JPH0245522B2 - - Google Patents

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Publication number
JPH0245522B2
JPH0245522B2 JP58136594A JP13659483A JPH0245522B2 JP H0245522 B2 JPH0245522 B2 JP H0245522B2 JP 58136594 A JP58136594 A JP 58136594A JP 13659483 A JP13659483 A JP 13659483A JP H0245522 B2 JPH0245522 B2 JP H0245522B2
Authority
JP
Japan
Prior art keywords
diameter
roller
neck
core
length
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 - Lifetime
Application number
JP58136594A
Other languages
Japanese (ja)
Other versions
JPS6027410A (en
Inventor
Yoshihiro Nakagawa
Yutaka Nakai
Hiroaki Katayama
Akinari Kitaoka
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.)
Kubota Corp
Original Assignee
Kubota Corp
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 by Kubota Corp filed Critical Kubota Corp
Priority to JP13659483A priority Critical patent/JPS6027410A/en
Publication of JPS6027410A publication Critical patent/JPS6027410A/en
Publication of JPH0245522B2 publication Critical patent/JPH0245522B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B27/00Rolls, roll alloys or roll fabrication; Lubricating, cooling or heating rolls while in use
    • B21B27/02Shape or construction of rolls
    • B21B27/03Sleeved rolls

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  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Reduction Rolling/Reduction Stand/Operation Of Reduction Machine (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は、胴部が細長くネツク部が胴長に比べ
て比較的短い複合鋳造ローラーの製造方法に関す
る。 一般に、鉄鋼材の圧延機に附属するローラー類
例えば、ホツトランテーブルローラー、搬送ロー
ラー、オーバーランテーブルローラー、デイレイ
テーブルローラー、コイラーのボトムピンチロー
ル、ラツパーローラー等は、第1図に示す如く、
胴部1の胴径D1に対して胴長lが長く、かつネ
ツク部2,3の直径Doは小さく、しかも胴部1
両端のネツク長l1及びl2は、胴長lに対して短い。
即ち、数値で示せば、 D1/l=0.12〜0.25 Do/D1=0.3〜0.55 l1/l又はl2/l=0.05〜0.55 であり、また、ローラーの廃却径D2については、 D2/D1=0.70〜0.95 の範囲である。 このような形状のローラーの製造に際して、従
来は、第2図に示す如く、胴スリーブ4を別に製
作し、軸5を固着部6,6で焼ばめや接着等の手
段で前記胴スリーブ4に固着する組み立て方式が
採用されている。ここで、前記胴スリーブ4は、
単層スリーブである他、表面層を耐摩耗性材料で
形成した第1外層とその下部を強靭な材料で形成
した第2外層とからなる複合スリーブとする場合
も有り、他方軸5としては炭素鋼や合金鋼等の強
靭材が用いられている。 また、第3図に示す如く、前記と同様の胴スリ
ーブ7の両端に一体物でない軸材8,9を固着部
10,11で焼ばめ等の方法で組み立てる場合も
ある。 しかし、前記第2図に示すローラーの場合、胴
スリーブ4が細長いため、その長寸小径の軸穴加
工が困難であり、且つ軸5も全長に亘り加工しな
ければならないので経済的でない。また第3図に
示すローラーの場合も胴スリーブ4に困難な軸穴
加工を行わなければならない上、軸が分割されて
いるので強度上不安な点が残る。即ち、第2図、
第3図に示すローラーは、ローラーの形状が前述
の数値に示した如く、非常に細長いため製造上困
難な点があり、又不経済な加工となる。 仮に、通常のロールの如く、胴径D1と胴長l
との寸法が比較的大きく、且つ、D1/lの値が
前述した値より大きく、太短いものであれば加工
上前述したような問題は起こらない。 本発明は上記の点に鑑みなされたもので、製造
が容易で且つ経済的な複合鋳造ローラーの製造法
を提供することを目的とし、その要旨とするとこ
ろは、 目的とするローラーの胴径及び全長よりやや大
径、長尺である円柱状複合材の外殻層を遠心力鋳
造し、次に目的とするローラーの胴芯部およびネ
ツク部となる円柱状複合材の芯部を鋳込み、前記
外殻層と冶金的に溶着一体化した後、該円柱状複
合材を削り出し、胴径:D1、廃却径:D2、ネツ
ク部径:Dn、胴長:l、胴部両端のネツク長:
l1・l2、胴芯部径:D3を、 D2/D1=0.7〜0.95 D1/l=0.12〜0.25 Dn/D1=0.3〜0.55 l1/l又はl2/l=0.05〜0.20 D3/D1=0.55〜0.70 Dn<D3<D2 とする点にある。 次に、この発明について詳述する。 第4図は、本発明方法により製造された複合鋳
造ローラーの一例を示しており、耐摩耗性、耐肌
荒性、耐熱亀裂性の優れた材料で形成された胴外
殻層13と、靭性の特に優れた強靭材で作成され
た胴芯部14とが冶金的に溶着一体化されてお
り、また、その寸法・形状は、本発明の要旨に述
べた関係を満しており、限定理由を下記に示す。 D2/D1=0.7〜0.95 胴径D1に対して廃却径D2が0.7未満の場合は廃
却時のローラー表面と胴芯部表面との肉厚が過少
となり、芯材が露出するおそれがあり、一方0.95
以上の場合は有効使用層が少なくなり経済的でな
い。また、ローラー形状として一般的でない。 D1/l=0.12〜0.25 D1/lは胴径D1と胴長lとの比を示し、この
値はローラーの形状が細長いことを示している。
0.25を越える短かいローラーの場合は内径を加工
することが比較的容易である。一方、0.12未満の
細長いローラーは一般的でなく、また後述の遠心
力鋳造の際、溶着不良や外殻層厚さの均一性に問
題が生じる。 Dn/D1=0.3〜0.55 Dn/D1はネツク部径Dnと胴径D1との比を示
し、0.3未満では後述の円柱状複合材からネツク
部を削り出す際不経済であり、0.55を越える場合
はD2も大きくなり、有効使用層が少なくなる。 l1/l又はl2/l=0.05〜0.20 l1又はl2はネツク長を示し、0.20を越える場合、
円柱状複合材からネツク部を削り出す時、不経済
である。0.05未満のものはローラー形状として一
般的でない。 Dn<D3<D2 D3軸芯部径すなわち外殻層と軸芯部との境界
の直径はネツク径Dnより大きく、廃却径D2より
小さくなければ、廃却時、外殻層の厚さが不足
し、胴表面に芯材が露出することになる。Dnよ
りD3が小さい場合はネツク部に硬い外殻材が残
り、ネツク部の強度が確保されない。尚、Dn<
D3<D2の各値をD1で除すと、上記Dn/D1および
D2/D1の限定よりD3/D1=0.55〜0.70となる。 この発明によつて複合鋳造ローラーを製造する
場合、先ず、本発明の目的とする、第4図に示す
最終形状の複合鋳造ローラーの胴径D1及び全長
Lより、加工分だけ大径且つ長尺な胴径D1′及び
全長L′を有し、異材質で形成された外殻層18と
芯部19とが冶金的に溶着一体化された、第5図
に示す円柱状複合材17をまず製造する。 前記円柱状複合材17の製造をより詳しく述べ
ると、先ず該円柱状複合材17の外殻層18を高
合金グレン材、高合金チルド材、高クロム鋳鉄、
高硬度アダマイト材、高合金ダクタイル鋳鉄等の
耐摩耗性、耐肌荒性、耐熱亀裂性の優れた材料で
遠心力鋳造した後、鋳鋼材、アダマイト材、黒鉛
鋼材、ダクタイル鋳鉄等の特に強靭な材料で芯部
19を鋳込み、前記外殻層18と冶金的に溶着一
体化させる。 この鋳込みに際して、前記外殻層18が水平型
遠心力鋳造の場合は、外殻層18が完全に凝固し
た後に遠心力鋳造機の金型を垂直に立てて芯部材
溶湯を鋳込み、また、傾斜型遠心力鋳造の場合
は、外殻層18の形成後引き続いて鋳造機金型内
へ芯部材溶湯を鋳込む。 この場合、該円柱状複合材17の芯部19は、
そのまま目的とする複合鋳造ローラーの胴芯部1
4となるので、本発明の要旨に述べた寸法関係、
即ちDn<D3<D2の関係を満足しなければならな
い。 次に、該円柱状複合材17に機械加工を施し、
目的とする複合鋳造ローラーの寸法・形状に削り
出す。この加工は、被加工材が棒状であり、加工
が困難な長寸小径の軸穴加工が伴わず、その上ネ
ツク部15,16の長さl1・l2が胴長lに比べて
l1/l又はl2/l=0.05〜0.2と短いので、加工が
非常に容易であり且つ削除部が少ないので経済的
である。 削り出されたネツク部15,16は、その直径
Dnの寸法がDn<D3と規定されているので胴芯部
14と同様の強靭材となり折損及び強度不足の不
安は解消する。 ところで、第6図に示す如く、遠心力鋳造機金
型20の両端にテーパー状の砂型スリーブ21,
21が内嵌固定された、従来の複合ロール用鋳型
を用いても、本発明のローラーは製作可能なので
あるが、この場合は、ローラーの胴径D1及びネ
ツク部径Dnが小径であるので、鋳型の形成及び
胴外殻層13の注湯が困難であり、更にこの方法
では、ネツク部の冷却が遅くなりネツク部の強靭
性が劣り、特に、胴芯部が鋼系材料のときは分子
荒れが生じネツク部の性能に問題を生じ好ましく
ない。また、胴部が長いため胴部末端付近で冷却
が早くなり、胴外殻部と胴芯部との溶着不良が発
生しやすいので好ましくない。 次に実施例を掲げて説明する。 実施例 1 製品胴径310φ×胴長2300mm、廃却径294φ、ネ
ツク部径130φ、片側ネツク長121mm、他方ネツク
長285mmのローラーの製造例。 (1) 遠心力鋳造(金型回転数830rpm、鋳込温度
1380℃)で外径322φ、全長2805mm、内径270〜
285φの円柱状複合材の外殻層を鋳込んだ。 (2) 前記外殻層凝固後、該金型を垂直に立てて静
置鋳型とし、上部より芯部材を鋳込み温度1370
℃で鋳込み、円柱状複合材を作成した。 (3) 前記円柱状複合材を歪取熱処理後、機械加工
により削り出し、製品ローラーを得た。 (4) 前記ローラーの胴外殻層及び胴芯部の成分及
び硬度は表1の通りであつた。 実施例 2 製品胴径280φ×胴長1727mm、廃却径256φ、ネ
ツク部径125φ、片側ネツク長152mm、他方ネツク
長310mmのローラーの製造例。 (1) 遠心力鋳造(金型回転数875rpm、鋳込温度
1410℃)で外径296φ、全長2290mm、内径135〜
145φの円柱状複合材の外殻層を鋳込んだ。 (2) 前記外殻層凝固後、該金型を垂直に立てて静
置鋳型とし、上部より芯部材を鋳込み温度1490
℃で鋳込み、円柱状複合材を作成した。 (3) 前記円柱状複合材を高温熱処理し、荒加工後
胴部のみ焼準を行ない、製品ローラー寸法に削
り出した。 (4) 前記ローラーの胴外殻層及び胴芯部の成分及
び硬度は表2の通りであつた。
The present invention relates to a method for manufacturing a composite casting roller having a long and narrow body and a relatively short neck compared to the length of the body. In general, rollers attached to rolling mills for steel materials, such as hot run table rollers, conveyance rollers, overrun table rollers, day table rollers, bottom pinch rolls of coilers, and wrapper rollers, are as shown in Figure 1.
The trunk length l is long with respect to the trunk diameter D 1 of the trunk 1, and the diameter D o of the neck parts 2 and 3 is small.
The neck lengths l 1 and l 2 at both ends are shorter than the trunk length l.
That is, in numerical terms, D 1 /l = 0.12 to 0.25 D o /D 1 = 0.3 to 0.55 l 1 /l or l 2 / l = 0.05 to 0.55, and regarding the waste diameter D 2 of the roller is in the range of D 2 /D 1 =0.70 to 0.95. Conventionally, when manufacturing a roller having such a shape, as shown in FIG. 2, the body sleeve 4 is manufactured separately, and the shaft 5 is attached to the body sleeve 4 by means of shrink fitting, gluing, etc. with the fixing portions 6, 6. An assembly method has been adopted in which it is fixed to the Here, the torso sleeve 4 is
In addition to being a single-layer sleeve, there is also a composite sleeve consisting of a first outer layer whose surface layer is made of a wear-resistant material and a second outer layer whose lower part is made of a tough material, while the shaft 5 is made of carbon. Tough materials such as steel and alloy steel are used. Further, as shown in FIG. 3, shaft members 8 and 9 which are not integrated at both ends of the body sleeve 7 similar to those described above may be assembled by a method such as shrink fitting using fixed portions 10 and 11. However, in the case of the roller shown in FIG. 2, since the body sleeve 4 is elongated, it is difficult to machine a long and small diameter shaft hole, and the shaft 5 must also be machined over its entire length, which is not economical. Further, in the case of the roller shown in FIG. 3, it is necessary to perform difficult shaft hole machining in the body sleeve 4, and since the shaft is divided, the strength remains unreliable. That is, Fig. 2,
The roller shown in FIG. 3 has a very elongated shape as shown in the above-mentioned numerical values, so it is difficult to manufacture and the processing is uneconomical. Suppose, like a normal roll, the body diameter D 1 and the body length l
If the dimensions are relatively large, the value of D 1 /l is larger than the above-mentioned value, and it is thick and short, the above-mentioned problems in processing will not occur. The present invention was made in view of the above points, and aims to provide a manufacturing method for a composite casting roller that is easy to manufacture and economical, and the gist thereof is to provide a method for manufacturing a composite casting roller that is easy to manufacture and is economical. The outer shell layer of the cylindrical composite material, which has a diameter slightly larger than the overall length and is longer, is centrifugally cast, and then the core of the cylindrical composite material, which will become the body core and neck portion of the desired roller, is cast. After being metallurgically welded and integrated with the outer shell layer, the cylindrical composite material is cut out, with body diameter: D 1 , waste diameter: D 2 , neck diameter: Dn, body length: l, and the shapes of both ends of the body. Chief Netsuku:
l 1 · l 2 , body core diameter: D 3 , D 2 /D 1 = 0.7 to 0.95 D 1 /l = 0.12 to 0.25 Dn/D 1 = 0.3 to 0.55 l 1 /l or l 2 /l = 0.05~0.20 D3 / D1 =0.55~0.70 Dn< D3 < D2 . Next, this invention will be explained in detail. FIG. 4 shows an example of a composite casting roller manufactured by the method of the present invention, in which the shell outer layer 13 is made of a material with excellent wear resistance, roughness resistance, and heat cracking resistance, and the outer shell layer 13 has excellent toughness. The core part 14 is metallurgically welded and integrated with the body core part 14 made of a particularly excellent tough material, and its dimensions and shape satisfy the relationships stated in the gist of the present invention. is shown below. D 2 /D 1 = 0.7 to 0.95 If the waste diameter D 2 is less than 0.7 with respect to the body diameter D 1 , the wall thickness between the roller surface and the body core surface during disposal will be too small, and the core material will be exposed. while 0.95
In the above case, the number of effective users decreases and it is not economical. Also, it is not a common roller shape. D 1 /l=0.12 to 0.25 D 1 /l indicates the ratio of the barrel diameter D 1 to the barrel length l, and this value indicates that the roller has an elongated shape.
In the case of short rollers exceeding 0.25 mm, it is relatively easy to process the inner diameter. On the other hand, elongated rollers with a diameter of less than 0.12 are not common, and also cause problems with poor welding and uniformity of the outer shell layer thickness during centrifugal casting described below. Dn/D 1 = 0.3 to 0.55 Dn/D 1 indicates the ratio of the neck diameter Dn to the body diameter D 1. If it is less than 0.3, it will be uneconomical to carve out the neck from the cylindrical composite material described below, and 0.55 If it exceeds , D 2 will also increase and the effective usage layer will decrease. l 1 /l or l 2 /l = 0.05 to 0.20 l 1 or l 2 indicates the neck length, and if it exceeds 0.20,
It is uneconomical to cut out the neck part from a cylindrical composite material. Anything less than 0.05 is not common for roller shapes. Dn<D 3 <D 2 D 3 If the diameter of the axial core, that is, the diameter of the boundary between the outer shell layer and the axial core, is larger than the neck diameter Dn and smaller than the disposal diameter D 2 , the outer shell layer will be removed during disposal. The thickness of the core material is insufficient, and the core material is exposed on the surface of the body. If D3 is smaller than Dn, a hard outer shell material remains at the neck, and the strength of the neck cannot be ensured. In addition, Dn<
If each value of D 3 < D 2 is divided by D 1 , the above Dn/D 1 and
Due to the limitation of D 2 /D 1 , D 3 /D 1 =0.55 to 0.70. When manufacturing a composite casting roller according to the present invention, first, a diameter and a length larger than the body diameter D 1 and overall length L of the composite casting roller in the final shape shown in FIG. A cylindrical composite material 17 shown in FIG. 5 has a long body diameter D1 ' and a full length L', and has an outer shell layer 18 and a core part 19 made of different materials that are metallurgically welded and integrated. is manufactured first. To describe the manufacture of the cylindrical composite material 17 in more detail, first, the outer shell layer 18 of the cylindrical composite material 17 is made of high alloy grain material, high alloy chilled material, high chromium cast iron,
After centrifugal casting of materials with excellent wear resistance, roughness resistance, and heat cracking resistance such as high-hardness adamite material and high-alloy ductile cast iron, particularly strong materials such as cast steel material, adamite material, graphite steel material, and ductile cast iron are used. The core portion 19 is cast with a material and is metallurgically welded and integrated with the outer shell layer 18. At the time of this casting, if the outer shell layer 18 is horizontal centrifugal casting, after the outer shell layer 18 is completely solidified, the mold of the centrifugal casting machine is stood vertically and the core member molten metal is cast. In the case of die centrifugal force casting, after the outer shell layer 18 is formed, the core member molten metal is subsequently cast into the casting machine mold. In this case, the core portion 19 of the cylindrical composite material 17 is
Core part 1 of the composite casting roller intended as it is
4, so the dimensional relationship stated in the gist of the present invention,
That is, the relationship Dn<D 3 <D 2 must be satisfied. Next, the cylindrical composite material 17 is machined,
Cut to the desired size and shape of the composite casting roller. In this machining, the workpiece is rod-shaped, and machining of long and small diameter shaft holes, which is difficult to machine, is not involved, and in addition, the lengths l1 and l2 of the neck portions 15 and 16 are longer than the body length l.
Since l 1 /l or l 2 /l is short (0.05 to 0.2), processing is very easy and there are few removed parts, so it is economical. The diameter of the cut out neck portions 15 and 16 is
Since the dimension Dn is specified as Dn<D 3 , it becomes a strong material similar to the trunk core 14, eliminating concerns about breakage and insufficient strength. By the way, as shown in FIG. 6, there are tapered sand mold sleeves 21 at both ends of the centrifugal casting machine mold 20.
The roller of the present invention can be manufactured even by using a conventional composite roll mold in which the roller 21 is fixedly fitted, but in this case, the roller body diameter D 1 and the neck diameter Dn are small. , it is difficult to form a mold and pour the metal into the shell shell layer 13, and furthermore, with this method, the cooling of the neck portion is slow and the toughness of the neck portion is poor, especially when the shell core portion is made of steel-based material. Molecular roughness occurs, causing problems in the performance of the neck portion, which is undesirable. Further, since the body is long, cooling occurs quickly near the end of the body, which is undesirable because poor welding between the body outer shell and the body core tends to occur. Next, examples will be given and explained. Example 1 An example of manufacturing a roller with a product body diameter of 310φ x body length of 2300mm, a waste diameter of 294φ, a neck diameter of 130φ, one side of the neck length of 121mm, and the other side of the neck length of 285mm. (1) Centrifugal force casting (mold rotation speed 830 rpm, casting temperature
1380℃), outer diameter 322φ, total length 2805mm, inner diameter 270~
A 285φ cylindrical composite outer shell layer was cast. (2) After solidification of the outer shell layer, the mold is stood vertically as a stationary mold, and the core member is poured from the top at a temperature of 1370°C.
A cylindrical composite material was created by casting at ℃. (3) After the cylindrical composite material was subjected to strain relief heat treatment, it was machined to obtain a product roller. (4) The components and hardness of the outer shell layer and the core of the roller were as shown in Table 1. Example 2 An example of manufacturing a roller with a product body diameter of 280φ x body length of 1727mm, a waste diameter of 256φ, a neck diameter of 125φ, one side of the neck length of 152mm, and the other side of the neck length of 310mm. (1) Centrifugal force casting (mold rotation speed 875 rpm, casting temperature
1410℃), outer diameter 296φ, total length 2290mm, inner diameter 135~
An outer shell layer of 145φ cylindrical composite material was cast. (2) After the outer shell layer solidifies, the mold is stood vertically to form a stationary mold, and the core member is poured from the top at a temperature of 1490°C.
A cylindrical composite material was created by casting at ℃. (3) The cylindrical composite material was subjected to high-temperature heat treatment, and after rough processing, only the body portion was normalized and machined to the dimensions of a product roller. (4) The components and hardness of the outer shell layer and the core of the roller were as shown in Table 2.

【表】【table】

【表】 以上述べたように本発明のローラー製造法によ
れば、胴部が細長く且つネツク部が胴長に比べて
比較的短い、目的とする複合鋳造ローラーの胴径
及び全長よりやや大径・長尺である円柱状複合材
を鋳造し、次に該円柱状複合材から前記目的とす
る複合鋳造ローラーを削り出すので、鋳造に際す
る造型工数及び加工工数が少なくて済み経済的で
ある上、ローラーの動バランスも良い。また小径
長尺複合材に起りがちな端部の溶着不良が生じて
も、この部分は削り取られるので最終製品には残
らない。またネツク部も胴芯部材より削り出され
るので、強靭性は良好である。もちろん、本発明
に係る複合ローラーの胴外殻層と胴芯部とは鋳造
により溶着一体化されるため、廃却径まで使用し
ても強度上の心配はなく、また従来のように焼ば
めに起因して発生し、ローラーの割れの原因とな
る過大な引張り応力がローラー胴内面に生じるこ
ともなく、長寿命である。
[Table] As described above, according to the roller manufacturing method of the present invention, the body diameter and overall length of the target composite casting roller, which has an elongated body and a relatively short neck portion compared to the body length, can be obtained. - Since a long cylindrical composite material is cast and then the desired composite casting roller is cut out from the cylindrical composite material, the number of molding and processing steps during casting is reduced, making it economical. Above, the dynamic balance of the rollers is also good. Furthermore, even if poor welding occurs at the ends, which tends to occur with small-diameter long composite materials, this portion is scraped off and does not remain in the final product. Furthermore, since the neck portion is also machined out from the body core member, it has good toughness. Of course, since the outer shell layer and the core part of the composite roller according to the present invention are welded and integrated by casting, there is no need to worry about strength even if it is used up to the scrap diameter, and there is no need to worry about the strength when it is used up to the scrap diameter. Excessive tensile stress, which is caused by mechanical problems and causes cracks in the roller, does not occur on the inner surface of the roller barrel, resulting in a long life.

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

第1図は本発明を適用するローラーの外形図、
第2図・第3図は従来のローラーの構造を示す断
面図、第4図は本発明のローラーの構造を示す断
面図、第5図は本発明ローラーの素材である円柱
状複合材の断面図、第6図は従来の複合ロール製
造用の遠心力鋳造機金型の断面図を示す。 1,12……胴部、2,3,15,16……ネ
ツク部、13……胴外殻層、14……胴芯部、1
7……円柱状複合材、18……外殻層、19……
芯部。
FIG. 1 is an external view of a roller to which the present invention is applied;
Figures 2 and 3 are cross-sectional views showing the structure of a conventional roller, Figure 4 is a cross-sectional view showing the structure of the roller of the present invention, and Figure 5 is a cross-section of a cylindrical composite material that is the material of the roller of the present invention. FIG. 6 shows a cross-sectional view of a conventional centrifugal casting machine mold for manufacturing composite rolls. 1, 12... Torso, 2, 3, 15, 16... Neck part, 13... Torso outer shell layer, 14... Trunk core, 1
7...Cylindrical composite material, 18...Outer shell layer, 19...
core.

Claims (1)

【特許請求の範囲】 1 目的とするローラーの胴径及び全長よりやや
大径・長尺である円柱状複合材の外殻層を遠心力
鋳造し、次に目的とするローラーの胴芯部および
ネツク部となる、円柱状複合材の芯部を鋳込み、
前記外殻層と冶金的に溶着一体化した後、該円柱
状複合材から削り出して、胴径:D1、廃却径:
D2、ネツク部径:Dn、胴長:l、胴部両端のネ
ツク長:l1・l2、胴芯部径:D3を、 D2/D1=0.7〜0.95 D1/l=0.12〜0.25 Dn/D1=0.3〜0.55 l1/l又はl2/l=0.05〜0.20 D3/D1=0.55〜0.70 Dn<D3<D2 とすることを特徴とする複合鋳造ローラーの製造
法。
[Claims] 1. An outer shell layer of a cylindrical composite material having a diameter and length slightly larger than the body diameter and overall length of the target roller is centrifugally cast, and then the core and body parts of the target roller are cast by centrifugal force. The core of the cylindrical composite material, which will become the neck part, is cast.
After metallurgically welding and integrating with the outer shell layer, the cylindrical composite material is machined to have a body diameter: D 1 and a waste diameter:
D2 , neck diameter: Dn, trunk length: l, neck length at both ends of the trunk: l1l2 , trunk core diameter: D3 , D2 / D1 =0.7~0.95 D1 /l= A composite casting roller characterized in that 0.12-0.25 Dn/ D1 = 0.3-0.55 l1 /l or l2 /l = 0.05-0.20 D3 / D1 = 0.55-0.70 Dn< D3 < D2 . manufacturing method.
JP13659483A 1983-07-25 1983-07-25 Composite cast roll and its manufacture Granted JPS6027410A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13659483A JPS6027410A (en) 1983-07-25 1983-07-25 Composite cast roll and its manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13659483A JPS6027410A (en) 1983-07-25 1983-07-25 Composite cast roll and its manufacture

Publications (2)

Publication Number Publication Date
JPS6027410A JPS6027410A (en) 1985-02-12
JPH0245522B2 true JPH0245522B2 (en) 1990-10-09

Family

ID=15178944

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13659483A Granted JPS6027410A (en) 1983-07-25 1983-07-25 Composite cast roll and its manufacture

Country Status (1)

Country Link
JP (1) JPS6027410A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105817595A (en) * 2015-01-07 2016-08-03 大连宝锋机器制造有限公司 Pouring method of centrifugal compound hollow roll

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5035888A (en) * 1973-08-01 1975-04-04

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5035888A (en) * 1973-08-01 1975-04-04

Also Published As

Publication number Publication date
JPS6027410A (en) 1985-02-12

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