JPH0469401B2 - - Google Patents
Info
- Publication number
- JPH0469401B2 JPH0469401B2 JP13688583A JP13688583A JPH0469401B2 JP H0469401 B2 JPH0469401 B2 JP H0469401B2 JP 13688583 A JP13688583 A JP 13688583A JP 13688583 A JP13688583 A JP 13688583A JP H0469401 B2 JPH0469401 B2 JP H0469401B2
- Authority
- JP
- Japan
- Prior art keywords
- wound
- amorphous alloy
- magnetic core
- alloy ribbon
- winding
- 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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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F3/00—Cores, Yokes, or armatures
- H01F3/04—Cores, Yokes, or armatures made from strips or ribbons
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F1/00—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
- H01F1/01—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
- H01F1/03—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
- H01F1/12—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials
- H01F1/14—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys
- H01F1/147—Alloys characterised by their composition
- H01F1/153—Amorphous metallic alloys, e.g. glassy metals
- H01F1/15383—Applying coatings thereon
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Chemical & Material Sciences (AREA)
- Dispersion Chemistry (AREA)
- Manufacturing Cores, Coils, And Magnets (AREA)
Description
(ア) 技術分野
本発明は非晶質合金薄帯巻磁心及びその製造方
法に関するものである。
更に詳しく述べるならば、本発明は粒子加速器
等に用いられる高出力磁気スイツチであつて、ス
イツチング時間が短かい磁気スイツチに用いられ
る磁心に関するものである。
粒子加速器においては、磁心は10KHz以上にも
及ぶ高周波数で短いスイツチング時間で1GW以
上にも及ぶ高い出力のパルスを発生することが要
求される。
従来、粒子加速器用パルス発生器としては、サ
イラトロン等の高圧ガススイツチが用いられてい
るが、出力及びスイツチング時間が不満足であ
る。
これに対し、第1図に示されるようなキヤパシ
ターC1,C2…,Coと可飽和インダクターL1,L2
…,Loとから構成され、各キヤパシターのキヤ
パシタンスは相等しくまた各インダクターのイン
ダクタンスは、高次段ほどより小さく構成し、直
流電源を入力側に印加させてキヤパシターC1に
電荷が充電し、充電後、インダクターL1が飽和
に達して、そのインピーダンスが下がり、電荷は
キヤパシターC2へ流れ、そして、このような充
電と飽和をn段まで順次行うことによつて、原波
形のエネルギーを保ちながら、パルス巾を順次圧
縮し、パルス巾が短かい、高出力パルスを得る磁
気スイツチは公知である。
このような磁気スイツチにおける各段のインダ
クターL1,L2…,Loには磁心が用いられ、そし
て磁心としては下記のような特性が要求される。
まず、第1に、可飽和性が良好でなければなら
ないので、角型性が良好で、しかも飽和領域での
透磁率μsatが小さいことが必要である、この場
合、本発明者らの検討結果によればBr/B10(Br
は残留磁束密度、B10は100eでの磁束密度、第2
図参照)が0.7以上であることが好ましい。また、
μsatは要求される磁心体積に比例するので、μsat
が小さいほど磁心を小型化できる。そして、パル
ス巾の理論的最大圧縮係数は(μunsat/μsat)1/
2に比例するので(μunsatは不飽和領域での透磁
率)、μunsatとμsatとの差が大きいほど、LC回路
の使用段数が少なくなり、磁気スイツチが小型化
される。
第2には、インダクターは、第2図に示したB
−H曲線の−BrからBs(Bsは飽和磁束密度)ま
で励磁されるので、△Bs=|−Br|+Bsが大き
くなければならない。
第3には、磁心は10KHz程度以上の電流にて励
磁されるので、高周波下のエネルギー損失が小さ
くなければならない。
第4には、特性の経時変化が少ないことが必要
である。
次に、磁気スイツチ用磁心は巻磁心であること
に関連する問題点を説明する。
一般に磁気スイツチ用巻磁心では、高周波電流
が磁心に加えられる際瞬間的に磁束密度が変化
し、この変化程度に比例する大電圧が発生するた
めに、巻回層間で短絡が起こる危険がある。この
ような短絡を防止するためには、巻回層間を絶縁
する必要がある。そこで、巻回層間を絶縁する方
法を実施する際に、上記第1〜第4の要求特性が
劣化してはならない。
(イ) 従来技術
磁気スイツチ用磁心材料としては、フエライト
が汎用されているが、フエライトは、上記第1〜
第3の磁気特性の点で不十分であるので、磁心が
大型化するという欠点がある。
これに対し、非晶質磁性合金の薄帯も磁心材料
として実用化されてきている。一般に磁心材料と
して用いられているケイ素鋼板の場合は、高温焼
鈍にて表面にガラス質皮膜が形成され、かつ絶縁
皮膜が塗付焼付されている。しかし、このような
層間絶縁処理を行うための温度は高いために、こ
の技術を非晶質合金の層間絶縁に応用することは
できない。そこで、非晶質合金薄帯の層間絶縁を
行うためには、MgO等の絶縁材料を塗設するか、
ポリイミド、ポリエチレンテレフタレート、など
の絶縁物質からなる層を、非晶質合金薄帯の間に
介挿する必要がある。前者のMgO等の絶縁材料
を塗設する方法は、一般的に非晶質合金の薄帯の
両端が、鋭くとがつているため、絶縁材料をうま
く塗設することが難しく、ここから層間短絡し易
いので実用的ではない。
次に、非晶質合金の特性として、良好な磁気特
性を得るためには、結晶化温度以下でかつ約300
〜500℃の間で非晶質合金を熱処理する必要があ
る。なお、ポリイミド等は上記熱処理温度におい
て十分な耐熱性をもたないから、ポリイミド膜等
が非晶質合金薄帯間に介挿された状態で、熱処理
を行うことができない。よつて、非晶質合金薄帯
を熱処理し、そして次に絶縁物質層を該薄帯間に
介挿することが行われる。
本発明者は非晶質合金薄帯巻磁心の磁気特性、
特に△Bs=|−Br|+Bs、を良好にするために
は、非晶質合金薄帯を巻回状態で熱処理しなけれ
ばならず、また絶縁物質層介挿状態を特定しなけ
ればならないことを見出した。
(ウ) 発明の目的
本発明の目的は磁気特性が良好な非晶質合金巻
磁心及びその製造方法を提供することである。
(エ) 発明の構成
本発明に係る非晶質合金巻磁心は、非晶質合金
薄帯磁心であつて、前記非晶質合金薄帯は熱処理
された状態の巻き方向に巻回されており、また非
晶質合金薄帯の巻回層間を絶縁する絶縁膜が該巻
回層間に介挿されていることを特徴とする。
本発明に係る製法は、非晶質合金薄帯巻磁心の
製造方法において、前記非晶質合金薄帯の第1末
端を内側に第2末端を外側になるように巻回して
第1巻回体を作り、次に前記第1巻回体に熱処理
し、続いて前記非晶質合金薄体上に絶縁膜を配置
し、そして、前記第1末端が内側に、第2末端が
外側に位置する第2巻回体に、該非晶質合金薄帯
及び絶縁膜を巻回すること且つ第2巻回体の内径
の第1巻回体の内径と実質的に同一としたことを
特徴とする。
以下、本発明の構成要件を説明する。
非晶質合金薄帯巻磁心(以下、単に磁心と称す
る)の製造において、非晶質合金薄帯を結晶化温
度以下で熱処理する場合に、本発明者の実験によ
ると、非晶質合金薄帯が展延された状態で熱処理
されると、磁心製造のため熱処理薄帯を巻回する
ことによつて磁気特性が劣化することが分かつ
た。したがつて、上記熱処理は巻回された状態の
非晶質合金薄帯(第1巻回体)について行う必要
がある。
第3図に熱処理された状態の非晶質合金巻回体
1(第1巻回体)ならびにその内径d1、外径D1、
及び内側の第1末端1b、外側の第2末端1aを
示す。熱処理温度は通常約300〜約500℃、約30〜
約10時間の範囲内で行われ、具体的には非晶質合
金の組成によつて上記範囲内で最良の磁気的特
性、特に△Bsが得られるように温度及び条件が
選択される。
このような処理は、通常、例えば5Oe以上、特
に10Oe以上程度の磁場中にて、キユリー点以下
の温度で適当な時間加熱し、これを冷却、例えば
空冷することによつて行う。磁場中熱処理後は薄
帯面内の長手方向に異方性が付与される。なお、
このような熱処理の雰囲気は、空気中、真空中、
不活性ガス中、非酸化性ガス中等いずれであつて
もよい。非晶質合金巻回体1は、20μm以下の厚
さと、概ね10〜500mm、特に12.7〜127mm程度の巾
をもつ長尺の薄板を巻回してなる。この場合、厚
さが20μmをこえると、高周波でのエネルギー損
失が大きくなり、発熱量が大きくなつてしまう。
厚みは、特に5〜18μm、より好ましくは8〜
15μmである。
上述のように磁心の製造においては、層間絶縁
を行う必要があるが、絶縁膜が層間に絶縁膜が介
挿した状態で熱処理を行うことはできない。熱処
理後に絶縁膜2を非晶質合金薄帯の相間に介挿し
た磁心10(第2巻回体)第4図に示す。磁心1
0の外径D2は、絶縁膜2を層間に介挿したため
に、非晶質合金巻回体1の外径D2より、一般に
大きくなる(D2>D1)。本発明に係る磁心(第2
巻回体)においては、第1末端1b及び第2末端
1aが熱処理時と同様にそれぞれ内側及び外側に
位置していること及び磁心10の内径d2が非晶質
合金巻回体1(第1巻回体)の内径d1とほぼ等し
い(d1≒d2)ことが必要である。上記内径d2とd1
の関係がd2≫d1又はd2≪d1であり且つ/または第
1末端1b(第2末端1a)が外側(内側)に位
置すると本発明の磁心に比較して△Bsが著しく
低くなる。望ましくは△d=|d2−d1/d1|×100
(%)が0〜約+40%、−20%である。△d=0%
の場合、△Bsが最も高くなる。以下に、熱処理
された巻き方向と同じ方向及び逆方向に非晶質合
金薄帯を巻回することを、それぞれ順方向巻回及
び逆方向巻回という。
本発明の磁心においては順方向巻回が必須の構
成要件である。一方、熱処理工程と磁心絶縁膜を
層間に介挿する工程の間では一旦逆方向巻回を行
いあるいは非晶質合金薄帯を平坦に展延するなど
の工程を行つても、磁心が順方向巻回されておれ
ば逆方向巻回又は平坦展延によつては磁心の非晶
質合金薄帯の磁気特性は劣化しない。したがつて
非晶質合金薄帯の磁気特性は、熱処理と最終巻回
工程の間の巻回(展延)履歴には影響されず、一
方該薄帯は磁気特性良好な順方向巻回を記憶する
一種の形状記憶効果を有する。
次に、本発明方法による第2巻回体製造の具体
例を第5図を参照としつつ説明する。
第5図において、20は熱処理された巻回帯
(第1巻回体)1(第3図)を逆方向に巻回した
非晶質合金薄帯、21は絶縁膜を示し、これらは
巻枠22,23に巻もどし可能に巻付けられてい
る。24は非晶質合金薄帯20と、好ましくは
0.1〜25μmの厚さの絶縁膜21が交互に層を為す
ように巻回されてなる磁心を示す。なお、磁心2
を巻き取るとき、非晶質合金薄帯20及び絶縁膜
21には、適切な張力のもとで行なわれる必要が
ある。適切な張力の強さは、一般的には数gから
数十gである。
また、非晶質合金薄帯20の端部間では絶縁膜
21程度の間隙しかないために放電が発生する可
能性があるので、放電を防止するために絶縁膜2
1の幅は薄帯20の幅よりも大きくしなければな
らない。大気放電、誘起電圧、磁心の使用条件
(磁気スイツチ駆動条件)、非晶質合金薄帯のサイ
ズ、磁心サイズなどを考慮した計算上の絶縁膜の
幅広分(片側で)は数十μm程で良いわけである
が、実際の巻取り作業では振れがどうしても発生
してしまうために絶縁膜幅広分(片側で)は2mm
以上、好ましくは3ないし5mmにするのが望まし
い。
この場合、熱処理後に絶縁材料を非晶質合金薄
帯に塗設ないし被着してもよいが、絶縁性能を第
5図に示したものより劣る。
非晶質合金薄帯20の端部(第2末端)及び絶
縁膜21の端部は磁心24の最外部に、接着剤、
溶接、テープ等あるいは、巻枠等に設けられたか
しめ爪によつてかしめる等によつて固定される。
(オ) 実施例
厚さ15μm、巾25.4mmの非晶質合金薄帯であつ
て、組成が(Fe0.949 Mo0.051)78(Si0.591 B0.273
C0.091 P0.045)22のものを外径(D1−第3図)127
mm、内径(d1)76mmに巻回した第1巻回体を400
℃×2時間で300eの磁場中で熱処理したところ、
得られた△Bsは2.7Teslaであつた。次に第1巻
回体を、これと内径(d1)で逆向きに巻回したと
ころ得られた△Bs=1.9Teslaであつた。この場
合厚さ2μmのポリエチレンテレフタレート膜を
非晶質合金薄帯層間に介挿した。
次に、上記第1巻回体を順方向に巻回した第2
巻回体を作つた。この場合、厚さ2μmのポリエ
チレンテレフタレート膜を非晶質合金薄帯の層間
に介挿し、且つ第2巻回体の内径(d2)及び外径
(D2)を次表のように変化させた。それぞれの△
Bsを表中に示す。
(A) Technical Field The present invention relates to an amorphous alloy ribbon-wound magnetic core and a method for manufacturing the same. More specifically, the present invention relates to a magnetic core used in a high-power magnetic switch used in a particle accelerator or the like, and which has a short switching time. In particle accelerators, the magnetic core is required to generate high-power pulses of more than 1 GW at high frequencies of more than 10 KHz and short switching times. Conventionally, high-pressure gas switches such as thyratrons have been used as pulse generators for particle accelerators, but their output and switching time are unsatisfactory. On the other hand, capacitors C 1 , C 2 . . . , C o and saturable inductors L 1 , L 2 as shown in FIG.
..., L o , the capacitance of each capacitor is equal, and the inductance of each inductor is configured to be smaller as the stage increases, and a DC power is applied to the input side to charge the capacitor C1 , After charging, the inductor L 1 reaches saturation, its impedance decreases, and the charge flows to the capacitor C 2. By sequentially performing this charging and saturation up to n stages, the energy of the original waveform is maintained. However, a magnetic switch is known that sequentially compresses the pulse width to obtain a short pulse width and high output pulse. A magnetic core is used for each stage of inductors L 1 , L 2 . . . , Lo in such a magnetic switch, and the magnetic core is required to have the following characteristics. First, since saturability must be good, it is necessary to have good squareness and small magnetic permeability μsat in the saturation region. According to Br/B 10 (Br
is the residual magnetic flux density, B 10 is the magnetic flux density at 100e, the second
(see figure) is preferably 0.7 or more. Also,
Since μsat is proportional to the required core volume, μsat
The smaller the value, the more compact the magnetic core can be. The theoretical maximum compression factor for pulse width is (μunsat/μsat)1/
2 (μunsat is the magnetic permeability in an unsaturated region), the larger the difference between μunsat and μsat, the fewer stages the LC circuit uses and the smaller the magnetic switch becomes. Second, the inductor is B
Since the magnet is excited from -Br on the -H curve to Bs (Bs is the saturation magnetic flux density), △Bs=|-Br|+Bs must be large. Thirdly, since the magnetic core is excited with a current of about 10 KHz or higher, energy loss under high frequencies must be small. Fourthly, it is necessary that the characteristics change little over time. Next, problems associated with the fact that the magnetic core for a magnetic switch is a wound core will be explained. Generally, in a wound core for a magnetic switch, when a high frequency current is applied to the magnetic core, the magnetic flux density changes instantaneously, and a large voltage proportional to the extent of this change is generated, so there is a risk of short circuiting between the wound layers. In order to prevent such short circuits, it is necessary to insulate the winding layers. Therefore, when implementing the method of insulating the winding layers, the first to fourth required characteristics must not deteriorate. (a) Prior art Ferrite is commonly used as a magnetic core material for magnetic switches.
Since the third magnetic property is insufficient, there is a drawback that the magnetic core becomes large. On the other hand, ribbons of amorphous magnetic alloys have also been put into practical use as magnetic core materials. In the case of silicon steel sheets, which are generally used as magnetic core materials, a glassy film is formed on the surface by high-temperature annealing, and an insulating film is applied and baked. However, since the temperature required to perform such interlayer insulation treatment is high, this technique cannot be applied to interlayer insulation of amorphous alloys. Therefore, in order to perform interlayer insulation of the amorphous alloy ribbon, it is necessary to apply an insulating material such as MgO or
A layer of insulating material such as polyimide or polyethylene terephthalate must be interposed between the amorphous alloy ribbons. In the former method of applying an insulating material such as MgO, it is difficult to apply the insulating material well because both ends of the amorphous alloy ribbon are generally sharp, which can lead to interlayer short circuits. It is not practical because it is easy to do. Next, as a characteristic of amorphous alloys, in order to obtain good magnetic properties, the temperature must be below the crystallization temperature and about 300%
It is necessary to heat treat the amorphous alloy between ~500°C. Note that polyimide and the like do not have sufficient heat resistance at the above heat treatment temperature, so heat treatment cannot be performed with a polyimide film or the like interposed between the amorphous alloy ribbons. Therefore, the amorphous alloy ribbons are heat treated and then a layer of insulating material is interposed between the ribbons. The present inventor has discovered the magnetic properties of an amorphous alloy ribbon-wound core,
In particular, in order to improve △Bs = |-Br|+Bs, the amorphous alloy ribbon must be heat-treated in a wound state, and the state of interposition of the insulating material layer must be specified. I found out. (c) Object of the invention The object of the invention is to provide an amorphous alloy-wound core with good magnetic properties and a method for manufacturing the same. (D) Structure of the Invention The amorphous alloy wound magnetic core according to the present invention is an amorphous alloy ribbon magnetic core, and the amorphous alloy ribbon is wound in the winding direction in a heat-treated state. , and is characterized in that an insulating film is inserted between the wound layers of the amorphous alloy ribbon to insulate the wound layers. The manufacturing method according to the present invention is a method for manufacturing an amorphous alloy ribbon-wound magnetic core, in which the first end of the amorphous alloy ribbon is wound on the inside and the second end is on the outside. Next, the first wound body is heat-treated, and then an insulating film is placed on the amorphous alloy thin body, and the first end is located on the inside and the second end is located on the outside. The amorphous alloy ribbon and the insulating film are wound around a second winding body, and the inner diameter of the second winding body is substantially the same as the inner diameter of the first winding body. . Hereinafter, the constituent elements of the present invention will be explained. According to experiments conducted by the present inventor, when an amorphous alloy thin ribbon is heat-treated at a temperature below the crystallization temperature in the production of an amorphous alloy thin ribbon wound magnetic core (hereinafter simply referred to as a magnetic core), It has been found that when the ribbon is heat-treated in an expanded state, the magnetic properties deteriorate due to the winding of the heat-treated ribbon to produce a magnetic core. Therefore, the above heat treatment needs to be performed on the wound amorphous alloy ribbon (first wound body). FIG. 3 shows the amorphous alloy wound body 1 (first wound body) in a heat-treated state, its inner diameter d 1 , outer diameter D 1 ,
and an inner first end 1b and an outer second end 1a. Heat treatment temperature is usually about 300 to about 500℃, about 30 to
The temperature and conditions are selected to obtain the best magnetic properties, especially ΔBs, within the above range, depending on the composition of the amorphous alloy. Such treatment is usually carried out by heating at a temperature below the Curie point for an appropriate time in a magnetic field of, for example, 5 Oe or more, particularly 10 Oe or more, and then cooling, for example air cooling. After heat treatment in a magnetic field, anisotropy is imparted in the longitudinal direction within the ribbon surface. In addition,
The atmosphere for such heat treatment is air, vacuum,
It may be in an inert gas, a non-oxidizing gas, or the like. The amorphous alloy wound body 1 is formed by winding a long thin plate having a thickness of 20 μm or less and a width of about 10 to 500 mm, particularly about 12.7 to 127 mm. In this case, if the thickness exceeds 20 μm, energy loss at high frequencies will increase and the amount of heat generated will increase.
The thickness is particularly 5 to 18 μm, more preferably 8 to 18 μm.
It is 15 μm. As described above, in manufacturing a magnetic core, it is necessary to perform interlayer insulation, but heat treatment cannot be performed with an insulating film interposed between layers. FIG. 4 shows a magnetic core 10 (second wound body) with an insulating film 2 interposed between the phases of the amorphous alloy ribbon after heat treatment. magnetic core 1
0 is generally larger than the outer diameter D 2 of the amorphous alloy wound body 1 (D 2 >D 1 ) because the insulating film 2 is interposed between the layers. Magnetic core according to the present invention (second
In the amorphous alloy wound body 1 (wound body), the first end 1b and the second end 1a are located on the inside and outside, respectively, as in the heat treatment, and the inner diameter d 2 of the magnetic core 10 is It is necessary that the inner diameter (d 1 ≈d 2 ) is approximately equal to the inner diameter d 1 of the one-wound body (d 1 ≒d 2 ). Above inner diameter d 2 and d 1
If the relationship is d 2 ≫ d 1 or d 2 ≪ d 1 and/or the first end 1b (second end 1a) is located outside (inside), ΔBs is significantly lower than in the magnetic core of the present invention. Become. Preferably, Δd=|d 2 −d 1 /d 1 |×100 (%) is 0 to about +40%, −20%. △d=0%
In the case of , △Bs is the highest. Hereinafter, winding the amorphous alloy ribbon in the same direction and in the opposite direction to the heat-treated winding direction will be referred to as forward winding and reverse winding, respectively. Forward winding is an essential component of the magnetic core of the present invention. On the other hand, between the heat treatment process and the process of inserting the magnetic core insulating film between the layers, even if the process of winding in the opposite direction or flattening the amorphous alloy ribbon is performed, the magnetic core will not move in the forward direction. As long as it is wound, the magnetic properties of the amorphous alloy ribbon of the magnetic core will not deteriorate due to reverse winding or flat rolling. Therefore, the magnetic properties of the amorphous alloy ribbon are not affected by the winding (rolling) history between the heat treatment and the final winding process, while the ribbon can be wound in the forward direction with good magnetic properties. It has a kind of shape memory effect. Next, a specific example of manufacturing the second wound body by the method of the present invention will be described with reference to FIG. In FIG. 5, 20 is an amorphous alloy ribbon obtained by winding the heat-treated wound band (first wound body) 1 (FIG. 3) in the opposite direction, and 21 is an insulating film. It is unwoundly wound around the frames 22 and 23. 24 is an amorphous alloy ribbon 20, preferably
A magnetic core is shown in which insulating films 21 having a thickness of 0.1 to 25 μm are wound in alternating layers. In addition, magnetic core 2
When winding up, it is necessary to apply appropriate tension to the amorphous alloy ribbon 20 and the insulating film 21. Appropriate tension strength is generally from several grams to several tens of grams. Furthermore, since there is a gap between the ends of the amorphous alloy ribbon 20 that is only about the size of the insulating film 21, there is a possibility that discharge may occur.
The width of the ribbon 1 must be larger than the width of the ribbon 20. The calculated wide width of the insulating film (on one side) is approximately several tens of μm, taking into consideration atmospheric discharge, induced voltage, magnetic core usage conditions (magnetic switch drive conditions), size of amorphous alloy ribbon, magnetic core size, etc. This is good, but in actual winding work, runout inevitably occurs, so the wide insulating film (on one side) is 2 mm.
In view of the above, it is preferable to set the thickness to 3 to 5 mm. In this case, an insulating material may be coated or adhered to the amorphous alloy ribbon after heat treatment, but the insulating performance will be inferior to that shown in FIG. 5. The end (second end) of the amorphous alloy ribbon 20 and the end of the insulating film 21 are attached to the outermost part of the magnetic core 24 with an adhesive,
It is fixed by welding, tape, etc., or by caulking with caulking claws provided on the winding frame, etc. (e) Example An amorphous alloy ribbon with a thickness of 15 μm and a width of 25.4 mm, with a composition of (F e0.949 M o0.051 ) 78 (S i0.591 B 0.273
C 0.091 P 0.045 ) 22 with outer diameter (D 1 - Figure 3) 127
mm, the first wound body wound to an inner diameter (d 1 ) of 76 mm is 400 mm.
When heat treated in a magnetic field of 300e for 2 hours at ℃,
The obtained △Bs was 2.7 Tesla. Next, the first wound body was wound in the opposite direction with the inner diameter (d 1 ), and ΔBs=1.9 Tesla was obtained. In this case, a 2 μm thick polyethylene terephthalate film was inserted between the amorphous alloy ribbon layers. Next, a second winding body is formed by winding the first winding body in the forward direction.
I made a rolled body. In this case, a polyethylene terephthalate film with a thickness of 2 μm is inserted between the layers of the amorphous alloy ribbon, and the inner diameter (d 2 ) and outer diameter (D 2 ) of the second wound body are changed as shown in the following table. Ta. Each △
Bs is shown in the table.
【表】
第1表より△dが等しく大きくならない場合
に、高い△Bsが得られることが分かる。
(カ) 発明の効果
本発明によると、熱処理と巻回を伴う磁心の製
造において、△Bsが高い磁心を製造することが
できる。[Table] From Table 1, it can be seen that a high ΔBs can be obtained when Δd is not equally large. (F) Effects of the Invention According to the present invention, a magnetic core with a high ΔBs can be manufactured in manufacturing a magnetic core that involves heat treatment and winding.
第1図は磁気スイツチの等価回路、第2図は磁
心のBH曲線、第3図は第1巻回体の概念図、第
4図は第2巻回体の概念図、第5図は第2巻回体
を巻回する方法の概念図である。
1……非晶質合金巻回体(第1巻回体)、1a
……第2末端、1b……第1末端、2……絶縁
膜、10……磁心、20……非晶質合金薄帯、2
1……絶縁膜、24……磁心(第2巻回体)、2
6……張力調節ロール。
Figure 1 is the equivalent circuit of the magnetic switch, Figure 2 is the BH curve of the magnetic core, Figure 3 is a conceptual diagram of the first winding body, Figure 4 is a conceptual diagram of the second winding body, and Figure 5 is the conceptual diagram of the second winding body. It is a conceptual diagram of the method of winding a two-wound body. 1... Amorphous alloy wound body (first wound body), 1a
...Second end, 1b...First end, 2...Insulating film, 10...Magnetic core, 20...Amorphous alloy ribbon, 2
1...Insulating film, 24...Magnetic core (second winding body), 2
6...Tension adjustment roll.
Claims (1)
合金薄帯は熱処理された状態の巻き方向に巻回さ
れており、また非晶質合金薄帯の巻回層間を絶縁
する絶縁膜が該巻回層間に介挿されていることを
特徴とする非晶質合金薄帯巻磁心。 2 非晶質合金薄帯巻磁心の製造方法において、
前記非晶質合金薄帯の第1末端を内側に第2末端
を外側になるように巻回して第1巻回体を作り、
次に前記第1巻回体に熱処理し、続いて前記非晶
質合金薄体上に絶縁膜を配置し、そして、前記第
1末端が内側に、第2末端が外側に位置する第2
巻回体に該非晶質合金薄帯及び絶縁膜を巻回する
こと、 且つ第2巻回体の内径の第1巻回体の内径と実
質的に同一としたことを特徴とする非晶質合金薄
帯磁心の製造方法。[Scope of Claims] 1. An amorphous alloy ribbon-wound magnetic core, wherein the amorphous alloy ribbon is wound in the winding direction of a heat-treated state, and the amorphous alloy ribbon is wound in a winding direction in a heat-treated state. An amorphous alloy ribbon-wound magnetic core characterized in that an insulating film for insulating between the wound layers is interposed between the wound layers. 2. In the method for manufacturing an amorphous alloy ribbon-wound core,
creating a first wound body by winding the amorphous alloy ribbon so that the first end is on the inside and the second end is on the outside;
Next, the first wound body is heat-treated, and then an insulating film is disposed on the amorphous alloy thin body, and a second wound body is heated, and the first end is located inside and the second end is located outside.
An amorphous material characterized in that the amorphous alloy ribbon and the insulating film are wound around a wound body, and the inner diameter of the second wound body is substantially the same as the inner diameter of the first wound body. Method for producing alloy thin ribbon magnetic core.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13688583A JPS6030103A (en) | 1983-07-28 | 1983-07-28 | Amorphous alloy wound core and manufacture of the same |
| US06/538,886 US4558297A (en) | 1982-10-05 | 1983-10-04 | Saturable core consisting of a thin strip of amorphous magnetic alloy and a method for manufacturing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13688583A JPS6030103A (en) | 1983-07-28 | 1983-07-28 | Amorphous alloy wound core and manufacture of the same |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7097026A Division JP2594776B2 (en) | 1995-04-21 | 1995-04-21 | Manufacturing method of amorphous alloy wound core |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6030103A JPS6030103A (en) | 1985-02-15 |
| JPH0469401B2 true JPH0469401B2 (en) | 1992-11-06 |
Family
ID=15185822
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13688583A Granted JPS6030103A (en) | 1982-10-05 | 1983-07-28 | Amorphous alloy wound core and manufacture of the same |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6030103A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS636822A (en) * | 1986-06-26 | 1988-01-12 | Toshiba Corp | Manufacture of mound core |
| JPH07123088B2 (en) * | 1986-11-25 | 1995-12-25 | 松下電工株式会社 | Power indicator |
-
1983
- 1983-07-28 JP JP13688583A patent/JPS6030103A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6030103A (en) | 1985-02-15 |
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