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JP3576397B2 - Energization control method of magnetic bearing used for high-speed rotating body and its control circuit - Google Patents
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JP3576397B2 - Energization control method of magnetic bearing used for high-speed rotating body and its control circuit - Google Patents

Energization control method of magnetic bearing used for high-speed rotating body and its control circuit Download PDF

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JP3576397B2
JP3576397B2 JP28036298A JP28036298A JP3576397B2 JP 3576397 B2 JP3576397 B2 JP 3576397B2 JP 28036298 A JP28036298 A JP 28036298A JP 28036298 A JP28036298 A JP 28036298A JP 3576397 B2 JP3576397 B2 JP 3576397B2
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magnetic
magnetic pole
magnetic bearing
rotating shaft
bearing
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JP2000110835A (en
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勝久 外山
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Mitsubishi Heavy Industries Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0444Details of devices to control the actuation of the electromagnets
    • F16C32/0457Details of the power supply to the electromagnets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/44Centrifugal pumps
    • F16C2360/45Turbo-molecular pumps

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は負荷に連結された回転軸若しくは該回転軸と一体的に回転する磁性部材(以下回転軸部という)を挟んで、夫々対称位置に配置した各対毎の磁気軸受の通電制御により前記回転軸部を空中維持しながら、該回転軸部を高速回転させるターボ分子ポンプ等の高速回転体の磁気軸受の通電制御方法とその制御回路に係り、特に半導体製造装置等に装備され、上部ケーシング内に設けられた静翼と回転軸に設けられた動翼とで構成された動静翼段を備えたターボ分子ポンプに用いる磁気軸受の通電制御方法とその制御回路に関する。
【0002】
【従来の技術】
従来より、球軸受や転がり軸受のように機械的に回転体や直線移動体を支持する機械的軸受の代りに、磁気の力により前記回転体や直線移動体を支持する磁気軸受は公知である。
かかる磁気軸受は従来の流体潤滑軸受よりロスが小さく、軸受のドライ化、雰囲気のクリーン化を図り得、特に真空状態では有用な軸受であるために、ターボ分子ポンプ等の直結モ−タにより高速駆動される高速回転体は回転部の軸受として多用されている。
このような磁気軸受を有するターボ分子ポンプの構成を図4に示す。
【0003】
図4は本発明に適用されるターボ分子ポンプの1例を示し、図4(A)において、1及び16は、ボルト21によりOリング15を介して一体的に組付けられている上部ケーシング及び下部ケーシングである。
該上部ケーシング1の上部開口はガス吸気口2となすとともに、その内側にはリング状空隙を介して複数のスペーサ13が軸方向に連設されている。
該スペーサ13は上端を前記上部ケーシング1の内端面に当接され、下端を前記下部ケーシング16の上端部にインロー嵌合されており、各スペーサ13の間には静翼4がその外周部を挟持固定されて、多段状に設けられている。
【0004】
6はロータで、該ロータ6には動翼5が多段状に設けられ、各動翼5と静翼4とが交互に噛み合う如く設けられての翼段を構成している。前記ロータ6の下部にはねじ溝ポンプ段8が設けられている。
14は複数のボルト18により前記下部ケーシング16の上面に固定されたテーパ状のシールリングで、前記ねじ溝ポンプ段8の外周と微小間隙を介して対向配置され、圧縮効果を上げている。
【0005】
前記下部ケーシング16の下方側部には排気口3が開口され、前記ねじ溝ポンプ段8を通ってきた流体が該排気口3から外部に送出されるようになっている。
17は前記下部ケーシング16の中心域において上方に突設された円筒状の支持筒で、該支持筒17の内周には上部から順に、ラジアル玉軸受からなる上部保護軸受19、ラジアル軸受である上部磁気軸受9、モータ12のステータ部12a、ラジアル軸受である下部磁気軸受10、ラジアル玉軸受からなる下部保護軸受20、並びに後述する回転軸7の下端のスラストディスク7aを挟んで設けられたスラスト磁気軸受11が配設されている。
【0006】
7は前記ロータ6の上部中心に固定された回転軸で、該回転軸7は前記ロータ6への固定部から軸方向に垂下され、上部から順に、上部磁気軸受9及び下部磁気軸受10に、半径方向荷重をそれぞれ支承され、下端に設けられた円盤状の磁性板からなるスラストディスク7aが前記スラスト磁気軸受11に挟まれて、スラスト方向(軸心方向)の空中維持制御を行なっている。
【0007】
前記回転軸7には、前記上部磁気軸受9と下部磁気軸受10との間に設けられた前記モータ12のステータ12aに対向して回転子12bが固着されている。
【0008】
また、該回転軸7の前記上部磁気軸受9の上側は前記上部保護軸受19が設けられて該回転軸7と上部保護軸受19とのラジアル方向の間隔を所要の値に設定している。
さらに、該回転軸7の前記下部磁気軸受10の下側は前記下部保護軸受20が設けられて、該回転軸7と下部保護軸受20とのラジアル方向及びスラスト方向の間隔を所要値に設定している。
【0009】
次に上部磁気軸受9及び下部磁気軸受10の磁極は、図4(B)に示すように、回転軸7の軸心(Z軸)と直交する面内において、左右(X軸)及び前後(Y軸)方向に夫々一対づつ配設され、前記回転軸7が倒れを生じることなく中心軸線上に空中維持可能に構成されている。
従って、該回転軸7は、該上部磁気軸受9及び下部磁気軸受10により左右(X軸)及び前後(Y軸)方向を、前記スラスト磁気軸受11により軸心(Z軸)方向を、つまり5軸方向を空中支持、かつ制御されて回転することとなる。
【0010】
上記のように構成されたターボ分子ポンプAの運転時において、
前記各磁気軸受9、10、11に通電し回転軸7、動翼5を有するロータ6等のポンプ回転部を空中維持した状態で、モータ12を駆動し、前記ポンプ回転部を例えば10,000〜100,000r.p.mで高速回転させる。該ポンプ回転部の高速回転により動翼5が静翼4の間を回転し、かつねじ溝ポンプ段8がテーパ状のシールリング14の内周面と対面しながら回転することによって、真空排気されるガスが上方のガス吸気口2から動翼5と静翼4との間で第1段の圧縮がなされた後、ねじ溝ポンプ段8の螺旋状溝通路で第2段階圧縮がなされ、ポンプ内ガス通路を経て排気口3の方向に流れることによって、ガス吸気口2側が高真空に保持される。
【0011】
そして、前記上・下部磁気軸受9、10及びスラスト磁気軸受11の磁気制御に異常をきたし、前記回転軸7が片側に偏心した際には、前記上部保護軸受19と下部保護軸受20に該回転軸7の外周が当接(タッチダウン)することにより、該回転軸7及びロータ6の回転を保証する。
【0012】
かかるターボ分子ポンプに取り付けられる電源ユニットは、図3のような構成を有す。
図3は、本発明の適用されるターボ分子ポンプユニットAと電源ユニットBの要部ブロック構成を示し、ポンプユニットA側には前記したようにロータ6及びこれに直結され回転軸7(以下これらを含めて回転体という)を浮上制御する磁気軸受9、10、11と、該磁気軸受9、10、11と回転体間の空隙を検知する位置センサ24,25,26を具えている。
【0013】
一方電源ユニットB側には前記ポンプユニットA側の回転軸7に直結されたモータ12を高速駆動するモータ駆動回路34(例えばインバータ回路を含む電源回路)が組込まれ、前記モータ12の回転制御を行なう。
一方、磁気軸受側の制御は、上部磁気軸受9については該上部磁気軸受9近傍の位置センサ24の信号を受けて、又下部磁気軸受10については該下部磁気軸受10近傍の位置センサ25の信号を受けて、更にスラスト磁気軸受11については該スラスト磁気軸受11近傍の位置センサ26の信号を受けて、夫々独立した制御手段により行なわれている。
【0014】
その一例を上部磁気軸受9の制御を代表して説明するに、該制御手段は、位置センサ24の信号を受けて、その偏差量に基づいて回転軸7のラジアル方向の浮上位置を中心に保持させる制御信号を送出する磁気軸受制御回路32と、前記制御信号に基づいてパルス幅変調されたパルス信号に基づいてスイッチング素子をON/OFF制御しながら上部磁気軸受9の駆動制御を行なう磁気軸受駆動回路33、及び磁気軸受駆動電源31が組み込まれている。
【0015】
そして前記磁気軸受制御回路32は、例えば実用新案登録第2522168号等に開示してあるように、位置センサ24よりの検知信号は偏差増幅器等の不図示の位置フィードバックゲインを介してその基準位置との偏差信号に変換した後、ローパスノッチフィルタに取込み、該ローパスノッチフィルタで中高周波数帯域のノイズ等の不安定化部分を広範囲に亙って阻止する。
そして前記ローパスノッチフィルタ通過後のフィードバック信号は比例要素、積分要素、微分要素であるPID制御回路を通した後、回転軸7の構造による数次の固有振動数を安定化するための位相補償回路を通して制御電流を得る。
【0016】
そして前記位置センサ24Χ、24Y及び磁気軸受制御回路32Χ、32Yは、図4に示すように各座標軸(Χ,Y)毎に設けられ、一方磁気軸受9の磁極も座標軸(Χ,Y)毎に回転軸7を挟んで対向する位置に夫々一対ずつ設けられている。
即ち、各座標軸(Χ,Y)毎の一の磁極と回転軸7を挟んで反対側に位置する対向磁極は基準位置よりの偏差量が正逆対称量であるために、各座標軸(Χ,Y)毎の磁気軸受制御回路32Χ、32Yの制御信号を一の磁極についてはそのまま、又対向磁極については反転させて磁気軸受駆動制御回路33に送信すればよい。
【0017】
【発明が解決しようとする課題】
さて前記ターボ分子ポンプは高速回転が行なわれるために、該ポンプの安定回転を図るために前記磁気軸受駆動制御回路33には高速応答性が要求される。
この為、前記磁気軸受駆動制御回路33のスイッチング素子には、可変抵抗型のトランジスタを用いていたが、かかるスイッチング素子では、抵抗損失による発熱が大きい為に、ヒートシンク等の放熱手段を設けねばならず、回路構成が大型化する。
この為、前記スイッチング素子にFETトランジスタを用い、前記磁気軸受制御回路32Χ、32Yの制御信号若しくは反転制御信号に対応させて変調させたパルス幅変調信号を前記トランジスタのベース側に印加させて前記スイッチング素子をON/OFF制御させて通電制御を行なっている。
【0018】
かかる磁気軸受駆動制御回路33を上部磁気軸受9について図2に基づいて説明するに、各座標軸(Χ,Y)毎に位置センサ24Χ、24Y及び磁気軸受制御回路32Χ、32Yが設けられ、各磁気軸受制御回路32Χ、32Yの制御信号をそのまま若しくは夫々反転回路41により反転させ、更に前記制御信号若しくは反転制御信号にバイアス回路49に生成されたバイアス重畳制御信号を夫々の磁極のパルス幅変調回路42に投入し、前記制御信号若しくは反転制御信号に対応する変調パルスを各座標軸(Χ,Y)毎に夫々一対づつ設けられた磁極夫々の下流側に接続されたスイッチング素子43YL、43YR…のFETトランジスタ44のベース側に印加させ、該スイッチング素子43YL、43YR…を介して直流電源31と接続された前記夫々の磁極コイル9YL、9YR…のON/OFF通電制御を行なっている。図中46は逆流防止用ダイオードであり、又スイッチング素子43YL、43YR…の下流側はFETトランジスタ44とダイオード45からなり、その下流側はアースされている。
【0019】
かかるスイッチング素子43YL、43YR…にFETトランジスタ44を用いている為に、熱抵抗損失は小さく、該ヒートシンク等の放熱手段を設ける必要がなく、例え設けても小さくて済むが、一方前記FETトランジスタ44は後記に詳説するように、応答性が落ちる欠点があり特にターボポンプ等の高速回転体においての高速応答性が確保できない。
この為、前記図2に示す磁気軸受駆動制御回路33において前記直流電源31(磁気軸受駆動電源31)の印加電圧を上げるか、若しくは転流抵抗追加の方法で対処している。
【0020】
しかしながら前者の方法では、電源容量が大きくなり大型化と高価格化につながる。又、後者の方法では、抵抗損失が大きくなり、抵抗の容量大及びヒートシンク等の冷却対策が必要となり大型化する。
【0021】
本発明は、かかる技術的課題に鑑み、ターボ分子ポンプ等の高速回転体の磁気軸受において、ヒートシンク等の冷却対策を必要とすることなく、有効に高速応答性が確保できる通電制御方法とその制御回路を提供することを目的とする。
本発明の他の目的は、回路構成を簡単化しつつ高速応答性が確保できる通電制御方法とその制御回路を提供することを目的とする。
【0022】
【課題を解決するための手段】
かかる課題を解決するために、請求項1記載の発明は、負荷に連結された回転軸若しくは該回転軸と一体的に回転する磁性部材(以下回転軸部という)を挟んで、夫々対称位置に配置した各対毎の磁気軸受の通電制御により前記回転軸部を空中維持しながら、該回転軸部を高速回転させる高速回転体に用いる磁気軸受の通電制御方法において、
前記回転軸部と磁気軸受との空隙変動に応じて、前記磁気軸受を構成する電磁石磁極コイル9YL、9YR…に流す通電電流の制御を、スイッチング素子43YL、43YR…に印加されるON/OFFパルスにより行なうとともに、該夫々の磁極コイル9YL、9YR…の電流エネルギーを、前記一の磁極コイルへのパルスOFF毎に、回転軸部の対向位置にある他側磁極コイル(以下対向磁極という)へ転流させて行なうことを特徴とする。
【0023】
尚、スイッチング素子43YL、43YR…に印加されるON/OFFパルスはパルス幅変調パルス(PMW)のみならず、周波数変調パルスを用いてもよい。
【0024】
かかる発明によれば、回転軸部を挟んで対称に配置した一対の磁極コイル9YL、9YR…の内、一の磁極コイル9ΧR、9YRはパルスON時に、前記直流電源31より直接電流を流すが、一方該一の磁極コイル9ΧR、9YRへのパルスOFF時に対向磁極コイル9ΧL、9YLには一の磁極コイル9ΧR、9YRにダイオード46が接続されている為に、一の磁極コイル9ΧR、9YRのエネルギーを対向磁極コイル9ΧL、9YL側に流すことが出来る。
この結果一の磁極コイル9ΧR、9YRのパルスOFF時のエネルギーを対向磁極コイル9ΧL、9YL側に供給し、速やかに消費することが出来、次に対向磁極コイル9ΧL、9YLのパルスOFF時のエネルギーも一の磁極コイル9ΧR、9YR側に供給し、速やかに消費することが出来る。
【0025】
従って、回転軸部を挟んで対称に配置した一対の磁極コイル9YL、9YR…はパルスOFF毎に、他側磁極コイル側にエネルギーを供給し、速やかに消費することが出来る為に、抵抗損失が発生することなく又ヒートシンク等の冷却対策を必要とすることなく、有効に高速応答性が確保できる。
【0026】
請求項3記載の発明は、前記請求項1記載の発明を効果的に実施するための回路構成に関する発明で、前記構成のターボ分子ポンプその他の高速回転体において、
前記回転軸部と磁気軸受との空隙変動に応じて、前記磁気軸受を構成する電磁石磁極コイル9YL、9YR…に流す通電電流の制御を行なう第一の制御回路33Aを具え、該第一の制御回路33Aが、夫々の磁極コイル9YL、9YR…に接続されたスイッチング素子43YL、43YR…のON/OFF制御を、空隙変動に応じて制御されるパルス印加により行なうとともに、前記スイッチング素子43YL、43YR…の上流側で回転軸部の対向位置にある一対の磁極コイル9YL、9YR…同士を接続させ、該夫々の磁極コイル9YL、9YR…の電流エネルギーを、一の磁極コイル9ΧR、9YRへのパルスOFF毎に、対向位置にある他側磁極コイル9ΧL、9YLへ転流させることを特徴とする。
【0027】
この場合、請求項2記載のように、前記夫々の磁気軸受の静的剛性を上げるために夫々の磁極コイル9YL、9YR…に流すバイアス電流の通電系統を請求項1の通電系統と別系統にするのがよい。
【0028】
例えば上部磁気軸受はΧ−Y二軸の座標軸に夫々一対づつ、計4個の磁極9YL、9YR…を必要とし、従来は個々の磁極9YL、9YR…毎にバイアス電流を印加しなければならず、この為上記ターボポンプの回転軸7のように、上部磁気軸受9及び下部磁気軸受10により左右(X軸)及び前後(Y軸)方向に夫々一対ずつ、又前記スラスト磁気軸受11により軸心(Z軸)方向に一対の磁極を有して、いわゆる5軸で空中支持を行なう装置においては、バイアス回路は前記磁極の数だけ10回路設けるか、若しくは図2に示すように、前記磁気制御回路32よりの制御信号若しくは反転制御信号をパルス幅変調回路42に投入する際に、バイアス回路49に生成されたバイアス信号を前記制御信号に重畳して、該バイアスを重畳した制御信号若しくは反転制御信号夫々の磁極のパルス幅変調回路42に投入して制御しようとすると、対向する二つの磁極(例えば9XR,9XL)に同時に電流が流れ、前記制御信号若しくは反転制御信号による空中支持電流制御に対し、高精度な磁気軸受制御が出来ない。
また、同時に電流が流れることにより、他極へ電流を転流させることができなくなり、応答性の改善を図ることができない。
【0029】
一方本発明によれば、上部磁気軸受9及び下部磁気軸受10スラスト磁気軸受11夫々の磁気軸受における磁極コイル9YL、9YR…のインダクタンス及び抵抗が同一であるために、夫々の磁気軸受毎にバイアス電源を共通化して、バイアス電流の通電系統を請求項1の通電系統と別系統にすることにより、上部磁気軸受9及び下部磁気軸受10スラスト磁気軸受11夫々の磁気軸受毎に一回路、計3回路のバイアス回路で足りる。
又バイアス電流の通電系統を請求項1の通電系統と別系統にすることにより、バイアス電流の印加と回転軸部と磁気軸受との空隙変動に応じた通電電流の制御が夫々独立して高精度に行なわれ、高精度な磁気軸受制御が可能となる。
【0030】
請求項4記載の発明は、請求項3記載の第一の制御回路33Aと、
前記夫々の磁気軸受の静的剛性を上げるために夫々の磁極コイル9YL、9YR…にバイアス電流を流す第二の制御回路33Bとを具え、
前記二つの制御回路が夫々別系統で前記磁極コイル9YL、9YR…に電流印加可能に構成したことを特徴とする。
【0031】
請求項5記載の発明は請求項4記載の発明を具体化したもので、前記回転軸のラジアル方向の二座標軸(Χ軸、Y軸)の位置制御を行なう為に、回転軸に対向して少なくとも二対の磁極コイル9YL、9YR…を具えた一又は複数のラジアル磁気軸受と、
前記回転軸のスラスト方向の座標軸(Z軸)の位置制御を行なう為に、回転軸と直交する磁性板に対向して少なくとも一対の磁極コイル9YL、9YR…を具えたスラスト磁気軸受とを具えた通電制御回路において、
前記ラジアル磁気軸受若しくはスラスト磁気軸受内の複数の磁極コイル9YL、9YR…群が、夫々対応する磁気軸受毎に共通する一のバイアス電流通電回路(第二の制御回路33B)によりバイアス電流が印加可能に構成されていることを特徴とする。
【0032】
【発明の実施の形態】
以下、図面を参照して本発明の好適な実施例を例示的に詳しく説明する。但しこの実施例に記載されている構成部品の寸法、材質、形状、その相対的配置等は特に特定的な記載がないかぎりは、この発明の範囲をそれに限定する趣旨ではなく、単なる説明例にすぎない。
【0033】
図1は本発明の実施形態に係る上部磁気軸受9の磁気軸受制御回路33で図2と同様な対応図を示すブロック図である。
即ち、本実施形態においても図2と同様に、各座標軸(Χ,Y)毎に位置センサ24Χ、24Y及び磁気軸受制御回路32Χ、32Yが設けられ、各磁気軸受制御回路32Χ、32Yの制御信号を夫々の磁極のパルス幅変調回路42に投入し、前記制御信号若しくは反転制御信号に対応する変調パルスをそのまま若しくは夫々反転回路41により反転させて各座標軸(Χ,Y)毎に夫々一対づつ設けられた磁極のスイッチング素子43YL、43YR…のFETトランジスタ44のベース側に印加させ、該スイッチング素子43YL、43YR…を介して直流電源31と直接若しくは間接的に接続された前記夫々の磁極コイル9YL、9YR…のON/OFF通電制御を行なっている。
【0034】
即ちより具体的に説明するに、前記一対の磁極コイル9YL、9YR…の内、一の磁極コイル9ΧR、9YRのアノード(上流)側にはダイオード47を介して直流電源31を接続して該一の磁極コイル9ΧR、9YR下流側に設けたスイッチング素子43ΧR、43YRを接続するとともに、該スイッチング素子43ΧR、43YRの上流側で分岐し、該分岐線路を逆流防止ダイオード46を介して回転軸7を挟んで対称位置にある対向磁極コイル9ΧL、9YLのアノード側に接続させ、該一の磁極コイル9ΧR、9YRへのスイッチング素子43ΧR、43YRがOFF毎に、言換えれば下流側に設けた対応磁極のスイッチング素子43ΧL、43YLのON毎に、一の磁極コイル9ΧR、9YRの電流エネルギーを対向磁極コイル9ΧL、9YLへ転流させるように構成している。
【0035】
一方回転軸7を挟んで対称位置にある対向磁極コイル9ΧL、9YLも同様に、該磁極コイル9ΧL、9YLのON/OFF通電制御を行なうスイッチング素子43ΧL、43YLの上流側で、逆流防止用ダイオード46を介して対称位置にある前記一の磁極コイル9ΧR、9YRに接続させるとともに、前記と同様に対向磁極のスイッチング素子43ΧL、43YLのOFF毎に、該対向磁極コイル9ΧL、9YLの電流エネルギーを一の磁極コイル9ΧR、9YRへ転流させるように構成している。
【0036】
一方磁気軸受9の静的剛性を上げるために夫々の磁極コイル9YL、9YR…にバイアス電流を流すバイアス駆動制御回路33Bは、前記位置センサ24により検知された回転軸部と磁気軸受との空隙変動に応じて、前記磁極コイル9YL、9YR…に流す通電電流の制御を行なう前記第一の駆動制御回路33Aと別系統で前記磁極コイル9YL、9YR…に電流を印加可能に構成している。
【0037】
かかるバイアス駆動制御回路33Bは、前記第一の駆動制御回路33Aの直流電源31を電圧変換器(1次側−2次側が絶縁できるもの)52によりバイアス直流電源を設定した後、該電源52を夫々の磁極コイル9YL、9YR…に順次接続した後、ダイオード48を介し、FETトランジスタ54とダイオード55からなるバイアス用スイッチング素子53に接続させる。
そして前記FETトランジスタ54のベース側には、パルス幅変調回路51にてパルス幅変調されたバイアス制御信号が印加され、これにより前記夫々の磁極コイル9YL、9YR…にバイアス制御信号により制御された一定バイアス電流が、前記第一の駆動制御回路33Aの制御電流に重畳されて通電されることになる。尚、50はバイアス回路である。
【0038】
かかる実施形態によれば、回転軸部を挟んで対称に配置した一対の磁極コイル9YL、9YR…夫々に対応するスイッチング素子43YL、43YR…のベース側に正転パルス幅変調信号と反転された正転パルス幅変調信号が印加される訳であるが、前記一対の磁極コイル9YL、9YR…の内、一の磁極コイル9ΧR、9YRにバイアス駆動制御回路33Bによりバイアス電流が通電された状態で、対応するスイッチング素子43ΧR、43YRが前記変調信号によりONされると、前記直流電源31より一の磁極コイル9ΧR、9YRに電流がダイオード47を介して通電される。
【0039】
一方対向磁極コイル9ΧL、9YLには対応するスイッチング素子43ΧL、43YLの上流側で逆流防止用ダイオード46を介して対称位置にある前記一の磁極コイル9ΧR、9YRに接続されているために、前記対向磁極コイル9ΧL、9YLにバイアス駆動制御回路33Bによりバイアス電流が通電された状態で、対応するスイッチング素子43YL、43YR…が前記変調信号によりONされると、言換えれば一の磁極コイル9ΧR、9YRへのパルスOFF時に一の磁極コイル9ΧR、9YRの電気エネルギーが消費されるとともに、直流電源31を対向磁極コイル9ΧL、9YL側に流して前記対向磁極コイル9ΧL、9YLの通電を行なうことが出来る。
【0040】
従って、かかる実施形態によれば、回転軸部を挟んで対称に配置した一対の磁極コイル9YL、9YR…はパルスOFF毎に、該一の磁極コイル9ΧR、9Yの電流エネルギーを対向磁極コイル9ΧL、9YL側に供給し、速やかに消費しながら通電制御を行なうことが出来るために、抵抗損失が発生することなく又ヒートシンク等の冷却対策を必要とすることなく、有効に高速応答性が確保できる。
【0041】
尚、前記上部磁気軸受9における磁極コイル9YL、9YR…のインダクタンス及び抵抗が同一であるために、バイアス電源を共通化して、バイアス電流の通電系統を別系統にすることにより、上部磁気軸受9のバイアス駆動制御回路33は一系統で足りる。
【0042】
【発明の効果】
以上記載のごとく請求項1及び3記載の発明によれば、ターボ分子ポンプ等の高速回転体の磁気軸受において、ヒートシンク等の冷却対策を必要とすることなく、有効に高速応答性が確保できる。
【0043】
又請求項2及び4記載の発明によれば、回路構成を簡単化しつつ高速応答性が確保できる。又バイアス電流の通電系統を請求項1の通電系統と別系統にすることにより、バイアス電流の印加と回転軸部と磁気軸受との空隙変動に応じた通電電流の制御が夫々独立して高精度に行なわれ、高精度な磁気軸受制御が可能となる。
【0044】
更に請求項5記載の発明によれば、回転軸のラジアル方向の二座標軸(Χ軸、Y軸)の位置制御を行なう為に、上部軸受と下部磁気軸受からなるラジアル磁気軸受と、前記回転軸のスラスト方向の座標軸(Z軸)の位置制御を行なうスラスト磁気軸受とを具えたターボ分子ポンプに好適に適用させることが出来る。
【図面の簡単な説明】
【図1】本発明の実施形態に係る上部磁気軸受の磁気軸受制御回路で図2と同様な対応図を示すブロック図である。
【図2】従来技術に係る上部磁気軸受の磁気軸受制御回路を示すブロック図である。
【図3】本発明が適用されるターボ分子ポンプのポンプユニットAと電源ユニットBの要部ブロック構成を示すブロック図である。
【図4】本発明が適用されるターボ分子ポンプの全体断面図である。
【符号の説明】
A ポンプ本体
B 電源ユニット
5 動翼
7 回転軸
9 上部磁気軸受
9YL、9YR… 磁極コイル
10 下部磁気軸受
11 スラスト磁気軸受
24Χ、24Y 位置センサ
31 磁気軸受駆動電源
32Χ、32Y 磁気軸受制御回路
33A 第一の駆動制御回路
33B バイアス駆動制御回路(第二の駆動制御回路)
41 反転回路
42 パルス幅変調回路
43YL、43YR… 磁極のスイッチング素子
44 FETトランジスタ
46 逆流防止用ダイオード
52 電圧変換器(バイアス直流電源)
53 バイアス用スイッチング素子
[0001]
TECHNICAL FIELD OF THE INVENTION
The present invention is characterized in that the pair of magnetic bearings disposed at symmetric positions with respect to a rotating shaft connected to a load or a magnetic member (hereinafter, referred to as a rotating shaft portion) that rotates integrally with the rotating shaft are controlled by energizing the pair. The present invention relates to an energization control method and a control circuit for a magnetic bearing of a high-speed rotating body such as a turbo molecular pump that rotates the rotating shaft at a high speed while maintaining the rotating shaft in the air. The present invention relates to a method for controlling energization of a magnetic bearing used in a turbo-molecular pump provided with a moving and stationary blade stage composed of a stationary blade provided in a rotating shaft and a moving blade provided on a rotating shaft, and a control circuit therefor.
[0002]
[Prior art]
Conventionally, instead of a mechanical bearing that mechanically supports a rotating body or a linear moving body such as a ball bearing or a rolling bearing, a magnetic bearing that supports the rotating body or the linear moving body by magnetic force is known. .
Such a magnetic bearing has a smaller loss than a conventional fluid lubricated bearing, and can achieve a dry bearing and a clean atmosphere. Especially, since it is a useful bearing in a vacuum state, it can be operated at high speed by a direct-coupled motor such as a turbo molecular pump. The driven high-speed rotating body is frequently used as a bearing for a rotating unit.
FIG. 4 shows the configuration of a turbo-molecular pump having such a magnetic bearing.
[0003]
FIG. 4 shows an example of a turbo-molecular pump applied to the present invention. In FIG. 4 (A), reference numerals 1 and 16 denote an upper casing and an upper casing which are integrally assembled via bolts 21 via an O-ring 15. The lower casing.
The upper opening of the upper casing 1 serves as a gas inlet port 2, and a plurality of spacers 13 are provided in the inside thereof in the axial direction through a ring-shaped gap.
The upper end of the spacer 13 is abutted against the inner end surface of the upper casing 1, and the lower end is spigot-fitted to the upper end of the lower casing 16. It is sandwiched and fixed and provided in a multi-stage shape.
[0004]
Reference numeral 6 denotes a rotor, and the rotor 6 is provided with a plurality of moving blades 5 in a multi-stage manner, and each of the moving blades 5 and the stationary blades 4 are provided so as to alternately mesh with each other to form a blade stage. At the lower part of the rotor 6, a thread groove pump stage 8 is provided.
Reference numeral 14 denotes a tapered seal ring fixed to the upper surface of the lower casing 16 by a plurality of bolts 18, and is disposed to face the outer periphery of the thread groove pump stage 8 via a small gap, thereby increasing the compression effect.
[0005]
An exhaust port 3 is opened at a lower side portion of the lower casing 16, and the fluid that has passed through the screw groove pump stage 8 is sent out from the exhaust port 3 to the outside.
Reference numeral 17 denotes a cylindrical support cylinder projecting upward in the center region of the lower casing 16, and an upper protection bearing 19 composed of a radial ball bearing and a radial bearing on the inner periphery of the support cylinder 17 in order from the top. An upper magnetic bearing 9, a stator portion 12a of a motor 12, a lower magnetic bearing 10 as a radial bearing, a lower protection bearing 20 made of a radial ball bearing, and a thrust provided with a thrust disk 7a at a lower end of the rotating shaft 7 described later interposed therebetween. A magnetic bearing 11 is provided.
[0006]
Reference numeral 7 denotes a rotating shaft fixed to the center of the upper portion of the rotor 6. The rotating shaft 7 hangs in an axial direction from a fixed portion to the rotor 6, and sequentially from an upper portion to an upper magnetic bearing 9 and a lower magnetic bearing 10. A radial load is supported, and a thrust disk 7a formed of a disk-shaped magnetic plate provided at the lower end is sandwiched between the thrust magnetic bearings 11 to perform airborne maintenance control in the thrust direction (axial direction).
[0007]
A rotor 12 b is fixed to the rotating shaft 7 so as to face a stator 12 a of the motor 12 provided between the upper magnetic bearing 9 and the lower magnetic bearing 10.
[0008]
The upper protection bearing 19 is provided above the upper magnetic bearing 9 of the rotating shaft 7, and a radial distance between the rotating shaft 7 and the upper protection bearing 19 is set to a required value.
Further, the lower protective bearing 20 is provided below the lower magnetic bearing 10 of the rotary shaft 7, and the radial and thrust intervals between the rotary shaft 7 and the lower protective bearing 20 are set to required values. ing.
[0009]
Next, as shown in FIG. 4B, the magnetic poles of the upper magnetic bearing 9 and the lower magnetic bearing 10 are moved right and left (X-axis) and front-back ( Each pair is arranged in the (Y-axis) direction so that the rotary shaft 7 can be maintained in the air on the center axis line without falling down.
Therefore, the rotating shaft 7 is moved in the left-right (X-axis) and front-rear (Y-axis) directions by the upper magnetic bearing 9 and the lower magnetic bearing 10, and is moved in the axial center (Z-axis) direction by the thrust magnetic bearing 11, that is, 5. The axial direction is supported in the air, and the rotation is controlled.
[0010]
During the operation of the turbo molecular pump A configured as described above,
The motor 12 is driven in a state in which the magnetic bearings 9, 10, and 11 are energized and a pump rotating unit such as the rotor 6 having the rotating shaft 7 and the moving blade 5 is maintained in the air, and the pump rotating unit is moved to, for example, 10,000. ~ 100,000 r. p. Rotate at high speed at m. The rotor 5 rotates between the stationary blades 4 due to the high-speed rotation of the pump rotating unit, and the thread groove pump stage 8 rotates while facing the inner peripheral surface of the tapered seal ring 14, thereby evacuating. After the first stage of compression is performed between the moving blades 5 and the stationary blades 4 from the upper gas inlet 2 through the upper gas inlet 2, a second stage of compression is performed in the spiral groove passage of the thread groove pump stage 8, By flowing in the direction of the exhaust port 3 through the internal gas passage, the gas intake port 2 side is maintained at a high vacuum.
[0011]
When the magnetic control of the upper / lower magnetic bearings 9 and 10 and the thrust magnetic bearing 11 becomes abnormal and the rotary shaft 7 is eccentric to one side, the upper protective bearing 19 and the lower protective bearing 20 When the outer periphery of the shaft 7 abuts (touch-down), the rotation of the rotating shaft 7 and the rotor 6 is guaranteed.
[0012]
The power supply unit attached to such a turbo molecular pump has a configuration as shown in FIG.
FIG. 3 shows a main block configuration of a turbo molecular pump unit A and a power supply unit B to which the present invention is applied. On the pump unit A side, as described above, the rotor 6 and the rotary shaft 7 directly connected to the rotor 6 (hereinafter referred to as these). ), And magnetic sensors 9, 10, 11 for controlling the levitation of the rotating bodies, and position sensors 24, 25, 26 for detecting the gaps between the magnetic bearings 9, 10, 11 and the rotating bodies.
[0013]
On the other hand, a motor drive circuit 34 (for example, a power supply circuit including an inverter circuit) for driving the motor 12 directly connected to the rotary shaft 7 of the pump unit A at a high speed is incorporated in the power supply unit B, and controls the rotation of the motor 12. Do.
On the other hand, the control on the magnetic bearing side is such that the upper magnetic bearing 9 receives a signal from the position sensor 24 near the upper magnetic bearing 9 and the lower magnetic bearing 10 receives a signal from the position sensor 25 near the lower magnetic bearing 10. Accordingly, the thrust magnetic bearing 11 is further controlled by independent control means in response to a signal from the position sensor 26 near the thrust magnetic bearing 11.
[0014]
An example of this will be described with the control of the upper magnetic bearing 9 as a representative. The control means receives a signal from the position sensor 24 and holds the center of the floating position of the rotary shaft 7 in the radial direction based on the deviation amount. A magnetic bearing control circuit 32 for sending a control signal to be controlled, and a magnetic bearing drive for controlling the drive of the upper magnetic bearing 9 while controlling the switching element to be ON / OFF based on a pulse signal pulse width modulated based on the control signal. A circuit 33 and a magnetic bearing drive power supply 31 are incorporated.
[0015]
Then, as disclosed in, for example, Utility Model Registration No. 2522168, the magnetic bearing control circuit 32 detects the detection signal from the position sensor 24 with its reference position via a position feedback gain (not shown) such as a deviation amplifier. After being converted into a deviation signal, the signal is taken into a low-pass notch filter, and the low-pass notch filter blocks an unstable portion such as noise in a middle and high frequency band over a wide range.
The feedback signal after passing through the low-pass notch filter passes through a PID control circuit, which is a proportional element, an integral element, and a differential element, and then a phase compensation circuit for stabilizing a natural frequency of several orders due to the structure of the rotating shaft 7. To obtain the control current.
[0016]
The position sensors 24 #, 24Y and the magnetic bearing control circuits 32 #, 32Y are provided for each coordinate axis (Χ, Y) as shown in FIG. 4, while the magnetic poles of the magnetic bearing 9 are also provided for each coordinate axis (Χ, Y). Each pair is provided at a position facing each other with the rotating shaft 7 interposed therebetween.
That is, since one magnetic pole for each coordinate axis (Χ, Y) and the opposite magnetic pole located on the opposite side with respect to the rotation axis 7 have a deviation amount from the reference position in forward and reverse symmetry, each of the coordinate axes (Χ, Y) The control signals of the magnetic bearing control circuits 32 # and 32Y for each Y) may be transmitted to the magnetic bearing drive control circuit 33 as it is for one magnetic pole or inverted for the opposite magnetic pole.
[0017]
[Problems to be solved by the invention]
Since the turbo molecular pump rotates at a high speed, the magnetic bearing drive control circuit 33 is required to have a high-speed response in order to stably rotate the pump.
For this reason, a variable resistance type transistor is used as the switching element of the magnetic bearing drive control circuit 33. However, since such a switching element generates a large amount of heat due to resistance loss, a heat radiating means such as a heat sink must be provided. And the circuit configuration becomes large.
Therefore, an FET transistor is used as the switching element, and a pulse width modulation signal modulated in accordance with a control signal or an inversion control signal of the magnetic bearing control circuits 32 # and 32Y is applied to the base side of the transistor to perform the switching. The energization control is performed by ON / OFF controlling the elements.
[0018]
The magnetic bearing drive control circuit 33 will be described with reference to FIG. 2 for the upper magnetic bearing 9. Position sensors 24 Χ, 24 Y and magnetic bearing control circuits 32 Χ, 32 Y are provided for each coordinate axis (Χ, Y). The control signals of the bearing control circuits 32 # and 32Y are inverted as they are or by an inversion circuit 41, respectively, and the control signal or the inversion control signal is further supplied with the bias superimposition control signal generated in the bias circuit 49 by the pulse width modulation circuit 42 of each magnetic pole. , And a modulation pulse corresponding to the control signal or the inversion control signal is connected to each of the coordinate axes (極, Y). The FET transistors of the switching elements 43YL, 43YR,. 44, and is connected to the DC power supply 31 through the switching elements 43YL, 43YR,. ON / OFF energization control of the magnetic pole coils 9YL, 9YR,... In the figure, reference numeral 46 denotes a backflow prevention diode. The downstream side of the switching elements 43YL, 43YR... Comprises an FET transistor 44 and a diode 45, and the downstream side is grounded.
[0019]
Since the FET transistors 44 are used for the switching elements 43YL, 43YR,..., The heat resistance loss is small, and there is no need to provide a heat radiating means such as a heat sink. As described in detail later, there is a disadvantage in that the response is reduced, and particularly high-speed response in a high-speed rotating body such as a turbo pump cannot be ensured.
For this reason, in the magnetic bearing drive control circuit 33 shown in FIG. 2, a method of increasing the applied voltage of the DC power supply 31 (magnetic bearing drive power supply 31) or adding a commutation resistance is used.
[0020]
However, in the former method, the power supply capacity is increased, which leads to an increase in size and cost. Also, in the latter method, the resistance loss increases, and a large capacity of the resistor and a cooling measure such as a heat sink are required, resulting in an increase in size.
[0021]
In view of the above technical problems, the present invention provides an energization control method and a control method for a magnetic bearing of a high-speed rotating body such as a turbo-molecular pump, which can ensure high-speed response effectively without requiring cooling measures such as a heat sink. It is intended to provide a circuit.
Another object of the present invention is to provide an energization control method capable of ensuring a high-speed response while simplifying a circuit configuration, and a control circuit therefor.
[0022]
[Means for Solving the Problems]
In order to solve such a problem, the invention according to claim 1 is arranged such that a rotating shaft connected to a load or a magnetic member that rotates integrally with the rotating shaft (hereinafter, referred to as a rotating shaft portion) is symmetrically positioned. In the energization control method of the magnetic bearing used for the high-speed rotating body that rotates the rotation shaft portion at high speed while maintaining the rotation shaft portion in the air by energization control of the magnetic bearing for each pair arranged,
Controlling the current flowing through the electromagnet pole coils 9YL, 9YR,... Constituting the magnetic bearing according to the air gap fluctuation between the rotating shaft portion and the magnetic bearing is controlled by ON / OFF pulses applied to the switching elements 43YL, 43YR,. .., And transfers the current energy of the respective magnetic pole coils 9YL, 9YR,... To the other magnetic pole coil (hereinafter referred to as the opposite magnetic pole) at the position opposite to the rotating shaft every time the pulse to the one magnetic pole coil is turned off. It is characterized by flowing.
[0023]
The ON / OFF pulses applied to the switching elements 43YL, 43YR... May be not only pulse width modulation pulses (PMW) but also frequency modulation pulses.
[0024]
According to this invention, of the pair of magnetic pole coils 9YL, 9YR,... Arranged symmetrically with respect to the rotating shaft portion, one of the magnetic pole coils 9 # R, 9YR allows a direct current to flow from the DC power supply 31 when the pulse is ON. On the other hand, when the pulse to the one magnetic pole coil 9 # R, 9YR is turned off, the diode 46 is connected to the one magnetic pole coil 9 # R, 9YR to the opposite magnetic pole coil 9 # L, 9YL, so that the energy of the one magnetic pole coil 9 # R, 9YR is reduced. The current can flow to the opposed magnetic pole coils 9 # L and 9YL.
As a result, the energy when the pulse of one magnetic pole coil 9 # R, 9YL is turned off can be supplied to the opposed magnetic pole coils 9 # L, 9YL side, and can be quickly consumed. Next, the energy when the pulse of the opposite magnetic pole coils 9 # L, 9YL is turned off is also reduced. It can be supplied to one magnetic pole coil 9 # R, 9YR side and consumed quickly.
[0025]
Therefore, the pair of magnetic pole coils 9YL, 9YR,... Arranged symmetrically with respect to the rotary shaft portion can supply energy to the other magnetic pole coil side every time the pulse is turned off and quickly consume the energy. High-speed responsiveness can be effectively secured without any occurrence and without requiring a cooling measure such as a heat sink.
[0026]
According to a third aspect of the present invention, there is provided an invention relating to a circuit configuration for effectively implementing the first aspect of the present invention.
A first control circuit 33A for controlling a current supplied to the electromagnet pole coils 9YL, 9YR,... Constituting the magnetic bearing in accordance with a gap variation between the rotating shaft portion and the magnetic bearing; The circuit 33A controls ON / OFF of the switching elements 43YL, 43YR,... Connected to the respective magnetic pole coils 9YL, 9YR,... By applying a pulse controlled according to the air gap variation, and at the same time, the switching elements 43YL, 43YR,. A pair of magnetic pole coils 9YL, 9YR,... Located at a position opposing the rotating shaft portion on the upstream side of the motor are connected to each other, and the current energy of the magnetic pole coils 9YL, 9YR,. Each time, it is commutated to the other-side magnetic pole coils 9 # L and 9YL located at opposing positions.
[0027]
In this case, an energizing system of a bias current flowing through each of the magnetic pole coils 9YL, 9YR... In order to increase the static rigidity of each of the magnetic bearings is provided separately from the energizing system of the first aspect. Good to do.
[0028]
For example, the upper magnetic bearing requires a total of four magnetic poles 9YL, 9YR..., One pair for each of the Χ-Y coordinate axes, and conventionally, a bias current must be applied to each of the magnetic poles 9YL, 9YR. Therefore, like the rotary shaft 7 of the turbopump, the upper magnetic bearing 9 and the lower magnetic bearing 10 respectively make a pair in the left-right (X-axis) and front-rear (Y-axis) directions. In a device having a pair of magnetic poles in the (Z-axis) direction and performing aerial support with so-called five axes, ten bias circuits are provided by the number of magnetic poles, or as shown in FIG. When the control signal or the inversion control signal from the circuit 32 is supplied to the pulse width modulation circuit 42, the bias signal generated by the bias circuit 49 is superimposed on the control signal, and the bias is superimposed. When the control signal or the inversion control signal is applied to the pulse width modulation circuit 42 for controlling the magnetic poles, current flows simultaneously in two opposing magnetic poles (for example, 9XR and 9XL), and the air support by the control signal or the inversion control signal is performed. High-precision magnetic bearing control cannot be performed for current control.
In addition, when current flows at the same time, current cannot be commutated to the other electrode, and responsiveness cannot be improved.
[0029]
On the other hand, according to the present invention, since the inductance and resistance of the magnetic pole coils 9YL, 9YR... In each of the upper magnetic bearing 9 and the lower magnetic bearing 10 and the thrust magnetic bearing 11 are the same, a bias power supply is provided for each magnetic bearing. And the bias current supply system is made different from the current supply system of claim 1, so that one circuit is provided for each magnetic bearing of the upper magnetic bearing 9 and the lower magnetic bearing 10 and the thrust magnetic bearing 11 for a total of three circuits. A bias circuit is sufficient.
In addition, the bias current supply system is different from the current supply system of the first aspect, so that the application of the bias current and the control of the supply current according to the air gap variation between the rotating shaft and the magnetic bearing are independently performed with high precision. , And high-precision magnetic bearing control becomes possible.
[0030]
According to a fourth aspect of the present invention, there is provided the first control circuit 33A according to the third aspect ,
A second control circuit 33B for supplying a bias current to each of the magnetic pole coils 9YL, 9YR,... In order to increase the static rigidity of each of the magnetic bearings.
The two control circuits are configured to be capable of applying current to the magnetic pole coils 9YL, 9YR,.
[0031]
A fifth aspect of the present invention is an embodiment of the fourth aspect of the present invention. In order to control the position of the rotating shaft in two radial axes (Χ axis, Y axis), the rotating shaft is opposed to the rotating shaft. One or more radial magnetic bearings comprising at least two pairs of magnetic pole coils 9YL, 9YR ...
In order to control the position of the coordinate axis (Z axis) in the thrust direction of the rotating shaft, a thrust magnetic bearing having at least one pair of magnetic pole coils 9YL, 9YR... In the energization control circuit,
A plurality of magnetic pole coils 9YL, 9YR... In the radial magnetic bearing or the thrust magnetic bearing can be applied with a bias current by a single bias current supply circuit (second control circuit 33B) common to each corresponding magnetic bearing. It is characterized by comprising.
[0032]
BEST MODE FOR CARRYING OUT THE INVENTION
Hereinafter, preferred embodiments of the present invention will be illustratively described in detail with reference to the drawings. However, the dimensions, materials, shapes, relative arrangements, and the like of the components described in this embodiment are not intended to limit the scope of the present invention unless otherwise specified, and are merely examples. Only.
[0033]
FIG. 1 is a block diagram showing a magnetic bearing control circuit 33 of the upper magnetic bearing 9 according to the embodiment of the present invention, which corresponds to FIG.
That is, also in this embodiment, similarly to FIG. 2, the position sensors 24 #, 24Y and the magnetic bearing control circuits 32 #, 32Y are provided for each coordinate axis (#, Y), and the control signals of the respective magnetic bearing control circuits 32 #, 32Y are provided. Is supplied to the pulse width modulation circuit 42 of each magnetic pole, and a modulation pulse corresponding to the control signal or the inversion control signal is provided as it is or inverted by the inversion circuit 41 to provide one pair for each coordinate axis (Χ, Y). Are applied to the bases of the FET transistors 44 of the switching elements 43YL, 43YR,... Of the magnetic poles, and the respective magnetic pole coils 9YL, 9YL, which are directly or indirectly connected to the DC power supply 31 through the switching elements 43YL, 43YR,. 9YR... ON / OFF energization control is performed.
[0034]
More specifically, the DC power supply 31 is connected via a diode 47 to the anode (upstream) side of one of the pair of magnetic pole coils 9YL, 9YR,. The switching elements 43 # R and 43YR provided on the downstream side of the magnetic pole coils 9 # R and 9YR are connected, and branching is performed on the upstream side of the switching elements 43 # R and 43YR, and the rotary shaft 7 is sandwiched between the branch lines via the backflow prevention diode 46. Is connected to the anode side of the opposing magnetic pole coils 9 # L and 9YL at the symmetrical positions, and the switching of the corresponding magnetic pole provided on the downstream side is performed every time the switching elements 43 # R and 43YR to the one magnetic pole coil 9 # R and 9YR are turned off. Each time the elements 43 # L and 43YL are turned on, the current energy of one magnetic pole coil 9 # R and 9YR is transferred to the opposite magnetic pole coil 9 # L, It is configured so as to commutated to YL.
[0035]
On the other hand, similarly, the opposite magnetic pole coils 9 # L and 9YL located symmetrically with respect to the rotary shaft 7 similarly have a backflow prevention diode 46 upstream of the switching elements 43 # L and 43YL for controlling ON / OFF energization of the magnetic pole coils 9 # L and 9YL. And connected to the one magnetic pole coil 9 # R, 9YR at the symmetrical position, and the current energy of the opposing magnetic pole coil 9 # L, 9YL is reduced by one for each OFF of the switching element 43 # L, 43YL of the opposite magnetic pole as described above. It is configured to commutate to the magnetic pole coils 9 # R and 9YR.
[0036]
On the other hand, in order to increase the static rigidity of the magnetic bearing 9, a bias drive control circuit 33B for supplying a bias current to each of the magnetic pole coils 9YL, 9YR,... , The current can be applied to the magnetic pole coils 9YL, 9YR,... In a different system from the first drive control circuit 33A that controls the current supplied to the magnetic pole coils 9YL, 9YR,.
[0037]
The bias drive control circuit 33B sets the DC power supply 31 of the first drive control circuit 33A to a bias DC power supply by using a voltage converter (a device capable of insulating the primary side and the secondary side) 52, and then switches the power supply 52. After being sequentially connected to the respective magnetic pole coils 9YL, 9YR,..., They are connected via a diode 48 to a bias switching element 53 composed of an FET transistor 54 and a diode 55.
A bias control signal pulse-width-modulated by a pulse width modulation circuit 51 is applied to the base side of the FET transistor 54, thereby controlling the respective magnetic pole coils 9YL, 9YR,. The bias current is superimposed on the control current of the first drive control circuit 33A, and the current is supplied. Incidentally, 50 is a bias circuit.
[0038]
According to this embodiment, a pair of magnetic pole coils 9YL, 9YR,... Arranged symmetrically with respect to the rotating shaft portion, and a switching element 43YL, 43YR. The pulse width modulation signal is applied to the magnetic pole coils 9YL, 9YR,... Of the pair of magnetic pole coils 9ΧR, 9YR. When the switching elements 43 # R and 43YR are turned on by the modulation signal, a current is supplied from the DC power supply 31 to one of the magnetic pole coils 9 # R and 9YR via the diode 47.
[0039]
On the other hand, the opposing magnetic pole coils 9 # L and 9YL are connected to the one magnetic pole coils 9 # R and 9YR at symmetrical positions via the backflow prevention diode 46 on the upstream side of the corresponding switching elements 43 # L and 43YL. When the corresponding switching elements 43YL, 43YR... Are turned on by the modulation signal in a state where a bias current is applied to the magnetic pole coils 9 # L and 9YL by the bias drive control circuit 33B, in other words, the one magnetic pole coil 9 # R and 9YR When the pulse is turned off, the electric energy of one of the magnetic pole coils 9 # R and 9YL is consumed, and the DC power supply 31 is supplied to the opposing magnetic pole coils 9 # L and 9YL to energize the opposing magnetic pole coils 9 # L and 9YL.
[0040]
Therefore, according to this embodiment, the pair of magnetic pole coils 9YL, 9YR,... Arranged symmetrically with respect to the rotary shaft portion, each time the pulse is turned off, changes the current energy of the one magnetic pole coil 9 # R, 9Y to the opposite magnetic pole coil 9 # L, Since the current is supplied to the 9YL side and the power supply control can be performed while quickly consuming the power, the high-speed response can be effectively secured without generating a resistance loss and without requiring a cooling measure such as a heat sink.
[0041]
Since the inductances and resistances of the magnetic pole coils 9YL, 9YR,... In the upper magnetic bearing 9 are the same, a common bias power supply is used, and a bias current supply system is provided as a separate system. One system is sufficient for the bias drive control circuit 33.
[0042]
【The invention's effect】
As described above, according to the first and third aspects of the present invention, in a magnetic bearing of a high-speed rotating body such as a turbo molecular pump, high-speed responsiveness can be effectively secured without requiring a cooling measure such as a heat sink.
[0043]
According to the second and fourth aspects of the invention, high-speed response can be ensured while simplifying the circuit configuration. In addition, the bias current supply system is different from the current supply system of the first aspect, so that the application of the bias current and the control of the supply current according to the air gap variation between the rotating shaft and the magnetic bearing are independently performed with high precision. , And high-precision magnetic bearing control becomes possible.
[0044]
According to the fifth aspect of the present invention, in order to perform position control of two coordinate axes (Χ axis, Y axis) in the radial direction of the rotating shaft, the radial magnetic bearing including an upper bearing and a lower magnetic bearing; And a thrust magnetic bearing for controlling the position of the coordinate axis (Z-axis) in the thrust direction.
[Brief description of the drawings]
FIG. 1 is a block diagram showing a correspondence diagram similar to FIG. 2 in a magnetic bearing control circuit of an upper magnetic bearing according to an embodiment of the present invention.
FIG. 2 is a block diagram showing a magnetic bearing control circuit of an upper magnetic bearing according to the related art.
FIG. 3 is a block diagram showing a main block configuration of a pump unit A and a power supply unit B of a turbo molecular pump to which the present invention is applied.
FIG. 4 is an overall sectional view of a turbo-molecular pump to which the present invention is applied.
[Explanation of symbols]
A Pump body B Power supply unit 5 Rotor blade 7 Rotating shaft 9 Upper magnetic bearings 9YL, 9YR ... Magnetic pole coil 10 Lower magnetic bearing 11 Thrust magnetic bearings 24 #, 24Y Position sensor 31 Magnetic bearing drive power supply 32 #, 32Y Magnetic bearing control circuit 33A First Driving control circuit 33B Bias driving control circuit (second driving control circuit)
41 Inversion circuit 42 Pulse width modulation circuit 43YL, 43YR ... Magnetic pole switching element 44 FET transistor 46 Backflow prevention diode 52 Voltage converter (bias DC power supply)
53 Switching element for bias

Claims (5)

負荷に連結された回転軸若しくは該回転軸と一体的に回転する磁性部材(以下回転軸部という)を挟んで、夫々対称位置に配置した各対毎の磁気軸受の通電制御により前記回転軸部を空中維持しながら、該回転軸部を高速回転させる高速回転体において、
前記回転軸部と磁気軸受との空隙変動に応じて、前記磁気軸受を構成する電磁石磁極コイルに流す通電電流の制御を、スイッチング素子に印加されるON/OFFパルスにより行なうとともに、該夫々の磁極コイルの電流エネルギーを、前記一の磁極コイルへのパルスOFF毎に、回転軸部の対向位置にある他側磁極コイルへ転流させて行なうことを特徴とする高速回転体に用いる磁気軸受の通電制御方法。
The rotating shaft portion is controlled by energizing each pair of magnetic bearings disposed at symmetric positions with a rotating shaft connected to a load or a magnetic member (hereinafter, referred to as a rotating shaft portion) rotating integrally with the rotating shaft interposed therebetween. In a high-speed rotating body that rotates the rotating shaft at a high speed while maintaining in the air,
In accordance with a variation in the air gap between the rotating shaft portion and the magnetic bearing, the control of the current supplied to the electromagnet magnetic pole coil constituting the magnetic bearing is performed by ON / OFF pulses applied to the switching element, and the respective magnetic poles are controlled. Energizing a magnetic bearing used for a high-speed rotating body, wherein the current energy of the coil is commutated to the other magnetic pole coil at a position facing the rotating shaft portion every time the pulse to the one magnetic pole coil is turned off. Control method.
前記夫々の磁気軸受の静的剛性を上げるために夫々の磁極コイルに流すバイアス電流の通電系統を請求項1の通電系統と別系統にしたことを特徴とする請求項1記載の磁気軸受制御方法。2. The magnetic bearing control method according to claim 1, wherein an energizing system of a bias current flowing through each magnetic pole coil is provided separately from the energizing system of claim 1 in order to increase the static rigidity of each magnetic bearing. . 負荷に連結された回転軸部を挟んで、夫々対称位置に配置した各対毎の磁気軸受の通電制御により前記回転軸部を空中維持しながら、該回転軸部を高速回転させる高速回転体において、
前記回転軸部と磁気軸受との空隙変動に応じて、前記磁気軸受を構成する電磁石磁極コイルに流す通電電流の制御を行なう第一の制御回路を具え、該第一の制御回路が、夫々の磁極コイルに接続されたスイッチング素子のON/OFF制御を、空隙変動に応じて制御されるパルス印加により行なうとともに、前記スイッチング素子の上流側で回転軸部の対向位置にある一対の磁極コイル同士を接続させ、該夫々の磁極コイルの電流エネルギーを、一の磁極コイルへのパルスOFF毎に、対向位置にある他側磁極コイルへ転流させることを特徴とする高速回転体に用いる磁気軸受の通電制御回路。
A high-speed rotating body that rotates the rotary shaft at a high speed while maintaining the rotary shaft in the air by energizing the magnetic bearings of each pair disposed at symmetrical positions with the rotary shaft connected to the load interposed therebetween. ,
A first control circuit for controlling a current supplied to an electromagnet coil constituting the magnetic bearing in accordance with a change in air gap between the rotating shaft portion and the magnetic bearing; ON / OFF control of the switching element connected to the magnetic pole coil is performed by applying a pulse that is controlled in accordance with the air gap variation, and a pair of magnetic pole coils at a position opposing the rotating shaft portion on the upstream side of the switching element are connected. And energizing the magnetic bearings used in the high-speed rotating body, wherein the current energy of each magnetic pole coil is commutated to the other magnetic pole coil at the opposing position every time the pulse to one magnetic pole coil is turned off. Control circuit.
請求項3記載の第一の制御回路と、
前記夫々の磁気軸受の静的剛性を上げるために夫々の磁極コイルにバイアス電流を流す第二の制御回路とを具え、
前記二つの制御回路が夫々別系統で前記磁極コイルに電流印加可能に構成したことを特徴とする請求項3記載の高速回転体に用いる磁気軸受の通電制御回路。
A first control circuit according to claim 3 ,
A second control circuit that supplies a bias current to each magnetic pole coil to increase the static rigidity of each magnetic bearing,
4. The current supply control circuit for a magnetic bearing used in a high-speed rotating body according to claim 3 , wherein said two control circuits are configured so that currents can be applied to said magnetic pole coils by separate systems.
前記回転軸のラジアル方向の二座標軸(Χ軸、Y軸)の位置制御を行なう為に、回転軸に対向して少なくとも二対の磁極コイルを具えた一又は複数のラジアル磁気軸受と、
前記回転軸のスラスト方向の座標軸(Z軸)の位置制御を行なう為に、回転軸と直交する磁性板に対向して少なくとも一対の磁極コイルを具えたスラスト磁気軸受とを具えた請求項4記載の通電制御回路において、
前記ラジアル磁気軸受若しくはスラスト磁気軸受内の複数の磁極コイル群が、夫々対応する磁気軸受毎に共通する第二の制御回路によりバイアス電流が印加可能に構成されていることを特徴とする通電制御回路。
One or a plurality of radial magnetic bearings having at least two pairs of magnetic pole coils facing the rotary shaft to perform position control of two coordinate axes (座標 axis, Y axis) in the radial direction of the rotary shaft;
5. A thrust magnetic bearing having at least one pair of magnetic pole coils opposed to a magnetic plate orthogonal to the rotation axis for performing position control of a coordinate axis (Z axis) in a thrust direction of the rotation axis. In the energization control circuit of
A plurality of magnetic pole coil groups in the radial magnetic bearing or the thrust magnetic bearing, wherein a bias current can be applied by a second control circuit common to each corresponding magnetic bearing; .
JP28036298A 1998-10-01 1998-10-01 Energization control method of magnetic bearing used for high-speed rotating body and its control circuit Expired - Fee Related JP3576397B2 (en)

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