JPS62207534A - Mold for continuous casting - Google Patents

Mold for continuous casting

Info

Publication number
JPS62207534A
JPS62207534A JP4931686A JP4931686A JPS62207534A JP S62207534 A JPS62207534 A JP S62207534A JP 4931686 A JP4931686 A JP 4931686A JP 4931686 A JP4931686 A JP 4931686A JP S62207534 A JPS62207534 A JP S62207534A
Authority
JP
Japan
Prior art keywords
layer
mold
weight
thickness
alloy
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.)
Pending
Application number
JP4931686A
Other languages
Japanese (ja)
Inventor
Kazuhisa Mitani
和久 三谷
Masato Takada
正人 高田
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.)
Mishima Kosan Co Ltd
Original Assignee
Mishima Kosan Co Ltd
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 Mishima Kosan Co Ltd filed Critical Mishima Kosan Co Ltd
Priority to JP4931686A priority Critical patent/JPS62207534A/en
Publication of JPS62207534A publication Critical patent/JPS62207534A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/04Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
    • B22D11/059Mould materials or platings

Abstract

PURPOSE:To lengthen service life of a mold and to improve the casting billet quality by forming the first layer composing Ni on the inner wall face of the Cu-made mold body and the second layer having the specified thickness, composing cermet thermal spraying layer with the specified composition on the lower half part of the first layer. CONSTITUTION:The first layer 2 composing of Ni or Ni-Fe alloy, in which Fe content is about 2-7wt%, is formed on the inner wall face of the mold body 1, composing Cu or Cu alloy. Then, the thickness of the first layer 2 is desirable to be thicker toward lower part. Next, the cermet thermal spraying layer, which contains 20-50wt% metallic binder, composing about 15-26wt% Cr, about 5-13wt% A$;, about 0.5-2wt% Y and the balance Ni or Co, is formed at the second layer 3 having 0.05-0.5mm thickness on the lower half part of the first layer 2. In this way, the mold for the continuous casting having about two times of service life of the conventional mold is obtd.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明の連続鋳造用鋳型、更に詳しくは鋳型本体の長手
方向の下半部に於ける耐摩耗性は増強せしめ、その寿命
延長と得られる鋳辺の品質向上とを図った連続鋳造用鋳
型に関するものである。
[Detailed Description of the Invention] <Industrial Application Field> The continuous casting mold of the present invention, more specifically, the wear resistance of the lower half in the longitudinal direction of the mold body is enhanced, and its life can be extended. This invention relates to a continuous casting mold that improves the quality of the cast side.

〈従来の技術及びその問題点〉 連続鋳造用鋳型としては、抜熱性の点から熱伝導性が良
好な銅若しくはその合金を本体とし、その内壁面を摩耗
から防止する為に、内壁面に各種の耐摩耗性を有する表
面層を形成した形態が一般的である。
<Prior art and its problems> Continuous casting molds have a main body made of copper or its alloy, which has good thermal conductivity from the viewpoint of heat removal, and various types of coatings are applied to the inner wall surface to prevent the inner wall surface from abrasion. Generally, a surface layer with wear resistance of 100% is formed.

ここで表面層として用いる耐摩耗性材料としてはNiや
Ni−Cr等の金属メッキ層や、Ni−Cr系自溶性合
金溶射層がある。しかし金属メッキ層は硬度が不足した
り、又はその組成によっては必要な厚さまで健全な状態
でメッキを施す事が出来ないという問題があり、一方向
溶性合金溶射層は耐摩耗性は十分ではあるが溶射後の溶
体化処理で約1000℃下に熱処理をしなければならず
、この熱処理による歪が大で鋳型寸法にくるいが生じた
り、又この様な高温熱処理に耐え得る組成の銅合金を本
体としなければならない等の問題がある。
Examples of wear-resistant materials used as the surface layer include metal plating layers such as Ni and Ni-Cr, and spray-sprayed Ni-Cr self-fluxing alloys. However, metal plating layers lack hardness or, depending on their composition, cannot be plated to the required thickness in a healthy state, and unidirectionally soluble alloy sprayed layers have sufficient wear resistance. However, in the solution treatment after thermal spraying, it must be heat-treated to a temperature of approximately 1000°C, and the distortion caused by this heat treatment is large, causing distortion in the mold dimensions, and copper alloys whose composition can withstand such high-temperature heat treatment. There are problems such as having to use the main body as the main body.

近年連続鋳造用鋳型の内壁面に、サーメットやセラミッ
ク製被覆層を施すという技術が提案されている。例えば
特開昭56−80356号公報や特開昭55−1513
64:11号公報に示されている技術がそれである。
In recent years, a technique has been proposed in which a cermet or ceramic coating layer is applied to the inner wall surface of a continuous casting mold. For example, JP-A-56-80356 and JP-A-55-1513.
This is the technique disclosed in Publication No. 64:11.

しかるにこの2つの公報で示される技術で用いられるサ
ーメットは、バインダー金属としてNi、 C。
However, the cermets used in the techniques disclosed in these two publications contain Ni and C as binder metals.

あるいはCrを用い、それと混練するセラミックとして
は何でもよい様になっているが、本発明者等の実験によ
れば、サーメットの組成によってはその密着力に大きな
差が生じ上記2つの公報に示されている組成のサーメッ
トでは密着力が不足し短い間に剥離を生じる事が判明し
た。又他の例として特開昭60−221151号公報で
示される技術があるが、これはセラミックあるいはサー
メツト層を施す前の下地処理として金属層を2段に施し
密着性の向上を図ると共に、セラミックやサーメットの
溶射時の粒子飛行速度を400m/秒以上に規制したも
のであるが、飛行速度が大であればより望ましいのは当
然としても、用いられているセラEツクやサーメットで
はやはりその密着性が不足するという問題がある。又特
開昭56−86655号公報や特開昭56−86656
号公報では、金属中間層の上面に特定の耐火物層を施し
た例が示されているが、これらは用いる耐火物層にバイ
ンダ一層を含まない為に、該耐火物層が脆弱であり、か
つその密着性も十分ではないという問題がある。
Alternatively, Cr can be used and any ceramic can be used to mix it with it, but according to the experiments of the present inventors, there is a large difference in the adhesion strength depending on the composition of the cermet, which is shown in the above two publications. It was found that cermets with a composition of Another example is a technique disclosed in Japanese Patent Application Laid-Open No. 60-221151, in which a metal layer is applied in two stages as a base treatment before applying a ceramic or cermet layer to improve adhesion. The particle flight speed during thermal spraying of ceramics and cermets is regulated to 400 m/s or more, but although it is natural that higher flight speeds are more desirable, the adhesion of the ceramics and cermets used is still limited. There is a problem of lack of sexuality. Also, JP-A-56-86655 and JP-A-56-86656
In the publication, an example is shown in which a specific refractory layer is applied on the upper surface of a metal intermediate layer, but since the refractory layer used in these does not include a binder layer, the refractory layer is fragile. Moreover, there is a problem that the adhesion is not sufficient.

〈問題点を解決する為の手段〉 本発明では上記諸問題を解決する為に、耐摩耗性表面層
として用いるサーメットの組成をより厳密に検討し、か
つ該サーメツト層を施す部所についても限定を加え、剥
離し難いサーメツト層を有する連続鋳造用鋳型を提供せ
んとするものであり、その要旨は銅若しくは銅合金製鋳
型本体の内壁面の少なくとも下半部に、ニッケル若しく
はニッケル−鉄合金メッキ層より成る第1層を形成し、
該第1層の表面で鋳型本体の下半部に相当する部所に、
炭化クロム若しくは炭化チタンに対しN1−Cr−Aj
−Y若しくはCo−Cr−人1−Y合金をバインダー金
属として全体の20〜50重量%含有せしめたサーメッ
ト溶射層より成る第2層を、その厚さが005〜05m
mとなるべく形成せしめたことを特徴とする連続鋳造用
鋳型である。
<Means for Solving the Problems> In order to solve the above-mentioned problems, the present invention more strictly examines the composition of the cermet used as the wear-resistant surface layer, and also limits the locations where the cermet layer is applied. In addition, the purpose is to provide a continuous casting mold having a cermet layer that is difficult to peel off, and the gist thereof is to provide nickel or nickel-iron alloy plating on at least the lower half of the inner wall surface of the copper or copper alloy mold body. forming a first layer of layers;
On the surface of the first layer, in a portion corresponding to the lower half of the mold body,
N1-Cr-Aj for chromium carbide or titanium carbide
A second layer consisting of a cermet sprayed layer containing 20 to 50% by weight of Y or Co-Cr-Y alloy as a binder metal is coated with a thickness of 005 to 05 m.
This is a continuous casting mold characterized in that it is formed as much as possible.

上記した第1層としてニッケル−鉄合金メッキを用いる
場合には、鉄の含有量は2〜7重量%が最適である。即
ちニッケルに鉄を含有せしめるのはその硬さ2強度を増
す為であるが、その効果は2重量%未満ではあまり期待
出来ず、逆に7重量%を越えると脆くなってクラックが
生じ易くなるからである。又第2層のサーメツト層のバ
インダーとして用いる合金は、C「15〜26重量%、
A15〜13重量%、Yo、5〜2重量%と残部がNi
若しくはC。
When using nickel-iron alloy plating as the first layer, the optimum iron content is 2 to 7% by weight. In other words, the purpose of adding iron to nickel is to increase its hardness and strength, but this effect cannot be expected if it is less than 2% by weight, and on the other hand, if it exceeds 7% by weight, it becomes brittle and prone to cracking. It is from. The alloy used as a binder for the second cermet layer contains C "15 to 26% by weight,
A15-13% by weight, Yo, 5-2% by weight and the balance Ni
Or C.

なる組成のものを用いる。そしてこの金属バインダーは
後に詳しく示す実験結果から判る如く、第2層の密着性
維持の為には20重量%以上は必要であるが50重量%
を越えると第2層自体の耐摩耗性が低下するので20〜
50重量%とする。
Use one with the following composition. As shown in the experimental results shown in detail later, this metal binder is required to be at least 20% by weight in order to maintain the adhesion of the second layer, but 50% by weight is required.
If it exceeds 20 to 20, the abrasion resistance of the second layer itself will decrease.
50% by weight.

本発明の連続鋳造用鋳型は第1図に示す様に鋳型本体(
1)の全表面に第1層(2)が形成されている形態と、
第2図に示す様に第1層(2)は鋳型本体の下半部にの
み形成されている場合とがあり、望ましくはこの第1層
(2)は下方へ行くにつれ、その厚さを大としておく。
The continuous casting mold of the present invention has a mold body (
1) in which the first layer (2) is formed on the entire surface;
As shown in Figure 2, the first layer (2) may be formed only in the lower half of the mold body, and preferably the thickness of the first layer (2) decreases as it goes downward. Keep it large.

第2層(3)は鋳型本体の下半部にのみ施すものであり
、その理由は鋳型本体の上半部にあっては未だ溶鋼の状
態であるので摩耗に起因する損傷は殆んど受けないが、
特にメスニカス部付近では加熱冷却の熱サイクルが激し
い為にサーメット溶射層から成る第2層(3)を施して
いても剥離し易く、シかも一部で剥離が起こればそれが
全体的に拡がり下半部の第2層までも剥離する危険性が
あるからである。
The second layer (3) is applied only to the lower half of the mold body, because the upper half of the mold body is still in the molten state, so it is hardly susceptible to damage caused by wear. No, but
Particularly near the mesonicus part, the thermal cycle of heating and cooling is intense, so even if the second layer (3) consisting of a cermet sprayed layer is applied, it is easy to peel off, and if peeling occurs in one part, it will spread throughout the area. This is because there is a risk that even the second layer in the lower half will peel off.

なお図示はしていないが、本発明の連続鋳造用鋳型にあ
っても、最外表面にクロム層を10〜50μmの厚みで
施し、鋳込み初期に於けるスプラッシュの付着防止を図
る事もある。
Although not shown, in the continuous casting mold of the present invention, a chromium layer with a thickness of 10 to 50 μm may be applied to the outermost surface to prevent splash adhesion during the initial stage of casting.

〈実施例〉 以下本発明を、実施例並びに比較例を示し乍ら詳述する
<Examples> The present invention will be described in detail below with reference to Examples and Comparative Examples.

まず各種サーメットの密着性その他を調べる目的で、銅
母材の表面にトI厚にNIメッキ層を施し該Niメッキ
層上にプラズマ溶射法により下記第1表に示す各種のセ
ラミックとバインダー金属との組合わせから成るサーメ
ツト層を厚さ0.3mmとなる様に形成した。この場合
サーメツト層中のバインダー金属はいずれも30重量%
とし、Ni−CrはNi80重量%、 Cr2O重量%
の合金、NニーCr−kl −YはCr16重量%、人
16重量%、Y0.8重量%残Niの合金、又Co−C
r−A R−Y11′Cr23重量%、 AJ 13重
量%、Y07重量%残Coの合金を用いた。得られた試
料について、サーメツト層の密着力、耐熱衝撃性及び剥
離性を調べた結果を第1表に示す。この第1表中耐熱衝
撃性については各試料を600℃に30分間保持した後
直ちに水中へ投入するという操作を繰返しクラックが生
じる迄の回数を示すもので最高回数を20回迄とした、
又剥離性については各試料を約180度曲げ加工を施し
た場合のサーメツト層の剥離状況を観察したもので、表
中Oは剥離なし、Xは剥離ありを示す。又総合評価は表
中に示す全ての特性から判断したもので0は良好、○は
普通、△はや一不良、×は不良を示す。
First, in order to examine the adhesion and other properties of various cermets, a Ni plating layer was applied to the surface of a copper base material to a thickness of 100 ml, and then various ceramics and binder metals shown in Table 1 below were applied onto the Ni plating layer by plasma spraying. A cermet layer consisting of the following combinations was formed to have a thickness of 0.3 mm. In this case, the binder metal in the cermet layer is 30% by weight.
and Ni-Cr is Ni80wt%, Cr2Owt%
Cr-kl-Y is an alloy of 16% by weight of Cr, 16% by weight of Ni, and 0.8% by weight of Y with the balance Ni, and also Co-C
r-A R-Y11' An alloy containing 23% by weight of Cr, 13% by weight of AJ, and 7% by weight of Y0 with a balance of Co was used. Table 1 shows the results of examining the adhesion, thermal shock resistance, and peelability of the cermet layer of the obtained samples. Thermal shock resistance in Table 1 indicates the number of times each sample was held at 600°C for 30 minutes and then immediately put into water until cracks appeared, with the maximum number of times being 20.
Regarding peelability, the state of peeling of the cermet layer was observed when each sample was bent approximately 180 degrees. In the table, O indicates no peeling and X indicates peeling. The overall evaluation was determined based on all the characteristics shown in the table, with 0 indicating good, ◯ fair, △ very poor, and × indicating poor.

思上の結果より、サーメットに用いるセラミックとして
はCr5CzあるいはTiCが望ましい事、更にバイン
ダー金属としてはNi−Cr−人1−YあるいはCo−
Cr−AJ−Yが望ましい事が判った。
From the expected results, Cr5Cz or TiC is preferable as the ceramic used for the cermet, and Ni-Cr-Y or Co- as the binder metal.
It was found that Cr-AJ-Y is preferable.

次に本発明の具体的な実施例を示す。Next, specific examples of the present invention will be shown.

11璽工 銅製鋳型本体の内壁面の下半部に、厚さ3.0mmにN
iメッキ層を施した。この旧メッキの条件は、金属Ni
80g/l、 H3B0330g/J 、ラウリル硫酸
ナトリウム< 0.1g/l 、 plr4. O,液
温50℃のメッキ浴を用いて行なった。この様にして得
られたNiメッキ層上にCr3 C280重重量、旧−
〇r−AJ −Y合金20重量%%より成るサーメット
層をプラズマ溶射法によってその厚さが0.3+nmと
なるべ(溶射した。N1−Cr−AIT−Y合金は、C
r16重量%重量16重量%、Yo、8重量%残部N1
なる組成の合金を用いた。得られた鋳型のサーメット溶
射層の硬さはHv750〜850の範囲にあり、1チャ
ージ当り150トンの溶鋼を処理する連続鋳造用鋳型と
して実機テストをした結果800チヤージまでは何ら支
障なく操業が出来、その時点で鋳型の表面を観察した結
果、剥離もクラックの発生も生じていなかった。
11 N
An i-plating layer was applied. The conditions for this old plating are metal Ni
80g/l, H3B0330g/J, sodium lauryl sulfate < 0.1g/l, plr4. The plating bath was conducted using a plating bath with a liquid temperature of 50°C. On the Ni plating layer obtained in this way, Cr3 C280 weight, old -
〇A cermet layer consisting of 20% by weight of r-AJ-Y alloy was sprayed to a thickness of 0.3+ nm by plasma spraying.
r16 weight% weight 16 weight%, Yo, 8 weight% balance N1
An alloy with the following composition was used. The hardness of the cermet sprayed layer of the mold obtained was in the range of Hv750 to Hv850, and as a result of an actual machine test as a continuous casting mold that processes 150 tons of molten steel per charge, it was possible to operate up to 800 charges without any problems. At that point, the surface of the mold was observed, and no peeling or cracking had occurred.

なお比較の為に従来からある銅製鋳型本体表面にNiメ
ッキ層のみをその厚さが5.0mmとなるべく施した鋳
型についても同様の実機テストをした結果は、1チャー
ジ当り1501−ン処理の場合で400チヤージで表面
N1メッキ層が摩耗しそれ以後は使用出来なかった。
For comparison, we conducted a similar actual test on a conventional copper mold body surface with only a Ni plating layer to a thickness of 5.0 mm, and the results were as follows: After 400 charges, the surface N1 plating layer wore out and it could no longer be used.

なお上記実施例Iに於いて、サーメツト層中のバインダ
ー金属の量を種々変化させた場合につき上述の実機テス
トを行なった結果、バインダー金属が18重量%では4
50チヤージでクラックを生じて剥離し、10重重量で
は僅か200チヤージしか寿命がなかった。又サーメツ
ト層の厚さについてはバインダー金属を35重重量含有
せしめた場合の例では、その厚さが1.0mmでは10
チヤージ目で早くもクラックが生じ、(1,6mmでは
350チヤージ目でクラックが生じ、0.5mmでは5
00チヤージでも異常がなく、サーメット層の厚さとし
ては0.5mm以下とすべきである事が確認された。し
かるに実際の溶射施工上均−厚さになす為、及び要求さ
れる一定以上の耐摩耗性を具備せしめる為に最小3.0
5mmは必要である。
In Example I, the above-mentioned actual machine test was conducted in which the amount of binder metal in the cermet layer was varied.
It cracked and peeled off after 50 charges, and its lifespan was only 200 charges at 10 weight. In addition, regarding the thickness of the cermet layer, in the case where the binder metal is contained in 35% by weight, if the thickness is 1.0 mm, the thickness is 10%.
Cracks occur as early as the 350th charge for 1.6 mm, and 5 for 0.5 mm.
There were no abnormalities even at 0.00 charge, and it was confirmed that the thickness of the cermet layer should be 0.5 mm or less. However, in actual thermal spraying, in order to achieve a uniform thickness and to provide a certain level of wear resistance required, a minimum of 3.0
5mm is necessary.

11五I 銅製鋳型本体の内壁面に対し、Ni−,5重量%Fe合
金を、鋳型本体の上半部に於ける厚さが0.5mmで、
下半部に於ける厚さが2.0mmとなる様にメッキ処理
をした。メッキ条件は金属Ni90g/J 、金属Fe
5g/l、■、BO330g/ J 、ラウリル硫酸(
0,1g/I 。
115I Ni-, 5% by weight Fe alloy is applied to the inner wall surface of the copper mold body, with a thickness of 0.5 mm in the upper half of the mold body,
Plating was performed so that the thickness of the lower half was 2.0 mm. Plating conditions are metal Ni90g/J, metal Fe
5g/l, ■, BO330g/J, lauryl sulfate (
0.1 g/I.

pH4,2p液温50℃で行なった。この旧−Fe合金
メッキ層上でしかも鋳型本体の下半部に、TiC65重
量%、重量−Cr−人1−Y合金35重量%より成るサ
ーメツト層を爆発溶射法によりその厚さが0.3mmと
なるべく溶射した。Co−Cr−人1−Y合金は、Cr
23重量%、A413重量%、Yo、7重量%残部Co
なる組成の合金を用いた。得られた鋳型のサーメツト層
の硬さはHv750〜830の範囲であった。この実施
例■の鋳型も上記実施例Iで示したのと同様の実機テス
トの結果800チヤージまでは何ら支障なく使用可能で
あった。
The pH was 4, 2p, and the liquid temperature was 50°C. On this old -Fe alloy plating layer and in the lower half of the mold body, a cermet layer consisting of 65% by weight of TiC and 35% by weight of -Cr-1-Y alloy was applied to a thickness of 0.3 mm by explosive spraying. It was sprayed as much as possible. Co-Cr-Human 1-Y alloy is Cr
23% by weight, A4 13% by weight, Yo, 7% by weight balance Co
An alloy with the following composition was used. The hardness of the cermet layer of the obtained mold was in the range of Hv 750 to 830. The mold of Example 2 was also tested on an actual machine similar to that shown in Example I above, and as a result, it could be used up to 800 charges without any problem.

なおこの実施例■で示したTiCとCo−Cr−AI−
Yから成るサーメットの場合にも、その溶射層が厚すぎ
るとクラックが入り易い事が確認され望ましい厚さはや
はり0.05〜0.5mmという事が判った。
Note that TiC and Co-Cr-AI- shown in this Example ①
In the case of a cermet made of Y, it has been confirmed that cracks are likely to occur if the sprayed layer is too thick, and the desirable thickness is also found to be 0.05 to 0.5 mm.

〈発明の効果) 以上述べて来た様に、本発明の連続鋳造用鋳型によれば
、第2層として用いるサーメットを構成するセラミック
と金属バインダーの組合わせを限られた範囲とし、実際
に強固な密着性、耐熱衝撃性を有するものとし、しかも
Cr3C2やTiCは鉄鋼に対しての耐焼付性や耐酸化
スケール反応性の点では他のセラミックに比して一段と
優れた性質を有するので長期に渡り安定して使用可能な
鋳型となるのである。更に又本発明ではサーメツト層を
薄くしてクラックが生じ難くしていると共に、実際の機
能上さほど耐摩耗性を要求されず、逆にその部所にサー
メツト層があれば剥離の出発点ともなるべき鋳型上半部
にはサーメツト層を施す事なく、結果的に必要な下半部
のサーメット層の剥離防止をもしているので上記実施例
で示した如〈従来の鋳型の約2倍もの寿命があるのであ
る。
<Effects of the Invention> As described above, according to the continuous casting mold of the present invention, the combination of the ceramic and metal binder constituting the cermet used as the second layer is limited to a limited range, and it is possible to achieve strong In addition, Cr3C2 and TiC have superior properties compared to other ceramics in terms of seizure resistance and oxidation scale reactivity to steel, so they can be used for a long time. This results in a mold that can be used stably over time. Furthermore, in the present invention, the cermet layer is made thinner so that cracks are less likely to occur, and wear resistance is not so required for actual functionality; on the other hand, if the cermet layer is present at that location, it can become a starting point for peeling. There is no need to apply a cermet layer to the upper half of the mold, and as a result, the required lower half of the cermet layer is prevented from peeling off.As shown in the example above, the lifespan is approximately twice as long as that of conventional molds. There is.

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

第1図及び第2図はそれぞれ本発明の断面説明図。 図中、  (1)゛鋳型本体 (2):第1層 (3)・第2層 1 and 2 are cross-sectional explanatory views of the present invention, respectively. In the figure, (1) ``Mold body (2): 1st layer (3)・Second layer

Claims (1)

【特許請求の範囲】[Claims] 1、銅若しくは銅合金製鋳型本体の内壁面の少なくとも
下半部に、ニッケル若しくはニッケル−鉄合金メッキ層
より成る第1層を形成し、該第1層の表面で鋳型本体の
下半部に相当する部所に、炭化クロム若しくは炭化チタ
ンに対しNi−Cr−Al−Y若しくはCo−Cr−A
l−Y合金をバインダー金属として全体の20〜50重
量%含有せしめたサーメット溶射層より成る第2層を、
その厚さが0.05〜0.5mmとなるべく形成せしめ
たことを特徴とする連続鋳造用鋳型。
1. A first layer consisting of a nickel or nickel-iron alloy plating layer is formed on at least the lower half of the inner wall surface of the copper or copper alloy mold body, and the surface of the first layer is applied to the lower half of the mold body. In corresponding parts, Ni-Cr-Al-Y or Co-Cr-A is added to chromium carbide or titanium carbide.
A second layer consisting of a cermet sprayed layer containing 20 to 50% by weight of l-Y alloy as a binder metal,
A mold for continuous casting, characterized in that the mold is formed to have a thickness of 0.05 to 0.5 mm.
JP4931686A 1986-03-05 1986-03-05 Mold for continuous casting Pending JPS62207534A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4931686A JPS62207534A (en) 1986-03-05 1986-03-05 Mold for continuous casting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4931686A JPS62207534A (en) 1986-03-05 1986-03-05 Mold for continuous casting

Publications (1)

Publication Number Publication Date
JPS62207534A true JPS62207534A (en) 1987-09-11

Family

ID=12827557

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4931686A Pending JPS62207534A (en) 1986-03-05 1986-03-05 Mold for continuous casting

Country Status (1)

Country Link
JP (1) JPS62207534A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01210152A (en) * 1988-02-17 1989-08-23 Tocalo Co Ltd Vessel for molten metal
EP0774525A1 (en) * 1995-11-17 1997-05-21 Ngk Insulators, Ltd. Copper alloy mold for casting aluminium or aluminium alloy
US6810941B2 (en) 2001-06-01 2004-11-02 Ngk Insulators, Ltd. Injection mold for semi-solidified Fe alloy
JP2009191318A (en) * 2008-02-14 2009-08-27 Tocalo Co Ltd Metallic member with sprayed coating having excellent carburizing resistance

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01210152A (en) * 1988-02-17 1989-08-23 Tocalo Co Ltd Vessel for molten metal
EP0774525A1 (en) * 1995-11-17 1997-05-21 Ngk Insulators, Ltd. Copper alloy mold for casting aluminium or aluminium alloy
US5799717A (en) * 1995-11-17 1998-09-01 Techno Coat Company, Ltd. Copper alloy mold for casting aluminum or aluminum alloy
US6810941B2 (en) 2001-06-01 2004-11-02 Ngk Insulators, Ltd. Injection mold for semi-solidified Fe alloy
JP2009191318A (en) * 2008-02-14 2009-08-27 Tocalo Co Ltd Metallic member with sprayed coating having excellent carburizing resistance

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