JPH0229428B2 - SHINZAINOKYOJINNAFUKUGOROORUNOSEIZOHOHO - Google Patents
SHINZAINOKYOJINNAFUKUGOROORUNOSEIZOHOHOInfo
- Publication number
- JPH0229428B2 JPH0229428B2 JP10380181A JP10380181A JPH0229428B2 JP H0229428 B2 JPH0229428 B2 JP H0229428B2 JP 10380181 A JP10380181 A JP 10380181A JP 10380181 A JP10380181 A JP 10380181A JP H0229428 B2 JPH0229428 B2 JP H0229428B2
- Authority
- JP
- Japan
- Prior art keywords
- outer shell
- intermediate layer
- cast
- layer
- shell 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 - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/16—Casting in, on, or around objects which form part of the product for making compound objects cast of two or more different metals, e.g. for making rolls for rolling mills
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
Description
(産業上の利用分野)
本発明は芯材の強靭な複合ロールの製造方法に
関する。
(従来の技術)
圧延用ロールにおいては、一般に圧延材と接す
るロール胴表面部には耐摩耗性、耐クラツク性、
耐肌荒性が要求され、一方芯部には圧延荷重に耐
える強靭性が要求されるため、その胴部外殻層は
高合金グレン材、高合金チルド材、高合金ダクタ
イル鋳鉄材等の組織中に高硬度の炭化物を有する
高合金鋳鉄材で形成し、一方その胴部芯部及びネ
ツク部は、経済性を考慮して、通常低合金の高級
鋳鉄又はダクタイル鋳鉄の強靭材で形成した複合
ロールが使用されてきている。
しかしながら、最近の圧延条件の変遷は、より
圧下率を大きくし、又低温材の圧延を行う傾向に
あり、このためその胴部芯部及びネツク部を形成
する芯材にはより強靭なものが求められ、上記従
来法では使用に耐えない場合も生じており、また
ホツトストリツプ用ワークロールなどにあつて
は、芯材の剛性を大きくしてロールの変形を少な
くする必要から、芯材に弾性係数の大きい材料を
用いることが要望されている。
このような要望に応えるものとして、出願人は
芯材を更に強靭な鋳鋼材、黒鉛鋳鋼材あるいはア
ダマイト材で形成した複合ロールを提案している
(実願昭55−170075〜170077号参照)。
(発明が解決しようとする課題)
しかしながら、このような強靭材によつて芯材
を形成する場合にあつては、その外殻層が比較的
溶融点の低い鋳鉄材から形成されるのに対し、芯
材はその溶融点が外殻層材のそれよりも高く、従
つてその鋳込温度を高くする必要があるため、製
造上次のような問題点を来たしている。
すなわち、この種の複合ロールを鋳造する場合
では、通常の遠心力鋳造法に従い外殻層を鋳造し
た後、外殻層と溶着一体化すべく芯材溶湯を鋳込
むと、外殻層材の溶融温度に比し芯材溶湯の温度
が相当高いため、外殻層内面の溶損量が多くなる
のみならず、第2図に示す如く、厚さ(a+b)
の外殻層1の内面側のかなりの肉厚部分bに、高
温の芯材3により再加熱されて外殻層鋳鉄組織中
の炭化物が黒鉛化する部分を生じることである。
これを更に具体的に説明すると、外殻層を形成
する鋳鉄材に対し、その芯材も鋳鉄材で形成する
場合では、その芯材の鋳込温度1300〜1400℃であ
り、この場合外殻層内面の黒鉛化する部分bの肉
厚は3〜7mm程度である。しかし、芯材が鋳鋼材
の場合にあつては、その鋳込温度は1400〜1550℃
と高くなり、その黒鉛化する部分bの肉厚は10〜
20mmにも達し、これに伴い外殻層の有効使用層a
の肉厚はそれだけ薄いものとなるのである。
このように、芯材としてC含有量の低い鋳鋼
材、黒鉛鋳鋼材あるいはアダマイト材のように、
特に強靭でかつ外殻層材よりも融点の高い材料を
用いる複合ロールにあつては、その鋳造時に外殻
層の内面側に不可避に耐摩耗性に劣る黒鉛化した
肉厚部分を生じてその有効使用層が減少し、同時
に又外殻層内面の溶損量も多くなるため、特に外
殻層の厚いロールが得難いという問題点がある。
(課題を解決するための手段)
上記問題点を解決するためになされた本発明の
芯材の強靭な複合ロールの製造方法は、高合金グ
レン材、高合金チルド材、高合金ダクタイル鋳鉄
材等の組織中に高硬度の炭化物を有し1150℃前後
の融点を有する高合金鋳鉄材により外殻層を遠心
力鋳造し、外殻層の凝固後その内面にC含有量が
2.5〜3.7重量%の高級鋳鉄、ダクタイル鋳鉄等の
鋳鉄材からなる中間層材を遠心力鋳造して外殻層
の内面を再溶解して中間層を溶着一体化し、該中
間層の内面に鋳鋼、黒鉛鋳鋼、アダマイト材等の
1300℃以上の融点を有する材料を鋳込んで中間層
の内面に芯材を溶着一体化することを発明の構成
とするものである。
(作用)
外殻層を遠心力鋳造し、該外殻層の凝固後にそ
の内面にC含有量が2.5〜3.7重量%の鋳鉄材から
なる中間層を遠心力鋳造するので、外殻層内面が
中間層材溶湯によつて溶損されにくく、更に外殻
層内面が未凝固時に中間層材溶湯を鋳込む場合に
比べて中間層の鋳造に伴う外殻層内面の溶損をよ
り一層軽減することができる。
前記中間層鋳鉄材のC含有量を2.5〜3.7重量%
に特定したのは、この範囲で外殻層材の融点と同
程度となり、従つて鋳込温度も高くしないで済
み、外殻層内面の溶損防止に資するからである。
すなわち、C2.5%未満では中間層の溶融点が高く
なり、必然的にその鋳込温度も高くなつて、本発
明の技術目的に適合できなくなるためである。一
方、C3.7%を越える場合では、溶融点が低く、そ
の鋳込温度の見地からは好都合であるが、ロール
材料としての見地からは強靭性が不足し、ロール
機能の面からは適合できなくなるからである。な
お、中間層に用いられる材料の他の合金成分につ
いては、その溶融点に対しては左程大きな影響を
与えないが、ロール材としての硬度や強度の観点
から適宜合金成分及びその含有量が調整される。
外殻層内面に中間層を溶着一体化し、その内面
に鋳鋼等の高融点芯材を鋳込むと、芯材は中間層
内面を溶損して中間層の肉厚を減少させるが、外
殻層内面を直接溶損しないため、芯材の鋳込みに
よる外殻層の溶損、黒鉛化を著しく軽減すること
ができる。すなわち、中間層は芯材の鋳込みに際
して、外殻層内面の溶損、黒鉛化に対する緩衝帯
として作用する。
(実施例)
本発明を実施するには、まず遠心力鋳造用金型
に圧延用ロールの使用層としての所要性質を備え
た高合金鋳鉄材を鋳込み、金型内面に外殻層を遠
心力鋳造する。遠心力鋳造法としては、水平型、
傾斜型、堅型のいずれの方式でも適用可能であ
る。
前記外殻層材としては、通常、Cを2.5〜3.7重
量%含有する下記の高合金グレン材、チルド材又
はダクタイル材が使用される。尚、下記の成分の
他に特殊成分としてTi、V、Nb、W等を含むこ
ともあるが、いずれにしてもC含有量は2.5〜3.7
%であり、組織中に高硬度の炭化物を有し、1150
℃前後の溶融点を有するのが通例である。
外殻層組成(重量%、残部実質的にFe)
イ 高合金グレン材
C:2.5〜3.7%、Si:0.5〜1.2%、
Mn:0.4〜1.0%、P:0.15%未満、
S:0.1%未満、Ni:2.0〜5.0%、
Cr:1.0〜2.5%、Mo:0.1〜1.0%
ロ 高合金チルド材
C:2.5〜3.7%、Si:0.1〜0.7%、
Mn:0.1〜0.6%、P:0.5%未満、
S:0.1%未満、Ni:2.0〜5.0%、
Cr:0.5〜1.2%、Mo:0.1〜1.0%
ハ 高合金ダクタイル材
C:3.0〜3.7%、Si:1.0〜2.0%、
Mn:0.2〜1.0%、P:0.1%未満、
S:0.015%未満、Ni:2.0〜5.0%、
Cr:0.3〜1.0%、Mo:0.1〜1.0%
Mg:0.03〜0.08%
次に、外殻層がすべて凝固後、その内面にC含
有量が2.5〜3.7重量%の高級鋳鉄又は低合金ダク
タイル鋳鉄などの鋳鉄材を鋳込み、外殻層の内面
に中間層を遠心力鋳造する。この中間層は、後述
の芯材の鋳込みに際して、芯材溶湯が外殻層内面
に直接接触して、これを溶損、黒鉛化するのを防
止するためのものである。
中間層の鋳込みにより、第3図に示すように、
外殻層(鋳込厚さT1)の内面側の一部(T3)は
再溶解して中間層材溶湯中に溶け込み、新中間層
(厚さT4)を形成する。図中、a1は最終(製品)
外殻層1の厚さ、T2は中間層の鋳込厚さである。
中間層材として高級鋳鉄又はダクタイル鋳鉄を
用いた場合の新中間層の好適な組成例を下記に示
す。
新中間層組成(重量%、残部実質的にFe)
イ 高級鋳鉄
C:2.5〜3.7%、Si:0.8〜1.5%、
Mn:0.4〜1.0%、P:0.3%未満、
S:0.1%未満、Ni:0.2〜3.0%、
Cr:1.0〜1.5%、Mo:0.1〜0.5%
ロ ダクタイル鋳鉄
C:2.5〜3.7%、Si:1.0〜2.0%、
Mn:0.2〜1.0%、P:0.3%未満、
S:0.1%未満、Ni:0.2〜3.0%、
Cr:0.1〜1.5%、Mo:0.1〜0.5%
Mg:0.01〜0.08%
次に、新中間層のすべて又は大部分が凝固した
時点で強靭性に優れる鋳鋼材又は鋳鉄材からなる
芯材を鋳込む。芯材の具体例としては、下記のよ
うに低C含有量の鋳鋼材、黒鉛鋼材又はアダマイ
ト材が用いられる。これらの溶融点は通常1300℃
以上であり、鋳込温度は1400〜1500℃になる。
鋳鉄材C:0.4〜1.1wt%
黒鉛鋼材C:1.0〜2.2wt%
アダマイト材C:1.0〜2.5wt%
芯材の鋳込みにより、第3図に示すように、新
中間層(厚さT4)の内面(厚さT5)は、芯材溶
湯により再溶解されて又は新中間層内面が未凝固
のときはそのまま芯材溶湯に溶け込み、これが凝
固して製品芯材3が形成される。図中、Cは最終
中間層2の厚さである。尚、最終中間層の組成は
新中間層と同様である。
製品芯材の好適な組成例を下記に示す。下記組
成は、芯部における強靭性のみならず、ネツク部
の軸受部に必要とされる耐摩耗性をも具備するも
のである。
芯材組成(重量%、残部実質的にFe)
イ 鋳鋼材
C:0.4〜1.1%、Si:0.1〜1.5%、
Mn:0.1〜1.5%、P:0.05%未満、
S:0.03%未満、Ni:0.01〜1.5%、
Cr:0.01〜1.5%、Mo:0.01〜1.0%
ロ 黒鉛鋼材
C:1.0〜2.2%、Si:1.0〜2.0%、
Mn:0.1〜1.5%、P:0.05%未満、
S:0.03%未満、Ni:0.01〜1.5%、
Cr:0.01〜1.0%、Mo:0.01〜1.0%
ハ アダマイト材
C:1.0〜2.5%、Si:0.1〜1.5%、
Mn:0.1〜1.5%、P:0.05%未満、
S:0.03%未満、Ni:0.01〜1.5%、
Cr:0.3〜2.0%、Mo:0.01〜1.0%
以上のようにして、第1図に示すように、外殻
層1、(最終)中間層2および(製品)芯材3の
三層が溶着一体化された複合ロールが製造され
る。
ここで、上記三層構造を有する複合ロールの外
殻層及び中間層の鋳込厚さについて述べる。外殻
層の鋳込厚さについては、もとより目的とするロ
ールの片肉使用厚さによつて決定される。すなわ
ち、胴表面の加工代、中間層として鋳込まれた溶
湯による内面の溶損代及び片肉使用厚さに必要な
若干の余裕を考慮して決定される。
一方、中間層の鋳込厚さを桁定するに当つて
は、ロール製品においてはその胴径とネツク径と
の差に限界があり、従つてこの点から中間層の鋳
込厚さはロール形状から上限があること、また一
方では中間層溶湯の鋳込量が少な過ぎると、取鍋
中での溶湯の温度低下が著しく、作業に支障を来
たす問題があるためその鋳込厚さの下限にも実質
的に限度があることに留意しなければならない。
またその鋳込厚さは、外殻層の形成材料並びに芯
材との組合せ条件により、上記実質的な制限範囲
内で適宜に選択すればよいが、中間層を介在せし
める目的が高温の芯材溶湯鋳込みによる外殻層へ
の不都合な熱影響の減少にあるため、余り薄いも
のでは要をなさない。
このような諸条件について総合的に勘案する
と、普通の形状寸法を有するロールについては、
中間層の鋳込厚さはT2=15〜80mm程度が適当で
ある。この場合、中間層材の鋳込重量は、200Kg
〜2Ton程度で足り、芯材を直接鋳込む場合(中
型乃至大型ロールでは10〜15Ton程度に達する。)
に比較してその熱容量が遥かに少なく、更には中
間層の鋳込みにより外殻層の内面一部が再溶解し
ても、鋳込まれた中間層自体が急激に温度低下す
るため、外殻層の内面側以外の大部分の肉厚には
大きな熱影響をこうむらない。またこのさいの外
殻層内面側での溶損代をT3=3〜15mm程度とす
ると、外殻層との溶着によつて新しく形成される
新中間層の厚さはT4=18〜95mmとなり、更には
芯材鋳込みによる溶損代をT5=15〜40mm程度に
見積ると、その鋳放製品における最終的な中間層
厚さはC=3〜55mm程度となる。
次に本発明の具体実施例を下記に掲げる。
実施例 1
胴部寸法600φ×2057の複合ロールを、外殻
層、中間層及び芯材について各々下記の鋳込成
分、鋳込条件で製造した。中間層溶湯は外殻層が
凝固完了直後に鋳込んだ(以下の実施例において
同じ)。
(Industrial Application Field) The present invention relates to a method for manufacturing a composite roll having a strong core material. (Prior art) In rolling rolls, the surface of the roll body that comes into contact with the rolled material is generally coated with wear-resistant, crack-resistant,
Surface roughness resistance is required, while the core is required to have the toughness to withstand rolling loads, so the outer shell layer of the body is made of high-alloy grain material, high-alloy chilled material, high-alloy ductile cast iron material, etc. It is made of a high-alloy cast iron material with high hardness carbide inside, while the core and neck part are usually made of a composite material made of a strong material such as low-alloy high-grade cast iron or ductile cast iron in consideration of economic efficiency. rolls are being used. However, with recent changes in rolling conditions, there is a tendency to increase the rolling reduction ratio and to roll low-temperature materials, and for this reason, the core material that forms the body core and neck portion needs to be stronger. However, in the case of work rolls for hot stripping, it is necessary to increase the rigidity of the core material to reduce deformation of the roll, so the core material has an elastic modulus. It is desired to use a material with a large value. In order to meet these demands, the applicant has proposed a composite roll in which the core material is made of stronger cast steel, graphite cast steel, or adamite (see Utility Model Application Nos. 170075 to 170077). (Problem to be Solved by the Invention) However, when forming the core material from such a strong material, while the outer shell layer is formed from a cast iron material with a relatively low melting point, The melting point of the core material is higher than that of the outer shell layer material, and therefore it is necessary to raise the casting temperature, which causes the following problems in manufacturing. In other words, when casting this type of composite roll, after casting the outer shell layer according to the normal centrifugal casting method, when the molten core material is cast to be welded and integrated with the outer shell layer, the melting of the outer shell layer material Since the temperature of the core material molten metal is considerably high compared to the temperature, not only the amount of erosion on the inner surface of the outer shell layer increases, but also the thickness (a + b)
The problem is that a considerably thick portion b on the inner surface side of the outer shell layer 1 is reheated by the high-temperature core material 3, and a portion is formed in which the carbides in the outer shell layer cast iron structure become graphitized. To explain this more specifically, when the core material is also made of cast iron material for the cast iron material that forms the outer shell layer, the casting temperature of the core material is 1300 to 1400°C; The thickness of the graphitized portion b on the inner surface of the layer is approximately 3 to 7 mm. However, when the core material is cast steel, the casting temperature is 1400 to 1550℃.
The thickness of the graphitized part b is 10~
It reaches 20mm, and as a result, the effective use layer a of the outer shell layer
The wall thickness becomes that much thinner. In this way, as a core material, cast steel materials with low C content, graphite cast steel materials, or adamite materials,
Particularly in the case of composite rolls that use a material that is tough and has a higher melting point than the outer shell material, a thick graphitized part with poor wear resistance inevitably occurs on the inner surface of the outer shell layer during casting. There is a problem in that it is difficult to obtain a roll with a particularly thick outer shell layer because the effective usable layer decreases and at the same time, the amount of erosion on the inner surface of the outer shell layer increases. (Means for Solving the Problems) The method for manufacturing a composite roll with a strong core material according to the present invention, which has been made in order to solve the above-mentioned problems, includes high-alloy grain material, high-alloy chilled material, high-alloy ductile cast iron material, etc. The outer shell layer is centrifugally cast using a high-alloy cast iron material that has highly hard carbides in its structure and has a melting point of around 1150℃, and after the outer shell layer solidifies, the C content is added to its inner surface.
An intermediate layer material made of cast iron such as high-grade cast iron or ductile cast iron containing 2.5 to 3.7% by weight is centrifugally cast, the inner surface of the outer shell layer is remelted, the intermediate layer is welded and integrated, and cast steel is applied to the inner surface of the intermediate layer. , graphite cast steel, adamite materials, etc.
The structure of the invention is to weld and integrate the core material onto the inner surface of the intermediate layer by casting a material having a melting point of 1300° C. or higher. (Function) The outer shell layer is centrifugally cast, and after solidification of the outer shell layer, an intermediate layer made of cast iron with a C content of 2.5 to 3.7% by weight is centrifugally cast on the inner surface. It is less likely to be eroded by the molten metal of the intermediate layer material, and further reduces the eroding damage of the inner surface of the outer shell layer due to casting of the intermediate layer, compared to when the molten metal of the intermediate layer material is cast when the inner surface of the outer shell layer is not yet solidified. be able to. The C content of the intermediate layer cast iron material is 2.5 to 3.7% by weight.
The reason for specifying this is that within this range, the melting point is comparable to that of the outer shell layer material, and therefore the casting temperature does not need to be raised, which contributes to preventing melting damage on the inner surface of the outer shell layer.
That is, if C is less than 2.5%, the melting point of the intermediate layer will be high, and the casting temperature will inevitably also be high, making it impossible to meet the technical purpose of the present invention. On the other hand, if the C content exceeds 3.7%, the melting point is low, which is advantageous from the viewpoint of casting temperature, but it lacks toughness from the viewpoint of a roll material and is not suitable from the viewpoint of roll function. Because it will disappear. The other alloy components of the material used for the intermediate layer do not have as great an effect on the melting point, but the alloy components and their content may be adjusted as appropriate from the viewpoint of hardness and strength as a roll material. be adjusted. When the intermediate layer is welded and integrated with the inner surface of the outer shell layer and a high melting point core material such as cast steel is cast into the inner surface, the core material melts the inner surface of the intermediate layer and reduces the thickness of the intermediate layer, but the outer shell layer Since the inner surface is not directly damaged by melting, it is possible to significantly reduce melting damage and graphitization of the outer shell layer due to casting of the core material. That is, the intermediate layer acts as a buffer zone against erosion and graphitization of the inner surface of the outer shell layer during casting of the core material. (Example) To carry out the present invention, first, a high-alloy cast iron material having the required properties as a layer used in a rolling roll is cast into a centrifugal casting mold, and an outer shell layer is placed on the inner surface of the mold using centrifugal force. to cast. Centrifugal force casting methods include horizontal type,
It is applicable to both inclined type and rigid type. As the outer shell layer material, the following high-alloy grain material, chilled material, or ductile material containing 2.5 to 3.7% by weight of C is usually used. In addition to the components listed below, special components such as Ti, V, Nb, and W may also be included, but in any case, the C content is 2.5 to 3.7.
%, has high hardness carbide in the structure, 1150
It typically has a melting point around ℃. Outer shell layer composition (wt%, remainder substantially Fe) High alloy grain material C: 2.5 to 3.7%, Si: 0.5 to 1.2%, Mn: 0.4 to 1.0%, P: less than 0.15%, S: 0.1% Ni: 2.0 to 5.0%, Cr: 1.0 to 2.5%, Mo: 0.1 to 1.0% B High alloy chilled material C: 2.5 to 3.7%, Si: 0.1 to 0.7%, Mn: 0.1 to 0.6%, P: Less than 0.5%, S: less than 0.1%, Ni: 2.0 to 5.0%, Cr: 0.5 to 1.2%, Mo: 0.1 to 1.0% C High alloy ductile material C: 3.0 to 3.7%, Si: 1.0 to 2.0%, Mn : 0.2 to 1.0%, P: less than 0.1%, S: less than 0.015%, Ni: 2.0 to 5.0%, Cr: 0.3 to 1.0%, Mo: 0.1 to 1.0% Mg: 0.03 to 0.08% Next, the outer shell layer After solidifying, a cast iron material such as high-grade cast iron or low-alloy ductile cast iron with a C content of 2.5 to 3.7% by weight is cast on the inner surface, and an intermediate layer is centrifugally cast on the inner surface of the outer shell layer. This intermediate layer is for preventing the core material molten metal from coming into direct contact with the inner surface of the outer shell layer and causing melt damage and graphitization during casting of the core material, which will be described later. By casting the intermediate layer, as shown in Figure 3,
A portion (T 3 ) of the inner surface of the outer shell layer (casting thickness T 1 ) is remelted and melted into the molten intermediate layer material to form a new intermediate layer (thickness T 4 ). In the diagram, a 1 is the final (product)
The thickness of the outer shell layer 1, T 2 is the casting thickness of the intermediate layer. A preferred composition example of the new intermediate layer when high-grade cast iron or ductile cast iron is used as the intermediate layer material is shown below. New intermediate layer composition (wt%, remainder substantially Fe) High-grade cast iron C: 2.5-3.7%, Si: 0.8-1.5%, Mn: 0.4-1.0%, P: less than 0.3%, S: less than 0.1%, Ni: 0.2-3.0%, Cr: 1.0-1.5%, Mo: 0.1-0.5% Ductile cast iron C: 2.5-3.7%, Si: 1.0-2.0%, Mn: 0.2-1.0%, P: less than 0.3%, S: less than 0.1%, Ni: 0.2-3.0%, Cr: 0.1-1.5%, Mo: 0.1-0.5% Mg: 0.01-0.08% Next, toughness is determined when all or most of the new intermediate layer has solidified. A core material made of cast steel or cast iron with excellent properties is cast. Specific examples of the core material include cast steel, graphite steel, or adamite material with a low C content, as described below. Their melting point is usually 1300℃
The casting temperature is 1400 to 1500°C. Cast iron material C: 0.4-1.1wt% Graphite steel material C: 1.0-2.2wt% Adamite material C: 1.0-2.5wt% By casting the core material, a new intermediate layer (thickness T 4 ) is created as shown in Figure 3. The inner surface (thickness T 5 ) is remelted by the molten core material, or when the inner surface of the new intermediate layer is unsolidified, it directly melts into the molten core material, and this is solidified to form the product core material 3. In the figure, C is the thickness of the final intermediate layer 2. Note that the composition of the final intermediate layer is the same as that of the new intermediate layer. Examples of suitable compositions for the product core material are shown below. The composition below provides not only the toughness in the core but also the wear resistance required for the bearing part of the neck part. Core material composition (weight%, remainder substantially Fe) A Cast steel material C: 0.4 to 1.1%, Si: 0.1 to 1.5%, Mn: 0.1 to 1.5%, P: less than 0.05%, S: less than 0.03%, Ni : 0.01~1.5%, Cr: 0.01~1.5%, Mo: 0.01~1.0% B Graphite steel C: 1.0~2.2%, Si: 1.0~2.0%, Mn: 0.1~1.5%, P: less than 0.05%, S : Less than 0.03%, Ni: 0.01-1.5%, Cr: 0.01-1.0%, Mo: 0.01-1.0% C Adamite material C: 1.0-2.5%, Si: 0.1-1.5%, Mn: 0.1-1.5%, P : less than 0.05%, S: less than 0.03%, Ni: 0.01 to 1.5%, Cr: 0.3 to 2.0%, Mo: 0.01 to 1.0% In the above manner, as shown in FIG. A composite roll is manufactured in which three layers, the (final) intermediate layer 2 and the (product) core material 3, are welded and integrated. Here, the casting thicknesses of the outer shell layer and the intermediate layer of the composite roll having the above three-layer structure will be described. The casting thickness of the outer shell layer is determined, of course, by the intended thickness of one side of the roll. That is, it is determined by taking into consideration the machining allowance for the shell surface, the erosion loss allowance for the inner surface due to the molten metal cast as the intermediate layer, and a slight margin necessary for the thickness of one wall. On the other hand, when determining the casting thickness of the intermediate layer, there is a limit to the difference between the body diameter and the neck diameter for roll products, so from this point of view, the casting thickness of the intermediate layer can be determined by rolling. There is an upper limit due to the shape, and on the other hand, if the amount of the middle layer molten metal is too small, the temperature of the molten metal in the ladle will drop significantly, which will hinder work, so there is a lower limit to the casting thickness. It must be kept in mind that there are practical limits to this.
In addition, the casting thickness may be appropriately selected within the above-mentioned practical limits depending on the material forming the outer shell layer and the combination conditions with the core material. Since the purpose is to reduce the unfavorable thermal influence on the outer shell layer due to molten metal casting, it is not necessary to make it too thin. Considering these conditions comprehensively, for rolls with normal shapes and dimensions,
The appropriate casting thickness of the intermediate layer is T 2 =15 to 80 mm. In this case, the casting weight of the intermediate layer material is 200Kg.
Approximately 2 tons is sufficient, and when the core material is directly cast (for medium to large rolls, the amount reaches approximately 10 to 15 tons).
Its heat capacity is much smaller than that of the outer shell layer, and even if part of the inner surface of the outer shell layer is remelted by casting the middle layer, the temperature of the cast middle layer itself will drop rapidly. The majority of the wall thickness other than the inner surface side is not significantly affected by heat. Also, if the erosion loss on the inner surface of the outer shell layer is approximately T 3 = 3 to 15 mm, the thickness of the new intermediate layer newly formed by welding with the outer shell layer is T 4 = 18 to 15 mm. If the thickness is 95 mm, and if the corrosion loss due to core casting is estimated to be T 5 =15 to 40 mm, the final intermediate layer thickness in the as-cast product will be C = 3 to 55 mm. Next, specific examples of the present invention are listed below. Example 1 A composite roll having a body size of 600φ×2057 mm was manufactured using the following casting components and casting conditions for the outer shell layer, intermediate layer, and core material. The middle layer molten metal was cast immediately after the outer shell layer had solidified (the same applies to the following examples).
【表】【table】
【表】
この複合ロールにおいては、外殻層の内面10mm
が中間層溶湯に再溶解されて中間層溶湯と混合
し、下記成分の厚さ40mmの新しい中間層が形成さ
れた。[Table] In this composite roll, the inner surface of the outer shell layer is 10mm
was remelted into the molten intermediate layer and mixed with the molten intermediate layer to form a new 40 mm thick intermediate layer with the following components:
【表】
この新中間層は芯材の鋳込により、内面で15〜
20mm溶損されて、鋳放製品での最終的な中間層厚
さは20〜25mmであつた。そして、外殻層内面の黒
鉛化された部分の肉厚は4〜5mmで、有効使用層
の厚い外殻層を有する複合ロールが得られた。
実施例 2
実施例1と同じ寸法の複合ロールを下記の鋳込
成分、鋳込条件で製造した。[Front] This new intermediate layer is made of core material that has a thickness of 15 to 15 mm on the inner surface.
With 20 mm melted away, the final intermediate layer thickness in the as-cast product was 20-25 mm. The thickness of the graphitized portion on the inner surface of the outer shell layer was 4 to 5 mm, and a composite roll having a thick outer shell layer as an effective usable layer was obtained. Example 2 A composite roll having the same dimensions as Example 1 was manufactured using the following casting components and casting conditions.
【表】【table】
【表】
この複合ロールにおいては、外殻層の内面約13
mmが中間層溶湯に再溶解されて中間層溶湯と混合
し、下記成分の厚さ43mmの新しい中間層が形成さ
れた。[Table] In this composite roll, the inner surface of the outer shell layer is approximately 13
mm was remelted into the intermediate layer molten metal and mixed with the intermediate layer molten metal to form a new intermediate layer with a thickness of 43 mm with the following components:
【表】
この新中間層は芯材の鋳込により、内面で19〜
25mm溶損されて、鋳放製品での最終的な中間層厚
さは18〜24mmであつた。そして、外殻層内面の黒
鉛化された部分の肉厚は5〜6mmで、有効使用層
の厚い外殻層を有する複合ロールが得られた。
実施例 3
実施例1と同じ寸法の複合ロールを下記の鋳込
成分、鋳込条件で製造した。[Front] This new intermediate layer has an inner surface of 19~19 mm due to core material casting.
With 25 mm melted away, the final intermediate layer thickness in the as-cast product was 18-24 mm. The thickness of the graphitized portion on the inner surface of the outer shell layer was 5 to 6 mm, and a composite roll having a thick outer shell layer as an effective usable layer was obtained. Example 3 A composite roll having the same dimensions as in Example 1 was manufactured using the following casting components and casting conditions.
【表】【table】
【表】
この複合ロールにおいては、外殻層の内面10mm
が中間層溶湯に再溶解されて中間層溶湯と混合
し、下記成分の厚さ40mmの新しい中間層が形成さ
れた。[Table] In this composite roll, the inner surface of the outer shell layer is 10mm
was remelted into the molten intermediate layer and mixed with the molten intermediate layer to form a new 40 mm thick intermediate layer with the following components:
【表】
この新中間層は芯材の鋳込により、内面で25〜
30mm溶損されて、鋳放製品での最終的な中間層厚
さは10〜15mmであつた。この場合、芯材が鋳鋼で
あるため、鋳込温度が高く、中間層の溶損量は多
くなつた。そして、外殻層内面の黒鉛化された部
分の肉厚も6〜10mmとやや多くなつたが、中間層
を設けない場合より遥かに少なく、有効使用層の
十分厚い外殻層を有する複合ロールが得られた。
実施例 4
実施例1と同じ寸法の複合ロールを下記の鋳込
成分、鋳込条件で製造した。[Front] This new intermediate layer is made of core material that has been cast into an inner surface of 25~25mm
With 30 mm melted away, the final intermediate layer thickness in the as-cast product was 10-15 mm. In this case, since the core material was cast steel, the casting temperature was high and the amount of erosion in the intermediate layer was large. The thickness of the graphitized part on the inner surface of the outer shell layer was also slightly larger at 6 to 10 mm, but it was much less than when no intermediate layer was provided, and the composite roll has a sufficiently thick outer shell layer for effective use. was gotten. Example 4 A composite roll having the same dimensions as Example 1 was manufactured using the following casting components and casting conditions.
【表】【table】
【表】
この複合ロールにおいては、外殻層の内面15mm
が中間層溶湯に再溶解されて中間層溶湯と混合
し、下記成分の厚さ45mmの新しい中間層が形成さ
れた。[Table] In this composite roll, the inner surface of the outer shell layer is 15mm
was remelted into the molten intermediate layer and mixed with the molten intermediate layer to form a new 45 mm thick intermediate layer with the following components:
【表】
この新中間層は芯材の鋳込により、内面で10〜
15mm溶損されて、鋳放製品での最終的な中間層厚
さは30〜35mmであつた。この場合、芯材がアダマ
イト材でその鋳込温度も他の例より低いので熱影
響が少なく、外殻層内面の黒鉛化される部分の肉
厚も5mm程度で、有効使用層の厚い外殻層を有す
る複合ロールが得られた。
以上の実施例では、主として鋳造条件と化学成
分について述べたが、製造された複合ロールは製
品化するに当り、粗加工後、歪取熱処理又は芯材
の強靭性向上のため900〜1000℃の高温熱処理に
供される。この場合、外殻層の耐摩耗性維持のた
め、焼準や恒温変態熱処理を行ない、基地組織を
ベーナイトやマルテンサイト組織にする工程を含
めることもできる。
なお、本発明に係る複合ロールの好ましい外殻
層、中間層及び芯材の各材料は、上記実施例の場
合以外にも、その目的に応じて、下記の各具体例
のものを任意に組合せることができる。
外殻層:高合金グレン材、高合金チルド材、高合
金ダクタイル鋳鉄材
中間層:高級鋳鉄材、ダクタイル鋳鉄材
芯材:鋳鉄材、黒鉛鋼材、アダマイト材
(発明の効果)
以上説明した通り、本発明の複合ロールの製造
方法によれば、高合金グレン材等の高合金鋳鉄材
により外殻層を遠心力鋳造し、外殻層の凝固後そ
の内面にC含有量2.5〜3.7%の鋳鉄材からなる中
間層材を遠心力鋳造して外殻層内面を再溶解して
中間層を溶着一体化するので、外殻層内面が溶損
や黒鉛化されにくく、更に外殻層内面が未凝固時
に中間層材を鋳込む場合に比べて、中間層材の鋳
込みによる外殻層内面の溶損をより一層軽減する
ことができる。更に、中間層の形成後、その内面
に鋳鋼等の高融点芯材を鋳込むので、外殻層内面
に芯材溶湯を直接鋳込む場合に比べて、中間層が
緩衝帯として作用し外殻層内面の芯材による溶損
および黒鉛化を著しく軽減することができ、外殻
層に高硬度の炭化物が存在する有効使用層の厚い
ものが容易に得られる。[Front] This new intermediate layer is made of core material that has a thickness of 10 to 10 mm on the inner surface.
After 15 mm was melted away, the final intermediate layer thickness in the as-cast product was 30-35 mm. In this case, the core material is adamite material and the casting temperature is lower than in other examples, so there is less heat influence, and the thickness of the graphitized part on the inner surface of the outer shell layer is about 5 mm, so the thick outer shell has an effective usable layer. A composite roll with layers was obtained. In the above examples, we mainly talked about the casting conditions and chemical composition, but when the manufactured composite roll is commercialized, after rough processing, it is subjected to strain relief heat treatment or heat treatment at 900 to 1000℃ to improve the toughness of the core material. Subjected to high temperature heat treatment. In this case, in order to maintain the wear resistance of the outer shell layer, a step of normalizing or isothermal transformation heat treatment to transform the base structure into a bainite or martensitic structure may be included. In addition to the above-mentioned examples, preferable materials for the outer shell layer, intermediate layer, and core material of the composite roll according to the present invention may be any combination of the following specific examples depending on the purpose. can be done. Outer shell layer: High alloy grain material, high alloy chilled material, high alloy ductile cast iron material Middle layer: High grade cast iron material, ductile cast iron material Core material: Cast iron material, graphite steel material, Adamite material (effects of the invention) As explained above, According to the method for manufacturing a composite roll of the present invention, the outer shell layer is centrifugally cast using a high alloy cast iron material such as a high alloy grain material, and after solidification of the outer shell layer, the inner surface of the cast iron is coated with a C content of 2.5 to 3.7%. The intermediate layer material made of wood is centrifugally cast, the inner surface of the outer shell layer is remelted, and the intermediate layer is welded and integrated, so the inner surface of the outer shell layer is less likely to melt or become graphitized, and furthermore, the inner surface of the outer shell layer is not left unfinished. Compared to the case where the intermediate layer material is cast during solidification, melting damage on the inner surface of the outer shell layer due to the casting of the intermediate layer material can be further reduced. Furthermore, since a high melting point core material such as cast steel is cast into the inner surface of the intermediate layer after forming the intermediate layer, the intermediate layer acts as a buffer zone and the outer shell Erosion damage and graphitization due to the core material on the inner surface of the layer can be significantly reduced, and a thick effective layer in which highly hard carbide is present in the outer shell layer can be easily obtained.
第1図は本発明に係る複合ロールの構造一例を
示す断面図である。第2図は比較のため外殻層内
面に直接高温芯材溶湯を鋳込んだ場合の問題点を
現わすための断面説明図である。第3図は本発明
に係る複合ロール外殻層及び中間層の肉厚変動を
現わすための断面説明図である。
1……外殻層、2……中間層、3……芯材。
FIG. 1 is a sectional view showing an example of the structure of a composite roll according to the present invention. FIG. 2 is a cross-sectional explanatory diagram for comparison, showing the problems when high-temperature core molten metal is directly cast into the inner surface of the outer shell layer. FIG. 3 is an explanatory cross-sectional view showing variations in thickness of the composite roll outer shell layer and intermediate layer according to the present invention. 1... Outer shell layer, 2... Middle layer, 3... Core material.
Claims (1)
クタイル鋳鉄材等の組織中に高硬度の炭化物を有
し1150℃前後の融点を有する高合金鋳鉄材により
外殻層を遠心力鋳造し、外殻層の凝固後その内面
にC含有量が2.5〜3.7重量%の高級鋳鉄、ダクタ
イル鋳鉄等の鋳鉄材からなる中間層材を遠心力鋳
造して外殻層の内面を再溶解して中間層を溶着一
体化し、該中間層の内面に鋳鋼、黒鉛鋳鋼、アダ
マイト材等の1300℃以上の融点を有する材料を鋳
込んで中間層の内面に芯材を溶着一体化すること
を特徴とする芯材の強靭な複合ロールの製造方
法。1 The outer shell layer is centrifugally cast using high-alloy cast iron materials such as high-alloy grain materials, high-alloy chilled materials, and high-alloy ductile cast iron materials that have high hardness carbides in their structures and have a melting point of around 1150℃. After solidifying the shell layer, an intermediate layer material made of cast iron material such as high-grade cast iron or ductile cast iron with a C content of 2.5 to 3.7% by weight is centrifugally cast on the inner surface of the shell layer, and the inner surface of the outer shell layer is remelted to form the intermediate layer. A core characterized in that a material having a melting point of 1300°C or higher, such as cast steel, graphite cast steel, or adamite material, is cast onto the inner surface of the intermediate layer, and a core material is integrally welded onto the inner surface of the intermediate layer. A method of manufacturing a composite roll made of strong materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10380181A JPH0229428B2 (en) | 1981-07-01 | 1981-07-01 | SHINZAINOKYOJINNAFUKUGOROORUNOSEIZOHOHO |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10380181A JPH0229428B2 (en) | 1981-07-01 | 1981-07-01 | SHINZAINOKYOJINNAFUKUGOROORUNOSEIZOHOHO |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS586770A JPS586770A (en) | 1983-01-14 |
| JPH0229428B2 true JPH0229428B2 (en) | 1990-06-29 |
Family
ID=14363494
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10380181A Expired - Lifetime JPH0229428B2 (en) | 1981-07-01 | 1981-07-01 | SHINZAINOKYOJINNAFUKUGOROORUNOSEIZOHOHO |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0229428B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS62176657A (en) * | 1986-01-28 | 1987-08-03 | Nippon Steel Corp | Production of centrifugal casting complex roll |
-
1981
- 1981-07-01 JP JP10380181A patent/JPH0229428B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS586770A (en) | 1983-01-14 |
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