JPH0323772Y2 - - Google Patents

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Publication number
JPH0323772Y2
JPH0323772Y2 JP1981123703U JP12370381U JPH0323772Y2 JP H0323772 Y2 JPH0323772 Y2 JP H0323772Y2 JP 1981123703 U JP1981123703 U JP 1981123703U JP 12370381 U JP12370381 U JP 12370381U JP H0323772 Y2 JPH0323772 Y2 JP H0323772Y2
Authority
JP
Japan
Prior art keywords
power transmission
transmission line
caterpillar
drive wheels
spacecraft
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
JP1981123703U
Other languages
Japanese (ja)
Other versions
JPS5831714U (en
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 filed Critical
Priority to JP12370381U priority Critical patent/JPS5831714U/en
Publication of JPS5831714U publication Critical patent/JPS5831714U/en
Application granted granted Critical
Publication of JPH0323772Y2 publication Critical patent/JPH0323772Y2/ja
Granted legal-status Critical Current

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Description

【考案の詳細な説明】 [産業上の利用分野] 本考案は送電線に使用する自走式宙乗機の改良
に関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to an improvement of a self-propelled spacecraft used for power transmission lines.

[従来の技術] 宙乗機は架線の再スペーサの取り付け、架線後
の保守などのために、電工をのせて送電線上を走
らせるものであるが、従来の宙乗機は第4図に示
すような構造よりなり、ゴンドラ1′が送電線W
上を走行するローラ2,2あるいはローラに回転
無端ベルトを取り付けた回転部(図示せず)によ
り吊り下げられており、人力により移動してい
た。
[Conventional technology] A spacecraft is used to run over power transmission lines with electricians on board for reinstallation of spacers on overhead lines, maintenance after the overhead lines, etc.A conventional spacecraft is shown in Figure 4. The gondola 1' is connected to the power transmission line W.
It was suspended by rollers 2, 2 running above or by a rotating part (not shown) in which an endless rotating belt was attached to the rollers, and was moved by human power.

しかし、山間地方において送電線が急角度の場
合人力による移動が困難であるため、第5図及び
第6図に示すようなローラ取付枠11の両端にロ
ーラ12を取り付けたものを送電線の上側、キヤ
タピラ13を送電線の下側に位置させ、ローラ1
2をハンドル10により降下させて送電線をキヤ
タピラ13に押しつけることにより送電線をロー
ラ12とキヤタピラ13で挟持し、エンジン6か
らベルト17を介してシヤフト18を回転させる
ことによりキヤタピラ13を走行させる歯車13
aに駆動力を与えて動力的に移動せしめる自走式
宙乗機が提案されている(特開昭52−7641号)。
なお、23はもう一方の送電線上を走行するロー
ラである。
However, in mountainous regions, where the power transmission line has a steep angle, it is difficult to move it manually, so a roller mounting frame 11 with rollers 12 attached to both ends of the roller mounting frame 11 as shown in Figs. 5 and 6 is installed above the power line. , the caterpillar 13 is positioned below the power transmission line, and the roller 1
2 is lowered by a handle 10 to press the power transmission line against the caterpillar 13, the power transmission line is held between the rollers 12 and the caterpillar 13, and the shaft 18 is rotated from the engine 6 via the belt 17, thereby making the caterpillar 13 run. 13
A self-propelled spacecraft has been proposed (Japanese Patent Laid-Open Publication No. 7641/1983) that applies driving force to a and moves it dynamically.
Note that 23 is a roller running on the other power transmission line.

ところが、近年になつて送電線Wは多導体化が
進み、この多導体化に伴ない電線間隔を保持する
スペーサSが取り付けられ、これらのクランプ部
の外径は電線外径の230%にも達するものがあり、
また導体の接続スリーブなども大型化し、電線径
の170%程度にもなり、あるいは難着雪化や低騒
音化のためのリングやスパイラルロツドなどが取
り付けられており、上記のようなスペーサ等の乗
り越えを考慮していないエンジン駆動等の自走式
宙乗機では、送電線にキヤタピラを常に強く接触
させようとして、ローラの高さを固定しローラと
キヤタピラの間隔が変化しないようにしているた
め、送電線上のスペーサ部又はクランプ部等の凹
凸部を走行するのが困難となり、ローラ及びキヤ
タピラが破損したり、最悪の場合には走行不能に
なるという問題があつた。
However, in recent years, power transmission lines W have become multi-conductor, and with this multi-conductor, spacers S have been installed to maintain the distance between the wires, and the outer diameter of these clamps has increased to 230% of the wire outer diameter. There is something to reach,
In addition, conductor connection sleeves have become larger, reaching about 170% of the wire diameter, and rings and spiral rods have been installed to prevent snow buildup and reduce noise. In engine-driven and other self-propelled spacecraft that do not take into account overcoming, the height of the rollers is fixed so that the distance between the rollers and the caterpillar does not change in order to keep the caterpillar in strong contact with the power transmission line. As a result, it becomes difficult to run over uneven parts such as spacers or clamps on the power transmission line, causing problems such as damage to the rollers and caterpillars, or in the worst case, the vehicle becoming unable to run.

そこで、第5図の昇降装置19内にバネ(図示
せず)を設置してローラ取付枠11をバネの弾性
により上下に移動可能にせしめることも考えられ
るが、第7図に示すように、ローラ12がスペー
サのクランプ部20に達し且つ乗り越えようとし
た場合、ローラ12には駆動力が付与されていな
いため、ローラ12がブレーキとして作用し、ま
た、ローラ取付枠11とキヤタピラ13は常に平
行であり、且つ、バネの弾性力はローラ取付枠の
中心点に作用するため、ローラ取付枠11とキヤ
タピラ13との間隔が拡がるようにバネを縮める
には非常に大きな力が必要となり、極めて大きな
動力がない限りクランプ部20を乗り越えること
ができなかつた。
Therefore, it is conceivable to install a spring (not shown) in the lifting device 19 shown in FIG. 5 so that the roller mounting frame 11 can be moved up and down by the elasticity of the spring, but as shown in FIG. When the roller 12 reaches the clamp portion 20 of the spacer and tries to get over it, since no driving force is applied to the roller 12, the roller 12 acts as a brake, and the roller mounting frame 11 and the caterpillar 13 are always parallel. In addition, since the elastic force of the spring acts on the center point of the roller mounting frame, a very large force is required to compress the spring so that the distance between the roller mounting frame 11 and the caterpillar 13 increases. It was not possible to get over the clamp part 20 unless there was power.

もし、第8図のようにローラ12(またはキヤ
タピラ13)がクランプ部20を乗り越えにかか
つたときは、宙乗機の自重により傾いてしまう。
そうすると、前方のローラ12とキヤタピラ13
が同時にクランプ部20の上に乗つたとき、送電
線Wに接するのは後方のローラ12だけであり、
もしも送電線Wが揺れたりした場合には前方のロ
ーラ12及びキヤタピラ13の進行方向がずれ、
クランプ部20を乗り越えた時点で脱輪するおそ
れがあり、非常に危険であつた。また、2つのロ
ーラ12がクランプ部20を乗り越える度に宙乗
機が傾いたり元に戻つたりすると、宙乗機が進行
方向に大きく揺れ、非常に危険であつた。このこ
とは、2つのローラ12間の距離とキヤタピラ1
3の長さとの差にかかわらず言えることであり、
これの改善が強く望まれていた。
If the roller 12 (or caterpillar 13) starts to climb over the clamp part 20 as shown in FIG. 8, it will tilt due to the weight of the spacecraft.
Then, the front roller 12 and the caterpillar 13
When simultaneously riding on the clamp part 20, only the rear roller 12 is in contact with the power transmission line W,
If the power transmission line W shakes, the moving direction of the front roller 12 and caterpillar 13 will shift,
There was a risk that the wheels would fall off once they got over the clamp portion 20, which was extremely dangerous. Furthermore, if the spacecraft were to tilt and return to its original position each time the two rollers 12 got over the clamp portion 20, the spacecraft would shake greatly in the direction of travel, which was very dangerous. This means that the distance between the two rollers 12 and the caterpillar 1
This is true regardless of the difference in length between 3 and 3.
Improvement of this was strongly desired.

[考案の目的] 本考案の目的は、上記した従来技術に鑑み、送
電線上の凹凸部も安定して走行可能な自走式宙乗
機を提供することにある。
[Purpose of the invention] In view of the above-mentioned prior art, the purpose of the invention is to provide a self-propelled spacecraft that can stably travel even on uneven surfaces on power transmission lines.

[考案の概要] 本願考案の要旨は、キヤタピラベルトを2つの
駆動輪外周に設けた2つのキヤタピラが送電線を
挟持するよう該送電線の上下に設けられており、
且つ、上下に位置する上記駆動輪が上記送電線を
挟持する方向にバネ弾性力を有しており、上下の
上記キヤタピラが走行するよう上下の上記駆動輪
に走行駆動力を付与するエンジンが下方のゴンド
ラに装備されていることにある。
[Summary of the invention] The gist of the invention is that two caterpillar belts are provided on the outer periphery of two drive wheels, and two caterpillar belts are provided above and below a power transmission line so as to sandwich the power transmission line.
In addition, the drive wheels positioned above and below have a spring elastic force in a direction that sandwiches the power transmission line, and an engine that applies running driving force to the drive wheels at the top and bottom is directed downward so that the above-mentioned caterpillars at the top and bottom run. This is because the gondola is equipped with this.

[実施例] 以下、本考案の実施例を図面に基づいて説明す
る。
[Example] Hereinafter, an example of the present invention will be described based on the drawings.

第1図は本考案に係る宙乗機の正面図を示し、
第2図はその側面図を示したものである。
Figure 1 shows a front view of the spacecraft according to the present invention,
FIG. 2 shows its side view.

この実施例では、4導体送電線に本考案を適用
した場合を示す。W,Wは送電線であり、1がゴ
ンドラである。
This example shows a case where the present invention is applied to a four-conductor power transmission line. W and W are power transmission lines, and 1 is a gondola.

本考案においてもゴンドラ1を吊下走行するロ
ーラ2,2は使用されているが、このローラ2,
2は宙乗機の自走のための駆動力にはあずから
ず、ゴンドラ1を支えることを主な目的としてい
る。
In the present invention, the rollers 2, 2 that suspend the gondola 1 are also used;
2 does not provide the driving force for self-propulsion of the spacecraft, but its main purpose is to support gondola 1.

この駆動はもつぱら送電線Wを挟持しているキ
ヤタピラ3,3′によつて行われる。
This drive is performed exclusively by the caterpillars 3, 3' which hold the power transmission line W between them.

第3図はキヤタピラ3,3′が送電線Wを挟持
している様子を示すものである。このようなキヤ
タピラ3,3′は2つの駆動輪3aまたは駆動輪
3′aと、それらの外周に設けられたキヤタピラ
ベルト3bまたはキヤタピラベルト3′bからな
り、第1図に示すように上下に位置する駆動輪3
aと駆動輪3′aは挟持力調節装置7のバネ4の
弾性力によりキヤタピラ3とキヤタピラ3′を送
電線Wに押し付けて挟持するようにしてある。ハ
ンドル5は挟持力調節装置7の一部であり、バネ
4の弾性力を調節するためのものである。
FIG. 3 shows how the power transmission line W is held between the caterpillars 3 and 3'. Such a caterpillar 3, 3' consists of two drive wheels 3a or 3'a and a caterpillar belt 3b or track belt 3'b provided on the outer periphery of the two drive wheels 3a or 3'a, which are positioned one above the other as shown in FIG. Drive wheel 3
a and the drive wheel 3'a are adapted to press and clamp the caterpillar 3 and the caterpillar 3' against the power transmission line W by the elastic force of the spring 4 of the clamping force adjustment device 7. The handle 5 is part of the clamping force adjustment device 7 and is used to adjust the elastic force of the spring 4.

6はエンジンであつて、油圧が作られ、パイプ
によりその油圧はキヤタピラ3,3′の駆動輪3
a,3′aに負荷されて油圧駆動がなされる。も
つとも油圧駆動に限るものではないが。
Reference numeral 6 is an engine that produces hydraulic pressure, and the hydraulic pressure is transmitted through a pipe to the driving wheels 3 of the caterpillars 3 and 3'.
A and 3'a are loaded and hydraulically driven. However, it is not limited to hydraulic drive.

7′はゴンドラ1を上下するシリンダー、8は
ブレーキであつてこれを引き下げれば積杆作用で
ブレーキシユー8aが送電線Wに接圧され、走行
が停止され、引き上げればブレーキシユー8aが
解放される。
7' is a cylinder that moves the gondola 1 up and down, and 8 is a brake. When this is pulled down, the brake shoe 8a is brought into contact with the power transmission line W by the lever action, and traveling is stopped. When it is pulled up, the brake shoe 8a is is released.

6aはエンジン操作のためのレバーである。9
はゴンドラの水平保持シリンダーである。
6a is a lever for operating the engine. 9
is the gondola's horizontal holding cylinder.

このように構成せられていれば、第9図に示す
ように、スペーサのクランプ部20を通過するに
もキヤタピラ3,3′の両方とも駆動されている
ため、従来のようにキヤタピラ3aがブレーキと
して作用することがなく、更に、前方のキヤタピ
ラ3,3′がその間隔を変えてクランプ部20の
上に乗り上げても後方のキヤタピラ3,3′がし
つかりと送電線Wを挟持しているため、多少の送
電線の揺れでは脱輪することなく、キヤタピラ
3,3′が変幻自在に形を変え容易にそのクラン
プ部20を乗り越えることができる。なお、キヤ
タピラ3,3′の間隔が変化しても駆動輪3a,
3′aの間隔が変化するだけなので、クランプ部
20を乗り越えるときでも宙乗機及びゴンドラが
傾いたりすることがない。
With this configuration, as shown in FIG. 9, both the caterpillars 3 and 3' are driven even when passing through the clamp portion 20 of the spacer, so the caterpillar 3a is braked as in the conventional case. Furthermore, even if the front caterpillars 3, 3' change their distance and ride on the clamp part 20, the rear caterpillars 3, 3' firmly clamp the power transmission line W. Therefore, the caterpillars 3, 3' can freely change their shape and easily climb over the clamp portion 20 without coming off the track even when the power transmission line swings to some extent. Note that even if the distance between the caterpillars 3 and 3' changes, the drive wheels 3a and
Since only the interval 3'a changes, the spacecraft and gondola will not tilt even when climbing over the clamp part 20.

また送電線Wとの接触は大きく、その駆動力も
絶大となつて、まことにたのもしい走行が約束せ
られるのである。
In addition, the contact with the power transmission line W is large, and the driving force is enormous, ensuring a truly enjoyable driving experience.

以上本考案の実施例によれば、 (1) 送電線の外径が著しく異なる、すなわち送電
線上に凹凸部がある場合でも、容易にかつ安全
に走行できる。
According to the embodiments of the present invention as described above, (1) Even when the outer diameters of the power transmission lines are significantly different, that is, even when there are uneven parts on the power transmission lines, it is possible to travel easily and safely.

(2) 最高温度40m/分が得られ、長径間の送電線
路の点検時間が大巾に短縮される。
(2) A maximum temperature of 40 m/min can be achieved, and the inspection time for long-span power transmission lines is greatly reduced.

(3) 電線表面の状態すなわち、マシン油、水分な
どが存在する場合でも走行が可能である。
(3) It is possible to run even in the presence of machine oil, moisture, etc. on the wire surface.

(4) 急傾斜(例えばカテナリ角度35〜40゜)にお
いても自走できる。
(4) Can run on its own even on steep slopes (for example, catenary angle of 35 to 40 degrees).

などの数々の効果が期待できる。A number of effects can be expected.

[考案の効果] 以上に説明した如く、本考案によれば、キヤタ
ピラベルトを2つの駆動輪外周に設けた2つのキ
ヤタピラが送電線を挟持するよう送電線の上下に
設けられ、且つ、上下に位置する駆動輪が送電線
を挟持する方向にバネ弾性力を有しており、上下
のキヤタピラが走行するよう上下の駆動輪に走行
駆動力が付与されていることにより、送電線上の
凹凸部も容易に且つ安定して走行することができ
る、という顕著な効果を奏する。
[Effects of the invention] As explained above, according to the invention, two caterpillar belts are provided above and below the power transmission line so as to sandwich the power transmission line, and two caterpillar belts are provided on the outer periphery of the two drive wheels. The drive wheels have a spring elastic force in the direction that grips the power transmission line, and the driving force is applied to the upper and lower drive wheels so that the upper and lower caterpillars move, making it easy to overcome uneven surfaces on the power transmission line. It has the remarkable effect of being able to run smoothly and stably.

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

第1図は本考案に係る宙乗機の正面図、第2図
はその側面図、第3図はキヤタピラの様子を示す
説明図、第4図乃至第6図は従来の宙乗機を示す
見取図、第7図及び第8図は従来の自走式宙乗機
がスペーサのクランプ部を乗り越える様子を示す
説明図、第9図は本発明の宙乗機のキヤタピラが
スペーサのクランプ部を乗り越える様子を示す説
明図である。 1,1′…ゴンドラ、2…ローラ、3,3′…キ
ヤタピラ、3a,3′a…駆動輪、3b,3′b…
キヤタピラベルト、4…バネ、5…ハンドル、W
…送電線、S…スペーサ。
Figure 1 is a front view of the spacecraft according to the present invention, Figure 2 is its side view, Figure 3 is an explanatory diagram showing the condition of the caterpillar, and Figures 4 to 6 show conventional spacecraft. The sketch, Figures 7 and 8 are explanatory diagrams showing how a conventional self-propelled spacecraft rides over the clamp part of the spacer, and Figure 9 shows how the caterpillar of the spacecraft of the present invention climbs over the clamp part of the spacer. FIG. 2 is an explanatory diagram showing the situation. 1, 1'... Gondola, 2... Roller, 3, 3'... Caterpillar, 3a, 3'a... Drive wheel, 3b, 3'b...
Caterpillar belt, 4...Spring, 5...Handle, W
...Power line, S...Spacer.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] キヤタピラベルトを2つの駆動輪外周に設けた
2つのキヤタピラが送電線を挟持するよう該送電
線の上下に設けられており、且つ、上下に位置す
る前記駆動輪が前記送電線を挟持する方向にバネ
弾性力を有しており、上下の前記キヤタピラが走
行するよう上下の前記駆動輪に走行駆動力を付与
するエンジンが下方のゴンドラに装備されている
ことを特徴とする送電線用自走式宙乗機。
Two caterpillar belts are provided on the outer peripheries of the two drive wheels, and two caterpillar belts are provided above and below the power transmission line so as to sandwich the power transmission line, and the drive wheels located above and below are provided with springs in the direction of sandwiching the power transmission line. A self-propelled aerial vehicle for a power transmission line, characterized in that a lower gondola is equipped with an engine that has elastic force and provides running driving force to the upper and lower drive wheels so that the upper and lower caterpillars run. Boarding machine.
JP12370381U 1981-08-21 1981-08-21 Self-propelled spacecraft for power transmission lines Granted JPS5831714U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12370381U JPS5831714U (en) 1981-08-21 1981-08-21 Self-propelled spacecraft for power transmission lines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12370381U JPS5831714U (en) 1981-08-21 1981-08-21 Self-propelled spacecraft for power transmission lines

Publications (2)

Publication Number Publication Date
JPS5831714U JPS5831714U (en) 1983-03-02
JPH0323772Y2 true JPH0323772Y2 (en) 1991-05-23

Family

ID=29917595

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12370381U Granted JPS5831714U (en) 1981-08-21 1981-08-21 Self-propelled spacecraft for power transmission lines

Country Status (1)

Country Link
JP (1) JPS5831714U (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6538643B2 (en) * 2016-12-27 2019-07-03 三桜電気工業株式会社 Fall prevention net device for multi-conductors

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS527641A (en) * 1975-06-23 1977-01-20 Sperry Rand Corp Pack loop memory with data operating performance

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5192901U (en) * 1975-01-23 1976-07-26

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS527641A (en) * 1975-06-23 1977-01-20 Sperry Rand Corp Pack loop memory with data operating performance

Also Published As

Publication number Publication date
JPS5831714U (en) 1983-03-02

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