JPH0235131Y2 - - Google Patents

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Publication number
JPH0235131Y2
JPH0235131Y2 JP4964986U JP4964986U JPH0235131Y2 JP H0235131 Y2 JPH0235131 Y2 JP H0235131Y2 JP 4964986 U JP4964986 U JP 4964986U JP 4964986 U JP4964986 U JP 4964986U JP H0235131 Y2 JPH0235131 Y2 JP H0235131Y2
Authority
JP
Japan
Prior art keywords
optical fiber
tape
heat
composite overhead
fiber composite
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
JP4964986U
Other languages
Japanese (ja)
Other versions
JPS62147216U (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 JP4964986U priority Critical patent/JPH0235131Y2/ja
Publication of JPS62147216U publication Critical patent/JPS62147216U/ja
Application granted granted Critical
Publication of JPH0235131Y2 publication Critical patent/JPH0235131Y2/ja
Expired 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) 本考案は架空送電線ないし架空地線に光フアイ
バを複合した複合架空線の改良に係る。
[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to the improvement of a composite overhead line in which an optical fiber is combined with an overhead power transmission line or an overhead ground wire.

(従来技術) 架空送電線の系統保護、制御を目的として架空
送電線ないし架空地線に光フアイバを収納した光
フアイバ複合架空線が用いられている。
(Prior Art) For the purpose of system protection and control of overhead power transmission lines, optical fiber composite overhead lines in which optical fibers are housed in overhead power transmission lines or overhead ground wires are used.

第1図は一般に知られている光フアイバ複合架
空線の横断面図を示す。この光フアイバ複合架空
線は中心に位置する光フアイバユニツト1とその
外周上の例えばアルミニウム被覆鋼線、アルミニ
ウム線等の導体素線6′の多数本を撚合せて構成
した導体撚線層6から成つている。
FIG. 1 shows a cross-sectional view of a generally known optical fiber composite overhead line. This optical fiber composite overhead line consists of an optical fiber unit 1 located at the center and a conductor strand layer 6 formed by twisting together a large number of conductor strands 6' such as aluminum-coated steel wires, aluminum wires, etc. on the outer periphery of the optical fiber unit 1. It is completed.

上記光フアイバユニツト1は周上に複数のらせ
ん溝3を設け、このらせん溝3の中に光フアイバ
4を収納した例えばアルミニウム製のスペーサ2
と、このスペーサ2を収納したアルミニウム製の
光フアイバ保護管5により形成されている。しか
して、上記スペーサ2のらせん溝3に収納する光
フアイバ4は第3図にその横断面図を示すよう
に、光フアイバガラス7の上にクツシヨン層とし
てのシリコーン樹脂等による一次被覆層8を設
け、その上に外傷から光フアイバガラス7及び一
次被覆層8を保護する耐熱性のある樹脂、例えば
フツ素樹脂の押出しによる二次被覆層9を施した
ものが用いられている。
The optical fiber unit 1 has a plurality of helical grooves 3 on its circumference, and a spacer 2 made of, for example, aluminum, with an optical fiber 4 housed in the helical groove 3.
It is formed by an aluminum optical fiber protection tube 5 that houses this spacer 2. As shown in FIG. 3, the optical fiber 4 accommodated in the spiral groove 3 of the spacer 2 has a primary coating layer 8 of silicone resin or the like as a cushion layer on the optical fiber glass 7. The optical fiber glass 7 and the primary coating layer 8 are provided with a secondary coating layer 9 formed by extrusion of a heat-resistant resin, such as a fluororesin, to protect the optical fiber glass 7 and the primary coating layer 8 from external damage.

(解決しようとする問題点) 上述の構造を有する光フアイバ架空線は、光フ
アイバ4がスペーサ2のらせん溝3の中に収納さ
れており、かつ、このスペーサ2が光フアイバ保
護管5の中に収納されているので、十分な機械的
強度を有している。しかし、一方既設架空線との
張替えを考えた場合、外径寸法は従来の架空線と
略等しくしなければならないが、本構造の光フア
イバ複合架空線ではスペーサ2の断面積分だけ光
フアイバを収納できる空間が少くなり、かつ外径
に対しても溝数が制限されるため、光フアイバの
多心化という点では不利となる。因みに、外径因
みに、外径125μmφの光フアイバガラス7にシ
リコーン樹脂の一次被覆層8を設けて外径0.4mm
φとし、その上にフツ素樹脂等の二次被覆層9を
押出し被覆した場合、製造条件を考慮した最小厚
さは0.15mmとなつて外径は0.7mmφとなり、この
光フアイバ4をスペーサ2のらせん溝3に収納す
る場合、外径4.0mmφのスペーサ2に対して計5
心までしか収納できなかつた。
(Problem to be Solved) In the optical fiber overhead line having the above structure, the optical fiber 4 is housed in the spiral groove 3 of the spacer 2, and the spacer 2 is housed in the optical fiber protection tube 5. It has sufficient mechanical strength. However, when considering replacing the existing overhead line, the outer diameter must be approximately the same as the conventional overhead line, but in the optical fiber composite overhead line of this structure, the optical fiber can be accommodated by the cross-sectional area of the spacer 2. Since the available space is reduced and the number of grooves is limited with respect to the outer diameter, this is disadvantageous in terms of increasing the number of optical fibers. By the way, the outer diameter is 0.4 mm by providing a silicone resin primary coating layer 8 on the optical fiber glass 7 with an outer diameter of 125 μmφ.
When the optical fiber 4 is extruded and coated with a secondary coating layer 9 made of fluororesin or the like, the minimum thickness considering the manufacturing conditions is 0.15 mm and the outer diameter is 0.7 mmφ. When storing in the spiral groove 3, a total of 5
It could only hold up to my heart.

又光フアイバ複合架空地線は導体を流れる電流
によつて常時100〜150℃の高温にさらされてお
り、特に短絡事故が発生した時には300℃近くま
で達するが、一方、光フアイバの高温での伝送損
失増加は二次被覆層の高温での収縮によるマイク
ロベンドによつて発生するという問題がある。
In addition, optical fiber composite overhead ground wires are constantly exposed to high temperatures of 100 to 150°C due to the current flowing through the conductor, and the temperature can reach nearly 300°C when a short circuit occurs. There is a problem in that the increase in transmission loss is caused by microbending caused by shrinkage of the secondary coating layer at high temperatures.

(問題点を解決するための手段) 本考案は上述の問題点を解消し光フアイバユニ
ツトの外径を大きくすることなく収納する光フア
イバの多心化を実現した光フアイバ複合架空線を
提供するもので、その特徴は、スペーサのらせん
溝の中に、光フアイバ上に一次被覆層を設けた光
フアイバ素線の複数本を撚合せその上に耐熱性薄
肉テープを施した光フアイバを収納したことにあ
る。
(Means for Solving the Problems) The present invention solves the above-mentioned problems and provides an optical fiber composite overhead line that can accommodate multiple optical fibers without increasing the outer diameter of the optical fiber unit. The feature is that an optical fiber is housed in the spiral groove of the spacer, which is made by twisting multiple optical fibers with a primary coating layer on them and applying a heat-resistant thin tape on top of them. There is a particular thing.

(実施例) 第2図イ及びロは第1図の光フアイバ複合架空
線において、スペーサ2のらせん溝3の中に収納
する光フアイバ4の実施例の斜視図を示す。
(Embodiment) FIGS. 2A and 2B show perspective views of an embodiment of the optical fiber 4 housed in the helical groove 3 of the spacer 2 in the optical fiber composite overhead line of FIG. 1.

第2図イは、例えば外径125μmφの光フアイ
バガラス7上にシリコーン樹脂の一次被覆層8を
施した外径0.4mmφの光フアイバ素線10の複数
本を撚合せた上に厚さ0.075mm、幅6mmの四弗化
樹脂テープの如き耐熱性薄肉テープ11を縦添え
して巻付け、テープ11の側縁の重なり合う部分
を接着剤により接合したものである。又同図ロは
同図イ同様の光フアイバ素線10の撚合せ上に厚
き0.0125mmのポリイミドテープの如き耐熱性薄肉
テープ11′をらせん状に巻回して形成したもの
で、巻回の仕方は重ね巻き、突き合せ巻きあるい
は開放らせん巻きのいずれであつても差支えな
い。
Figure 2A shows, for example, an optical fiber glass 7 with an outer diameter of 125 μmφ and a silicone resin primary coating layer 8 on which a plurality of optical fiber wires 10 with an outer diameter of 0.4 mmφ are twisted together and a thickness of 0.075 mm. A thin heat-resistant tape 11 such as a tetrafluoride resin tape having a width of 6 mm is wound vertically, and the overlapping portions of the side edges of the tape 11 are bonded with an adhesive. In addition, the figure (B) is formed by winding a heat-resistant thin tape 11' such as a polyimide tape with a thickness of 0.0125 mm in a spiral shape on the twisted optical fiber wires 10 similar to the figure (A). The method may be lap winding, butt winding, or open spiral winding.

なお耐熱性薄肉テープの材質としては上記の実
施例に限定されるわけではなく、所望耐熱要求に
応じて三弗化樹脂二弗化樹脂やポリフエニレンサ
ルフアイド等のエンジニアリングプラスチツクの
薄肉の耐熱性テープであればよい。
Note that the material of the heat-resistant thin tape is not limited to the above-mentioned examples, and may be made of thin-walled engineering plastics such as trifluoride resin, difluoride resin, polyphenylene sulfide, etc., depending on the desired heat resistance requirements. Any tape is fine.

又高温での被覆の収縮による光フアイバのマイ
クロベンドを軽減するため及び曲げ特性の点か
ら、テープの厚さは0.1mm以下が望ましい。
Further, in order to reduce microbending of the optical fiber due to shrinkage of the coating at high temperatures and from the viewpoint of bending properties, the thickness of the tape is preferably 0.1 mm or less.

(考案の効果) 上述した本考案の光フアイバ複合架空線によれ
ば、以下のような効果を奏するものである。
(Effects of the invention) The optical fiber composite overhead line of the invention described above provides the following effects.

光フアイバの細径、多心化が可能となる。即
ち本考案においては光フアイバガラス上に一次
被覆のみを施した光フアイバ素線(外径0.4mm
φ)を撚合せた上に一括して耐熱性薄肉テープ
を施した光フアイバを用いるので、従来の一次
被覆層上に二次被覆層を押出し被覆したものに
比し、収納する光フアイバそのものが細くな
り、第3図の光フアイバの場合外径4.0mmφの
スペーサに対して5心までしか収納できなかつ
たが、第2図の光フアイバを用いることによつ
て同一スペーサ外径で18心まで収納可能となつ
た。
It becomes possible to make the diameter of the optical fiber smaller and increase the number of fibers. In other words, in the present invention, an optical fiber wire (outer diameter 0.4 mm) with only a primary coating on the optical fiber glass
Since we use optical fibers that are made by twisting φ) and applying heat-resistant thin tape all at once, the optical fiber itself to be housed is The optical fiber shown in Figure 3 could only accommodate up to 5 fibers in a spacer with an outer diameter of 4.0 mmφ, but by using the optical fiber shown in Figure 2, up to 18 fibers can be accommodated with the same spacer outer diameter. It is now possible to store it.

一次被覆層のシリコーン樹脂は摩擦係数が大
きいため、このような光フアイバ素線をスペー
サの溝内に収納すると、溝の内壁をシリコーン
樹脂被覆層との間の接触程度によつて摩擦力が
不均一となるため、光フアイバ複合架空線に収
縮、振動等の外力が加わつたときに光フアイバ
に局所的な応力がかかり易く、マイクロベンド
ロスが発生し易い。これに対し、本考案では光
フアイバ素線を集合した上に耐熱性テープを施
しているために、スペーサの溝内壁とのすべり
が良くなり伝送損失に影響を与えることがな
い。
The silicone resin of the primary coating layer has a large coefficient of friction, so when such an optical fiber wire is housed in the groove of the spacer, the frictional force is reduced depending on the degree of contact between the inner wall of the groove and the silicone resin coating layer. Because it is uniform, when an external force such as contraction or vibration is applied to the optical fiber composite overhead wire, local stress is likely to be applied to the optical fiber, and microbend loss is likely to occur. On the other hand, in the present invention, since a heat-resistant tape is applied to a collection of optical fiber strands, the spacer slides well against the inner wall of the groove, and the transmission loss is not affected.

第4図は長さ10mの光フアイバユニツトに振
幅±5mm、周波数35Hzの振動を加えながら光フ
アイバの伝送損失変化を連続測定した結果を示
すもので、図中の実線は本考案による第2図イ
の光フアイバ及びテープにポリイミドテープ、
ポリフエニレンサルフアイドテープを用いた光
フアイバと、第2図ロの光フアイバ及びテープ
にポリフエニレンサルフアイドテープ、四弗化
樹脂テープを用いた光フアイバの結果であり、
点線は光フアイバ素線を集合した後耐熱テープ
を施すことなくそのままスペーサの溝に収納し
た結果で、本考案によつて振動による伝送損失
増加量を0.6dB/mから損失変化なしに改善す
ることができた。
Figure 4 shows the results of continuous measurement of changes in optical fiber transmission loss while applying vibrations with an amplitude of ±5 mm and a frequency of 35 Hz to an optical fiber unit with a length of 10 m. polyimide tape on the optical fiber and tape,
These are the results of an optical fiber using polyphenylene sulfide tape, and an optical fiber using polyphenylene sulfide tape and tetrafluoride resin tape as the optical fiber and tape in Figure 2 (b).
The dotted line shows the result of assembling the optical fibers and then storing them in the groove of the spacer without applying heat-resistant tape.The present invention shows that the increase in transmission loss due to vibration is improved from 0.6 dB/m without loss change. was completed.

前述のように、光フアイバの高温での伝送損
失増加は二次被覆の収縮によるマイクロベンド
によつて発生するが、本考案で用いる光フアイ
バは従来の二次被覆に相当する耐熱テープの厚
さを、従来の押出し成形によつて得られる製造
条件を考慮した最小限の厚みである0.15mmに比
し1/2以下又はそれに近い厚さの薄肉テープを
用いることが出来るので、二次被覆の収縮によ
つて光フアイバに加わる収縮応力を小さくする
ことができる。
As mentioned above, the increase in transmission loss of optical fibers at high temperatures is caused by microbending due to shrinkage of the secondary coating, but the optical fiber used in this invention has a thickness of heat-resistant tape that corresponds to the conventional secondary coating. It is possible to use a thin tape with a thickness of 1/2 or less or close to 0.15 mm, which is the minimum thickness considering the manufacturing conditions obtained by conventional extrusion molding, so the secondary coating can be The shrinkage stress applied to the optical fiber due to shrinkage can be reduced.

さらに附随的利点として、従来の押出し成形
により二次被覆層を形成した光フアイバより
も、光フアイバ接続時における二次被覆の除去
が極めて容易となる。
An additional advantage is that the secondary coating is much easier to remove when the optical fibers are spliced than in conventional extruded optical fibers.

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

第1図は光フアイバ複合架空線の一例の横断面
図、第2図イ及びロはいずれも本考案における光
フアイバの実施例の斜視図、第3図は従来の光フ
アイバの横断面図、第4図は光フアイバの振動試
験の特性図である。 1……光フアイバユニツト、2……スペーサ、
3……らせん溝、4……光フアイバ、5……光フ
アイバ保護管、6……導体撚線層、7……光フア
イバガラス、8……一次被覆層、9……二次被覆
層、10……光フアイバ素線、11,11′……
耐熱性薄肉テープ。
FIG. 1 is a cross-sectional view of an example of an optical fiber composite overhead line, FIG. 2 A and B are both perspective views of an embodiment of the optical fiber according to the present invention, and FIG. FIG. 4 is a characteristic diagram of an optical fiber vibration test. 1... Optical fiber unit, 2... Spacer,
3... Spiral groove, 4... Optical fiber, 5... Optical fiber protection tube, 6... Conductor twisted wire layer, 7... Optical fiber glass, 8... Primary coating layer, 9... Secondary coating layer, 10... Optical fiber wire, 11, 11'...
Heat resistant thin tape.

Claims (1)

【実用新案登録請求の範囲】 (1) 周上に設けた複数のらせん溝の中に光フアイ
バを収納したスペーサの上に光フアイバ保護管
を有する光フアイバユニツトとその外周上に設
けた導体撚線層とより成る光フアイバ複合架空
線において、前記らせん溝の中に、光フアイバ
ガラス上に樹脂による一次被覆層を設けた光フ
アイバ素線の複数本を撚合せその上に一括して
厚さ0.1mm以下の耐熱性薄肉テープを施した光
フアイバを収納したことを特徴とする光フアイ
バ複合架空線。 (2) 光フアイバ素線の撚合せ上に耐熱性薄肉テー
プを縦添えしその側縁の合せ目を接合したこと
を特徴とする実用新案登録請求の範囲第1項記
載の光フアイバ複合架空線。 (3) 光フアイバ素線の撚合せ上に耐熱性薄肉テー
プを巻回したことを特徴とする実用新案登録請
求の範囲第1項記載の光フアイバ複合架空線。 (4) 耐熱性薄肉テープが四弗化樹脂テープ、三弗
化樹脂テープ、二弗化樹脂テープ、ポリイミド
テープ、ポリフエニレンサルフアイドテープで
あることを特徴とする実用新案登録請求の範囲
第1項ないし第3項記載の光フアイバ複合架空
線。
[Claims for Utility Model Registration] (1) An optical fiber unit having an optical fiber protection tube on a spacer in which optical fibers are housed in a plurality of spiral grooves provided on the periphery, and a twisted conductor provided on the outer periphery of the optical fiber unit. In the optical fiber composite overhead wire consisting of a wire layer, a plurality of optical fiber wires each having a primary coating layer of resin on the optical fiber glass are twisted together in the spiral groove, and the thickness is An optical fiber composite overhead line that houses optical fibers coated with heat-resistant thin tape of 0.1 mm or less. (2) The optical fiber composite overhead line as set forth in claim 1 of the utility model registration claim, characterized in that a heat-resistant thin tape is longitudinally attached to the twisted optical fiber wires and the joints of the side edges are joined. . (3) The optical fiber composite overhead wire according to claim 1, which is characterized in that a heat-resistant thin tape is wound around the twisted optical fiber wires. (4) Utility model registration claim 1 characterized in that the heat-resistant thin tape is a tetrafluoride resin tape, a trifluoride resin tape, a difluoride resin tape, a polyimide tape, or a polyphenylene sulfide tape. The optical fiber composite overhead line according to items 1 to 3.
JP4964986U 1985-04-17 1986-04-01 Expired JPH0235131Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4964986U JPH0235131Y2 (en) 1985-04-17 1986-04-01

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP5790885 1985-04-17
JP4964986U JPH0235131Y2 (en) 1985-04-17 1986-04-01

Publications (2)

Publication Number Publication Date
JPS62147216U JPS62147216U (en) 1987-09-17
JPH0235131Y2 true JPH0235131Y2 (en) 1990-09-21

Family

ID=33454904

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4964986U Expired JPH0235131Y2 (en) 1985-04-17 1986-04-01

Country Status (1)

Country Link
JP (1) JPH0235131Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013160882A (en) * 2012-02-03 2013-08-19 Fujikura Ltd Optical fiber cable and optical unit extraction method

Also Published As

Publication number Publication date
JPS62147216U (en) 1987-09-17

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