JPH0359769B2 - - Google Patents
Info
- Publication number
- JPH0359769B2 JPH0359769B2 JP30599486A JP30599486A JPH0359769B2 JP H0359769 B2 JPH0359769 B2 JP H0359769B2 JP 30599486 A JP30599486 A JP 30599486A JP 30599486 A JP30599486 A JP 30599486A JP H0359769 B2 JPH0359769 B2 JP H0359769B2
- Authority
- JP
- Japan
- Prior art keywords
- aluminum
- core material
- cross
- wire
- coating layer
- 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
Links
- 239000011162 core material Substances 0.000 claims description 32
- 239000011247 coating layer Substances 0.000 claims description 30
- 238000000034 method Methods 0.000 claims description 21
- 238000005491 wire drawing Methods 0.000 claims description 18
- 238000004519 manufacturing process Methods 0.000 claims description 17
- 229910052751 metal Inorganic materials 0.000 claims description 17
- 239000002184 metal Substances 0.000 claims description 17
- 239000002131 composite material Substances 0.000 claims description 15
- 230000001788 irregular Effects 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 description 54
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 54
- 229910000831 Steel Inorganic materials 0.000 description 38
- 239000010959 steel Substances 0.000 description 38
- 239000000463 material Substances 0.000 description 19
- 238000007796 conventional method Methods 0.000 description 7
- 239000010410 layer Substances 0.000 description 5
- 239000000314 lubricant Substances 0.000 description 4
- 238000003754 machining Methods 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 238000011946 reduction process Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- CWQXQMHSOZUFJS-UHFFFAOYSA-N molybdenum disulfide Chemical compound S=[Mo]=S CWQXQMHSOZUFJS-UHFFFAOYSA-N 0.000 description 2
- 229910052982 molybdenum disulfide Inorganic materials 0.000 description 2
- 239000013307 optical fiber Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
Landscapes
- Metal Extraction Processes (AREA)
Description
「産業上の利用分野」
本発明は、光フアイバ複合送電線に使用される
アルミ被覆異形鋼線等の異形複合線の製造方法に
関し、特別な形状の種芯材から伸線加工すること
によつて均一な厚さの被覆層を有する複合線を製
造する方法によつて関するものである。
「従来の技術」
従来、光フアイバ複合送電線等に使用される異
形アルミ被覆鋼線を製造する方法として、アルミ
被覆母材に伸線加工を施して製造する方法が知ら
れていう。この製造方法は、鋼線の外面にアルミ
層を被覆してアルミ被覆母材を形成した後に、ダ
イスにより縮径加工を施した所定の形状に仕上げ
る方法である。
「発明が解決しようとする問題点」
ところが従来、前述の方法によつて異形アルミ
被覆鋼線を製造した場合、鋼線にアルミ層を被覆
する際に、アルミ被覆層を均一な厚さに形成した
場合であつても、ダイスによる縮径加工を施すう
ちに、アルミ被覆層の厚さが局部的に不均一にな
る問題を生じていた。これはダイスを用いて縮径
加工を施す際に、硬度の低いアルミ被覆層を通し
て鋼線が加工され、しかも丸線から異形断面条に
縮径される関係から、縮径時に作用する圧縮力が
不均一になり、芯材(鋼線)がダイス孔の形状と
は異なつた形に加工され易く、結果的にアルミ被
覆層の厚さの不均一が生じていた。そこで従来、
第5図ないし第7図を基に以下に説明する方法を
用いて異形アルミ被覆鋼線を製造するようにして
いる。
この従来方法は、第5図に示すように鋼線1を
アルミ被覆層2で覆つて構成された横断面略扇形
のアルミ被覆鋼線3を製造する場合、このアルミ
被覆鋼線3と相似形状で断面積の大きな第6図に
示す種線4を用意し、この種線4に縮径加工を施
して所要のアルミ被覆鋼線を製造する方法であ
る。
ところが、前記従来の方法によつて横断面略扇
形のアルミ被覆鋼線を製造した場合、実質的には
長径方向の加工率が短径方向の加工率に比較して
大きくなり、周辺部の加工比率の大小が伸線性に
影響し、アルミ被覆層の厚さや芯材の形状に大き
く影響するために、結果的に第7図に示すうにア
ルミ被覆層6の厚さが不均一になる問題を生じて
いた。これは、相似形状で加工することで加工部
の表面にダイスによつて作用する圧力(面圧)が
不均一になり、そのために柔らかいアルミニウム
が面圧の小さい部分に移動していることを示すも
のである。
なお、このように相似形状で伸線加工した場合
に、柔らかいアルミニウムが面圧の低い部分に移
動するという現象が起こる原因は、第8図と第9
図に示す例を基に以下に説明する理由によりもの
と推定される。なお、第8図と第9図に示す例に
おいては、説明が容易になるように、被覆層を省
略した芯材のみの場合について推定する。
第8図Aに示す横断面であつて縦20mm、横40mm
の種線15を第8図Bに示す横断面であつて縦10
mm、横20mmの相似形状のアルミ被覆鋼線16にダ
イスにより伸線加工する場合、ダイスと種線15
との接触状態は、横方向で第9図Aに示すように
なり、縦方向で第9図Bに示すようになつている
と思われる。
即ち、ダイス21による伸線加工において、第
9図Aに示す横方向の寸法減縮では種線15の横
寸法の40mmを20mmまで減少させ、第9図Bに示す
縦方向の寸法減縮では種線15の縦寸法の20mmを
10mmまで減少させることになる。従つて第9図
A,Bに示すように、種線15がダイス21のダ
イス孔に到達する位置が縦方向と横方向で異なる
ことになる。すると、寸法が大きく、ダイス孔に
先に到達した部分から先に加工が進行する結果、
寸法が小さく加工が遅れる部分側に柔らかいアル
ミニウム移動すると思われる。
以上のことから、形状が相似形状であれば、均
一な加工ができるといつた従来の考えかたは誤り
であることが明らかになつた。
また、このような加工率の差異を生じると縮径
加工中に焼き付きを生じる虞があるため、従来、
二硫化モリブデン等を含有した高価な潤滑剤を使
用しているが、この潤滑剤を使用しても焼き付き
を生じ易い傾向があつた。そして、このような焼
き付きを生じる部分は、加工材の全周ではなく、
加工がきつい部分であつて、被覆層が薄くなる部
分で特に生じ易いものであり、このことからも従
来方法の加工の不均一性がわかるものである。
本発明は、前記問題を鑑みてなされたもので、
均一な厚さの金属被覆層を有する異形複合線を製
造できる方法を提供することを目的とする。
「問題点を解決するための手段」
本発明は、前記問題点を解決するために、3つ
以上の辺によつて囲まれる横断面形状の金属芯材
の周囲に、この金属芯材よりも硬度の低い金属被
覆層を形成してなる異形複合線の製造方法におい
て、加工後に得るべき最終形状の金属芯材の横断
面を構成する複数の辺の1つ1つをそれぞれ同一
長さ長くして辺から構成される横断面形状の種芯
材を用い、この種芯材に均一厚さの金属被覆層を
形成した後に伸線加工を施し、前記金属芯材の
個々の辺を全て同一寸法だけ減少させて異形複合
線を形成するものである。
「作用」
本発明方法を実施するならば、種芯材の横断面
を構成する3つ以上の辺において、各辺を同一寸
法のみ縮径することになるために、各辺を均一に
縮径することができ、種芯材の全周にわたり等し
く減縮できるので均一な厚さの金属被覆層を有す
る異形複合線を製造できるとともに、伸線加工時
の焼き付きを防止できる。
「実施例」
第1図と第2図は、本発明方法の一実施例を説
明するためのもので、第2図に示す横断面略扇形
のアルミ被覆鋼線10を製造する場合には、ま
ず、第1図に示すように、横断面略扇形の種芯材
11の周囲にAlからなる金属被覆層12を形成
した横断面略扇形の母材13を用意する。この母
材13は、アルミ被覆鋼線10をその全体にわた
り等厚的に増径した形状をなしている。
即ち、母材13の横断面に沿う縦方向の辺の寸
法aは、最終形状のアルミ被覆鋼線10の縦方向
の辺の寸法Aに所定長さを加えた長さに設定さ
れ、母材13の横断面に沿う横方向の辺(この例
と場合は円弧)の寸法bは、最終形状のアルミ被
覆鋼線10の横方向の辺の寸法Bに、前記所定長
さを加えた長さに設定される。
なお、当然のことながら、横断面扇型の種芯材
11は4つの辺からなり、第1図と第2図に示す
扇型の左右の辺はどちらも同一寸法でその値はa
であるので、種芯材11の左右2つの片の寸法は
どちらも同一寸法とする。そして、種芯材11の
上下の辺(円弧)のうち、上側の辺(円弧)は先
に説明したbの値とするが、下側の辺(円弧)
は、第2図に示す扇型のアルミ被覆鋼線10の下
側の辺(円弧)に所定長さ加えた寸法とするのは
勿論である。
次に前記母材13にダイスを用いて断面減少率
15〜25%にて等厚的に縮径加工を施し、アルミ被
覆鋼線10を製造する。ここで、断面減少率の範
囲を前述のように限定したのは、25%より大きい
断面減少率では伸線加工に要する引き抜き力が大
きくなり、断線を生じることがあり、また、15%
未満の断面減少率では加工によつて表層近傍のみ
が加工され、芯材の中心部に欠陥が生じるととも
に、伸線回数が増加するためである。
前述のように縮径加工を施す場合、母材13の
横断面におて、縦方向の辺の縮径割合に対する横
方向の辺の縮径割合は異なるが、縦方向の辺の縮
径寸法と横方向の辺の縮径寸法は同一になため
に、両方向で(即ち全周で)等厚的に縮径するこ
とができ、第2図に示すような均一の厚さの被覆
層を有するアルミ被覆鋼線10を製造することが
できる。
また、縦方向の辺と横方向の辺で等厚的に縮径
させて伸線するために、周辺部での加工率を均一
化でき、伸線加工時の焼き付きも防止できる。ま
た、ダイスに加わる圧力を縦方向の辺と横方向の
辺で均一にできるために、ダイスの片減りを防止
でき、ダイス寿命を長くすることができる。この
ため、二硫化モリブデンを含有した高価な潤滑剤
ではなく通常の安価な潤滑剤を使用できるように
なり、製造コストの削減をなしうる。
ここで、前記のように等厚的に伸線加工する場
合において、ダイスと母材との関係は、第3図と
第4図に示す例を基に以下に説明する状態となつ
ていると推定される。なお、第3図と第4図に示
す例においては、理解の容易のために、アルミニ
ウムの被覆層を省略した状態で説明する。
ここでは、第3図Aに示す横断面であつて縦24
mm、横34mmの母材17を第3図Bに示す横断面で
あつて縦10mm、横20mmのアルミ被覆鋼線18にダ
イスにより伸線加工する場合、ダイス21と母材
17との接触状態は、横方向で第4図Aに示すよ
うになり、縦方向で第4図Bに示すようになつて
いると思われる。
即ち、第4図Aに示す横方向の減縮でほ母材1
7の横寸法の34mmを20mmまで減少させ、第4図B
に示す縦方向の伸線加工状態では母材17の縦寸
法の24mmを10mmまで減少させることになる。従つ
て第4図A,Bに示すように、縦方向と横方向で
同一値(14mm)だけ縮径することになり、この場
合、母材17の外周部分がダイス21のダイス孔
に到達する位置は、引き抜き方向に沿つて縦方向
と横方向で同一位置になると推定できる。即ち、
寸法の大きさ部分と寸法の小さい部分のいずれで
も同時にダイス孔に母材が到達する結果、柔らか
いアルミニウム部分が他の方向に流れることなく
伸線加工されるものと推定できる。この結果とし
て均一な加工が進行するものと推定できる。
なお、前述した方法は、アルミ以外の金属から
なる被覆層と、鋼以外の金属材料からなる芯材と
から構成される異形被覆複合線であつて、芯材に
芯材よりも柔らかい被覆層を形成する他の異形複
合線にも適用できるのは勿論である。
製造例 1
横断面積が9.6mm2で最終の横断面形状が略扇形
とアルミ被覆鋼線を製造するにあたり、この略扇
形の断面形状を等厚的に増径して得られる横断面
積41mm2の母材(0.71%C−0.75%Mn−0.2%Si−
残部Fe)を用意した。この母材に被覆率30%で
アルミを被覆した後に、減面率15〜23%の割合で
伸線加工を施してアルミ被覆鋼線を製造した。こ
のアルミ被覆鋼線においては、均一な厚さのアル
ミ被覆層を有しており、伸線加工中に焼き付きも
生じなかつた。このように製造されたアルミ被覆
鋼線のアルミ被覆層の厚さを測定した結果を後記
する第1表に示す。
「比較例」
最終の横断面形状が略扇形のアルミ被覆鋼線を
製造するにあたり、このアルミ被覆鋼線と相似形
の横断面形状を有し、横断面積40.5mm2の異形鋼線
を用意して、これにパンテイング処理を施し、更
に、被覆率30%となるようにアルミ層を被覆した
後に、伸線加工を施した。この伸線加工中、異形
鋼線の長径方向の端部に焼き付きを生じた。
以上のように製造されたアルミ被覆鋼線のアル
ミ被覆層の厚さを測定した結果を先の製造例の結
果と併せて第1表に示す。
"Industrial Application Field" The present invention relates to a method for manufacturing deformed composite wires such as aluminum-coated deformed steel wires used in optical fiber composite power transmission lines, by drawing from a seed core material of a special shape. The present invention relates to a method for manufacturing a composite wire having a coating layer of uniform thickness. "Prior Art" Conventionally, as a method for manufacturing deformed aluminum-coated steel wires used for optical fiber composite power transmission lines and the like, a method is known in which a wire-drawing process is performed on an aluminum-coated base material. This manufacturing method is a method in which the outer surface of a steel wire is coated with an aluminum layer to form an aluminum coated base material, and then the wire is finished into a predetermined shape by performing diameter reduction processing using a die. ``Problems to be Solved by the Invention'' However, in the past, when a deformed aluminum-coated steel wire was manufactured by the method described above, when coating the steel wire with an aluminum layer, it was difficult to form the aluminum coating layer to a uniform thickness. Even in this case, a problem occurred in that the thickness of the aluminum coating layer became locally non-uniform during the diameter reduction process using a die. This is because when performing diameter reduction using a die, the steel wire is processed through the aluminum coating layer with low hardness, and the diameter is reduced from a round wire to a strip with an irregular cross section, so the compressive force that acts during diameter reduction is The core material (steel wire) tends to be processed into a shape different from the shape of the die hole, resulting in uneven thickness of the aluminum coating layer. Therefore, conventionally,
A deformed aluminum coated steel wire is manufactured using the method described below based on FIGS. 5 to 7. As shown in FIG. 5, when producing an aluminum-coated steel wire 3 having a substantially fan-shaped cross section by covering a steel wire 1 with an aluminum coating layer 2, this conventional method has a similar shape to that of the aluminum-coated steel wire 3. In this method, a seed wire 4 shown in FIG. 6 having a large cross-sectional area is prepared, and this seed wire 4 is subjected to a diameter reduction process to produce the required aluminum-coated steel wire. However, when an aluminum-coated steel wire with a substantially fan-shaped cross section is manufactured by the conventional method, the processing rate in the major axis direction is substantially larger than that in the minor axis direction, and the machining of the peripheral portion is difficult. The size of the ratio affects the wire drawability and greatly influences the thickness of the aluminum coating layer and the shape of the core material, resulting in the problem of uneven thickness of the aluminum coating layer 6 as shown in Fig. 7. It was happening. This indicates that by machining similar shapes, the pressure (contact pressure) applied by the die to the surface of the machined part becomes uneven, and as a result, the soft aluminum moves to the area where the contact pressure is low. It is something. The reason for the phenomenon in which soft aluminum moves to areas with lower surface pressure when wire drawing is performed with similar shapes is shown in Figures 8 and 9.
This is presumed to be due to the reasons explained below based on the example shown in the figure. In addition, in the examples shown in FIGS. 8 and 9, for ease of explanation, the case where only the core material is used without the covering layer is assumed. The cross section shown in Figure 8A is 20 mm long and 40 mm wide.
The seed line 15 is a cross section shown in Figure 8B, and the length is 10.
When drawing an aluminum-coated steel wire 16 with a similar shape of 20 mm wide and 20 mm wide using a die, the die and the seed wire 15
It seems that the contact state is as shown in FIG. 9A in the horizontal direction and as shown in FIG. 9B in the vertical direction. That is, in the wire drawing process using the die 21, in the horizontal dimension reduction shown in FIG. 9A, the horizontal dimension of the seed line 15 is reduced from 40 mm to 20 mm, and in the vertical dimension reduction shown in FIG. 9 B, the seed line is reduced. The vertical dimension of 15 is 20mm.
It will be reduced to 10mm. Therefore, as shown in FIGS. 9A and 9B, the position where the seed line 15 reaches the die hole of the die 21 is different in the vertical direction and the horizontal direction. As a result, machining proceeds from the part that is larger in size and reaches the die hole first.
It is thought that the softer aluminum will move to the part where the dimensions are smaller and machining will be delayed. From the above, it has become clear that the conventional idea that uniform processing is possible if the shapes are similar is incorrect. In addition, if such a difference in processing rate occurs, there is a risk of burn-in during diameter reduction processing, so conventionally,
An expensive lubricant containing molybdenum disulfide or the like is used, but even with this lubricant, seizure tends to occur. The part where this kind of seizure occurs is not the entire circumference of the workpiece, but
This phenomenon is particularly likely to occur in areas where processing is difficult and where the coating layer is thin, and this fact also shows the non-uniformity of processing in conventional methods. The present invention was made in view of the above problems, and
It is an object of the present invention to provide a method capable of manufacturing a deformed composite wire having a metal coating layer of uniform thickness. "Means for Solving the Problems" In order to solve the above-mentioned problems, the present invention provides a structure in which a metal core material having a cross-sectional shape surrounded by three or more sides is surrounded by a metal core material that is larger than the metal core material. In a method for manufacturing a deformed composite wire formed by forming a metal coating layer with low hardness, each of a plurality of sides constituting a cross section of a metal core material in the final shape to be obtained after processing is lengthened by the same length. Using a seed core material with a cross-sectional shape consisting of two sides, a metal coating layer of uniform thickness is formed on this seed core material, and then wire drawing is performed, so that all the individual sides of the metal core material have the same size. , to form an irregularly shaped composite line. "Operation" If the method of the present invention is carried out, each side will be reduced in diameter by the same dimension on three or more sides constituting the cross section of the seed core material, so each side will be reduced in diameter uniformly. Since the seed core material can be equally reduced over the entire circumference, it is possible to manufacture a deformed composite wire having a metal coating layer of uniform thickness, and it is also possible to prevent seizure during wire drawing. "Example" FIGS. 1 and 2 are for explaining an example of the method of the present invention. When manufacturing an aluminum-coated steel wire 10 having a substantially fan-shaped cross section as shown in FIG. First, as shown in FIG. 1, a base material 13 having a substantially fan-shaped cross section is prepared, in which a metal coating layer 12 made of Al is formed around a seed core material 11 having a substantially fan-shaped cross section. This base material 13 has a shape in which the diameter of the aluminum-coated steel wire 10 is increased uniformly over its entire length. That is, the length a of the vertical side along the cross section of the base material 13 is set to the length A of the vertical side of the aluminum-coated steel wire 10 in the final shape plus a predetermined length. The dimension b of the lateral side (arc in this example) along the cross section of 13 is the length obtained by adding the predetermined length to the lateral side dimension B of the aluminum-coated steel wire 10 in the final shape. is set to As a matter of course, the seed core material 11 having a fan-shaped cross section consists of four sides, and the left and right sides of the fan-shaped shape shown in FIGS. 1 and 2 both have the same dimensions and the value is a.
Therefore, the dimensions of the two left and right pieces of the seed core material 11 are the same. Of the upper and lower sides (arcs) of the seed core material 11, the upper side (arc) has the value of b explained earlier, but the lower side (arc)
Of course, the dimension is the sum of the lower side (arc) of the fan-shaped aluminum-coated steel wire 10 shown in FIG. 2 plus a predetermined length. Next, a die is used for the base material 13 to reduce the area reduction rate.
The aluminum-coated steel wire 10 is manufactured by performing diameter reduction processing at a constant thickness of 15 to 25%. Here, the range of the area reduction rate was limited as mentioned above because if the area reduction rate is greater than 25%, the pulling force required for wire drawing becomes large and wire breakage may occur.
This is because if the cross-sectional area reduction ratio is less than that, only the vicinity of the surface layer will be processed, defects will occur in the center of the core material, and the number of wire drawings will increase. When performing the diameter reduction process as described above, in the cross section of the base material 13, the diameter reduction ratio of the horizontal sides is different from the diameter reduction ratio of the vertical sides, but the diameter reduction dimension of the vertical sides is Since the reduced diameter dimensions of the horizontal sides are the same, the diameter can be reduced uniformly in both directions (i.e., all around the circumference), creating a coating layer with a uniform thickness as shown in Figure 2. The aluminum-coated steel wire 10 can be manufactured. In addition, since the wire is drawn by reducing the diameter equally on the vertical and horizontal sides, the processing rate in the peripheral area can be made uniform, and seizure during wire drawing can be prevented. Furthermore, since the pressure applied to the die can be made uniform on the vertical and horizontal sides, it is possible to prevent the die from wearing out unevenly, and the life of the die can be extended. Therefore, instead of an expensive lubricant containing molybdenum disulfide, a normal, inexpensive lubricant can be used, and manufacturing costs can be reduced. Here, in the case of wire drawing with equal thickness as described above, the relationship between the die and the base material is as described below based on the examples shown in FIGS. 3 and 4. Presumed. Note that the examples shown in FIGS. 3 and 4 will be explained with the aluminum coating layer omitted for ease of understanding. Here, the cross section shown in Figure 3A and the vertical 24
When drawing a base material 17 with a diameter of 34 mm and a width of 34 mm into an aluminum coated steel wire 18 with a cross section of 10 mm in length and 20 mm in width using a die, the state of contact between the die 21 and the base material 17 is as follows. It seems that the horizontal direction is as shown in FIG. 4A, and the vertical direction is as shown in FIG. 4B. That is, by the lateral reduction shown in FIG. 4A, the base material 1
Reduce the horizontal dimension of 7 from 34mm to 20mm, and make
In the vertical wire drawing state shown in , the vertical dimension of the base material 17 of 24 mm is reduced to 10 mm. Therefore, as shown in FIGS. 4A and 4B, the diameter is reduced by the same value (14 mm) in the vertical and horizontal directions, and in this case, the outer peripheral portion of the base material 17 reaches the die hole of the die 21. It can be estimated that the position is the same in the vertical and horizontal directions along the drawing direction. That is,
As a result of the base material reaching the die hole at the same time in both the large-sized portion and the small-sized portion, it can be assumed that the soft aluminum portion is wire-drawn without flowing in other directions. As a result, it can be assumed that uniform processing progresses. Note that the method described above applies to a deformed coated composite wire consisting of a coating layer made of a metal other than aluminum and a core material made of a metal material other than steel, and the core material is coated with a coating layer that is softer than the core material. Of course, the present invention can also be applied to other irregularly shaped composite lines to be formed. Manufacturing example 1 When manufacturing an aluminum-coated steel wire with a cross-sectional area of 9.6 mm 2 and a final cross-sectional shape of approximately fan-shaped, the cross-sectional area of 41 mm 2 obtained by increasing the diameter of this approximately fan-shaped cross-sectional shape to the same thickness is obtained. Base material (0.71%C-0.75%Mn-0.2%Si-
The remainder Fe) was prepared. After coating this base material with aluminum at a coverage rate of 30%, wire drawing was performed at a rate of area reduction of 15 to 23% to produce an aluminum coated steel wire. This aluminum-coated steel wire had an aluminum coating layer with a uniform thickness, and no seizure occurred during wire drawing. The results of measuring the thickness of the aluminum coating layer of the aluminum coated steel wire produced in this manner are shown in Table 1 below. "Comparative Example" In order to manufacture an aluminum-coated steel wire whose final cross-sectional shape is approximately fan-shaped, a deformed steel wire with a cross-sectional shape similar to this aluminum-coated steel wire and a cross-sectional area of 40.5 mm 2 was prepared. Then, this was subjected to a panting treatment, and then coated with an aluminum layer to a coverage rate of 30%, and then subjected to a wire drawing process. During this wire drawing process, seizure occurred at the ends of the deformed steel wire in the major diameter direction. The results of measuring the thickness of the aluminum coating layer of the aluminum coated steel wire produced as described above are shown in Table 1 together with the results of the previous production examples.
【表】
第1表に示す結果より、本発明方法を適用して
製造された製造例のアルミ被覆異形鋼線のアルミ
被覆層の方が、従来方法によつて製造されたアル
ミ被覆異形鋼線のアルミ被覆層に比較して厚さが
揃つていることが明らかであり、本願発明によつ
て均一な厚さの被覆層を有した異形鋼線を製造で
きることが明らかになつた。
本願発明においては、第1表に示すように、
Al層の厚さが平均的な厚さに対するかたよりが、
約3%であるのに対し、比較例では±20%もの差
を生じており、本願発明方法で均一に加工できて
いることが明らかになつた。
「発明の効果」
以上説明したように本発明は、得るべき最終形
状の芯材の横断面形状の全ての片の寸法を同一寸
法分、均一増径した種芯材に被覆層を形成してか
ら縮径するものであり、縦方向の辺と横方向の辺
で同一寸法分縮径し、被覆層の厚さを均一に維持
しつつ縮径できるために、均一な厚さの被覆層を
有する異形複合線を製造できる効果がある。ま
た、種芯材の縦方向の辺と横方向の辺において均
一に縮径するために、伸線加工時にダイスに焼き
付きを生じないとともに、ダイス寿命が長くなる
効果がある。[Table] From the results shown in Table 1, the aluminum coating layer of the aluminum-coated deformed steel wire of the manufacturing example manufactured by applying the method of the present invention is superior to that of the aluminum-coated deformed steel wire manufactured by the conventional method. It is clear that the thickness is more uniform than that of the aluminum coating layer, and it is clear that the present invention can produce a deformed steel wire having a coating layer of uniform thickness. In the present invention, as shown in Table 1,
The deviation of the thickness of the Al layer from the average thickness is
While the difference was about 3%, the difference was as much as ±20% in the comparative example, and it became clear that uniform processing could be achieved by the method of the present invention. "Effects of the Invention" As explained above, the present invention forms a coating layer on a seed core material whose diameter is uniformly increased by the same dimension in all pieces of the cross-sectional shape of the core material in the final shape to be obtained. The diameter is reduced by the same size on the vertical and horizontal sides, and the diameter can be reduced while maintaining the thickness of the coating layer, making it possible to create a coating layer with a uniform thickness. There is an effect that it is possible to manufacture a deformed composite wire having the following properties. Furthermore, since the diameter of the seed core material is uniformly reduced on the vertical and horizontal sides, the die does not seize during wire drawing, and the life of the die is extended.
第1図と第2図は、本発明の一実施例を説明す
るためのもので、第1図は種芯材の横断面図、第
2図は本発明方法によつて製造されたアルミ被覆
鋼線の断面図、第3図A,Bは本発明における伸
線加工状態を推定するための種線の例を示す正面
図、第4図A,Bは第3図に示す種線を伸線加工
している状態の推定例を示す説明図、第5図は従
来の方法で製造しようとする異形断面条を示す横
断面図、第6図は従来方法に使用された種線の横
断面図、第7図は従来の方法で製造されたアルミ
被覆異形断面条の横断面図、第8図A,Bは従来
の伸線加工状態を推定するための母材を示す正面
図、第9図A,Bは第8図に示す母材を伸線加工
している状態を示す説明図である。
10……アルミ被覆鋼線(異形複合線)、11
……種芯材、12……アルミ被覆層、13……母
材、21……ダイス。
Figures 1 and 2 are for explaining one embodiment of the present invention. Figure 1 is a cross-sectional view of a seed core material, and Figure 2 is an aluminum coating manufactured by the method of the present invention. A cross-sectional view of a steel wire, FIGS. 3A and 3B are front views showing examples of seed lines for estimating the wire drawing state in the present invention, and FIGS. 4A and B are cross-sectional views of steel wires shown in FIG. An explanatory diagram showing an estimated example of the wire processing state, Fig. 5 is a cross-sectional view showing an irregular cross-section strip to be manufactured by the conventional method, and Fig. 6 is a cross-sectional view of the seed line used in the conventional method. 7 is a cross-sectional view of an aluminum coated irregular cross-section strip manufactured by the conventional method, FIG. 8 A and B are front views showing the base material for estimating the conventional wire drawing state, and FIG. Figures A and B are explanatory diagrams showing a state in which the base material shown in Figure 8 is being wire-drawn. 10... Aluminum coated steel wire (deformed composite wire), 11
... Seed core material, 12 ... Aluminum coating layer, 13 ... Base material, 21 ... Dice.
Claims (1)
金属芯材の周囲に、この金属芯材よりも硬度の低
い金属被覆層を形成してなる異形複合線の製造方
法において、 加工後に得るべき最終形状の金属芯材の横断面
を構成する複数の辺の1つ1つをそれぞれ同一長
さ長くして辺から構成される横断面形状の種芯材
を用い、この種芯材に均一厚さの金属被覆層を形
成した後に伸線加工を施し、前記金属芯材の個々
の辺を全て同一寸法だけ減少させて異形複合線を
形成することを特徴とする異形複合線の製造方
法。[Claims] 1. Manufacture of a deformed composite wire by forming a metal coating layer having a lower hardness than the metal core material around a metal core material having a cross-sectional shape surrounded by three or more sides. In the method, each of the plurality of sides constituting the cross section of the metal core material in the final shape to be obtained after processing is lengthened by the same length, using a seed core material having a cross-sectional shape made up of sides, An irregular shape characterized by forming a metal coating layer of uniform thickness on this type of core material and then subjecting it to wire drawing processing, reducing all the individual sides of the metal core material by the same dimension to form an irregularly shaped composite wire. Method of manufacturing composite wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP30599486A JPS63157715A (en) | 1986-12-22 | 1986-12-22 | Manufacture of special-shaped composite wire |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP30599486A JPS63157715A (en) | 1986-12-22 | 1986-12-22 | Manufacture of special-shaped composite wire |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63157715A JPS63157715A (en) | 1988-06-30 |
| JPH0359769B2 true JPH0359769B2 (en) | 1991-09-11 |
Family
ID=17951791
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP30599486A Granted JPS63157715A (en) | 1986-12-22 | 1986-12-22 | Manufacture of special-shaped composite wire |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63157715A (en) |
-
1986
- 1986-12-22 JP JP30599486A patent/JPS63157715A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63157715A (en) | 1988-06-30 |
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