JPH08227816A - Amorphous wound core - Google Patents

Amorphous wound core

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Publication number
JPH08227816A
JPH08227816A JP27526295A JP27526295A JPH08227816A JP H08227816 A JPH08227816 A JP H08227816A JP 27526295 A JP27526295 A JP 27526295A JP 27526295 A JP27526295 A JP 27526295A JP H08227816 A JPH08227816 A JP H08227816A
Authority
JP
Japan
Prior art keywords
iron core
block
core
amorphous
wound
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.)
Granted
Application number
JP27526295A
Other languages
Japanese (ja)
Other versions
JP2776337B2 (en
Inventor
Tatsu Saito
達 斉藤
Shuya Hagiwara
修哉 萩原
Masaru Higaki
勝 檜垣
Shoyu Yamaguchi
彰宥 山口
Masaru Sakamoto
勝 坂本
Koji Yamanaka
功治 山中
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP7275262A priority Critical patent/JP2776337B2/en
Publication of JPH08227816A publication Critical patent/JPH08227816A/en
Application granted granted Critical
Publication of JP2776337B2 publication Critical patent/JP2776337B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

PURPOSE: To increase a productivity and magnetic characteristics of a core by forming the core in such a structure that nearly rectangular blocks which are made by winding thin belts in the stacking direction in a specified thickness and which have specified outer diameters are substantially adhered tightly to each other. CONSTITUTION: An amorphous magnetic alloy-made thin belt 2 is wound from a material hoop 4 around an iron block 3 which is nearly square and has a specified size. By this method, a set of nearly square-shaped three iron blocks 3a, 3b, and 3c, each of which has curved sections only at four corners, are adhered tightly at linear sections. At the four corners, nearly crescent-shaped spaces 7 are formed between the iron blocks 3a, 3b, and 3c. By this, over- tightening is prevented at the corners of a core and thereby the transmission of excess compressive force to the inside of a core window can be prevented and the deterioration in characteristics of the amorphous magnetic alloy-made thin belts can be remarkably lessened.

Description

【発明の詳細な説明】 【0001】 【発明の利用分野】本発明は非晶質磁性合金巻鉄心に関
するものである。 【0002】 【発明の背景】最近、非晶質磁性合金の薄帯を用いて変
圧器などの誘導電器の鉄心を構成し、従来の珪素鋼板の
ものに比べ大幅な鉄損低減を図る試みが盛んに行なわれ
ている。この非晶質磁性合金の薄帯は金属(Fe,Co
など)と非金属元素(B,Siなど)との融体をノズル
から高速回転するドラムに噴射・超急冷し製造されるの
で、厚さが約30μmと非常に薄く、かつ硬くて脆い性
質を有している。このような性質の非晶質磁性合金の薄
帯を用いて積層鉄心を製作することは通常容易でないた
め、一般に巻鉄心として用いられることが多いが、急冷
したままでは大きな残留ひずみがあり本来の低鉄損特性
が十分に発揮できないので、必ず事前に焼鈍が行なわれ
ている。この際に180度磁区を整列させるため、巻鉄
心の周方向に磁界をかけ乍ら行なわれている。 【0003】このようにして製作される非晶質磁性合金
の薄帯の巻鉄心は特開昭59−27511号公報や図1
0にその例が示されているように、鉄心ブロック1aか
ら1gが組み合わされており、その脚部とヨーク部との
一部が直線で他が曲線となり、しかも曲線部の半径が外
周部ほど大きくなるほぼ小判形で、その断面形状は図1
1に示されているようにほぼ円形をしているものが多か
った。 【0004】このような構造で容量が数10kVAから
数100kVAの非晶質磁性合金の薄帯の巻鉄心を製作
しようとすると、板厚が約30μmの薄帯では数千回か
ら数万回巻回しなければならない。このため図10の曲
線部で過大な巻締り現象が起き、図中矢印表示の圧縮力
Fが鉄心窓内方向に働くので、応力に敏感な非晶質磁性
合金の薄帯の特性を著しく損なう。 【0005】また、非晶質磁性合金の薄帯で大形の巻鉄
心を製作しようとすると、焼鈍の点でも大きな問題が生
じてくる。通常の焼鈍では温度350から400℃の不
活性ガス中で1から2時間保持される条件で行なわれる
が、大形の巻鉄心ではこのような雰囲気を作る焼鈍炉自
身が大形化してしまうのみならず、巻鉄心各部の温度分
布がどうしても不均一となる。このため巻鉄心の外層側
では過焼鈍、内部では不足焼鈍となり、非晶質磁性合金
の薄帯の本来の低鉄損特性を十分引き出せず、これらの
点が非晶質合金の薄帯を使用して大形の巻鉄心を実現さ
せる上での障害となっていた。 【0006】 【発明の目的】本発明は以上の点に鑑みなされたもので
あり、生産性及び磁気特性に優れた非晶質巻鉄心を提供
することを目的とするものである。 【0007】 【発明の概要】すなわち本発明は、非晶質磁性合金の薄
帯が巻回されて略矩形状に形成された非晶質巻鉄心にお
いて、薄帯が積層方向に所定の厚さで巻回されて所定の
外径を有する略矩形状の第1のブロックと、薄帯が積層
方向に所定の厚さで巻回されて第1のブロックの外形と
ほぼ等しい内径を有する略矩形状の第2のブロックを少
なくとも備え、第1のブロックの外側に第2のブロック
を実質的に密着させて構成されたことを特徴とするもの
である。 【0008】好ましい実施態様においては、第1のブロ
ックと第2のブロックは積層方向の厚さが実質的に同一
に形成される。 【0009】他の好ましい実施態様においては、第2の
ブロックの積層方向の厚さは第1のブロックの積層方向
の厚さより大となるよう形成される。 【0010】4.さらに好ましい実施態様においては、
第1のブロックと第2のブロックはそれぞれのブロック
の内側形状に沿って配設されて薄帯より剛性のある剛性
部材を有する。 【0011】 【発明の実施例】以下、図示した実施例に基づいて本発
明を説明する。図1(A),(B),(C)から図5に
は本発明の一実施例が示されている。なお従来と同じ部
品には同じ符号を付したので説明を省略する。本実施例
では巻鉄心を非晶質磁性合金の薄帯2の積層方向に分割
し、かつ所定の形状に巻取りおよび焼鈍した複数の鉄心
ブロック3a,3b,3cで構成した。このようにする
ことにより巻鉄心は薄帯2の積層方向に分割し、かつ所
定の形状に巻取りおよび焼鈍した複数の鉄心ブロック3
a,3b,3cで構成されるようになって、巻締り現象
および不均一焼鈍が防止されるようになり、非晶質磁性
合金の薄帯2の有する低鉄損特性を十分に確保できるこ
とを可能とした非晶質磁性合金巻鉄心を得ることができ
る。 【0012】すなわち図1(A),(B),(C)の
(A)に示されているように、非晶質磁性合金の薄帯2
を素材フープ4からほぼ四角形の所定寸法の鉄心ブロッ
ク3(3a,3b,3c)に巻回形成する。次いで同図
(B)に示されているように、所定寸法に巻回形成した
鉄心ブロック3に励磁コイル5を巻回して直流または交
流の電流を流し、鉄心ブロック3内に磁束を流し乍ら焼
鈍する。この際に素材の酸化を防ぐために不活性ガスを
充満した容器6中で焼鈍する。このように夫々巻回・焼
鈍した鉄心ブロック3a,3b,3cを同図(C)に示
されているように、必要な電気絶縁材や寸法調整用スペ
ーサ等を介して組み立てる。このように夫々別個に巻回
・焼鈍した鉄心ブロック3a,3b,3cを組み立てる
が、これらの鉄心ブロック3a,3b,3cを図2にも
示されているように四隅でのみ曲線となる相似形とし、
曲線部の内径Ri,外径R0および積層厚さtをほぼ同
一にした。 【0013】このようにすることにより巻鉄心は図3に
も示されているように、曲線部が四隅にのみ見られるほ
ぼ四角形の3組の鉄心ブロック3a,3b,3cが直線
部で密着し、四隅では各鉄心ブロック3a,3b,3c
間で三日月状に近い形状の空隙7が形成されるようにな
って、巻鉄心隅部での巻締り現象が防止されるようにな
り、巻鉄心窓内側への過大な圧縮力の伝達を阻止するこ
とができ、非晶質磁性合金の薄帯の特性劣化が大幅に緩
和できる。また、3個の鉄心ブロック3a,3b,3c
は上述のように夫々別個に焼鈍したので、一体で焼鈍し
た場合に問題となる巻鉄心各部の温度分布の不均一によ
る過焼鈍や不足焼鈍がなくなり、非晶質磁性合金の薄帯
に要求される厳しい焼鈍温度条件を満足し、特性の低下
を未然に防止することができる。 【0014】そしてまた、各鉄心ブロック3a,3b,
3cが図4および図5にも示されているように直線部で
は密着し、隅部の曲線部では空隙7が発生するので、そ
の空間寸法gの数だけ鉄心幅が見掛上広がるようにな
る。従って、この空隙7に治具などを配して鉄心ブロッ
ク3a,3b,3cの組み立てを容易にすることがで
き、この空隙7に部材を挿入して鉄心の特性を劣化する
ような応力がかからないように支持することもできる。
更にこの空隙7をそのままとした場合でも、この空隙7
を介して十分な油冷却や空気冷却をすることができるよ
うになり、通常問題となる鉄心内部の発熱を効率よく除
去することができる。 【0015】なお、本実施例では、鉄心ブロック3a,
3b,3cの曲線部の内径Ri,外径R0および積層厚
さtをほぼ同一にした場合について説明したが、これの
みに限るものではなく、曲線部の内径Riのみをほぼ同
一にしても、各鉄心ブロック3a,3b,3c間の四隅
に三日月状に近い形状の空隙7を形成することができ、
前述の場合と同様な作用効果を奏することができる。こ
の場合に鉄心ブロック3a,3b,3cはその角部が曲
線となるほぼ四角形のほぼ相似形にされることは云うま
でもない。また、鉄心の分割個数(鉄心ブロック数)、
その巻厚、内外径などは巻鉄心の仕様,容量により適宜
選択することができる。 【0016】このように本実施例によれば次に述べるよ
うな効果を奏することができる。 【0017】(1)同一幅の鉄心ブロックを曲線部でほ
ぼ同一な内径,外径を有するほぼ四角形に巻取るので、
必要な治具,行程が統一され、作業性が大幅に向上す
る。 【0018】(2)鉄心(薄帯)の巻回数が鉄心ブロッ
クの分割個数だけ減るので、従来問題視されていた巻締
り現象が大幅に緩和され、鉄損特性の低下が防止でき
る。 【0019】(3)鉄心が分割されるので、焼鈍がし易
く、鉄心中の温度むらによる局部的な過焼鈍や不足焼鈍
がなくなり、非晶質磁性合金の薄帯の本来の低鉄損特性
を発揮させることができる。 【0020】(4)鉄心四隅に空隙を形成することがで
きるので、この空隙を利用して鉄心の組み立てや支持、
更に鉄心内部の冷却などを効率よく行なうことができ
る。 【0021】図6には本発明の他の実施例が示されてい
る。本実施例では3組の鉄心ブロック3a,3b,3c
の内側に、非晶質磁性合金の薄帯より剛性のある剛性部
材8を内側の形状に沿って配設した。このようにするこ
とにより巻鉄心の機械的強度を前述の場合よりも向上さ
せることができる。 【0022】すなわち現在の非晶質磁性合金の薄帯の厚
さが約30μmと薄く、機械的強度が弱いために鉄心ブ
ロック3a,3b,3cを組み立てる場合に変形するこ
とや、十分な組立精度を確保できない問題を解決するも
ので、剛性部材8の材質としては非晶質磁性合金の薄帯
と成分的に近く、かつ剛性のある例えば珪素鋼帯などが
考えられる。 【0023】図7には本発明の更に他の実施例が示され
ている。本実施例では同一鉄心幅でその巻厚(積層厚
さ)が大となる場合には鉄心ブロック3b1,3b2の
ように鉄心を分割し、その間に空隙7を形成した。この
場合にも巻厚が大となる部分に空隙7が形成されるよう
になって、上述の場合と同様な作用効果を奏することが
できる。 【0024】すなわちこれまでの実施例では同一鉄心幅
毎に鉄心を分割した(鉄心ブロックを形成した)が、本
実施例ではこれまでの例と異なり、同一鉄心幅でもその
巻厚が大となる場合は、その巻厚の大きい部分を鉄心ブ
ロック3b1,3b2のように分割し、空隙7を形成す
るようにしたもので、鉄心が大形化する場合に特に有効
である。またこれまでの実施例では鉄心を積層方向にの
み分割した例を示したが、現状の非晶質磁性合金の薄帯
では最大鉄心幅が200mm程度が限度であることを考
えると、所定の鉄心幅とするには幅方向に鉄心を組合わ
せなければならない。このような場合においても実施例
で示したのと同様な構成が当然可能である。 【0025】図8には本発明の更に他の実施例が示され
ている。本実施例では鉄心ブロック3a,3b,3cの
内側に、非晶質磁性合金の薄帯より機械的強度にすぐれ
た鋼帯9を配設した。そしてこの鋼帯9を非晶質磁性合
金の通常の厚さ30μmよりも数倍から数10倍厚く、
機械的強度にすぐれた非晶質磁性合金で形成した。この
ようにすることにより各鉄心ブロック3a,3b,3c
の内側で大きくなる巻締り現象による鉄心の変形を防止
することができると共に、各鉄心ブロック3a,3b,
3cの組み立てを容易にすることができる。なお本実施
例では鋼帯9を各鉄心ブロック3a,3b,3cの内側
に極く僅か(積層厚さtに対して)配設したが、その割
合は各鉄心ブロック3a,3b,3cの積層厚さ(巻厚
さ)tと巻締りによる応力の程度とにより、適宜その配
設量が決定される。 【0026】図9には本発明の更に他の実施例が示され
ている。本実施例では鉄心ブロック3a,3b,3cの
内側に、絶縁皮膜を有し、かつ機械的強度にすぐれた非
晶質磁性合金10を配設した。このようにすることによ
り各鉄心ブロック3a,3b,3c間の電気的絶縁を確
保することができ、鉄心ブロック3a,3b,3c間を
流れるうず電流による鉄損の増加を防止することができ
る。 【0027】 【発明の効果】本発明によれば生産性及び磁気特性に優
れた非晶質巻鉄心を得ることができる。
Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an amorphous magnetic alloy wound iron core. BACKGROUND OF THE INVENTION Recently, an attempt has been made to construct an iron core of an induction electric appliance such as a transformer by using a ribbon of an amorphous magnetic alloy, and to significantly reduce the iron loss as compared with a conventional silicon steel sheet. It is being actively conducted. The ribbon of this amorphous magnetic alloy is made of metal (Fe, Co
Etc.) and non-metallic elements (B, Si, etc.) are sprayed from a nozzle onto a drum that rotates at high speed and are super-cooled to produce a very thin, approximately 30 μm thick, hard and brittle property. Have Since it is usually not easy to manufacture a laminated core using a ribbon of an amorphous magnetic alloy having such a property, it is generally used as a wound core, but if it is rapidly cooled, there is a large residual strain and the original Since low iron loss characteristics cannot be fully exhibited, annealing is always performed in advance. At this time, in order to align the 180 degree magnetic domains, a magnetic field is applied in the circumferential direction of the wound core. Amorphous magnetic alloy thin ribbon winding cores manufactured in this manner are disclosed in Japanese Patent Laid-Open No. 59-27511 and FIG.
As shown in Fig. 0, the iron core blocks 1a to 1g are combined, a part of the leg and the yoke part is a straight line and the other is a curve, and the radius of the curved part is closer to the outer peripheral part. It is almost oval in shape and its cross-sectional shape is shown in Figure 1.
Most of them were almost circular as shown in 1. When it is attempted to manufacture a wound core of a ribbon of amorphous magnetic alloy having a capacity of several tens kVA to several hundreds kVA with such a structure, a thin ribbon having a plate thickness of about 30 μm is wound several thousand to tens of thousands of times. I have to turn. For this reason, an excessive winding tightening phenomenon occurs in the curved portion of FIG. 10, and the compressive force F indicated by the arrow in the drawing acts in the inward direction of the iron core window, so that the characteristics of the ribbon of the amorphous magnetic alloy, which is sensitive to stress, is significantly impaired. . In addition, if a large-sized wound iron core is manufactured by using a ribbon of an amorphous magnetic alloy, a big problem also occurs in terms of annealing. Normal annealing is carried out under the condition that the temperature is maintained in an inert gas at a temperature of 350 to 400 ° C for 1 to 2 hours, but with a large wound iron core, the annealing furnace itself that creates such an atmosphere becomes large. Inevitably, the temperature distribution of each part of the wound iron core will be nonuniform. Therefore, the outer layer side of the wound core is over-annealed and the inner side is under-annealed, and the original low iron loss characteristics of the amorphous magnetic alloy ribbon cannot be sufficiently drawn out. Then, it was an obstacle to the realization of a large wound iron core. SUMMARY OF THE INVENTION The present invention has been made in view of the above points, and an object of the present invention is to provide an amorphous wound iron core excellent in productivity and magnetic characteristics. SUMMARY OF THE INVENTION That is, according to the present invention, in an amorphous winding iron core formed by winding a ribbon of an amorphous magnetic alloy into a substantially rectangular shape, the ribbon has a predetermined thickness in the stacking direction. A first block having a substantially rectangular shape and having a predetermined outer diameter, and a substantially rectangular block having a predetermined thickness in the laminating direction and having an inner diameter substantially equal to the outer shape of the first block. At least a second block having a shape is provided, and the second block is substantially in close contact with the outside of the first block. In a preferred embodiment, the first block and the second block are formed to have substantially the same thickness in the stacking direction. In another preferred embodiment, the thickness of the second block in the stacking direction is formed to be larger than the thickness of the first block in the stacking direction. 4. In a further preferred embodiment,
The first block and the second block have a rigid member that is arranged along the inner shape of each block and is stiffer than the ribbon. BEST MODE FOR CARRYING OUT THE INVENTION The present invention will now be described based on the illustrated embodiments. 1 (A), (B), (C) to FIG. 5 show an embodiment of the present invention. The same parts as those in the related art are denoted by the same reference numerals, and the description thereof will be omitted. In this embodiment, the wound core is divided into a plurality of amorphous magnetic alloy ribbons 2 in the stacking direction, and is composed of a plurality of core blocks 3a, 3b and 3c which are wound and annealed into a predetermined shape. By doing so, the wound core is divided in the stacking direction of the ribbons 2, and the plurality of core blocks 3 wound and annealed into a predetermined shape are formed.
Since it is composed of a, 3b and 3c, the winding tightening phenomenon and the non-uniform annealing can be prevented, and the low iron loss characteristic of the ribbon 2 of the amorphous magnetic alloy can be sufficiently secured. It is possible to obtain a possible amorphous magnetic alloy wound iron core. That is, as shown in (A) of FIGS. 1A, 1B, and 1C, a ribbon 2 of amorphous magnetic alloy is used.
Is wound from the material hoop 4 and wound around an iron core block 3 (3a, 3b, 3c) having a substantially rectangular shape and a predetermined size. Then, as shown in FIG. 2B, the exciting coil 5 is wound around the iron core block 3 formed to have a predetermined size, and a direct current or an alternating current is passed through the iron core block 3 to flow a magnetic flux. Anneal. At this time, the material is annealed in a container 6 filled with an inert gas in order to prevent the material from being oxidized. The iron core blocks 3a, 3b and 3c thus wound and annealed are assembled through necessary electric insulating materials and spacers for adjusting dimensions as shown in FIG. In this way, the iron core blocks 3a, 3b, 3c which are individually wound and annealed are assembled, and the iron core blocks 3a, 3b, 3c are similar to each other, as shown in FIG. age,
The inner diameter Ri, the outer diameter R0, and the laminated thickness t of the curved portion are made substantially the same. By doing so, as shown in FIG. 3, in the wound iron core, three sets of substantially quadrangular iron core blocks 3a, 3b, 3c whose curved portions are seen only at the four corners adhere to each other at the straight portions. , Core blocks 3a, 3b, 3c at the four corners
A space 7 with a shape close to a crescent shape is formed between the winding cores to prevent the winding tightening phenomenon at the corners of the winding core, preventing the transmission of excessive compressive force to the inside of the winding core window. Therefore, the characteristic deterioration of the ribbon of the amorphous magnetic alloy can be remarkably alleviated. Also, three core blocks 3a, 3b, 3c
Since they were annealed separately as described above, over-annealing and under-annealing due to the uneven temperature distribution of each part of the wound iron core, which is a problem when annealed integrally, is eliminated, and it is required for the amorphous magnetic alloy ribbon. Satisfactory annealing temperature conditions can be satisfied and deterioration of properties can be prevented. Further, each core block 3a, 3b,
As shown in FIGS. 4 and 5, 3c closely adheres to each other in a straight line portion and a void 7 is generated in a curved portion in a corner, so that the core width is apparently widened by the number of the space dimension g. Become. Therefore, a jig or the like can be arranged in the space 7 to facilitate the assembly of the iron core blocks 3a, 3b, 3c, and no stress that would deteriorate the characteristics of the iron core by inserting a member into the space 7 is applied. Can also be supported.
Further, even when the void 7 is left as it is, the void 7
Thus, sufficient oil cooling and air cooling can be performed through the heat generation, and heat generation inside the iron core, which is usually a problem, can be efficiently removed. In this embodiment, the iron core blocks 3a,
Although the case where the inner diameter Ri, the outer diameter R0 and the laminated thickness t of the curved portions 3b and 3c are substantially the same has been described, the present invention is not limited to this, and only the inner diameter Ri of the curved portion may be substantially the same. Voids 7 having a shape close to a crescent shape can be formed at the four corners between the core blocks 3a, 3b, 3c,
It is possible to achieve the same effect as the above case. In this case, it goes without saying that the iron core blocks 3a, 3b, 3c are formed in a substantially quadrangular shape having curved corners. Also, the number of iron core divisions (number of iron core blocks),
The winding thickness, inner and outer diameters, etc. can be appropriately selected according to the specifications and capacity of the wound core. As described above, according to this embodiment, the following effects can be obtained. (1) Since the iron core block having the same width is wound around the curved portion into a substantially square shape having substantially the same inner diameter and outer diameter,
Necessary jigs and processes are unified and workability is greatly improved. (2) Since the number of windings of the iron core (thin band) is reduced by the number of divisions of the iron core block, the winding tightening phenomenon, which has been regarded as a problem in the past, is greatly alleviated, and the deterioration of iron loss characteristics can be prevented. (3) Since the iron core is divided, it is easy to anneal, local over-annealing and under-annealing due to temperature unevenness in the iron core are eliminated, and the original low iron loss characteristic of the ribbon of the amorphous magnetic alloy is eliminated. Can be demonstrated. (4) Since voids can be formed at the four corners of the iron core, the voids can be used to assemble and support the iron core,
Further, the inside of the iron core can be cooled efficiently. FIG. 6 shows another embodiment of the present invention. In this embodiment, three sets of iron core blocks 3a, 3b, 3c
A rigid member 8 having a rigidity higher than that of a ribbon of an amorphous magnetic alloy was arranged inside the above, along the inner shape. By doing so, the mechanical strength of the wound core can be improved as compared with the case described above. That is, since the thin ribbon of the present amorphous magnetic alloy is as thin as about 30 μm and its mechanical strength is weak, it may be deformed when assembling the iron core blocks 3a, 3b, 3c and sufficient assembling accuracy. In order to solve the problem that it is not possible to secure the above, it is conceivable that the rigid member 8 is made of, for example, a silicon steel strip which is close in composition to the amorphous magnetic alloy ribbon and has rigidity. FIG. 7 shows still another embodiment of the present invention. In this embodiment, when the core width is the same and the winding thickness (lamination thickness) is large, the cores are divided like the core blocks 3b1 and 3b2, and the voids 7 are formed between them. Also in this case, the void 7 is formed in the portion where the winding thickness is large, and the same effect as the above case can be obtained. That is, in the above-described embodiments, the iron core is divided into the same iron core widths (the iron core blocks are formed), but in the present embodiment, the winding thickness is large even with the same iron core width unlike the previous examples. In this case, the portion having a large winding thickness is divided into iron core blocks 3b1 and 3b2 to form the voids 7, which is particularly effective when the iron core becomes large. Further, in the above-mentioned embodiments, an example in which the iron core is divided only in the stacking direction is shown. However, considering that the maximum iron core width is about 200 mm in the current amorphous magnetic alloy thin ribbon, a predetermined iron core is given. To make the width, iron cores must be combined in the width direction. Even in such a case, the same configuration as that shown in the embodiment is naturally possible. FIG. 8 shows still another embodiment of the present invention. In this embodiment, a steel strip 9 having mechanical strength superior to that of the amorphous magnetic alloy ribbon is disposed inside the iron core blocks 3a, 3b, 3c. And this steel strip 9 is several times to several tens times thicker than the usual thickness 30 μm of the amorphous magnetic alloy,
It was formed of an amorphous magnetic alloy having excellent mechanical strength. By doing so, each core block 3a, 3b, 3c
It is possible to prevent the deformation of the iron core due to the winding tightening phenomenon that increases inside the core, and to prevent the iron core blocks 3a, 3b,
The assembly of 3c can be facilitated. In the present embodiment, the steel strip 9 is arranged very slightly inside the core blocks 3a, 3b, 3c (with respect to the stacking thickness t), but the ratio is the stacking of the core blocks 3a, 3b, 3c. The arrangement amount is appropriately determined depending on the thickness (roll thickness) t and the degree of stress due to winding tightening. FIG. 9 shows still another embodiment of the present invention. In this embodiment, the amorphous magnetic alloy 10 having an insulating film and excellent in mechanical strength is arranged inside the iron core blocks 3a, 3b, 3c. By doing so, electrical insulation between the core blocks 3a, 3b, 3c can be ensured, and an increase in iron loss due to an eddy current flowing between the core blocks 3a, 3b, 3c can be prevented. According to the present invention, it is possible to obtain an amorphous wound iron core excellent in productivity and magnetic characteristics.

【図面の簡単な説明】 【図1】本発明の一実施例の非晶質巻鉄心の鉄心ブロッ
クによる巻鉄心の組み立てを示す斜視図で、同図(A)
は鉄心ブロックの巻回状態を示す斜視図、同図(B)は
鉄心ブロックの焼鈍状態を示す斜視図、同図(C)は焼
鈍の終了した各鉄心ブロックの組み立て状態を示す斜視
図である。 【図2】本発明の一実施例の非晶質巻鉄心の曲線部周り
の拡大平面図である。 【図3】本発明の一実施例の非晶質巻鉄心の平面図であ
る。 【図4】本発明の一実施例の非晶質巻鉄心の図3のP−
P線に沿う断面図である。 【図5】本発明の一実施例の非晶質巻鉄心の図3のQ−
Q線に沿う断面図である。 【図6】本発明の他の実施例の非晶質巻鉄心の曲線部周
りの拡大平面図である。 【図7】本発明の更に他の実施例の非晶質巻鉄心の曲線
部周り(図3のQ−Q線に相当する部分)の断面図であ
る。 【図8】本発明の更に他の実施例の非晶質巻鉄心の曲線
部周りの拡大平面図である。 【図9】本発明の更に他の実施例の非晶質巻鉄心の両直
線部(図3のP−P線に相当する部分)の断面図であ
る。 【図10】従来の非晶質巻鉄心の平面図である。 【図11】従来の非晶質巻鉄心の図10のX−X線に沿
う断面図である。 【符号の説明】 2…非晶質磁性合金の薄帯、3,3a,3b,3b1,
3b2,3c…鉄心ブロック、4…素材フープ、5…励
磁コイル、6…容器、7…空隙、8…剛性部材、9…鋼
帯、10…非晶質磁性合金、t…積層厚さ(巻厚さ)、
g…空間寸法。
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a perspective view showing an assembly of a winding core by an iron core block of an amorphous winding core according to an embodiment of the present invention.
Is a perspective view showing a wound state of the iron core block, FIG. 7B is a perspective view showing an annealed state of the iron core block, and FIG. 8C is a perspective view showing an assembled state of each iron core block after annealing. . FIG. 2 is an enlarged plan view around a curved portion of an amorphous winding iron core according to an embodiment of the present invention. FIG. 3 is a plan view of an amorphous wound iron core according to an embodiment of the present invention. FIG. 4 shows P- of FIG. 3 of an amorphous winding iron core of one embodiment of the present invention.
It is sectional drawing which follows the P line. 5 is a graph of Q- of FIG. 3 of the amorphous wound iron core of one embodiment of the present invention.
It is sectional drawing which follows the Q line. FIG. 6 is an enlarged plan view around a curved portion of an amorphous winding iron core according to another embodiment of the present invention. FIG. 7 is a cross-sectional view around a curved portion (a portion corresponding to the line Q-Q in FIG. 3) of an amorphous winding iron core according to still another embodiment of the present invention. FIG. 8 is an enlarged plan view around a curved portion of an amorphous winding iron core according to still another embodiment of the present invention. FIG. 9 is a cross-sectional view of both straight line portions (portions corresponding to the line P-P in FIG. 3) of an amorphous wound iron core according to still another example of the present invention. FIG. 10 is a plan view of a conventional amorphous wound iron core. 11 is a cross-sectional view of a conventional amorphous wound iron core taken along line XX in FIG. [Explanation of Codes] 2 ... Amorphous magnetic alloy ribbon, 3, 3a, 3b, 3b1,
3b2, 3c ... iron core block, 4 ... material hoop, 5 ... excitation coil, 6 ... container, 7 ... void, 8 ... rigid member, 9 ... steel strip, 10 ... amorphous magnetic alloy, t ... laminated thickness (winding thickness),
g ... spatial dimensions.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 山口 彰宥 新潟県北蒲原郡中条町大字富岡46番地1 株式会社日立製作所中条工場内 (72)発明者 坂本 勝 新潟県北蒲原郡中条町大字富岡46番地1 株式会社日立製作所中条工場内 (72)発明者 山中 功治 新潟県北蒲原郡中条町大字富岡46番地1 株式会社日立製作所中条工場内   ─────────────────────────────────────────────────── ─── Continued front page    (72) Inventor Akiyo Yamaguchi             46-1 Tomioka, Nakajo-cho, Kitakanbara-gun, Niigata Prefecture             Hitachi Ltd. Nakajo Factory (72) Inventor Masaru Sakamoto             46-1 Tomioka, Nakajo-cho, Kitakanbara-gun, Niigata Prefecture             Hitachi Ltd. Nakajo Factory (72) Inventor Koji Yamanaka             46-1 Tomioka, Nakajo-cho, Kitakanbara-gun, Niigata Prefecture             Hitachi Ltd. Nakajo Factory

Claims (1)

【特許請求の範囲】 1.非晶質磁性合金の薄帯が巻回されて略矩形状に形成
された非晶質巻鉄心において、前記薄帯が積層方向に所
定の厚さで巻回されて所定の外径を有する略矩形状の第
1のブロックと、前記薄帯が積層方向に所定の厚さで巻
回されて前記第1のブロックの外形とほぼ等しい内径を
有する略矩形状の第2のブロックを少なくとも備え、前
記第1のブロックの外側に前記第2のブロックを実質的
に密着させて構成されたことを特徴とする非晶質巻鉄
心。 2.前記第1のブロックと前記第2のブロックは積層方
向の厚さが実質的に同一に形成されたことを特徴とする
特許請求の範囲第1項記載の非晶質巻鉄心。 3.前記第2のブロックの積層方向の厚さは前記第1の
ブロックの積層方向の厚さより大となるよう形成された
ことを特徴とする特許請求の範囲第1項記載の非晶質巻
鉄心。 4.前記第1のブロックと前記第2のブロックはそれぞ
れのブロックの内側形状に沿って配設されて前記薄帯よ
り剛性のある剛性部材を有することを特徴とする特許請
求の範囲第1項記載の非晶質巻鉄心。
[Claims] 1. In an amorphous winding iron core formed by winding a ribbon of an amorphous magnetic alloy into a substantially rectangular shape, the ribbon is wound in a stacking direction with a predetermined thickness and has a predetermined outer diameter. At least a rectangular first block and a substantially rectangular second block in which the strips are wound in a stacking direction with a predetermined thickness and have an inner diameter substantially equal to the outer shape of the first block, An amorphous winding iron core, characterized in that the second block is substantially brought into close contact with the outside of the first block. 2. The amorphous winding iron core according to claim 1, wherein the first block and the second block are formed to have substantially the same thickness in the stacking direction. 3. The amorphous wound iron core according to claim 1, wherein the second block is formed so that the thickness in the stacking direction is larger than the thickness in the stacking direction of the first block. 4. The first block and the second block have a rigid member that is arranged along the inner shape of each block and is stiffer than the ribbon. Amorphous winding iron core.
JP7275262A 1995-10-24 1995-10-24 Amorphous core Expired - Lifetime JP2776337B2 (en)

Priority Applications (1)

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JP7275262A JP2776337B2 (en) 1995-10-24 1995-10-24 Amorphous core

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Application Number Priority Date Filing Date Title
JP7275262A JP2776337B2 (en) 1995-10-24 1995-10-24 Amorphous core

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
JP60152942A Division JPH0697646B2 (en) 1985-07-11 1985-07-11 Amorphous magnetic alloy winding iron core

Publications (2)

Publication Number Publication Date
JPH08227816A true JPH08227816A (en) 1996-09-03
JP2776337B2 JP2776337B2 (en) 1998-07-16

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011096267A1 (en) 2010-02-04 2011-08-11 株式会社日立産機システム Amorphous core annealing method
CN103286215A (en) * 2013-06-07 2013-09-11 无锡微研有限公司 Complete cycle tightening-up structure of iron cores
CN105830180A (en) * 2014-01-27 2016-08-03 东芝产业机器系统株式会社 Wound core and method for manufacturing wound core

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50124122A (en) * 1974-03-19 1975-09-30
JPS5286155A (en) * 1976-01-14 1977-07-18 Hitachi Ltd Wound core with opening
JPS5790917A (en) * 1980-11-27 1982-06-05 Toshiba Corp Noncut type wound core
JPS5998621U (en) * 1982-12-22 1984-07-04 株式会社日立製作所 Winding core of stationary induction electric appliances

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50124122A (en) * 1974-03-19 1975-09-30
JPS5286155A (en) * 1976-01-14 1977-07-18 Hitachi Ltd Wound core with opening
JPS5790917A (en) * 1980-11-27 1982-06-05 Toshiba Corp Noncut type wound core
JPS5998621U (en) * 1982-12-22 1984-07-04 株式会社日立製作所 Winding core of stationary induction electric appliances

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011096267A1 (en) 2010-02-04 2011-08-11 株式会社日立産機システム Amorphous core annealing method
CN103286215A (en) * 2013-06-07 2013-09-11 无锡微研有限公司 Complete cycle tightening-up structure of iron cores
CN105830180A (en) * 2014-01-27 2016-08-03 东芝产业机器系统株式会社 Wound core and method for manufacturing wound core

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