JP3438825B2 - Wound core, method of manufacturing wound core, high-voltage pulse generator, and laser device - Google Patents
Wound core, method of manufacturing wound core, high-voltage pulse generator, and laser deviceInfo
- Publication number
- JP3438825B2 JP3438825B2 JP06780493A JP6780493A JP3438825B2 JP 3438825 B2 JP3438825 B2 JP 3438825B2 JP 06780493 A JP06780493 A JP 06780493A JP 6780493 A JP6780493 A JP 6780493A JP 3438825 B2 JP3438825 B2 JP 3438825B2
- Authority
- JP
- Japan
- Prior art keywords
- magnetic core
- racetrack
- heat
- amorphous alloy
- 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.)
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- Manufacturing Cores, Coils, And Magnets (AREA)
- Lasers (AREA)
- Generation Of Surge Voltage And Current (AREA)
Description
【0001】[0001]
【産業上の利用分野】本発明はエキシマレーザ、TEA(Tr
ansversely excited atmospheric)−CO2レーザ、TEMA(T
ransversely excited multi-atmospheric)-CO2レーザを
始めとするレーザ装置などに用いられる高電圧パルス発
生装置に使用されるレーストラック形状の巻磁心および
これを用いた高電圧パルス発生装置ならびにレーザ装置
に関するものである。The present invention relates to an excimer laser, TEA (Tr
ansversely excited atmospheric) -CO 2 laser, TEMA (T
ransversely excited multi-atmospheric) -race track winding core used in high voltage pulse generators used in laser devices such as CO 2 lasers, and high voltage pulse generators and laser devices using the same Is.
【0002】[0002]
【従来の技術】エキシマレーザ、TEA-CO2レーザあるい
はTEMA-CO2レーザなどの横放電励起ガスレーザで、大口
径かつ高エネルギ−のレーザを得るためには主放電電極
の間隔と有効長を長くするととも、発振させるレーザの
種類に応じた適切なパルス幅で大きなエネルギ−を持っ
た高電圧パルスをレーザガス中に投入する必要があるこ
とが知られている。 2. Description of the Related Art In a transverse discharge excitation gas laser such as an excimer laser, a TEA-CO 2 laser or a TEMA-CO 2 laser, in order to obtain a laser with a large diameter and high energy, the interval between the main discharge electrodes and the effective length must be long. At the same time, it is known that it is necessary to introduce a high voltage pulse having a large energy with a pulse width suitable for the type of laser to be oscillated into the laser gas.
【0003】このような高電圧パルスを高繰り返しで発
生させる高効率で信頼性の高い高電圧パルス発生装置を
実現するには、飽和時のインダクタンスが極力小さく、
非飽和時のインダクタンスと飽和時のインダクタンスの
比が大きくて低損失の可飽和リアクトルあるいは可飽和
変圧器が必要である。In order to realize a highly efficient and highly reliable high voltage pulse generator that generates such high voltage pulses with high repetition, the inductance at saturation is as small as possible.
A saturable reactor or a saturable transformer that has a large ratio of non-saturated inductance to saturated inductance and has low loss is required.
【0004】このため高電圧パルス発生装置として、E.
Y. Chu, G. Honfmann, H. Kent, T.Bernhart, "Magnet
ic modulator for low-impedance discharge lasers",
IEEEConf. Record of 15th Power Modulator Symposiu
m, p.32〜36 (1982), R. S.Taylor, K. E. Leopold, "M
icrosecond duration optical pulses from a UV-preio
nized XeCl laser", Appl. Phys. Lett. 47 (2), p.81
〜83 (1985), C. H.Fisher, M. J. Kushner, T. E. DeH
art, J. P. McDaniel, R. A. Petr, J. J.Ewing, "High
efficiency XeCl laser with spiker and magnetic is
olation",Appl. Phys. Lett. 48 (23), p.1574〜1576
(1986)、S. Watanabe, M. Watanabe,A. Endoh, "High r
epetition long pulse XeCl laser with a coaxial cer
amicpulse-forming line", Rev. Sci. Instrum. 57 (1
2), p.2970〜2973 (1986)、Taylor, K. E. Leopold, "U
ltralong optical-pulse corona preionized XeCllase
r", J. Appl. Phys. 65 (1), p.22〜29 (1989)、特開平
4−211185あるいは、井上、“エキシマレーザ大
出力化技術の研究”、超先端加工システム技術研究組
合、第4回 超先端加工システム技術シンポジウム予稿
集 p.18〜21(1992)に記載されるように図4に示すよう
なレーストラック形状磁心を用い構成した可飽和リアク
トルあるいは可飽和変圧器を利用するのが有効なことが
知られている。Therefore, as a high voltage pulse generator, E.
Y. Chu, G. Honfmann, H. Kent, T. Bernhart, "Magnet
ic modulator for low-impedance discharge lasers ",
IEEEConf. Record of 15th Power Modulator Symposiu
m, p.32-36 (1982), RSTaylor, KE Leopold, "M
icrosecond duration optical pulses from a UV-preio
nized XeCl laser ", Appl. Phys. Lett. 47 (2), p.81
~ 83 (1985), CHFisher, MJ Kushner, TE DeH
art, JP McDaniel, RA Petr, JJEwing, "High
efficiency XeCl laser with spiker and magnetic is
olation ", Appl. Phys. Lett. 48 (23), p.1574-1576
(1986), S. Watanabe, M. Watanabe, A. Endoh, "High r
epetition long pulse XeCl laser with a coaxial cer
amicpulse-forming line ", Rev. Sci. Instrum. 57 (1
2), p.2970〜2973 (1986), Taylor, KE Leopold, "U
ltralong optical-pulse corona preionized XeCllase
r ", J. Appl. Phys. 65 (1), p.22-29 (1989), Japanese Patent Laid-Open No. 4-111185 or Inoue," Research on high output technology of excimer laser ", Ultra Advanced Machining System Technology Research Association , Proceedings of the 4th Symposium on Ultra-advanced Machining Systems, p.18-21 (1992), use saturable reactor or saturable transformer composed of racetrack-shaped magnetic core as shown in Fig.4. It is known to be effective.
【0005】このレーストラック形状の可飽和磁心に
は、前記文献に示されるようにNi−Znフェライト磁
心、鉄基あるいはコバルト基非晶質合金薄帯とポリエチ
レンテレフタレートフィルム(商品名、マイラーフィル
ム、デュポン社製あるいはルミラーフィルム、東レ社製
など、以下PETフィルムと称す)などの高分子フィル
ムを同時に巻回して構成した巻磁心が用いられている。This racetrack-type saturable magnetic core includes Ni--Zn ferrite magnetic core, iron-based or cobalt-based amorphous alloy ribbon and polyethylene terephthalate film (trade name, Mylar film, DuPont) as described in the above-mentioned document. A wound magnetic core formed by simultaneously winding polymer films such as those manufactured by the same company, Lumirror film, manufactured by Toray Co., Ltd. (hereinafter referred to as PET films) is used.
【0006】Ni−Znフェライトを用いたレーストラ
ック形状磁心を製作するには磁心形状ごとに専用のプレ
ス整形用金型を製作する必要があり、しかも原料粉末を
前記金形でレーストラック形状にプレスした後の焼結時
の収縮応力により割れや欠けが生じ易く、製作できる寸
法に制限がある問題がある。このため前記 C. H.Fishe
r, M. J. Kushner, T. E. DeHart, J. P. McDaniel, R.
A. Petr, J. J.Ewing, "High efficiency XeCl laser
with spiker and magnetic isolation",Appl. Phys. Le
tt. 48 (23), p.1574〜1576 (1986)に記載されるよう
に、フェライトブロックを多数組み合わせてレーストラ
ック形状磁心を構成することも行われているが、この場
合磁気特性が本来の材料特性に比べて大幅に劣化してし
まう問題がある。In order to manufacture a racetrack-shaped magnetic core using Ni-Zn ferrite, it is necessary to manufacture a dedicated press shaping die for each magnetic core shape, and moreover, the raw material powder is pressed into the racetrack shape by the above-mentioned die. There is a problem that cracks and chips are apt to occur due to shrinkage stress at the time of sintering after that, and the size that can be manufactured is limited. For this reason the above CHFishe
r, MJ Kushner, TE DeHart, JP McDaniel, R.
A. Petr, JJEwing, "High efficiency XeCl laser
with spiker and magnetic isolation ", Appl. Phys. Le
As described in tt. 48 (23), p.1574 to 1576 (1986), a large number of ferrite blocks are combined to form a racetrack-shaped magnetic core. There is a problem that it is significantly deteriorated compared to the material properties.
【0007】これに対して、鉄基あるいはコバルト基非
晶質合金薄帯と高分子フィルムを同時に巻回してレース
トラック形状巻磁心を構成する場合、フェライト磁心の
ように特殊なプレス成形用金型が不要であり任意の形状
を容易に製作することのできる利点を有する。On the other hand, when a racetrack-shaped wound magnetic core is formed by simultaneously winding an iron-based or cobalt-based amorphous alloy ribbon and a polymer film, a special press-molding die like a ferrite magnetic core. Is unnecessary and has an advantage that an arbitrary shape can be easily manufactured.
【0008】一般の可飽和磁心の体積は、例えば中島、
香川、平尾、渡部、“鉄基超微結晶質合金を用いた磁気
スイッチ磁心の動特性評価”、電気学会 プラズマ研究
会資料、EP-91-13, p.1〜10 (1991)などに記載されるよ
うに磁心の動特性から定められる。すなわち磁心の平均
磁路長は磁心の飽和領域の比透磁率(μrs)に比例し、
磁心の占積率(K)と最大動作磁束密度量(ΔBm)の
積である実効最大動作磁束密度量(K・ΔBm)に反比例
する関係にある。一方、磁心の断面積は磁心の実効最大
動作磁束密度量(K・ΔBm)に反比例するから、磁心体
積は磁心の飽和領域の比透磁率(μrs)に比例し、実効
最大動作磁束密度量(K・ΔBm)の2乗に反比例するこ
とになる。The volume of a general saturable magnetic core is, for example, Nakashima,
Kagawa, Hirao, Watanabe, "Evaluation of dynamic characteristics of magnetic switch magnetic core using iron-based ultrafine crystalline alloy", Material of Plasma Research Society of the Institute of Electrical Engineers of Japan, EP-91-13, p.1-10 (1991), etc. As described above, it is determined from the dynamic characteristics of the magnetic core. That is, the average magnetic path length of the magnetic core is proportional to the relative permeability (μ rs ) in the saturated region of the magnetic core,
It is inversely proportional to the effective maximum operating magnetic flux density amount (K · ΔBm) which is the product of the space factor (K) of the magnetic core and the maximum operating magnetic flux density amount (ΔBm). On the other hand, since the cross-sectional area of the magnetic core is inversely proportional to the effective maximum operating magnetic flux density (K · ΔBm) of the magnetic core, the magnetic core volume is proportional to the relative permeability (μ rs ) in the saturation region of the magnetic core, and the effective maximum operating magnetic flux density is It is inversely proportional to the square of (K · ΔBm).
【0009】しかし、横放電励起ガスレーザなどで使用
されるレーストラック形状の可飽和磁心の場合、同磁心
を用いて構成した可飽和リアクトルの飽和後のインダク
タンスを極力小さくするためその平均磁路長はレーザ主
放電電極の有効長に応じて選定せざるをえないので、実
際に使用するレーストラック形状磁心の平均磁路長は前
記磁心の動特性から定められる磁心の平均磁路長よりは
るかに長くなる。その結果、実際の磁心体積は前記磁心
の動特性から定められる磁心体積もより大きくなってし
まう。このため鉄基非晶質合金薄帯と高分子フィルムを
同時に巻回した巻磁心のように実効最大動作磁束密度量
(K・ΔBm)が大きく、単位体積当たりのゲート半周期
の磁心損失Pcgが大きい(一般に(Pcg)は(K・ΔBm
2)に比例する)磁心をレーストラック形状とすると前
記のように本来磁心の動特性で定められる寸法より大き
な磁心体積となるため損失が大きくなってしまう問題が
ある。したがって繰り返し周波数が高く高効率化が必要
な用途では、レーストラック形状巻磁心として前記特開
平4−211185号あるいは、井上、“エキシマレー
ザ大出力化技術の研究”、超先端加工システム技術研究
組合、第4回 超先端加工システム技術シンポジウム予
稿集 p.18〜21 (1992)に記載されるように、コバルト基
非晶質合金薄帯と高分子フィルムを同時に巻回した巻磁
心が用いられる。However, in the case of a racetrack-shaped saturable magnetic core used in a transverse discharge pumped gas laser or the like, the average magnetic path length of the saturable reactor constructed by using the same magnetic core is set to be as small as possible after saturation. Since the choice must be made according to the effective length of the laser main discharge electrode, the average magnetic path length of the actually used racetrack-shaped magnetic core is much longer than the average magnetic path length of the magnetic core determined from the dynamic characteristics of the magnetic core. Become. As a result, the actual magnetic core volume becomes larger than the magnetic core volume determined from the dynamic characteristics of the magnetic core. Therefore, the effective maximum operating magnetic flux density (K · ΔBm) is large like a wound magnetic core in which an iron-based amorphous alloy ribbon and a polymer film are wound at the same time, and the magnetic core loss Pcg of a gate half cycle per unit volume is large. Large (generally (Pcg) is (K · ΔBm
If the magnetic core has a racetrack shape (proportional to 2 ), the magnetic core volume will be larger than the dimension originally determined by the dynamic characteristics of the magnetic core, and the loss will be large. Therefore, in applications where the repetition frequency is high and high efficiency is required, as the racetrack-shaped winding magnetic core, the above-mentioned Japanese Patent Laid-Open No. 4-211185 or Inoue, “Research on high output technology of excimer laser”, Ultra-advanced machining system technology research association, As described in Proceedings of the 4th Symposium on Ultra-advanced Machining System Technology, p.18-21 (1992), a magnetic core is used in which a cobalt-based amorphous alloy ribbon and a polymer film are simultaneously wound.
【0010】コバルト基非晶質合金薄帯と高分子フィル
ムを用いて構成したレーストラック形状巻磁心として
は、例えば特開昭64−65889号、特開平2−19
4504号に記載される製造法により形状をレーストラ
ック形として製造したもの、あるいは特開平3−278
503号あるいは特開平4−10603号に記載される
ように、前記コバルト基非晶質合金薄帯と高分子フィル
ムを同時に巻き回してトロイダル形状巻磁心を構成した
後、同巻磁心形状をレーストラック形状に変形して製造
したものなどが知られている。A racetrack-shaped wound magnetic core formed by using a cobalt-based amorphous alloy ribbon and a polymer film is disclosed in, for example, JP-A-64-65889 and JP-A-2-19.
Those manufactured in the shape of a racetrack by the manufacturing method described in 4504, or JP-A-3-278.
No. 503 or JP-A-4-10603, the cobalt-based amorphous alloy ribbon and the polymer film are simultaneously wound to form a toroidal winding core, and then the winding core is racetracked. Those manufactured by deforming the shape are known.
【0011】[0011]
【発明が解決しようとする問題点】しかるに前記特開昭
64−65889号あるいは特開平2−19504号に
記載される従来技術によるコバルト基非晶質合金薄帯を
用いたレーストラック形状巻磁心および前記特開平3−
278503号あるいは特開平4−10603号に記載
されるコバルト基非晶質合金薄帯を用いたレーストラッ
ク形状巻磁心では以下のような問題がある。However, a racetrack-shaped wound magnetic core using a cobalt-based amorphous alloy ribbon according to the prior art described in JP-A-64-65889 or JP-A-2-19504, and JP-A-3-
The racetrack-shaped wound magnetic core using the cobalt-based amorphous alloy ribbon described in 278503 or JP-A-4-10603 has the following problems.
【0012】特開昭64−65889号に記載される未
熱処理状態のコバルト基非晶質合金薄帯と高分子フィル
ムを同時に巻回して構成したレーストラック形状巻磁心
では、融体急冷法で製作されたコバルト基非晶質合金薄
帯に不可避的に加えられた応力と同非晶質合金薄帯と高
分子フィルムを同時に巻回して巻磁心を製作したときに
加えられた応力の影響により、パルスパワー用可飽和磁
心として用いた場合にその動特性が悪い問題がある。す
なわち、未熱処理状態のコバルト基非晶質合金薄帯と高
分子フィルムを同時に巻回して構成したレーストラック
形状巻磁心をパルスパワー用可飽和磁心として用いた場
合、飽和領域の比透磁率(μrs)が2よりも大きくなっ
てしまい単位体積あたりのゲート半周期の磁心損失(P
cg)も極めて大きくなる。The racetrack-shaped wound magnetic core described in JP-A-64-65889, which is formed by simultaneously winding an unheated cobalt-based amorphous alloy ribbon and a polymer film, is manufactured by a melt quenching method. Due to the stress unavoidably applied to the cobalt-based amorphous alloy ribbon and the stress applied when the amorphous magnetic alloy ribbon and the polymer film are simultaneously wound to manufacture a wound magnetic core, When used as a saturable magnetic core for pulse power, there is a problem that its dynamic characteristics are poor. That is, when a racetrack-shaped wound magnetic core formed by simultaneously winding an unheated cobalt-based amorphous alloy ribbon and a polymer film is used as a saturable magnetic core for pulse power, the relative magnetic permeability (μ rs ) becomes larger than 2 and the gate core loss per unit volume (P)
cg) also becomes extremely large.
【0013】このような問題を解決するため未熱処理状
態のコバルト基非晶質合金薄帯と高分子フィルムを同時
に巻回してレーストラック形状巻磁心を構成した後に熱
処理を行うことが考えられる。前記未熱処理状態のコバ
ルト基非晶質合金薄帯に加えられている前記2つの原因
による応力を緩和させるには、結晶化温度以下のその合
金組成に応じた比較的高い温度で熱処理することが好ま
しく、一般に350℃程度以上で数時間程度の熱処理が
行われている。現状350℃程度以上で数時間程度の熱
処理を行っても支障のない高分子フィルムとしてはポリ
イミドフィルム(商品名、カプトンフィルム、デュポン
社製など、以下PIフィルムと称す)があるが、現状入
手し得るPIフィルムの厚みは最少でも7.5μmであ
りパルスパワー用可飽和磁心に必要と考えられるフィル
ムの厚みの下限値である2μmに対し厚すぎてレースト
ラック形状巻磁心の占積率Kを不要に低下させてしまう
問題がある。In order to solve such a problem, it is conceivable that the unheated cobalt-based amorphous alloy ribbon and the polymer film are simultaneously wound to form a racetrack-shaped wound magnetic core, and then the heat treatment is performed. In order to relieve the stresses applied to the unheated cobalt-based amorphous alloy ribbon due to the above two causes, heat treatment at a relatively high temperature corresponding to the alloy composition below the crystallization temperature is performed. Preferably, heat treatment is generally performed at about 350 ° C. or higher for about several hours. Currently, there is a polyimide film (trade name, Kapton film, manufactured by DuPont, etc., hereinafter referred to as PI film) as a polymer film that does not interfere with heat treatment at about 350 ° C. or higher for several hours, but currently available. The thickness of the PI film obtained is at least 7.5 μm, which is too large compared to the lower limit of 2 μm of the film thickness considered necessary for the saturable magnetic core for pulse power, and the space factor K of the racetrack-shaped wound magnetic core is unnecessary. There is a problem that it lowers.
【0014】このため、特開平2−194504号に記
載されるようにパルスパワー用可飽和磁心に使用する高
分子フィルムとして、厚さ2μm程度から6μm程度の
PETフィルムあるいはポリアミドフィルム(商品名、
アラミドフィルム、東レ社製)等が主として用いられて
いる。しかし、これらのフィルムの実用上の熱処理温度
は熱処理時間を5時間程度に制限した場合でも、PET
フィルムの場合で180℃程度、ポリアミドフィルムの
場合で250℃程度に制限される。このような比較的低
温で数時間程度の熱処理では、コバルト基非晶質合金薄
帯と高分子フィルムを同時に巻回したときに加えられた
応力を緩和させることはできても、融体急冷法で製作さ
れたときに同合金薄帯に加えられた大きな応力を十分に
緩和することはできず、パルスパワー用可飽和磁心とし
ての性能は十分でなかった。Therefore, as a polymer film used for a saturable magnetic core for pulse power as described in JP-A-2-194504, a PET film or a polyamide film (trade name, having a thickness of about 2 μm to 6 μm) (trade name,
Aramid film, manufactured by Toray Industries, Inc., etc. are mainly used. However, the practical heat treatment temperature of these films is PET even when the heat treatment time is limited to about 5 hours.
The film is limited to about 180 ° C and the polyamide film is limited to about 250 ° C. Such a heat treatment at a relatively low temperature for about several hours can alleviate the stress applied when the cobalt-based amorphous alloy ribbon and the polymer film are wound at the same time, but the melt quenching method The large stress applied to the alloy ribbon when manufactured in 1) could not be sufficiently relaxed, and the performance as a saturable magnetic core for pulse power was not sufficient.
【0015】上記問題点を対策するため特開昭64−6
5889号に記載されるように未熱処理状態の非晶質合
金薄帯をトロイダル形状に巻回し400℃程度で数時間
熱処理を行い十分冷却することによって融体急冷法によ
って非晶質合金薄帯を製造したときに同非晶質合金薄帯
に不可避的に加えられた応力を緩和した後、このトロイ
ダル形状巻磁心に巻き込まれた熱処理した非晶質合金薄
帯とに高分子フィルムを同時に巻き回してレーストラッ
ク形状巻磁心として構成することが試みられている。し
かし、コバルト基非晶質合金薄帯を400℃程度で熱処
理するとその熱処理時間が1時間程度と短時間であって
も脆化が著しく進行してしまい、上記のような手法によ
り高分子フィルムと同時に巻回して占積率(K)の高い
レーストラック形状巻磁心を構成するのが著しく困難に
なる。To solve the above problems, Japanese Patent Laid-Open No. 64-6
No. 5889, the amorphous alloy ribbon in an unheated state is wound into a toroidal shape, heat-treated at about 400 ° C. for several hours, and sufficiently cooled to form an amorphous alloy ribbon by the melt quenching method. After alleviating the stress that was inevitably applied to the amorphous alloy ribbon when it was manufactured, a polymer film was simultaneously wound around the heat-treated amorphous alloy ribbon that was wound around the toroidal winding core. Attempts have been made to construct it as a racetrack-shaped wound magnetic core. However, when the cobalt-based amorphous alloy ribbon is heat-treated at about 400 ° C., the embrittlement significantly progresses even if the heat-treatment time is as short as about 1 hour. At the same time, it becomes extremely difficult to form a racetrack-shaped wound magnetic core having a high space factor (K) by winding at the same time.
【0016】例えば、厚さtが20μm、幅が25.4
mmのコバルト基非晶質合金薄帯と厚さ4μmのPET
フィルムを同時に巻回してその占積率(K)が65%程
度以上の巻磁心を得るには、前記コバルト基非晶質合金
薄帯に0.2N程度以上の張力を加えながら巻回すこと
が必要になる。しかし、前記400℃程度で1時間程度
の熱処理を行ったコバルト基非晶質合金薄帯に0.2N
程度以上の張力を加えて高分子フィルムと同時に巻回す
と、特に応力が集中する図4の破線内に示すレーストラ
ック形状巻磁心の曲率半径の小さな部分で前記熱処理し
たコバルト基非晶質合金薄帯が頻繁に破断し、レースト
ラック形状巻磁心を構成することが極めて困難となる。
なお、レーストラック形状巻磁心を構成する磁性合金薄
帯が頻繁に破断した状態で構成された巻磁心は占積率
(K)の低下とパルスパワー用可飽和磁心として使用し
たときの非飽和領域の比透磁率(μru)が低下し、飽和
領域の比透磁率(μrs)が大きくなってしまう問題があ
る。For example, the thickness t is 20 μm and the width is 25.4.
mm Cobalt-based amorphous alloy ribbon and 4 μm thick PET
In order to obtain a wound magnetic core having a space factor (K) of about 65% or more by simultaneously winding the film, it is necessary to wind the cobalt-based amorphous alloy ribbon while applying a tension of about 0.2N or more. You will need it. However, the cobalt-based amorphous alloy ribbon, which has been heat-treated at about 400 ° C. for about 1 hour, is 0.2N.
When the polymer film is wound at the same time as a high tension, the stress is particularly concentrated, and the stress is particularly concentrated. The band is frequently broken, which makes it extremely difficult to form a racetrack-shaped wound magnetic core.
A wound magnetic core formed by frequently breaking the magnetic alloy thin ribbon forming the racetrack-shaped wound magnetic core has a reduced space factor (K) and an unsaturated region when used as a saturable magnetic core for pulse power. However, there is a problem that the relative permeability (μ ru ) of is decreased and the relative permeability (μ rs ) of the saturated region is increased.
【0017】前記熱処理したコバルト基非晶質合金薄帯
の破断を防止するには、同合金薄帯に加える張力を低下
させれば良いが、その場合占積率(K)が著しくて以下
してしまう問題があった。In order to prevent breakage of the heat-treated cobalt-based amorphous alloy ribbon, the tension applied to the alloy ribbon may be lowered, but in that case, the space factor (K) is remarkably low. There was a problem that caused it.
【0018】また、ここまで説明したレーストラック形
状巻磁心では図4の破線内に応力が集中する反面、同図
の一点鎖線内では十分な張力が加えられず、この一点鎖
線で示す部分が巻心5側から外側に向かってふくらんで
しまい占積率(K)が低下するとともに目的の磁心形状
にするのが困難という問題もあった。Further, in the racetrack-shaped wound magnetic core described above, stress concentrates in the broken line in FIG. 4, but on the other hand, sufficient tension is not applied within the dashed-dotted line in FIG. 4, and the portion indicated by the dashed-dotted line is wound. There is also a problem that the space factor (K) is reduced by bulging from the core 5 side toward the outside, and it is difficult to form the target magnetic core shape.
【0019】このような問題を対策するため、例えば特
開平3−78215号に記載されるようにレーストラッ
ク形状磁心の長径と短径の比を規定して巻磁心を構成し
たり、図4のレーストラック形状巻磁心の一点鎖線内に
示す部分を直線から楕円アーチ状とする方法がある。し
かし、この方法ではレーストラック形状巻磁心の短径が
大きくなるため平均磁路長がレーザ主放電電極の有効長
に比べて不要に長くなってしまう問題があった。In order to solve such a problem, for example, as described in Japanese Patent Application Laid-Open No. 3-78215, a winding magnetic core is formed by defining the ratio of the major axis to the minor axis of the racetrack-shaped magnetic core, or the structure shown in FIG. There is a method in which the portion shown in the alternate long and short dash line of the racetrack-shaped wound magnetic core is changed from a straight line to an elliptic arch. However, this method has a problem that the average magnetic path length becomes unnecessarily long as compared with the effective length of the laser main discharge electrode because the minor axis of the racetrack-shaped winding magnetic core becomes large.
【0020】一方、特開平3−278503号あるいは
特開平4−10603号に記載されるコバルト基非晶質
合金薄帯と高分子フィルムを同時に巻回してトロイダル
形状巻磁心を製作後レーストラック形状に変形、熱処理
して構成したレーストラック形状巻磁心の場合には、レ
ーストラック形状巻磁心を直接製作することに伴う問題
点は解決できるが前記特開平2−194504号に記載
される巻磁心同様、融体急冷法で非晶質合金薄帯を製造
したときに同非晶質合金薄帯に不可避的に加えられた応
力を十分に緩和できないなどの問題があった。そこで本
発明は、レーザ装置を高繰り返し運転するときに問題で
あった繰り返し周波数の制限、連続動作時間の制限ある
いはパルスを発生させるためのスイッチ素子の安全動作
と寿命に起因する信頼性の問題を解消することを課題と
する。On the other hand, a cobalt-based amorphous alloy ribbon described in JP-A-3-278503 or JP-A-4-10603 and a polymer film are simultaneously wound to form a toroidal wound magnetic core into a racetrack shape after being manufactured. In the case of a racetrack-shaped winding magnetic core formed by deformation and heat treatment, the problems associated with directly manufacturing the racetrack-shaped winding magnetic core can be solved, but like the winding magnetic core described in JP-A-2-194504, When an amorphous alloy ribbon was manufactured by the melt quenching method, there was a problem that the stress unavoidably applied to the amorphous alloy ribbon could not be sufficiently relaxed. Therefore, the present invention solves the problem of reliability due to the safe operation and life of the switch element for limiting the repetition frequency, limiting the continuous operation time or generating the pulse, which were problems when the laser device was operated at high repetition rates. The problem is to solve it.
【0021】[0021]
【問題を解決するための手段】本発明は、コバルト基非
晶質合金薄帯をその脆化が進行しても巻回し可能な可撓
性を保持し得る範囲内で熱処理後、この熱処理したコバ
ルト基非晶質合金薄帯の表面に電気的絶縁材を介在させ
巻回し、その後再度熱処理するという製造方法を採用す
るものである。すなわち、レーストラック形状巻磁心を
構成する磁性薄帯として巻回し可能な可撓性を保持し得
る範囲内で熱処理したコバルト基非晶質合金薄帯を用い
同合金薄帯の表面に電気的絶縁材を介在させて巻回し構
成した巻磁心は、同非晶質合金薄帯を融体急冷法で製造
するときに不可避的に加えられた応力を実用状十分なレ
ベルまで緩和でき、占積率(K)を高めるために必要な
張力を加えても同非晶質合金薄帯の破断を防止すること
ができるため占積率(K)が高く、パルスパワー用磁心
として動作させたときの最大動作磁束密度量(ΔBm)
が大きく、飽和領域の比透磁率(μrs)も小さいため磁
心の小型化が図れ、その単位体積当たりの磁心損失も小
さくすることができる。According to the present invention, a cobalt-based amorphous alloy ribbon is heat-treated after being heat-treated within a range capable of maintaining the flexibility of winding even if the embrittlement progresses. In this method, a cobalt-based amorphous alloy ribbon is wound on the surface thereof with an electrically insulating material interposed and then heat-treated again . That is, a cobalt-based amorphous alloy ribbon that has been heat-treated within a range that can maintain the flexibility that can be wound as a magnetic ribbon that constitutes a racetrack-shaped wound magnetic core is used, and the surface of the alloy ribbon is electrically insulated. The wound magnetic core formed by interposing a material intervening material can alleviate the stress unavoidably applied when manufacturing the amorphous alloy ribbon by the melt quenching method to a practically sufficient level, and the space factor Since the fracture of the amorphous alloy ribbon can be prevented even if the tension required to increase (K) is applied, the space factor (K) is high and the maximum when operating as a pulse power magnetic core. Amount of operating magnetic flux density (ΔBm)
Is large and the relative permeability (μ rs ) in the saturation region is small, the magnetic core can be downsized, and the magnetic core loss per unit volume can be reduced.
【0022】また、前記熱処理したコバルト基非晶質合
金薄帯の表面に電気的絶縁材を介在させ巻回して構成し
たレーストラック形状巻磁心を再度熱処理することによ
り、巻磁心を構成するため前記熱処理した非晶質合金薄
帯を巻回したときに同非晶質合金薄帯に加えられた応力
も緩和することができるため、パルスパワー用磁心とし
て使用した際に磁心の小型化と低損失化の面でより優れ
た性能が得られる。 The heat-treated cobalt-based amorphous alloy
It is constructed by winding an electrical insulating material on the surface of the gold ribbon.
By re-heat treating the racetrack-shaped wound core
The heat-treated amorphous alloy to form a wound magnetic core.
Stresses applied to the amorphous alloy ribbon when the ribbon is wound.
Since it can also be relaxed,
Better in terms of downsizing and loss reduction of the magnetic core
Excellent performance can be obtained.
【0023】さらに本発明では上記本発明の巻磁心にお
いて、前記巻磁心を構成する熱処理されたコバルト基非
晶質合金薄帯は熱処理された状態の巻方向と反対方向に
巻回してレーストラック形状巻磁心を構成したパルスパ
ワー用磁心の特性は、従来行われていた巻磁心を構成す
る熱処理された非晶質合金薄帯の巻方向と同非晶質合金
薄帯を熱処理しているときの巻方向を同じにするのに比
べ、熱処理した非晶質合金薄帯を再巻きする回数を減ら
せることにより占積率(K)を容易に向上させることが
できるためその実効最大動作磁束密度量(K・ΔBm)も
向上し、損失も同時に減少させることができることを見
いだした。Further, according to the present invention, in the above wound magnetic core of the present invention, the heat-treated cobalt-based amorphous alloy ribbon forming the wound magnetic core is wound in a direction opposite to the winding direction in the heat-treated state to form a racetrack shape. The characteristics of the pulse power magnetic core forming the winding magnetic core are the same as those of the winding direction of the heat-treated amorphous alloy ribbon forming the winding magnetic core, which is conventionally used, when the amorphous alloy ribbon is heat-treated. The space factor (K) can be easily improved by reducing the number of times of re-winding the heat-treated amorphous alloy ribbon, as compared with the case where the winding direction is the same. We have found that (K · ΔBm) can be improved and loss can be reduced at the same time.
【0024】[0024]
【0025】さらに、コバルト基非晶質合金薄帯をレー
ストラック形状に巻回した後、その直線部を機械的に拘
束した状態で熱処理することにより当該直線部の膨らみ
を防止できる。本発明によるレーストラック形状巻磁心
を用いて構成した高電圧パルス発生装置は、小型で消費
電力の小さな冷却装置でこの巻磁心の冷却が可能となる
ため高繰り返し連続運転時の信頼製に優れ、システム全
体の効率も高い。本発明によるレーストラック形状巻磁
心を用いて構成したレーザ装置は、高効率で信頼製が高
く、従来困難であった高繰り返し周波数領域での連続運
転が可能となる。Further, the cobalt-based amorphous alloy ribbon is wound into a racetrack shape and then heat-treated while the linear portion is mechanically restrained, whereby the bulging of the linear portion can be prevented. The high-voltage pulse generator configured by using the racetrack-shaped winding magnetic core according to the present invention is capable of cooling the winding magnetic core with a cooling device having a small size and small power consumption, and thus is excellent in reliability during high repetition continuous operation, The efficiency of the entire system is also high. The laser device configured by using the racetrack-shaped wound magnetic core according to the present invention is highly efficient and highly reliable, and can be continuously operated in a high repetition frequency region which has been difficult in the past.
【0026】[0026]
【実施例】以下本発明の実施例について詳細に説明する
が、本発明はこれら実施例に限るものではない。
(実施例1)融体急冷法により製作した組成Co68Fe
4Si15B13、飽和磁歪定数+0.2×10-7、キュリー
温度220℃、幅25.4mm、厚さ20μmの非晶質
合金薄帯を巻回し、外径400mm、内径200mmの
トロイダル形状巻磁心1を構成し、このトロイダル形状
巻磁心1を窒素雰囲気中で磁路方向に800A/mの直
流磁場を加えながら所定の1段目熱処理温度まで2時間
で昇温し、この1段目の熱処理温度で2時間熱処理後1
80℃まで2時間で降温し、180℃で4時間保持した
後、常温まで徐冷する2段熱処理を行う。次に、熱処理
したトロイダル形状巻磁心1を図1に示すようにして巻
直し、新たに図5に示すようなレーストラック形状巻磁
心を構成した。前記熱処理したトロイダル形状巻磁心1
を構成する非晶質合金薄帯3を巻戻し、同非晶質合金薄
帯3に0.3Nの張力が加わるようにして同非晶質合金
薄帯3と幅27mm、厚さ4μmのPETフィルム4を
外長径dox500mm、内長径dix480mm、外短径
dom30mm、内短径dim10mm、高さ25.4mm
のSUS304製の巻心5に外長径Dox600mm、外
短径Dom130mmになるまで巻き込み、その最外周を
幅25.4mm、厚さ0.1mmのSUS304製の薄帯
をその両端が20mm重なるようにして一周巻回しこの
SUS304薄帯の重なり部分をスポット溶接し構成す
る。EXAMPLES Examples of the present invention will be described in detail below, but the present invention is not limited to these examples. (Example 1) Composition Co 68 Fe produced by melt quenching method
4 Si 15 B 13 , saturation magnetostriction constant + 0.2 × 10 −7 , Curie temperature 220 ° C., width 25.4 mm, thickness 20 μm amorphous alloy ribbon wound, toroidal shape with outer diameter 400 mm, inner diameter 200 mm The wound magnetic core 1 is constituted, and the toroidal wound magnetic core 1 is heated in a nitrogen atmosphere to a predetermined first step heat treatment temperature for 2 hours while applying a direct current magnetic field of 800 A / m in the magnetic path direction. After 2 hours heat treatment at the heat treatment temperature of 1
The temperature is lowered to 80 ° C. in 2 hours, the temperature is kept at 180 ° C. for 4 hours, and then a two-stage heat treatment is performed to gradually cool to room temperature. Next, the heat-treated toroidal winding core 1 was rewound as shown in FIG. 1 to newly form a racetrack winding core as shown in FIG. The heat-treated toroidal wound magnetic core 1
The amorphous alloy ribbon 3 constituting the above is unwound, and a tension of 0.3 N is applied to the amorphous alloy ribbon 3 and the PET having a width of 27 mm and a thickness of 4 μm. The film 4 has an outer long diameter dox 500 mm, an inner long diameter dix 480 mm, an outer short diameter dom 30 mm, an inner short diameter dim 10 mm, and a height 25.4 mm.
It is wound around the core 5 made of SUS304 until the outer long diameter Dox 600 mm and the outer short diameter Dom 130 mm, and the outermost circumference is made of SUS304 thin strips having a width of 25.4 mm and a thickness of 0.1 mm so that both ends overlap each other by 20 mm. It is wound around once, and the overlapping portion of this SUS304 ribbon is spot-welded to form.
【0027】1段目の熱処理温度を200℃から350
℃までの範囲で変えて熱処理した前記組成の非晶質合金
薄帯3を用い、上記のようにしてレーストラック形状巻
磁心を構成した結果を表1に示す。なお、表1において
破壊時の最大歪εfは磁心を構成するのに用いた熱処理
した非晶質合金薄帯3を湾曲させて2枚の平行板の間に
挟んだときに同合金薄帯3が破壊しない最少の平行板間
隔をL、同合金薄帯3の厚みをtとし、次式で定義し
た。
εf=t/(L−t) (1)
表1からもわかるように、εfが0.05より小さくなる
1段目の熱処理温度が300℃を越える場合には頻繁に
破断するためレーストラック形状巻磁心を構成するのを
断念した。The heat treatment temperature of the first step is set from 200 ° C. to 350
Table 1 shows the results of constructing the racetrack-shaped wound magnetic core as described above by using the amorphous alloy ribbon 3 having the above-mentioned composition which was heat-treated while being changed in the range up to ° C. It should be noted that in Table 1, the maximum strain ε f at the time of breakage is obtained by bending the heat-treated amorphous alloy ribbon 3 used to construct the magnetic core and sandwiching it between two parallel plates. The minimum parallel plate distance that does not cause damage is L, and the thickness of the alloy thin ribbon 3 is t. ε f = t / (Lt) (1) As can be seen from Table 1, when the heat treatment temperature of the first step, where ε f is less than 0.05, exceeds 300 ° C, it frequently breaks and races. Abandoned the construction of track-shaped wound cores.
【0028】[0028]
【表1】 [Table 1]
【0029】表1の4つのレーストラック形状巻磁心を
図2のパルス駆動時の磁気特性測定回路を用いリセット
磁化力を16A/mとし、中島、香川、平尾、渡部、
“鉄基超微結晶質合金を用いた磁気スイッチ磁心の動特
性評価”、電気学会 プラズマ研究会資料、EP-91-13、
p.1〜10 (1991)にその詳細が記載される方法により測定
時に試料に設けられた1タ−ンの巻線間に誘起する電圧
パルスの半値幅τhを0.1μsとなるようにして測定し
た結果を表2に示す。図2において11は直流高電圧電
源、12はコンデンサ15の充電抵抗、13はサイラト
ロン、14は配線により生じるインダクタンス、15は
コンデンサ、16は測定する巻磁心に1タ−ンの巻線の
施された可飽和リアクトル、17はサイラトロン13が
オンしたときに直流電源18に流れようとするサージ電
流阻止用のリアクトル、18は測定する磁心で構成され
た可飽和リアクトル16をリセットするための直流電源
である。The four racetrack-shaped wound magnetic cores shown in Table 1 were set to a reset magnetizing force of 16 A / m by using the magnetic characteristic measuring circuit at the time of pulse driving shown in FIG. 2, and Nakajima, Kagawa, Hirao, Watanabe,
"Evaluation of dynamic characteristics of magnetic switch magnetic core using iron-based ultrafine crystalline alloy", Institute of Electrical Engineers of Japan Plasma Research Material, EP-91-13,
The half-value width τ h of the voltage pulse induced between the 1-turn windings provided on the sample at the time of measurement should be 0.1 μs by the method described in detail in p.1-10 (1991). Table 2 shows the results of the measurement. In FIG. 2, 11 is a DC high-voltage power supply, 12 is a charging resistance of a capacitor 15, 13 is a thyratron, 14 is an inductance generated by wiring, 15 is a capacitor, 16 is a winding core to be measured, and a 1-turn winding is applied. Saturable reactor, 17 is a reactor for blocking surge current which tends to flow to the DC power supply 18 when the thyratron 13 is turned on, and 18 is a DC power supply for resetting the saturable reactor 16 composed of the magnetic core to be measured. is there.
【0030】表2において比較例1から比較例5は、前
記参考例1から参考例4と同一組成、同一幅かつ同一厚
みのコバルト基非晶質合金薄帯を用い、下記の手法によ
り製作したものである。比較例1は熱処理した非晶質合
金薄帯の代わりに熱処理してない非晶質合金薄帯を用い
他は参考例と同一手法で製作した。比較例2は熱処理前
の非晶質合金薄帯を幅27mm、厚さ7.5μmのPI
フィルムとともに巻回してレーストラック形状巻磁心を
構成した後、窒素雰囲気中で磁路方向に800A/mの
直流磁場を加えながら2時間で350℃まで昇温後2時
間保持し、2時間で180℃まで降温後4時間保持した
後、常温まで徐冷した。比較例3は熱処理前の非晶質合
金薄帯を幅27mm、厚さ4μmのPETフィルムとと
もに巻回してレーストラック形状巻磁心を構成した後、
窒素雰囲気中で磁路方向に800A/mの直流磁場を加
えながら2時間で180℃まで昇温後3時間保持した
後、常温まで徐冷した。比較例4は、1段目の熱処理温
度を350℃として前記参考例と同様にして熱処理し十
分冷却した第1のトロイダル形状巻磁心を別のトロイダ
ル形状の第2の巻磁心として巻回し直し、これをさらに
前記本発明と同様にPETフィルムを介在させながら前
記第2のトロイダル形状巻磁心に巻き込まれた熱処理し
た非晶質合金薄帯に0.1Nの弱い張力を加えながら巻
回して構成したレーストラック形状の巻磁心である。な
お、本磁心を製作する際に熱処理した非晶質合金薄帯の
破断回数は21回にも及んだ。比較例5は熱処理前の非
晶質合金薄帯とPETフィルムを同時に巻回してトロイ
ダル形状巻磁心を製作した後レーストラック形状に変形
し、窒素雰囲気中で磁路方向に800A/mの直流磁場
を加えながら2時間で180℃まで昇温後3時間保持し
た後、常温まで徐冷して構成した。[0030] Example Comparative Comparative Example 1 in Table 2 5, using a cobalt-based amorphous alloy ribbon of the same composition as Example 4 from Example 1, the same width and the same thickness, were manufactured by the following method It is a thing. Comparative Example 1 was manufactured in the same manner as in Reference Example except that the amorphous alloy ribbon which was not heat-treated was used instead of the heat-treated amorphous alloy ribbon. In Comparative Example 2, an amorphous alloy ribbon before heat treatment was used as a PI having a width of 27 mm and a thickness of 7.5 μm.
After winding together with the film to form a racetrack-shaped wound magnetic core, a direct current magnetic field of 800 A / m was applied in the magnetic path direction in a nitrogen atmosphere, the temperature was raised to 350 ° C. in 2 hours, then held for 2 hours, and then 180 ° in 2 hours. After the temperature was lowered to 0 ° C., the temperature was maintained for 4 hours, and then gradually cooled to room temperature. In Comparative Example 3, an amorphous alloy ribbon before heat treatment was wound together with a PET film having a width of 27 mm and a thickness of 4 μm to form a racetrack-shaped wound magnetic core.
In a nitrogen atmosphere, a direct current magnetic field of 800 A / m was applied in the magnetic path direction, the temperature was raised to 180 ° C. in 2 hours, then held for 3 hours, and then gradually cooled to room temperature. In Comparative Example 4, the first toroidal-shaped winding magnetic core, which was heat-treated and sufficiently cooled in the same manner as the above-mentioned Reference Example with the first-stage heat treatment temperature set at 350 ° C., was rewound as another toroidal-shaped second winding magnetic core, As in the case of the present invention, this was further wound by applying a weak tension of 0.1 N to the heat-treated amorphous alloy ribbon wound around the second toroidal winding magnetic core while interposing a PET film therebetween. It is a racetrack-shaped wound magnetic core. The number of times of rupture of the amorphous alloy ribbon subjected to the heat treatment when manufacturing the magnetic core reached 21 times. In Comparative Example 5, an amorphous alloy ribbon before heat treatment and a PET film were wound at the same time to produce a toroidal wound magnetic core, which was then transformed into a racetrack shape and a DC magnetic field of 800 A / m in the magnetic path direction in a nitrogen atmosphere. Was added, the temperature was raised to 180 ° C. in 2 hours, the temperature was maintained for 3 hours, and then gradually cooled to room temperature.
【0031】[0031]
【表2】 [Table 2]
【0032】表2からもわかるように参考例1から参考
例4は占積率Kが0.67以上、最大動作磁束密度量Δ
Bmが実効飽和磁束密度Bms0.57Tの1.9倍以上の
1.09T以上かつ飽和領域の比透磁率μrsも1.3以下
であり、比較例に比べて優れることがわかる。As can be seen from Table 2, reference from Reference Example 1
In Example 4, the space factor K is 0.67 or more, and the maximum operating magnetic flux density amount Δ
Bm is the relative magnetic permeability mu rs of 1.9 times or more 1.09T or more and the saturation region of the effective saturation flux density Bms0.57T also 1.3 or less, it can be seen that excellent as compared with the ratio Comparative Examples.
【0033】上記参考例1から参考例4および比較例1
から比較例5のレーストラック形状巻磁心を図3の回路
構成のKrFエキシマレーザ用高電圧パルス発生装置の
磁気アシスト用可飽和リアクトル24の磁心に実装して
特性評価を行った。図3において21は入力直流高電圧
電源、22は主コンデンサ25の充電抵抗、23はサイ
ラトロン、24は磁気アシスト用可飽和リアクトル、2
5は主コンデンサ、26は主コンデンサ25の充電用リ
アクトル、27はピーキング・コンデンサ、28は紫外
光予備電離用ギャップ、29はレーザ主放電電極であ
る。なお、実装試験では、入力直流高電圧電源21の電
圧を30kV、主コンデンサ22とピーキング・コンデ
ンサ27の容量を50nF、レーザ主放電電極の有効長
と間隔を各々800mmおよび30mm、繰り返し周波
数を100Hz、磁気アシスト用可飽和リアクトルの巻
数を1としレーストラック形状巻磁心はシリコンオイル
で強制冷却した。[0033] Reference from the above-mentioned Reference Example 1 Example 4 and Comparative Example 1
From the above, the racetrack-shaped wound magnetic core of Comparative Example 5 was mounted on the magnetic core of the magnetically assistable saturable reactor 24 of the high-voltage pulse generator for the KrF excimer laser having the circuit configuration of FIG. In FIG. 3, 21 is an input DC high voltage power supply, 22 is a charging resistance of the main capacitor 25, 23 is a thyratron, 24 is a magnetic assist saturable reactor, 2
Reference numeral 5 is a main capacitor, 26 is a reactor for charging the main capacitor 25, 27 is a peaking capacitor, 28 is a gap for ultraviolet light preionization, and 29 is a laser main discharge electrode. In the mounting test, the voltage of the input DC high voltage power source 21 was 30 kV, the capacities of the main capacitor 22 and the peaking capacitor 27 were 50 nF, the effective lengths and intervals of the laser main discharge electrodes were 800 mm and 30 mm, respectively, and the repetition frequency was 100 Hz. The number of turns of the saturable reactor for magnetic assist was 1, and the racetrack-shaped wound magnetic core was forcibly cooled with silicon oil.
【0034】上記参考例1から参考例4および比較例1
から比較例5のレーストラック形状巻磁心を図3の回路
に実装したときのエネルギ−転送効率ηt、レーザ発振
効率ηおよび磁心の温度上昇ΔTの比較を表3に示す。
ここで、エネルギ−転送効率ηtはピーキング・コンデ
ンサ27に転送されたエネルギ−を主コンデンサ25の
蓄積エネルギ−で割った値、レーザ発振効率ηはレーザ
エネルギ−を主コンデンサ25の蓄積エネルギ−で割っ
た値である。参考例による磁心を用いた場合にはエネル
ギ−転送効率ηtが比較例の磁心を用いた場合より4%
以上高くなり、レーザ発振効率ηも1.26倍以上向上
できた。また、磁心の温度上昇も11℃以上低下させる
ことができるため消費電力の小さな冷却装置を用いて従
来困難であったより高い繰り返し周波数での連続運転も
可能となる。[0034] Reference from the above-mentioned Reference Example 1 Example 4 and Comparative Example 1
Table 3 shows a comparison of the energy transfer efficiency η t , the laser oscillation efficiency η, and the temperature rise ΔT of the magnetic core when the racetrack-shaped wound magnetic core of Comparative Example 5 is mounted on the circuit of FIG.
Here, the energy transfer efficiency η t is a value obtained by dividing the energy transferred to the peaking capacitor 27 by the stored energy of the main capacitor 25, and the laser oscillation efficiency η is the laser energy stored energy of the main capacitor 25. It is the divided value. When the magnetic core according to the reference example is used, the energy transfer efficiency η t is 4% as compared with the magnetic core of the comparative example.
As a result, the laser oscillation efficiency η was improved by 1.26 times or more. Further, since the temperature rise of the magnetic core can be reduced by 11 ° C. or more, continuous operation at a higher repetition frequency, which has been difficult in the past, can be performed by using a cooling device with low power consumption.
【0035】[0035]
【表3】 [Table 3]
【0036】(実施例2)実施例1と同一組成同一寸法
の非晶質合金薄帯を巻き回し外径400mm、内径20
0mmのトロイダル形状の第一の巻磁心を構成し、この
巻磁心を窒素雰囲気中で磁路方向に800A/mの直流
磁場を加えながら250℃まで2時間で昇温し所定の時
間保持した後、常温まで徐冷する熱処理を行う。次に、
熱処理した第一の巻磁心1を実施例1と同様にして巻き
直し、新たに図5に示すようなレーストラック形状巻磁
心を構成した。なお、レーストラック形状巻磁心の寸法
および構造は前記実施例1と同一とした。(Example 2) An amorphous alloy ribbon having the same composition and size as in Example 1 was wound and the outer diameter was 400 mm and the inner diameter was 20.
After constructing a toroidal first wound magnetic core of 0 mm, and heating the wound magnetic core to 250 ° C. for 2 hours while applying a direct current magnetic field of 800 A / m in the magnetic path direction in a nitrogen atmosphere, and holding for a predetermined time Then, heat treatment is performed to gradually cool to room temperature. next,
The heat-treated first wound magnetic core 1 was rewound in the same manner as in Example 1 to newly form a racetrack-shaped wound magnetic core as shown in FIG. The size and structure of the racetrack-shaped wound magnetic core were the same as in Example 1.
【0037】250℃における保持時間を2時間、5時
間、10時間、20時間、50時間、100時間、20
0時間として熱処理した前記組成の非晶質合金薄帯を用
い、上記のようにしてレーストラック形状巻磁心を構成
した結果を表4に示す。なお、表4において破壊時の最
大歪εfは前記実施例1の場合と同様に定義し測定し
た。表4からもわかるように250℃の保持時間が50
時間を越えると破断が急増し、100時間以上の場合に
は頻繁に破断するためレーストラック形状巻磁心を構成
するのを断念した。The holding time at 250 ° C. is 2 hours, 5 hours, 10 hours, 20 hours, 50 hours, 100 hours, 20 hours.
Table 4 shows the results of forming the racetrack-shaped wound magnetic core as described above using the amorphous alloy ribbon of the above composition which was heat-treated for 0 hours. In Table 4, the maximum strain ε f at break was defined and measured in the same manner as in Example 1 above. As can be seen from Table 4, the holding time at 250 ° C is 50
When the time was exceeded, the number of fractures increased sharply, and when the time was 100 hours or more, the fractures frequently occurred. Therefore, the race track-shaped wound magnetic core was abandoned.
【0038】[0038]
【表4】 [Table 4]
【0039】表4の5つのレーストラック形状巻磁心と
前記比較例1から比較例5を前記図2のパルス駆動時の
磁気特性測定回路を用いリセット磁化力を16A/mと
し、測定時に試料に設けられた1タ−ンの巻線間に誘起
する電圧パルスの半値幅τhを0.1μsとなるようにし
て測定した結果を表5に示す。表5からもわかるように
参考例2、参考例5から参考例8は占積率Kが0.68
以上、最大動作磁束密度量ΔBmが実効飽和磁束密度Bm
s0.57Tの1.9倍以上の1.12T以上かつ飽和領域
の比透磁率μrsも1.2以下と小さく、比較例に比べて
優れることがわかる。Using the five racetrack-shaped winding magnetic cores of Table 4 and the comparative examples 1 to 5 with the magnetic characteristic measuring circuit at the time of pulse driving shown in FIG. 2, the reset magnetizing force was set to 16 A / m, and the sample was measured at the time of measurement. Table 5 shows the results of measurement with the half-value width τ h of the voltage pulse induced between the provided 1-turn windings set to 0.1 μs. As you can see from Table 5
Reference Example 2, Reference from Reference Example 5 Example 8 space factor K is 0.68
As described above, the maximum operating magnetic flux density amount ΔBm is the effective saturation magnetic flux density Bm.
or 1.12T 1.9 times more s0.57T and also relative permeability mu rs saturation region as small as 1.2 or less, it can be seen that excellent as compared with the ratio Comparative Examples.
【0040】上記参考例2、参考例5から参考例8およ
び比較例1から比較例5のレーストラック形状巻磁心を
図3の回路構成のKrFエキシマレーザ用高電圧パルス
発生装置の磁気アシスト用可飽和リアクトル14の磁心
に実装して特性評価を行った。なお、実装試験の条件は
前記実施例1の時と同じとした。上記参考例2、参考例
5から参考例8および比較例1から比較例5のレースト
ラック形状巻磁心を図3の回路に実装したときのエネル
ギ−転送効率ηt、レーザ発振効率ηおよびレーストラ
ック形状巻磁心の温度上昇ΔTの比較を表6に示す。表
6からわかるように参考例のレーストラック形状巻磁心
を用いた場合にはエネルギ−転送効率ηtが比較例のレ
ーストラック形状巻磁心を用いた場合より5%以上高
く、レーザ発振効率ηは1.37倍向上する。また、磁
心の温度上昇も従来例に比べて13℃以上低減でき、消
費電力の小さな冷却装置を用いより高い繰り返し周波数
での連続運転も可能となる。The racetrack-shaped winding magnetic cores of Reference Example 2, Reference Example 5 to Reference Example 8 and Comparative Example 1 to Comparative Example 5 can be used for magnetic assist of the high voltage pulse generator for the KrF excimer laser having the circuit configuration of FIG. The characteristics were evaluated by mounting on the magnetic core of the saturated reactor 14. The conditions of the mounting test were the same as those in the first embodiment. Energy transfer efficiency η t , laser oscillation efficiency η and race track when the racetrack-shaped winding cores of Reference Example 2, Reference Example 5 to Reference Example 8 and Comparative Example 1 to Comparative Example 5 are mounted in the circuit of FIG. Table 6 shows a comparison of the temperature increase ΔT of the shape wound magnetic core. As can be seen from Table 6, the energy transfer efficiency η t in the case of using the racetrack-shaped winding magnetic core of the reference example is 5% or more higher than that in the case of using the racetrack-shaped winding magnetic core of the comparative example, and the laser oscillation efficiency η is 1.37 times improvement. Further, the temperature rise of the magnetic core can be reduced by 13 ° C. or more as compared with the conventional example, and continuous operation at a higher repetition frequency is possible using a cooling device with low power consumption.
【0041】[0041]
【表5】 [Table 5]
【0042】[0042]
【表6】 [Table 6]
【0043】(実施例3)
前記実施例1で使用したコバルト基非晶質合金薄帯を使
用し外径400mm、内径200mmのトロイダル形状
の第一の巻磁心を構成し、この巻磁心を窒素雰囲気中で
磁路方向に800A/mの直流磁場を加えながら250
℃まで2時間で昇温し20時間保持した後、常温まで徐
冷する熱処理を行う。図1に示すように前記熱処理した
トロイダル形状巻磁心1を構成する非晶質合金薄帯3を
巻戻し、前記実施例1と同様の手法で条件で同非晶質合
金薄帯3と幅27mm、厚さ4μmのPETフィルム4
を外長径dox500mm、内長径dix480mm、外短
径dom30mm、内短径dim10mm、高さ25.4m
mのSUS304製の巻心5に外長径Dox600mm、
外短径Dom130mmになるまで巻き込んだ。このと
き、熱処理した非晶質合金薄帯は1度も破断せず、磁心
の占積率Kは0.70、熱処理した非晶質合金薄帯の破
壊時の最大歪εfは0.062であった。このレーストラ
ック形状巻磁心を図6に示すようにSUS304製の押
さえ板6ではさみこの押さえ板の両端をボルト7で締め
込むことによりレーストラック形状磁心の直線部の膨ら
みを押さえ込んで、さらに大気中で磁路方向に800A
/mの直流磁場を加えながら150℃まで2時間で昇
温、10時間保持した後、常温まで徐冷した。その後、
前記押さえ板6を取り外し、その最外周を幅25.4m
m、厚さ0.1mmのSUS304製の薄帯をその両端
が20mm重なるようにして一周巻回し、このSUS3
04薄帯の重なり部分をスポット溶接して本発明1のレ
ーストラック形状巻磁心を構成した。(Example 3) The cobalt-based amorphous alloy ribbon used in Example 1 was used to form a toroidal first winding core having an outer diameter of 400 mm and an inner diameter of 200 mm. 250 while applying a DC magnetic field of 800 A / m in the magnetic path direction in the atmosphere
After the temperature is raised to 0 ° C. in 2 hours and the temperature is maintained for 20 hours, heat treatment is performed to gradually cool to room temperature. As shown in FIG. 1, the amorphous alloy ribbon 3 constituting the heat-treated toroidal wound magnetic core 1 is unwound, and the amorphous alloy ribbon 3 and the width 27 mm under the same conditions as in Example 1 are used. , PET film 4 with a thickness of 4 μm
Outer major axis dox 500 mm, inner major axis dix 480 mm, outer minor axis dom 30 mm, inner minor axis dim 10 mm, height 25.4 m
m of SUS304 core 5 with an outer long diameter Dox 600 mm,
It was rolled up until the outer short diameter Dom 130mm. At this time, the heat-treated amorphous alloy ribbon was never broken, the space factor K of the magnetic core was 0.70, and the maximum strain ε f at the time of fracture of the heat-treated amorphous alloy ribbon was 0.062. Met. As shown in FIG. 6, this racetrack-shaped wound magnetic core is clamped by a pressing plate 6 made of SUS304, and both ends of the pressing plate are tightened with bolts 7 to press down the bulge of the straight portion of the racetrack-shaped magnetic core, and further in the atmosphere. 800A in the magnetic path direction
The temperature was raised to 150 ° C. in 2 hours while maintaining a direct current magnetic field of / m, held for 10 hours, and then gradually cooled to room temperature. afterwards,
The pressing plate 6 is removed, and the outermost circumference is 25.4 m wide.
A SUS304 thin strip having a thickness of 0.1 mm and a thickness of 0.1 mm is wound once with both ends overlapping each other by 20 mm.
The overlapping portion of the 04 ribbon was spot-welded to form the racetrack-shaped wound magnetic core of the present invention 1 .
【0044】本発明1のレーストラック形状巻磁心と最
終熱処理以外は同様に構成した前記実施例2の参考例7
のレーストラック形状巻磁心および比較例1から比較例
5のレーストラック形状巻磁心の短パルス駆動時の動特
性の比較を表7に示す。表7からわかるように本実施例
による本発明1のレーストラック形状巻磁心は前記実施
例2における参考例7のレーストラック形状巻磁心に比
べて実効動作磁束密度量K・ΔBmが増加するととも
に、単位体積当たりのゲート半周期の磁心損失Pcgも減
少する。レーストラック形状巻磁心構成後の熱処理によ
って巻磁心動特性が改善されるのは、熱処理した非晶質
合金薄帯を巻回して磁心を製作した際にこの熱処理した
非晶質合金薄帯に加えられた応力が緩和されるとともに
図6に示す押さえ板6の使用により図4の一点鎖線部の
不要な膨らみが押さえられたためである。なお、レース
トラック形状巻磁心構成後の熱処理は、本実施例のよう
に層間絶縁に用いている絶縁材の耐熱温度の制約で定め
られる熱処理温度の上限を越えない範囲で適切な時間行
わなくてはならないことは言うまでもない。 Reference Example 7 of Example 2 having the same structure except for the racetrack-shaped wound magnetic core of the present invention 1 and the final heat treatment.
Table 7 shows the comparison of the dynamic characteristic during the short pulse drive of racetrack winding core and racetrack winding magnetic core of Comparative Example 5 Comparative Example 1. As can be seen from Table 7, in the racetrack-shaped winding core of the present invention 1 according to the present embodiment, the effective operating magnetic flux density amount K · ΔBm increases as compared with the racetrack-shaped winding core of Reference Example 7 in the second embodiment. The magnetic core loss Pcg of the gate half cycle per unit volume is also reduced. The dynamic characteristics of the wound magnetic core are improved by the heat treatment after the formation of the racetrack-shaped wound magnetic core when the heat-treated amorphous alloy ribbon is added to the heat-treated amorphous alloy ribbon when the magnetic core is manufactured by winding the heat-treated amorphous alloy ribbon. This is because the applied stress is relieved and unnecessary bulging of the one-dot chain line portion in FIG. 4 is suppressed by using the pressing plate 6 shown in FIG. The heat treatment after the formation of the racetrack-shaped wound magnetic core must be performed for an appropriate time within the range not exceeding the upper limit of the heat treatment temperature determined by the restriction of the heat resistant temperature of the insulating material used for the interlayer insulation as in this example. It goes without saying that this should not be the case.
【0045】[0045]
【表7】 [Table 7]
【0046】本実施例のレーストラック形状巻磁心につ
いて図3の回路構成のKrFエキシマレーザ用高電圧パ
ルス発生装置の磁気アシスト用可飽和リアクトル14の
磁心に実装して前記実施例2と同一条件で特性評価を行
った。本実施例のレーストラック形状巻磁心と前記実施
例2の参考例7のレーストラック形状巻磁心および比較
例5から比較例8の磁心を図3の回路に実装したときの
エネルギ−転送効率ηt、レーザ発振効率ηおよび巻磁
心の温度上昇ΔTの比較を表8に示す。表8からわかる
ように本発明によるレーストラック形状巻磁心を用いた
場合にはエネルギ−転送効率ηtが比較例のレーストラ
ック形状巻磁心を用いた場合より6%以上高く、レーザ
発振効率ηは1.42倍向上する。また、磁心の温度上
昇も比較例に比べて15℃以上低減でき、前記実施例2
の場合よりも消費電力の小さな冷却装置を用いより高い
繰り返し周波数での連続運転も可能となる。なお、本実
施例に記載した熱処理したコバルト基非晶質合金薄帯を
巻回してレーストラック形状巻磁心を構成した後に、再
度同レーストラック形状巻磁心を熱処理して磁気特性の
向上図ることは、本実施例以外の組成のコバルト基非晶
質合金を用いた場合にも有効である。The racetrack-shaped wound magnetic core of this embodiment was mounted on the magnetic core of the magnetically assistable saturable reactor 14 of the high voltage pulse generator for the KrF excimer laser having the circuit configuration shown in FIG. 3 under the same conditions as in the second embodiment. The characteristics were evaluated. Energy-transfer efficiency η t when the racetrack-shaped winding magnetic core of the present embodiment, the racetrack-shaped winding magnetic core of Reference Example 7 of the second embodiment and the magnetic cores of Comparative Examples 5 to 8 are mounted in the circuit of FIG. Table 8 shows a comparison between the laser oscillation efficiency η and the temperature rise ΔT of the winding magnetic core. As can be seen from Table 8, the energy transfer efficiency η t in the case of using the racetrack-shaped winding magnetic core according to the present invention is 6% or more higher than that in the case of using the racetrack-shaped winding magnetic core of the comparative example, and the laser oscillation efficiency η is Improves 1.42 times. Further, the temperature rise of the magnetic core can be reduced by 15 ° C. or more as compared with the comparative example.
Continuous operation at a higher repetition frequency is also possible using a cooling device that consumes less power than in the above case. In addition, after the heat treatment of the cobalt-based amorphous alloy ribbon described in this example is wound to form a racetrack-shaped winding core, the racetrack-shaped winding core is heat-treated again to improve the magnetic characteristics. It is also effective when a cobalt-based amorphous alloy having a composition other than that of this embodiment is used.
【0047】[0047]
【表8】 [Table 8]
【0048】[0048]
【発明の効果】以上説明したように本発明によれば、エ
キシマレーザ、TEA−CO2レーザ、TEMA−CO2
レーザ、銅蒸気レーザを始めとするレーザ装置を高繰り
返し運転するときに問題であった繰り返し周波数の制
限、連続動作時間の制限あるいはパルスを発生させるた
めのスイッチ素子の安全動作と寿命に起因する信頼性の
問題を対策することができる。As described above, according to the present invention, an excimer laser, a TEA-CO 2 laser, a TEMA-CO 2
Reliable due to safe operation and life of switching element for limiting repetition frequency, continuous operation time or pulse, which was a problem when operating laser equipment such as laser and copper vapor laser at high repetition rate. You can deal with sexual problems.
【図1】本発明の一実施例におけるレーストラック形状
巻磁心の製作方法を説明するための概念図である。FIG. 1 is a conceptual diagram for explaining a method of manufacturing a racetrack-shaped wound magnetic core according to an embodiment of the present invention.
【図2】レーストラック形状巻磁心の高電圧パルス駆動
時の動特性を測定するための回路構成概念図である。FIG. 2 is a conceptual diagram of a circuit configuration for measuring dynamic characteristics of a racetrack-shaped wound magnetic core when driven by a high voltage pulse.
【図3】磁気アシスト回路を用いたエキシマレーザ主回
路の回路構成概念図である。FIG. 3 is a conceptual diagram of a circuit configuration of an excimer laser main circuit using a magnetic assist circuit.
【図4】レーストラック形状巻磁心の構成図である。FIG. 4 is a configuration diagram of a racetrack-shaped wound magnetic core.
【図5】レーストラック形状巻磁心の構成図である。FIG. 5 is a configuration diagram of a racetrack-shaped wound magnetic core.
【図6】本発明の一実施例におけるレーストラック形状
巻磁心の製作法中の巻磁心構成後の再熱処理方法の説明
図である。FIG. 6 is an explanatory diagram of a reheat treatment method after the winding core is configured during the method of manufacturing the racetrack-shaped winding core according to the embodiment of the present invention.
1巻磁心、2レーストラック形状巻磁心、3非晶質合金
薄帯、4PETフィルム
5巻心1 winding core, 2 racetrack shape winding core, 3 amorphous alloy ribbon, 4 PET film 5 winding core
───────────────────────────────────────────────────── フロントページの続き (58)調査した分野(Int.Cl.7,DB名) H01F 27/25 H01F 41/02 H01S 3/097 H02M 9/04 ─────────────────────────────────────────────────── ─── Continuation of front page (58) Fields surveyed (Int.Cl. 7 , DB name) H01F 27/25 H01F 41/02 H01S 3/097 H02M 9/04
Claims (5)
進行しても巻回し可能な可撓性を保持し得る範囲内で熱
処理後、この熱処理したコバルト基非晶質合金薄帯の表
面に電気的絶縁材を介在させ巻回し、その後再度熱処理
することを特徴とするレーストラック形状巻磁心の製造
方法。1. A cobalt-based amorphous alloy ribbon which has been heat-treated after being heat-treated within a range capable of maintaining the flexibility of winding even if the embrittlement progresses. The surface of the product is wound with an electrically insulating material interposed and then heat treated again.
A method of manufacturing a racetrack-shaped wound magnetic core, comprising:
ルト基非晶質合金薄帯は熱処理された状態の巻方向と反
対方向に巻回す請求項1に記載のレーストラック形状巻
磁心の製造方法。2. A method for producing a race track shape wound core according to claim 1 wherein the heat treated cobalt-based amorphous alloy ribbon constituting the winding core is rotating around the direction opposite to the winding direction in a state of being heat-treated .
進行しても巻回し可能な可撓性を保持し得る範囲内で熱
処理後、この熱処理したコバルト基非晶質合金薄帯の表
面に電気的絶縁材を介在させレーストラック形状に巻回
した後、その直線部を機械的に拘束した状態で熱処理す
ることを特徴とするレーストラック形状巻磁心の製造方
法。3. A cobalt-based amorphous alloy ribbon which has been heat-treated after being heat-treated within a range capable of maintaining the flexibility of winding even if the embrittlement progresses. A method for producing a racetrack-shaped wound magnetic core, comprising: winding a racetrack shape with an electrically insulating material interposed on the surface of the core and heat-treating the wire while mechanically restraining the straight portion.
ーストラック形状巻磁心を用いて構成したことを特徴と
する高電圧パルス発生装置。4. A high-voltage pulse generator comprising the racetrack-shaped wound magnetic core according to any one of claims 1 to 3 .
ーストラック形状巻磁心を用いて構成したことを特徴と
するレーザ装置。5. A laser device comprising the racetrack-shaped wound magnetic core according to any one of claims 1 to 3 .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP06780493A JP3438825B2 (en) | 1993-03-26 | 1993-03-26 | Wound core, method of manufacturing wound core, high-voltage pulse generator, and laser device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP06780493A JP3438825B2 (en) | 1993-03-26 | 1993-03-26 | Wound core, method of manufacturing wound core, high-voltage pulse generator, and laser device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH06283355A JPH06283355A (en) | 1994-10-07 |
| JP3438825B2 true JP3438825B2 (en) | 2003-08-18 |
Family
ID=13355512
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP06780493A Expired - Fee Related JP3438825B2 (en) | 1993-03-26 | 1993-03-26 | Wound core, method of manufacturing wound core, high-voltage pulse generator, and laser device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3438825B2 (en) |
-
1993
- 1993-03-26 JP JP06780493A patent/JP3438825B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH06283355A (en) | 1994-10-07 |
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