To explain the above with reference to Figures 1 and 2,
1.2 is sent! A ground wire 4 is connected to a power transmission line 5 between one end of the arms 3 and 3 attached to the top of the steel tower 1.2.
Further, a conductive wire 7 is stretched between the other ends of the arms 3, 3 via insulators 6, 6. The conductive wire 7 is stretched along the power transmission line 5, and the conductive wire 7 is not limited to being stretched between a pair of steel towers, but may be stretched across two or more steel towers to obtain the required length. be done. Further, as shown in FIG. 2, 8 m of the primary winding of the transformer 8 is connected between the wire 7 and the steel tower 1, which is insulated from the ground.
The secondary winding 8b is connected in series with a load, that is, an aircraft obstacle light 9 installed at the top of the tower 1 and an aircraft obstruction light 10.11 installed at the middle of the tower 1. In this case, since the aircraft obstruction lights are neon tubes, choke coils or current limiting closing resistors are connected in series.

したがって、送電線に送電がなされれは、絶縁された導
電線7と送電線5間に第1図の如く静電答iCが生じる
ことになυ、この結果導電線7に誘起された静電誘導電
圧はトランス8により降圧また祉昇圧され、その二次側
電圧がリード線12を通して谷障害灯9〜11に印加さ
れ、各障害灯を所定の明るさに点灯させる。
Therefore, when power is transmitted to the power transmission line, an electrostatic response iC occurs between the insulated conductive wire 7 and the power transmission line 5 as shown in FIG. The induced voltage is stepped down or stepped up by the transformer 8, and the secondary side voltage is applied to the valley obstacle lights 9 to 11 through the lead wire 12 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
浮かせたグランドワイヤの長さく500m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
グランドワイヤ3間のCが大きいので(電流が大きい、
数10mA)、電力は充分あり、したがってトランス8
によシ昇圧すれは、3〜4個のネオン管を安定に点灯す
るのに十分な電圧(17KV)が得られることになる。
In this example, when the power transmission voltage is low and the length of the ground wire 3 floating above the ground is long (500 m or more), the generated voltage is low, but the C between the power transmission line and the ground wire 3 floating above the ground is large ( large current,
(several tens of mA), there is enough power, so the transformer 8
If the voltage is increased, enough voltage (17KV) will be obtained to stably light 3 to 4 neon tubes.

また、上記と逆に送電電圧が高く、かつアースから浮か
せたクランドワイヤの長さが短い場合、Cが小さいので
、ネオン管の点灯に必要な電流(数10mh )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?FIA )が確保されること
になる。
Also, contrary to the above, if the power transmission voltage is high and the length of the gland wire suspended from the ground is short, C will be small and the current (several 10 mh) required to light the neon tube will not be obtained, but the generated voltage If the voltage is stepped down by the transformer 8, the current (several tens of FIA) necessary 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、送電線鉄塔の一部いし
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、静電誘導電圧の取出しに必
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前便にかつ安全に
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 earth is stretched along the power transmission line between part or several spans of the power transmission line tower, and the static electricity from the power transmission line induced by the conductive wire is Since the induced voltage is taken out via 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, making it possible to light neon tubes with good quality. At the same time, even if the length of the conductive wire required to take out the electrostatically induced voltage becomes longer, it becomes easier to support it, and it is also possible to supply power quickly and safely even in areas where it is not possible to install power distribution lines. .

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-described embodiments have been described with reference to aircraft 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。 f12・・・送電線鉄塔、3・・・アーム、4・・・グ
ランドワイヤ、訃・・送電線、6・・・碍子、7・・・
導電線、8・・・トランス、9.10.11・・・航空
障害灯、C・・・静電容量。 特許出願人 代理人 弁理士 門 間 正 −
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. f12...Power transmission line tower, 3...Arm, 4...Ground wire, Death...Power transmission line, 6...Insulator, 7...
Conductive wire, 8...Transformer, 9.10.11...Aircraft obstruction light, C...Capacitance. Patent applicant Representative patent attorney Tadashi Monma −

Claims (1)

【特許請求の範囲】[Claims] 送電線鉄塔の−ないし数スパン間に送電線路に沿って導
電線をアースから絶縁して張設し、この導電線に送電線
からの静[誘導電圧を誘起させると共に、上記導電線と
アース間に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巷線には航
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。
A conductive wire is insulated from the ground and stretched along the power transmission line between one to several spans of the transmission line tower, and the conductive wire is induced to induce static [induced voltage] from the power transmission line, as well as to reduce the voltage between the conductive wire and the ground. Electrostatic induction in a power transmission line, characterized in that a primary winding of a transformer is connected to the transformer for stably supplying electric power, and a load such as an aircraft obstruction light is connected to the secondary side wire of the transformer. Voltage extraction device.
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 How can I help you?
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 How can I help you?
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 true JPS5983537A (en) 1984-05-15
JPS6030188B2 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 How can I help you?
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 How can I help you?

Country Status (1)

Country Link
JP (2) JPS593090B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3340430A4 (en) * 2015-08-21 2019-04-17 Dyden Corporation Power supply device

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
JPH052248Y2 (en) * 1985-09-04 1993-01-20
JPS6257812A (en) * 1985-09-04 1987-03-13 Honda Motor Co Ltd Cutting tool
JPS6246521U (en) * 1985-09-05 1987-03-20
JPS6446086A (en) * 1987-08-10 1989-02-20 Mekajiyon Service Eng Kk Pipe joint
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
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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3340430A4 (en) * 2015-08-21 2019-04-17 Dyden Corporation Power supply device

Also Published As

Publication number Publication date
JPS593090B2 (en) 1984-01-23
JPS5020294A (en) 1975-03-04
JPS6030188B2 (en) 1985-07-15

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