JP2004090391A - Thin belt of amorphous alloy with resin layer formed and its production method - Google Patents

Thin belt of amorphous alloy with resin layer formed and its production method Download PDF

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Publication number
JP2004090391A
JP2004090391A JP2002254394A JP2002254394A JP2004090391A JP 2004090391 A JP2004090391 A JP 2004090391A JP 2002254394 A JP2002254394 A JP 2002254394A JP 2002254394 A JP2002254394 A JP 2002254394A JP 2004090391 A JP2004090391 A JP 2004090391A
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Prior art keywords
amorphous alloy
heat
alloy ribbon
resistant resin
organic solvent
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JP2002254394A
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JP4201552B2 (en
Inventor
Takashi Ono
小野 隆
Hiroshi Watanabe
渡辺 洋
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Mitsui Chemicals Inc
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Mitsui Chemicals Inc
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Abstract

<P>PROBLEM TO BE SOLVED: To provide a thin belt of an amorphous alloy which can produce a good laminate in which no blister is produced on its surface when the laminate is produced by lamination adhesion and annealing. <P>SOLUTION: In the thin belt in which a heat-resistant resin layer is formed on one surface or both surfaces, the heat-resistant resin is a thermoplastic resin. By adjusting the amount of an organic solvent contained in the resin to be 0.5 wt.% or below of amount of the resin, the good laminate having no blister on its surface can be produced. <P>COPYRIGHT: (C)2004,JPO

Description

【0001】
【産業上の利用分野】
本発明は、耐熱樹脂層が形成された非晶質合金薄帯およびその製造方法に関する。
【0002】
【従来の技術】
非晶質合金薄帯は、各種金属を原材料に溶融状態から急激に冷却することで製造される非結晶の固体であり、通常は厚さ約0.01〜0.1ミリメートル程度の薄帯である。これら非晶質合金薄帯においては、原子は配列に規則性がないランダム構造であり、軟磁性材料として優れた特性を有している。特にCo元素を含むCo系非晶質合金薄帯は、高い透磁率を特徴とする材料であり、種々の磁気応用部品、例えばインダクタンス、各種コイル、各種トランス、ノイズフィルター、磁気センサー、磁気ヘッド、アンテナ、電波吸収体、モーター、各種コア、配線基板など、幅広い分野において用いられることが期待されている。
【0003】
非晶質合金薄帯は、その優れた磁気特性を発現させるために、予め所定の焼鈍熱処理を施す方法が一般に用いられている。焼鈍熱処理の条件は発現させたい磁気特性や非晶質合金の種類によって異なるが、概ね不活性雰囲気下において温度300〜500℃程度、時間0.1〜100時間程度の高温長時間で行われることが一般的である。ところが焼鈍熱処理によって優れた磁気特性を発現する反面、極めて脆弱な薄帯となり、物理的に取り扱いにくくなる問題を抱えている。
【0004】
この問題に対処する方法として、ポリイミド樹脂などの焼鈍温度に耐える耐熱性高分子化合物を接着剤として用い、非晶質合金薄帯を積層接着する方法が開示されている(特開昭58−175654)。この方法によれば、焼鈍と同時に耐熱性樹脂による接着積層ができるため、脆弱な薄帯を取り扱う問題を解決できる。
【0005】
しかし、片面または両面に耐熱樹脂層が形成された非晶質合金薄帯を積層接着して積層体を製造するに際し、積層体の表面に膨れが生じる問題があり、この問題を解決することが望まれている。
【0006】
【本発明が解決しようとする課題】
本発明の目的は、上記従来技術の問題点に鑑み、片面または両面に耐熱樹脂層が形成された非晶質合金薄帯を積層接着および焼鈍して積層体を製造するに際し、積層体の表面に膨れが生じない非晶質合金薄帯およびその製造方法を提供することにある。
【0007】
【課題を解決するための手段】
本発明者らは、前記課題を解決するために鋭意検討を重ねた結果、片面または両面に形成されている耐熱樹脂層中に含有される有機溶剤の量を所定量以下とすることにより、積層体を製造するに際して積層体の表面に膨れが生じないことを見出し、本発明を完成した。
【0008】
本発明は、片面または両面に耐熱樹脂層が形成された非晶質合金薄帯において、該耐熱樹脂が熱可塑性樹脂であり、該樹脂中に含有されている有機溶剤の量が該樹脂に対して0.5重量%以下であることを特徴とする非晶質合金薄帯を提供する。
【0009】
本発明は、熱可塑性耐熱樹脂または熱可塑性耐熱樹脂の前駆体が有機溶剤に溶解している溶液を非晶質合金薄帯の片面または両面に塗布し、該熱可塑性耐熱樹脂のガラス転移温度より40℃以上高い温度で有機溶剤を除去乾燥することを特徴とする、片面または両面に耐熱樹脂層が形成された非晶質合金薄帯の製造方法を提供する。
【0010】
本発明の望ましい態様の1つとして非晶質合金薄帯を積層させて製造される非晶質合金薄帯積層体を挙げることができる。
【0011】
さらに、本発明の非晶質合金薄帯積層体を含んで構成される磁気応用部品は本発明の態様の1つである。
【0012】
【発明の実施の形態】
本発明の非晶質合金薄帯は、片面または両面に耐熱樹脂層が形成された非晶質合金薄帯である。
【0013】
本発明において用いる非晶質合金薄帯は、軟磁性材料が対象となる。例えば、Fe系やCo系などの非晶質金属材料、Fe系やCo系などのナノ結晶質金属材料などが挙げられる。具体的には例えば、Fe系非晶質金属材料としては、Fe−Si−B系、Fe−B系、Fe−P−C系などのFe−半金属系非晶質金属材料や、Fe−Zr系、Fe−Hf系、Fe−Ti系などのFe−遷移金属系非晶質金属材料などを挙げることができ、またCo系非晶質金属材料としては、Co−Si−B系、Co−B系などの非晶質金属材料を挙げることができる。また、非晶質金属材料を熱処理によりナノサイズに結晶化させたナノ結晶質金属材料においては、Fe−Si−B−Cu−Nb系、Fe−B−Cu−Nb系、Fe−Zr−B−(Cu)系、Fe−Zr−Nb−B−(Cu)系、Fe−Zr−P−(Cu)系、Fe−Zr−Nb−P−(Cu)系、Fe−Ta−C系、Fe−Al−Si−Nb−B系、Fe−Al−Si−Ni−Nb−B系、Fe−Al−Nb−B系、Co−Ta−C系などを挙げることができる。これらはいずれも、特定の磁気特性を発現させるために、通常使用される前に所定の条件において焼鈍熱処理を施す。焼鈍熱処理の条件は用いる材料の種類や発現させたい磁気特性によって異なるが、非晶質金属材料では温度範囲が概ね300〜500℃、ナノ結晶質金属材料では温度範囲が概ね400〜700℃とするのが一般的である。
【0014】
本発明において用いる非晶質合金薄帯の厚さは、特に限定されるものではないが、5〜50ミクロンであることが好ましく、10〜30ミクロンであることがより好ましい。
【0015】
本発明において用いる耐熱樹脂は、熱可塑性を有する樹脂である。本発明の非晶質合金薄帯を積層接着して積層体とする際の熱処理条件によって必要な性能は異なるが、具体的には、ポリイミド系樹脂、ポリエーテルイミド系樹脂、ポリアミドイミド系樹脂、ポリアミド系樹脂、ポリスルホン系樹脂、ポリエーテルケトン系樹脂を好適に用いることができ、より具体的には化学式(1)〜(10)で表される繰り返し単位を主鎖骨格に有する樹脂を好適に用いることができる。
【0016】
【化1】

Figure 2004090391
【0017】
但し、化学式(1)においてaおよびbは、a+b=1、0≦a≦1、0≦b≦1を満たす数であり、XおよびYは、直接結合、エーテル結合、イソプロピリデン結合、スルフィド結合、スルホン結合、並びにカルボニル結合から選ばれる結合基で、同一でも異なっていても良い。また化学式(2)においてZは、直接結合、エーテル結合、イソプロピリデン結合、スルフィド結合、スルホン結合、並びにカルボニル結合から選ばれる結合基である。また化学式(6)においてcおよびdは、c+d=1、0≦c≦1、0≦d≦1を満たす数である。
【0018】
本発明の非晶質合金薄帯は、片面または両面に形成されている耐熱樹脂層中に含有されている有機溶剤の量が該樹脂に対して通常0.5重量%以下である。好ましくは、本発明の非晶質合金薄帯は、片面または両面に形成されている耐熱樹脂層中に含有されている有機溶剤の量が該樹脂に対して0.2重量%以下であり、より好ましくは0.1重量%以下である。含有されている有機溶剤の量が該樹脂に対して0.5重量%を超えると、非晶質合金薄帯を積層接着して積層体を製造した際に、積層体表面に膨れが生じる恐れがある。なお、含有されている有機溶剤量の下限は特に定められるものではなく、実質的に零であっても本発明の効果は十分に得ることができる。また有機溶剤の種類についても、特に定められるものではないが、本願で用いられている有機溶剤とは、本願発明の耐熱性樹脂やその前駆体、製造過程に用いられた一般的な有機溶剤はもちろん、本発明の焼鈍条件下で揮発性となる物質も含む概念で用いられている場合がある。また、複数種類の有機溶剤が含有される場合には、その合計量とする。
【0019】
本発明における樹脂層中に含有されている有機溶剤の定量は、FID型ガスクロマトグラフィーにより行う。サンプルをガスクロマトグラフィーに内蔵された加熱器にて、400℃で加熱して有機溶媒を分離し、予め作成しておいた種々の有機溶媒の検量線を用いて定量する。
【0020】
本発明の非晶質合金薄帯積層体の製造方法としては、熱可塑性耐熱樹脂または熱可塑性耐熱樹脂の前駆体が有機溶剤に溶解している溶液を非晶質合金薄帯の片面または両面に塗布し、該熱可塑性耐熱樹脂のガラス転移温度より40℃以上高い温度で有機溶剤を除去乾燥する方法を好適に用いることができる。有機溶剤を除去乾燥させる温度は、熱可塑性耐熱樹脂のガラス転移温度より50℃以上高い温度であることがより好ましく、60℃以上高い温度であることがさらに好ましい。例えば化学式(11)で表される繰り返し単位を主鎖骨格に有するポリアミド酸が20重量%溶解したN,N―ジメチルアセトアミド溶液を用いた場合、ポリアミド酸は化学式(12)で表される繰り返し単位を主鎖骨格に有するポリイミド樹脂となり、そのガラス転移温度は190℃であるため、有機溶剤を除去乾燥させる温度は230℃以上であり、240℃以上がより好ましく、250℃以上がさらに好ましい。有機溶剤を除去乾燥させる時間は、5秒以上であることが好ましく、15秒以上であることがより好ましい。
【0021】
【化2】
Figure 2004090391
【0022】
本発明の非晶質合金薄帯を用いることにより、膨れがない良好な非晶質合金薄帯積層体を製造することができ、この非晶質合金薄帯積層体は、それを含んで構成される磁気応用部品として好適に用いることができる。より具体的には、例えばインダクタンス、各種コイル、各種トランス、ノイズフィルター、磁気センサー、磁気ヘッド、アンテナ、電波吸収体、モーター、各種コア、配線基板に好適に用いることができる。
【0023】
【実施例】
以下、本発明を実施例により詳細に説明する。
【0024】
【合成例】
米国ハネウェル社製の非晶質合金薄帯Metglas2714A(元素比Co:Fe:Ni:Si:B=66:4:1:15:14)の片面に、化学式(11)で表される繰り返し単位を主鎖骨格に有するポリアミド酸が20重量%溶解した溶液(溶媒:N,N―ジメチルアセトアミド)を薄く塗布し、窒素流通下、温度130℃、時間1分の条件で、予備乾燥を行い、複合薄帯を得た。この薄帯を内径25ミリメートル、外径40ミリメートルに打ち抜き、リング状の複合薄帯を得た。なお、化学式(11)で表される繰り返し単位を主鎖骨格に有するポリアミド酸は、およそ200℃以上の加熱によりイミド化されて、化学式(12)で表される繰り返し単位を主鎖骨格に有するポリイミドとなる。化学式(12)で表される繰り返し単位を主鎖骨格に有するポリイミドのガラス転移温度は、DSC法(島津DSC−50)により測定したところ、190℃であった。
【0025】
【実施例1】
合成例で示したリング状の複合薄帯を、窒素流通下、温度250℃、時間15秒の条件で加熱した。得られたリング状の複合薄帯の一部をサンプルとして、残存する有機溶媒の量をFID型ガスクロマトグラフィー(島津GC−8A)を用いて測定した。サンプルをガスクロマトグラフィーに内蔵された加熱器にて、400℃で加熱して有機溶媒を分離し、予め作成しておいた種々の有機溶媒の検量線を用いて定量した。その結果、樹脂中に含有されている有機溶剤N,N−ジメチルアセトアミドの量は、樹脂に対して0.05重量%であった。このリング状の複合薄帯を5枚重ね合わせ、窒素流通下、圧力10MPa、温度250℃、時間30分の条件で積層接着して積層体を得た。次いで窒素流通下、無加圧、温度420℃、時間60分の条件で、積層体を焼鈍した。焼鈍後の積層体の表面には膨れがなく、良好な部品であった。結果をまとめて表1に示す。
【0026】
【実施例2〜4】
実施例1と同様にして、表1に示した条件で熱処理等を行い、評価した。結果を表1に示す。
【0027】
【比較例1〜2】
実施例1と同様にして、表1に示した条件で熱処理等を行い、評価した。結果を表1に示す。
【0028】
【表1】
Figure 2004090391
【0029】
【発明の効果】
本発明の非晶質合金薄帯は、片面または両面に耐熱樹脂層が形成された非晶質合金薄帯であり、積層接着および焼鈍して積層体を製造するに際し、積層体の表面に膨れが生じず、良好な積層体を製造することができる非晶質合金薄帯である。[0001]
[Industrial applications]
The present invention relates to an amorphous alloy ribbon having a heat-resistant resin layer formed thereon and a method for producing the same.
[0002]
[Prior art]
An amorphous alloy ribbon is an amorphous solid produced by rapidly cooling various metals from a molten state to a raw material, and is usually a ribbon having a thickness of about 0.01 to 0.1 mm. is there. In these amorphous alloy ribbons, the atoms have a random structure in which the arrangement is not regular, and have excellent characteristics as a soft magnetic material. In particular, a Co-based amorphous alloy ribbon containing a Co element is a material characterized by high magnetic permeability, and various magnetic application parts, such as inductance, various coils, various transformers, noise filters, magnetic sensors, magnetic heads, It is expected to be used in a wide range of fields such as antennas, radio wave absorbers, motors, various cores, and wiring boards.
[0003]
In order to exhibit the excellent magnetic properties of the amorphous alloy ribbon, a method of performing a predetermined annealing heat treatment in advance is generally used. Annealing heat treatment conditions vary depending on the magnetic properties and the type of amorphous alloy to be developed, but generally should be performed at a high temperature and a long time of about 300 to 500 ° C. for about 0.1 to 100 hours in an inert atmosphere. Is common. However, although excellent magnetic properties are exhibited by the annealing heat treatment, there is a problem that the strip becomes extremely brittle and becomes physically difficult to handle.
[0004]
As a method for addressing this problem, a method of laminating and bonding amorphous alloy ribbons using a heat-resistant polymer compound such as a polyimide resin that can withstand the annealing temperature is disclosed (JP-A-58-175654). ). According to this method, bonding and lamination with a heat-resistant resin can be performed at the same time as annealing, so that the problem of handling fragile ribbons can be solved.
[0005]
However, when producing a laminate by laminating and bonding an amorphous alloy ribbon having a heat-resistant resin layer formed on one or both surfaces, there is a problem that the surface of the laminate swells, and this problem can be solved. Is desired.
[0006]
[Problems to be solved by the present invention]
An object of the present invention is to provide a laminate by laminating and annealing an amorphous alloy ribbon having a heat-resistant resin layer formed on one side or both sides in view of the above-mentioned problems of the prior art, and producing a laminate. An object of the present invention is to provide an amorphous alloy ribbon in which no swelling occurs and a method for producing the same.
[0007]
[Means for Solving the Problems]
The present inventors have conducted intensive studies in order to solve the above-mentioned problems, and as a result, the amount of the organic solvent contained in the heat-resistant resin layer formed on one side or both sides is reduced to a predetermined amount or less, thereby laminating. The present inventors have found that no swelling occurs on the surface of the laminate when manufacturing the body, and have completed the present invention.
[0008]
The present invention provides an amorphous alloy ribbon having a heat-resistant resin layer formed on one or both surfaces, wherein the heat-resistant resin is a thermoplastic resin, and the amount of the organic solvent contained in the resin is relative to the resin. 0.5% by weight or less.
[0009]
The present invention applies a solution in which a thermoplastic heat-resistant resin or a precursor of a thermoplastic heat-resistant resin is dissolved in an organic solvent to one or both surfaces of an amorphous alloy ribbon, and calculates the glass transition temperature of the thermoplastic heat-resistant resin. Provided is a method for producing an amorphous alloy ribbon having a heat-resistant resin layer formed on one or both surfaces thereof, wherein an organic solvent is removed and dried at a temperature higher than 40 ° C.
[0010]
One of the desirable aspects of the present invention is an amorphous alloy ribbon laminate manufactured by laminating amorphous alloy ribbons.
[0011]
Furthermore, a magnetic application part including the amorphous alloy ribbon laminate of the present invention is one aspect of the present invention.
[0012]
BEST MODE FOR CARRYING OUT THE INVENTION
The amorphous alloy ribbon of the present invention is an amorphous alloy ribbon having a heat-resistant resin layer formed on one or both surfaces.
[0013]
The amorphous alloy ribbon used in the present invention is a soft magnetic material. For example, an amorphous metal material such as an Fe-based or Co-based material, and a nanocrystalline metal material such as an Fe-based or Co-based material can be used. Specifically, for example, as an Fe-based amorphous metal material, an Fe-semimetal-based amorphous metal material such as an Fe-Si-B-based, Fe-B-based, or Fe-PC-based material; Examples include Fe-transition metal-based amorphous metal materials such as Zr-based, Fe-Hf-based, and Fe-Ti-based materials. Examples of the Co-based amorphous metal materials include Co-Si-B-based and Co-based amorphous metal materials. And -B type amorphous metal materials. Further, in a nanocrystalline metal material obtained by crystallizing an amorphous metal material to a nano size by heat treatment, Fe-Si-B-Cu-Nb, Fe-B-Cu-Nb, Fe-Zr-B -(Cu) system, Fe-Zr-Nb-B- (Cu) system, Fe-Zr-P- (Cu) system, Fe-Zr-Nb-P- (Cu) system, Fe-Ta-C system, Fe-Al-Si-Nb-B system, Fe-Al-Si-Ni-Nb-B system, Fe-Al-Nb-B system, Co-Ta-C system and the like can be mentioned. Each of these is subjected to an annealing heat treatment under predetermined conditions before it is usually used in order to develop specific magnetic properties. The conditions of the annealing heat treatment vary depending on the type of material used and the magnetic properties to be developed, but the temperature range is approximately 300 to 500 ° C. for amorphous metal materials and approximately 400 to 700 ° C. for nanocrystalline metal materials. It is common.
[0014]
The thickness of the amorphous alloy ribbon used in the present invention is not particularly limited, but is preferably 5 to 50 microns, and more preferably 10 to 30 microns.
[0015]
The heat-resistant resin used in the present invention is a resin having thermoplasticity. The required performance varies depending on the heat treatment conditions when the amorphous alloy ribbons of the present invention are laminated and bonded to form a laminate, but specifically, a polyimide resin, a polyetherimide resin, a polyamideimide resin, Polyamide-based resins, polysulfone-based resins, and polyetherketone-based resins can be suitably used, and more specifically, resins having a repeating unit represented by chemical formulas (1) to (10) in the main chain skeleton are preferred. Can be used.
[0016]
Embedded image
Figure 2004090391
[0017]
However, in the chemical formula (1), a and b are numbers satisfying a + b = 1, 0 ≦ a ≦ 1, 0 ≦ b ≦ 1, and X and Y are a direct bond, an ether bond, an isopropylidene bond, a sulfide bond. , A sulfone bond and a carbonyl bond, which may be the same or different. In the chemical formula (2), Z is a bonding group selected from a direct bond, an ether bond, an isopropylidene bond, a sulfide bond, a sulfone bond, and a carbonyl bond. In the chemical formula (6), c and d are numbers satisfying c + d = 1, 0 ≦ c ≦ 1, and 0 ≦ d ≦ 1.
[0018]
In the amorphous alloy ribbon of the present invention, the amount of the organic solvent contained in the heat-resistant resin layer formed on one or both surfaces is usually 0.5% by weight or less based on the resin. Preferably, in the amorphous alloy ribbon of the present invention, the amount of the organic solvent contained in the heat-resistant resin layer formed on one or both surfaces is 0.2% by weight or less based on the resin. It is more preferably at most 0.1% by weight. When the amount of the contained organic solvent exceeds 0.5% by weight with respect to the resin, when the amorphous alloy ribbon is laminated and bonded to produce a laminate, the surface of the laminate may be swollen. There is. The lower limit of the amount of the organic solvent contained is not particularly limited. Even if the lower limit is substantially zero, the effect of the present invention can be sufficiently obtained. Also, the type of the organic solvent is not particularly limited, but the organic solvent used in the present application is a heat-resistant resin and its precursor of the present invention, a general organic solvent used in the production process is Of course, in some cases, the concept of the present invention is used with the concept including a substance that is volatile under the annealing conditions. When a plurality of types of organic solvents are contained, the total amount is used.
[0019]
The quantitative determination of the organic solvent contained in the resin layer in the present invention is performed by FID type gas chromatography. The sample is heated at 400 ° C. by a heater built in the gas chromatography to separate the organic solvent, and the sample is quantified using calibration curves of various organic solvents prepared in advance.
[0020]
As a method for producing an amorphous alloy ribbon laminate of the present invention, a solution in which a thermoplastic heat-resistant resin or a precursor of a thermoplastic heat-resistant resin is dissolved in an organic solvent is applied to one or both surfaces of the amorphous alloy ribbon. A method of applying and removing the organic solvent at a temperature higher than the glass transition temperature of the thermoplastic heat-resistant resin by 40 ° C. or more can be suitably used. The temperature at which the organic solvent is removed and dried is more preferably a temperature higher than the glass transition temperature of the thermoplastic heat-resistant resin by 50 ° C. or more, and further preferably a temperature higher by 60 ° C. or more. For example, when an N, N-dimethylacetamide solution in which 20% by weight of a polyamic acid having a repeating unit represented by the chemical formula (11) in the main chain skeleton is used, the polyamic acid is a repeating unit represented by the chemical formula (12) And a glass transition temperature of 190 ° C., the temperature for removing and drying the organic solvent is 230 ° C. or higher, preferably 240 ° C. or higher, more preferably 250 ° C. or higher. The time for removing and drying the organic solvent is preferably at least 5 seconds, more preferably at least 15 seconds.
[0021]
Embedded image
Figure 2004090391
[0022]
By using the amorphous alloy ribbon of the present invention, it is possible to produce a good amorphous alloy ribbon laminate without swelling, and the amorphous alloy ribbon laminate includes the same. It can be suitably used as a magnetic application part. More specifically, it can be suitably used for, for example, inductance, various coils, various transformers, noise filters, magnetic sensors, magnetic heads, antennas, radio wave absorbers, motors, various cores, and wiring boards.
[0023]
【Example】
Hereinafter, the present invention will be described in detail with reference to examples.
[0024]
[Synthesis example]
On one surface of an amorphous alloy ribbon Metglas2714A (element ratio Co: Fe: Ni: Si: B = 66: 4: 1: 15: 14) manufactured by Honeywell, USA, a repeating unit represented by the chemical formula (11) was added. A solution (solvent: N, N-dimethylacetamide) in which 20% by weight of a polyamic acid having a main chain skeleton was dissolved was thinly applied, and preliminarily dried under a flow of nitrogen at a temperature of 130 ° C. for a time of 1 minute. I got a ribbon. This ribbon was punched into an inner diameter of 25 mm and an outer diameter of 40 mm to obtain a ring-shaped composite ribbon. In addition, the polyamic acid having the repeating unit represented by the chemical formula (11) in the main chain skeleton is imidized by heating at about 200 ° C. or more, and has the repeating unit represented by the chemical formula (12) in the main chain skeleton. It becomes polyimide. The glass transition temperature of the polyimide having the repeating unit represented by the chemical formula (12) in the main chain skeleton was 190 ° C. as measured by the DSC method (Shimadzu DSC-50).
[0025]
Embodiment 1
The ring-shaped composite ribbon shown in the synthesis example was heated under a nitrogen flow at a temperature of 250 ° C. for 15 seconds. Using a part of the obtained ring-shaped composite ribbon as a sample, the amount of the remaining organic solvent was measured using FID type gas chromatography (Shimadzu GC-8A). The sample was heated at 400 ° C. with a heater built in the gas chromatography to separate the organic solvent, and the sample was quantified using calibration curves of various organic solvents prepared in advance. As a result, the amount of the organic solvent N, N-dimethylacetamide contained in the resin was 0.05% by weight based on the resin. Five such ring-shaped composite ribbons were superimposed and laminated and bonded under a flow of nitrogen under the conditions of a pressure of 10 MPa, a temperature of 250 ° C. and a time of 30 minutes to obtain a laminate. Next, the laminate was annealed under nitrogen flow under no pressure, at a temperature of 420 ° C., and for a time of 60 minutes. The surface of the laminated body after annealing did not swell and was a good part. The results are summarized in Table 1.
[0026]
[Examples 2 to 4]
In the same manner as in Example 1, heat treatment and the like were performed under the conditions shown in Table 1 and evaluated. Table 1 shows the results.
[0027]
[Comparative Examples 1-2]
In the same manner as in Example 1, heat treatment and the like were performed under the conditions shown in Table 1 and evaluated. Table 1 shows the results.
[0028]
[Table 1]
Figure 2004090391
[0029]
【The invention's effect】
The amorphous alloy ribbon of the present invention is an amorphous alloy ribbon in which a heat-resistant resin layer is formed on one or both surfaces, and when the laminate is manufactured by laminating and annealing, the surface of the laminate swells. This is an amorphous alloy ribbon capable of producing a good laminated body without generation of a thin film.

Claims (4)

片面または両面に耐熱樹脂層が形成された非晶質合金薄帯において、該耐熱樹脂が熱可塑性樹脂であり、該樹脂中に含有されている有機溶剤の量が該樹脂に対して0.5重量%以下であることを特徴とする非晶質合金薄帯。In the amorphous alloy ribbon having a heat-resistant resin layer formed on one or both surfaces, the heat-resistant resin is a thermoplastic resin, and the amount of the organic solvent contained in the resin is 0.5 to the resin. % By weight or less. 熱可塑性耐熱樹脂または熱可塑性耐熱樹脂の前駆体が有機溶剤に溶解している溶液を非晶質合金薄帯の片面または両面に塗布し、該熱可塑性耐熱樹脂のガラス転移温度より40℃以上高い温度で有機溶剤を除去乾燥することを特徴とする、片面または両面に耐熱樹脂層が形成された非晶質合金薄帯の製造方法。A solution in which a thermoplastic heat-resistant resin or a precursor of a thermoplastic heat-resistant resin is dissolved in an organic solvent is applied to one or both surfaces of an amorphous alloy ribbon, and is 40 ° C. or more higher than the glass transition temperature of the thermoplastic heat-resistant resin. A method for producing an amorphous alloy ribbon having a heat-resistant resin layer formed on one or both sides, wherein the organic solvent is removed by drying at a temperature. 上記請求項1または請求項2記載の非晶質合金薄帯を積層させて製造される非晶質合金薄帯積層体。An amorphous alloy ribbon laminate produced by laminating the amorphous alloy ribbon according to claim 1 or 2. 上記請求項3記載の非晶質合金薄帯積層体を含んで構成される磁気応用部品。A magnetic application component comprising the amorphous alloy ribbon laminate according to claim 3.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007105738A1 (en) * 2006-03-13 2007-09-20 National Institute For Materials Science Amorphous-metal composite material, process for producing the same, and article obtained by the same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007105738A1 (en) * 2006-03-13 2007-09-20 National Institute For Materials Science Amorphous-metal composite material, process for producing the same, and article obtained by the same
JP4900617B2 (en) * 2006-03-13 2012-03-21 独立行政法人物質・材料研究機構 Amorphous metal composite, method for producing the same, and article thereby

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