JPS648691B2 - - Google Patents
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- Publication number
- JPS648691B2 JPS648691B2 JP59162789A JP16278984A JPS648691B2 JP S648691 B2 JPS648691 B2 JP S648691B2 JP 59162789 A JP59162789 A JP 59162789A JP 16278984 A JP16278984 A JP 16278984A JP S648691 B2 JPS648691 B2 JP S648691B2
- Authority
- JP
- Japan
- Prior art keywords
- temperature
- base material
- molten
- roll
- ribbon
- 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
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- 239000000463 material Substances 0.000 claims description 40
- 239000000956 alloy Substances 0.000 claims description 30
- 229910045601 alloy Inorganic materials 0.000 claims description 29
- 238000002844 melting Methods 0.000 claims description 17
- 230000008018 melting Effects 0.000 claims description 17
- 238000001816 cooling Methods 0.000 claims description 16
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 claims description 6
- 230000035699 permeability Effects 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 description 21
- 238000000034 method Methods 0.000 description 11
- 239000012768 molten material Substances 0.000 description 9
- 229910000702 sendust Inorganic materials 0.000 description 7
- 239000000203 mixture Substances 0.000 description 5
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 3
- 230000008602 contraction Effects 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 229910000669 Chrome steel Inorganic materials 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 229910052761 rare earth metal Inorganic materials 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- YLZOPXRUQYQQID-UHFFFAOYSA-N 3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)-1-[4-[2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidin-5-yl]piperazin-1-yl]propan-1-one Chemical compound N1N=NC=2CN(CCC=21)CCC(=O)N1CCN(CC1)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F YLZOPXRUQYQQID-UHFFFAOYSA-N 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- AFCARXCZXQIEQB-UHFFFAOYSA-N N-[3-oxo-3-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)propyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CCNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 AFCARXCZXQIEQB-UHFFFAOYSA-N 0.000 description 1
- 229910002796 Si–Al Inorganic materials 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 239000003779 heat-resistant material Substances 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Landscapes
- Continuous Casting (AREA)
- Soft Magnetic Materials (AREA)
Description
本発明は、いわゆるセンダストと称される高透
磁率合金の薄帯を製造する方法に関する。
Al4〜7%、Si8〜11%、残部主として鉄より
なるFe―Si―Al金(センダスト)、あるいは磁気
特性や機械特性を改善するためにこの合金にNi、
Co、Ti、B、希土類元素その他の元素を少量添
加した合金は、磁気特性に優れ、かつ硬度が高い
ので耐摩耗性にも優れていることから、磁気録音
や磁気録画のための磁気ヘツド用コアとして使用
されている。しかしこの使用のためには母合金を
機械的に切削して薄片を得、それをラミネートし
てコアを形成する方法がとられているが、センダ
スト合金は硬度が高いのみならず脆弱であること
からその機械加工が困難である点に問題があつ
た。最近、この問題を解決する方法として、セン
ダスト母合金を加熱溶融させ、その溶融材を高速
回転するシングルロールやツインロール上に供給
してロール上で超急冷し一体に凝固させて薄帯を
製造し、この薄帯をエツチングや打抜き加工によ
りコア形状に成形する方法が提案されている。こ
の方法によれば、連続的に製造される高透磁率セ
ンダスト合金薄帯を加工すればよいので、センダ
スト合金ブロツクから直接コア用薄片を切削する
方法に比べて薄片への切削加工を必要としない点
で加工性に極めて優れている特長がある。しかし
ながら、この溶融材料を急冷凝固させて薄帯を得
る方法では、溶融材料を移動体の移動面上に供給
する際に溶融材料の温度が融点よりもかけはなれ
て高いと、急冷凝固されるときに供給材料の各部
分、例えば移動面との接触部と非接触部とで冷却
度合が大きく異なり熱収縮が均一に行なわれず、
このために薄帯にマイクロクラツクが生ずる問題
があり、このマイクロクラツクは熱処理をしても
とれない根本的な欠陥があつた。
本発明は、かかる従来の問題に鑑みてなされた
ものであり、Al4〜7%、Si8〜11%、残部主と
して鉄よりなる合金母材を加熱溶融し、この溶融
合金母材を移動体のロール面上に供給し、ロール
面上で急冷して薄帯状に凝固させる高透磁率合金
薄帯の製造方法において、上記溶融合金母材の移
動面上に供給する直前の温度この合金母材の融点
直上ないし融点より100℃を越えない温度範囲に
設定し、前記溶融合金母材の移動面上に供給する
直前の粘度を6.5×10-2〜4×10-2dyne.sec/cm2と
すると共に移動体の表面温度を常温ないし460℃
に保持し、かつ前記溶融母材と冷却ロールとの間
の温度差を920゜〜1350℃とすることにより急冷時
の冷却度合の不均一性を抑え、マイクロクラツク
の生じない薄帯を製造する方法を提供するもので
ある。
本発明を以下に詳細に説明する。
合金母材はいわゆるセンダスト組成のもの、す
なわちAl4〜7%、Si8〜11%、残部主として鉄
よりなり、機械特性や磁気特性の向上のために必
要に応じてV、Nb、Ta、Cr、Mo、W、Ni、
Co、Cu、Ti、Mn、Ge、Zr、Sb、Sn、Be、B、
Bi、Pb、Y、希土類元素が少量添加されたもの
も使用される。この溶融母材の融点は組成により
若干の高低があるが、1280℃前後である。
第1図は本発明の方法に使用する製造装置を示
す。この装置によりまず母合金1を抵抗器または
コイルによる加熱手段2にて加熱筒3内でアルゴ
ンガスのような非酸化性ガス雰囲気下に加熱溶融
させ、しかるのち加熱手段2の加熱温度を母合金
1の融点近くまで、好ましくは融点以上、約10%
の範囲(即ち約100℃)まで温度を下げ、加熱筒
3内の非酸化性ガスの圧力を上げて溶融母材1を
ノズル3aから高速回転するツインロール4a,
4b上へ噴出させ、ツインロール4a,4bとの
接触により急冷すると同時に圧延し一体に凝固さ
せて薄帯5を得る。ここで母合金1の加熱溶融時
の温度は1500℃前後とし、噴出直前に融点直上の
温度まで下げる手順をとると、加熱時間が短かく
て済むが、はじめから低い温度で加熱溶融させる
手順をとることもできる。またロール4a,4b
の材質は高耐熱性を有する平滑な表面状態のもの
が良く、ステンレス鋼、鋳鉄、クローム鋼などが
用いられる。
加熱筒3は母材1との反応をさける必要があ
り、シリカ、高純度アルミナなどの高耐熱性材質
のものが用いられる。また加熱筒3のノズル3a
の形状は得ようとする薄帯のサイズにより決定す
べきものであるが、第2図に示すような幅広で多
孔のものを使用するとロール4a,4b上に幅広
く溶融材を噴出させることができて冷却度合の均
一化をさらに改善することができる。さらに多孔
ノズルの場合に、各孔間の間隔を大きくとると、
一度に複数枚の薄帯を得ることができる。第3図
は他の製造装置を示し、エンドレスベルト6とロ
ール7との間に溶融材1を供給して超急冷し圧延
する構成を有する。この装置にあつてもベルト6
とロール7の材質、加熱筒3の材質、形状等は上
記第1図のツインロール4a,4bを用いた装置
とほとんど同じである。
このようにして得られる薄帯にあつては、加熱
溶融された母材を移動体の供給する直前の母材の
温度をその融点直上(融点より100℃をこえない
温度)にするので、供給直後における移動体の移
動面と接触する部分と接触しない部分との冷却度
合に大きな差が生ぜず、このために溶融母材は比
較的緩やかな冷却を受けることになつて急冷によ
る熱収縮が材料全体で比較的均一に起こり、マイ
クロクラツクの生じない薄帯を得ることができる
のである。尚、母材の融点直上の温度としては、
発明者の実験から融点からその上約10%、約100
℃程度の範囲で効果が得られ、特に融点から上約
5%、約50℃程度の範囲において著しい効果があ
る。
なお移動体であるロールの温度を常温乃至460
℃に保持すると、超急冷による熱収縮が緩和さ
れ、熱収縮が材料全体で比較的均一に起り、マイ
クロクラツクの発生が防止できる顕著な効果があ
る。移動体であるロール温度の好ましい範囲は
100℃ないし300℃である。
溶融母材の噴出直前の温度を母材の融点より
100℃を越えない範囲にすると共に、その粘度を
比較的高く保持することが必要であり、その粘度
は6.5×10-2〜4×10-2dyne.sec/cm2がよい。しか
しながら溶融母材の粘度が上述の上限より大きい
と、粘度が大きすぎて押出圧力が大きくなりす
ぎ、実施上困難となるので必要がない。また粘度
が上述の下限より以下であると、粘度が小さくな
りすぎて、押出圧力が大きすぎると、ミスト状ま
たはすだれ状になつたり、波をうつたりする欠点
が生じ好ましくないので、上述の範囲が好まし
い。
溶融母材と冷却ロールとの間の温度差920℃〜
1350℃位に余り過大でない方がよい結果が得られ
る。これは超急冷による熱収縮が材料全体で比較
的均一に起ると、マイクロクラツクが生じないた
めである。
ロール回転数は650〜10000RPMがよい。ロー
ル回転数が小さいと100μ位の厚い薄帯が得られ、
ロールの回転数が大きいと50μ〜10μ位の薄い薄
帯が得られる。溶融母材の噴出温度が1500℃位に
高いときは回転速度の大きい方が溶融母材と冷却
ロールとの間の温度差を小さくしたのと同じ効果
となり、マイクロクラツクが生じ難くなる。溶融
母材と冷却ロールとの間の温度差がその下限以下
であると、ロールの回転速度を種々に変更しても
超急冷が得られないので好ましくない。またその
温度差が上述の上限以上であると、超急冷による
熱収縮が材料全体で不均一に生じ、その中心部分
にマイクロクラツクを生ずる。このマイクロクラ
ツクは爾後の熱処理により消すことができないの
で、材料が脆くなり加工性が劣化し、所期の可撓
性が得られない。
移動体としてツインロールを使用するとロール
と接触した面より内方に発達する柱状晶が生ず
る。これを600℃〜950℃好ましくは850℃位で1
分ないし5時間熱処理すると、結晶が粗大化し可
撓性は若干劣るが抗磁力がよくなるので、熱処理
は施した方がよい。
本発明を次に実施例に基き具体的に説明する。
実施例 1
Al5.38、Si9.37、Fe85.25の組成を有する母合
金ブロツク1の2gを、第1図に示す装置の加熱
筒3内に入れて、Arガス雰囲気下でSiCヒータの
加熱手段2により約1450℃で加熱溶融させ、しか
るのち加熱手段2への給電量を抑えて約1320℃ま
で温度を下げ、Arガス圧を0.5気圧に上げてノズ
ル3aから溶融材1をツインロール4a,4b上
に噴出させ、このツインロール4a,4bで急冷
圧延し薄帯5を得た。ここにおいて加熱筒3は外
径8mm、内径6mmのシリカ製であつて、ノズルは
0.5mm径であつた。またロール4a,4bはクロ
ーム鋼製65mm径のものでロール4a,4b間を密
着させ、材料1噴出時のノズル3aとロール4
a,4bとの距離は約0.2mm以下の可能な限り接
近させた状態で、1000rpmの回転数において実施
した。
得られた薄帯は、100μm厚、約2mm幅、約10
m長のものであり、これを真空中、約850℃以下
で熱処理し、しかる後コア用薄片5aを打抜いて
その表面状態および磁気特性を測定した。
実施例 2
実施例1と同一組成の母合金2gを高純度アル
ミナ製加熱筒に入れ、実施例1と同一の装置で実
施した。ただし、ノズル径は1.0mm、ロール回転
数は650rpm、溶融材の噴出直前の温度は約1380
℃とした。
得られた薄帯は、100μm厚、約2mm幅、約5
m長のものであり、これを実施例1と同一条件で
熱処理し、コア用薄片5bを打抜いてその表面状
態および磁気特性を測定した。
比較例
実施例1と同一組成の母合金2gにより実施例
1と同一の装置で実施した。ただし母合金の加熱
温度は約1450℃にしてその温度のまま噴出させ
た。
得られた薄帯は、80μm厚、約2mm幅、約10m
長のものであり、これを実施例1と同一条件で熱
処理した後、コア用薄片5cを得、その表面状態お
よび磁気特性を測定した。
上記実施例および比較例による表面状態および
磁気特性の測定結果は次表および第4図のように
なつた。
The present invention relates to a method for manufacturing a ribbon of a high magnetic permeability alloy called Sendust. Fe-Si-Al gold (sendust), which consists of 4 to 7% Al, 8 to 11% Si, and the remainder mainly iron, or Ni to improve the magnetic and mechanical properties of this alloy.
Alloys containing small amounts of Co, Ti, B, rare earth elements, and other elements have excellent magnetic properties and are highly hard and wear resistant, so they are used in magnetic heads for magnetic recording. used as a core. However, for this purpose, the mother alloy is mechanically cut to obtain thin pieces, which are then laminated to form the core, but Sendust alloy is not only hard but also brittle. The problem was that machining was difficult. Recently, as a method to solve this problem, the sendust master alloy is heated and melted, the molten material is fed onto a single roll or twin rolls rotating at high speed, and the molten material is ultra-quenched on the rolls and solidified into a single piece to produce a ribbon. However, a method has been proposed in which this ribbon is formed into a core shape by etching or punching. According to this method, since it is only necessary to process the continuously manufactured high permeability Sendust alloy thin strip, there is no need for cutting into the thin section compared to the method of directly cutting the core thin section from the Sendust alloy block. It has the advantage of being extremely easy to work with. However, in this method of obtaining a ribbon by rapidly cooling and solidifying a molten material, if the temperature of the molten material is far higher than the melting point when the molten material is supplied onto the moving surface of the moving body, the material may be rapidly solidified. The degree of cooling differs greatly between each part of the supplied material, for example, the part in contact with the moving surface and the part not in contact with it, and heat shrinkage is not performed uniformly.
For this reason, there was a problem that microcracks were generated in the ribbon, and these microcracks had a fundamental defect that could not be removed even by heat treatment. The present invention was made in view of such conventional problems, and involves heating and melting an alloy base material consisting of 4 to 7% Al, 8 to 11% Si, and the remainder mainly iron, and applying this molten alloy base material to the roll of a moving body. In a method for manufacturing a high magnetic permeability alloy ribbon, which is supplied onto a surface and rapidly cooled on a roll surface to solidify into a ribbon, the temperature immediately before supplying the molten alloy base material onto a moving surface is the melting point of this alloy base material. The temperature is set at a temperature range that is directly above or does not exceed 100°C above the melting point, and the viscosity immediately before being supplied onto the moving surface of the molten alloy base material is 6.5 × 10 -2 to 4 × 10 -2 dyne.sec/cm 2 together with the surface temperature of the moving object from room temperature to 460℃
By maintaining the molten base material at a temperature of 920° to 1350°C between the molten base material and the cooling roll, non-uniformity in the degree of cooling during rapid cooling is suppressed, and a ribbon without microcracks is produced. This provides a method to do so. The invention will be explained in detail below. The alloy base material has a so-called sendust composition, that is, Al4~7%, Si8~11%, and the remainder is mainly iron, with V, Nb, Ta, Cr, and Mo added as necessary to improve mechanical and magnetic properties. ,W,Ni,
Co, Cu, Ti, Mn, Ge, Zr, Sb, Sn, Be, B,
Those with small amounts of Bi, Pb, Y, and rare earth elements added are also used. The melting point of this molten base material varies slightly depending on the composition, but is around 1280°C. FIG. 1 shows a manufacturing apparatus used in the method of the invention. With this device, the master alloy 1 is first heated and melted in a non-oxidizing gas atmosphere such as argon gas in the heating cylinder 3 by the heating means 2 using a resistor or coil, and then the heating temperature of the heating means 2 is adjusted to the master alloy. Near the melting point of 1, preferably above the melting point, about 10%
twin rolls 4a, which rotate the molten base material 1 at high speed from the nozzle 3a by lowering the temperature to a range of
4b, and is rapidly cooled by contact with twin rolls 4a and 4b, and simultaneously rolled and solidified to obtain a ribbon 5. Here, the temperature when heating and melting the master alloy 1 is around 1500℃, and if you lower the temperature to just above the melting point just before ejecting, the heating time will be shorter, but it is better to heat and melt it at a low temperature from the beginning. You can also take it. Also rolls 4a, 4b
The material should preferably have a smooth surface with high heat resistance, such as stainless steel, cast iron, or chrome steel. The heating cylinder 3 needs to avoid reaction with the base material 1, and is made of a highly heat-resistant material such as silica or high-purity alumina. Also, the nozzle 3a of the heating cylinder 3
The shape of the strip should be determined depending on the size of the ribbon to be obtained, but if a wide and porous one as shown in Fig. 2 is used, the molten material can be sprayed over a wide range onto the rolls 4a and 4b. The uniformity of the cooling degree can be further improved. Furthermore, in the case of a multi-hole nozzle, if the distance between each hole is increased,
You can get multiple thin strips at once. FIG. 3 shows another manufacturing apparatus, which has a configuration in which a molten material 1 is supplied between an endless belt 6 and a roll 7, and is ultra-quenched and rolled. Even with this device, the belt 6
The material of the roll 7 and the material and shape of the heating tube 3 are almost the same as the apparatus using the twin rolls 4a and 4b shown in FIG. 1 above. In the case of the ribbon obtained in this way, the temperature of the base material immediately before it is supplied by the moving body is just above its melting point (temperature not exceeding 100°C above the melting point), so the supply Immediately afterward, there is no significant difference in the degree of cooling between the parts that come into contact with the moving surface of the moving body and the parts that do not, and as a result, the molten base material is cooled relatively slowly, causing thermal contraction due to rapid cooling. This process occurs relatively uniformly throughout, making it possible to obtain a ribbon free of microcracks. In addition, the temperature just above the melting point of the base material is:
From the inventor's experiments, it is about 10% above the melting point, about 100
The effect is obtained in a range of approximately 50°C, and the effect is particularly remarkable in a range of about 50°C, which is about 5% above the melting point. Please note that the temperature of the roll, which is a moving body, is between room temperature and 460℃.
By holding the material at a temperature of 0.degree. C., the thermal shrinkage caused by ultra-rapid cooling is alleviated, and the thermal shrinkage occurs relatively uniformly throughout the material, which has the remarkable effect of preventing the generation of microcracks. The preferred temperature range for the roll, which is a moving body, is
The temperature is between 100℃ and 300℃. The temperature just before ejection of the molten base material is determined from the melting point of the base material.
It is necessary to keep the temperature within a range of not exceeding 100°C and to maintain a relatively high viscosity, and the viscosity is preferably 6.5×10 -2 to 4×10 -2 dyne.sec/cm 2 . However, if the viscosity of the molten base material is higher than the above-mentioned upper limit, the viscosity will be too high and the extrusion pressure will be too high, making it difficult to implement, so this is not necessary. In addition, if the viscosity is less than the lower limit mentioned above, the viscosity will become too small, and if the extrusion pressure is too high, it will become mist-like, blind-like, or wave-like, which is undesirable. is preferred. Temperature difference between molten base material and cooling roll: 920℃~
Better results can be obtained if the temperature is not too high, around 1350°C. This is because microcracks do not occur when thermal contraction due to ultra-rapid cooling occurs relatively uniformly throughout the material. The roll rotation speed is preferably 650 to 10,000 RPM. If the roll rotation speed is low, a thick ribbon of about 100μ can be obtained,
If the rotation speed of the roll is high, a thin ribbon of about 50μ to 10μ can be obtained. When the jetting temperature of the molten base material is as high as about 1500°C, a higher rotation speed has the same effect as reducing the temperature difference between the molten base material and the cooling roll, making it difficult for microcracks to occur. If the temperature difference between the molten base material and the cooling roll is below the lower limit, ultra-rapid cooling cannot be obtained even if the rotational speed of the roll is variously changed, which is not preferable. Furthermore, if the temperature difference is above the above-mentioned upper limit, thermal contraction due to ultra-rapid cooling occurs unevenly throughout the material, producing microcracks in the central portion. Since these microcracks cannot be eliminated by subsequent heat treatment, the material becomes brittle and its workability deteriorates, making it impossible to obtain the desired flexibility. When twin rolls are used as a moving body, columnar crystals develop inward from the surface in contact with the rolls. This is heated at 600°C to 950°C, preferably around 850°C.
Heat treatment for 5 minutes to 5 hours will cause the crystals to become coarse and the flexibility will be slightly inferior, but the coercive force will improve, so it is better to perform heat treatment. The present invention will now be described in detail based on Examples. Example 1 2 g of master alloy block 1 having a composition of Al5.38, Si9.37, and Fe85.25 was placed in the heating cylinder 3 of the apparatus shown in Fig. 1, and heated by a SiC heater in an Ar gas atmosphere. The material is heated and melted at approximately 1450°C by means 2, and then the amount of power supplied to heating means 2 is reduced to lower the temperature to approximately 1320°C, the Ar gas pressure is increased to 0.5 atm, and the molten material 1 is transferred from the nozzle 3a to the twin roll 4a. , 4b, and was rapidly cooled and rolled with twin rolls 4a and 4b to obtain a ribbon 5. Here, the heating cylinder 3 is made of silica with an outer diameter of 8 mm and an inner diameter of 6 mm, and the nozzle is
It was 0.5mm in diameter. Further, the rolls 4a and 4b are made of chrome steel with a diameter of 65 mm, and the rolls 4a and 4b are brought into close contact with each other, and the nozzle 3a and the roll 4 when the material 1 is ejected are
The test was carried out at a rotational speed of 1000 rpm with the distance between a and 4b being as close as possible to approximately 0.2 mm or less. The obtained ribbon is 100 μm thick, about 2 mm wide, and about 10
It was heat-treated in vacuum at about 850° C. or less, and then a core thin piece 5a was punched out and its surface condition and magnetic properties were measured. Example 2 2 g of a master alloy having the same composition as in Example 1 was placed in a heating cylinder made of high purity alumina, and the experiment was carried out using the same apparatus as in Example 1. However, the nozzle diameter is 1.0 mm, the roll rotation speed is 650 rpm, and the temperature just before ejecting the molten material is approximately 1380.
℃. The obtained ribbon is 100 μm thick, about 2 mm wide, and about 5
This was heat-treated under the same conditions as in Example 1, and a core thin piece 5b was punched out to measure its surface condition and magnetic properties. Comparative Example A test was carried out using 2 g of a master alloy having the same composition as in Example 1 and using the same apparatus as in Example 1. However, the heating temperature of the master alloy was approximately 1450°C and it was ejected at that temperature. The obtained ribbon is 80 μm thick, approximately 2 mm wide, and approximately 10 m long.
After heat treating it under the same conditions as in Example 1, a core thin piece 5c was obtained, and its surface condition and magnetic properties were measured. The measurement results of the surface condition and magnetic properties in the above Examples and Comparative Examples are as shown in the following table and FIG. 4.
【表】【table】
【表】
上記表および第4図よりわかるように、磁気特
性においては各実施例および比較例において全く
差異が生じないが、表面状態において材料噴出時
の温度が低い本発明の実施例1のコアではマイク
ロクラツクの発生がほとんどなく、温度がやや高
めの本発明の実施例2のコアでもわずかながらマ
イクロクラツク8が発生しているが、比較例のよ
うにコアの厚み全体に及ぶことがなく、従つて本
発明によればきわめて表面状態が良く、磁気特性
には影響のないコアを得ることができた。[Table] As can be seen from the above table and FIG. 4, there is no difference in magnetic properties between the Examples and Comparative Examples, but the core of Example 1 of the present invention has a lower surface temperature at the time of material ejection. There were almost no micro-cracks in the core of Example 2 of the present invention, which had a slightly higher temperature, but a few micro-cracks 8 were generated in the core of Example 2 of the present invention. Therefore, according to the present invention, a core with an extremely good surface condition and no influence on magnetic properties could be obtained.
第1図は本発明の一実施例に使用する装置の全
体図、第2図は同上装置に用いる多孔ノズルの斜
視図、第3図は本発明の他の実施例に使用する装
置の全体図、第4図は本発明の実施例および従来
例により得られた薄帯のコア片の断面図である。
1…母合金材料、2…加熱手段、3…加熱筒、
3a…ノズル、4a,4b…ロール、5…薄帯、
6…ベルト、7…ロール、8…マイクロクラツ
ク。
Fig. 1 is an overall view of the device used in one embodiment of the present invention, Fig. 2 is a perspective view of a multi-hole nozzle used in the same device, and Fig. 3 is an overall view of the device used in another embodiment of the present invention. , FIG. 4 is a cross-sectional view of a ribbon core piece obtained by an example of the present invention and a conventional example. 1... Master alloy material, 2... Heating means, 3... Heating tube,
3a... Nozzle, 4a, 4b... Roll, 5... Thin strip,
6...belt, 7...roll, 8...micro crack.
Claims (1)
りなる合金母材を加熱溶融し、この溶融合金母材
を移動体のロール面上に供給し、ロール面上で急
冷して一体に凝固させる高透磁率合金薄帯の製造
方法において、上記溶融合金母材の移動面上に供
給する直前の温度をこの合金母材の融点直上ない
し融点より100℃を越えない温度範囲に設定し、
前記溶融合金母材の移動面上に供給する直前の粘
度を6.5×10-2〜4×10-2dyne.sec/cm2とすると共
に移動体の表面温度を常温ないし460℃に保持し、
かつ前記溶融母材と冷却ロールとの間の温度差を
920゜〜1350℃とすることを特徴とする高透磁率合
金薄帯の製造方法。1 An alloy base material consisting of Al4~7%, Si8~11%, and the remainder mainly iron is heated and melted, this molten alloy base material is supplied onto the roll surface of a moving body, and is rapidly cooled on the roll surface to solidify into one piece. In the method for producing a high magnetic permeability alloy ribbon, the temperature immediately before supplying the molten alloy base material onto the moving surface is set to a temperature range that is immediately above the melting point of the alloy base material or does not exceed 100 ° C above the melting point,
The viscosity of the molten alloy base material immediately before being supplied onto the moving surface is set to 6.5×10 -2 to 4×10 -2 dyne.sec/cm 2 and the surface temperature of the moving body is maintained at room temperature to 460°C,
and the temperature difference between the molten base material and the cooling roll.
A method for producing a high magnetic permeability alloy ribbon, characterized in that the temperature is 920° to 1350°C.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59162789A JPS6070161A (en) | 1984-08-03 | 1984-08-03 | Production of light-gauge high permeability alloy strip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59162789A JPS6070161A (en) | 1984-08-03 | 1984-08-03 | Production of light-gauge high permeability alloy strip |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP54081037A Division JPS5853705B2 (en) | 1979-06-27 | 1979-06-27 | Manufacturing method of high permeability alloy ribbon |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6070161A JPS6070161A (en) | 1985-04-20 |
| JPS648691B2 true JPS648691B2 (en) | 1989-02-15 |
Family
ID=15761236
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59162789A Granted JPS6070161A (en) | 1984-08-03 | 1984-08-03 | Production of light-gauge high permeability alloy strip |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6070161A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0191941A (en) * | 1987-10-02 | 1989-04-11 | Nippon Steel Corp | Method for continuously casting metal strip |
-
1984
- 1984-08-03 JP JP59162789A patent/JPS6070161A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6070161A (en) | 1985-04-20 |
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