JP2000110777A - Turbo molecular pump and protective operating method for the same - Google Patents

Turbo molecular pump and protective operating method for the same

Info

Publication number
JP2000110777A
JP2000110777A JP10280361A JP28036198A JP2000110777A JP 2000110777 A JP2000110777 A JP 2000110777A JP 10280361 A JP10280361 A JP 10280361A JP 28036198 A JP28036198 A JP 28036198A JP 2000110777 A JP2000110777 A JP 2000110777A
Authority
JP
Japan
Prior art keywords
rotating shaft
magnetic bearing
abnormality
bearing
rotary shaft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP10280361A
Other languages
Japanese (ja)
Other versions
JP3546144B2 (en
Inventor
Katsuhisa Toyama
勝久 外山
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP28036198A priority Critical patent/JP3546144B2/en
Publication of JP2000110777A publication Critical patent/JP2000110777A/en
Application granted granted Critical
Publication of JP3546144B2 publication Critical patent/JP3546144B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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

Abstract

PROBLEM TO BE SOLVED: To guarantee rotation of a turbo molecular pump while eliminating a possible danger of breakdown when an abnormal vibration of a rotor that comprises dynamic blades and a rotary shaft or an erratic operation of an energization control unit of a magnetic bearing is detected, by forcing to move the rotary shaft to one side and supporting rotatably through contact the rotary shaft with a support portion located on that side. SOLUTION: A rotary shaft is given an aerial support by an electromagnetic portion on one side of an upper magnetic bearing and an electromagnetic portion on one side of a lower magnetic bearing in a longitudinal and crosswise direction, and by an electromagnetic portion on one side of a thrust magnetic bearing in an axial direction. Evaluation means 33B determines that a broken dynamic blade will result if a comparison output provided by a comparator 31, i.e., a detected amplitude is 125 μm or more. In this case, a drive control circuit 37 that controls energization of a drive power source 36 of each magnetic bearing changes from inverter control, with which the rotary shaft is normally held in an aerial position, to a rectifier circuit. This results in the rotary shaft being forced to move to the right by a magnetic attraction, thus allowing the rotary shaft to come into contact with a protective bearing to eliminate a danger of breakdown. At the same time, it guarantees good rotation of a turbo molecular pump.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は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、吸気
口からのガスを排気口へ真空排気するターボ分子ポンプ
に係り、特に前記動翼と回転軸からなるロータの異常振
動若しくは前記回転軸を空中維持する磁気軸受の通電制
御部の異常が生じた場合に、該異常に起因して、前記動
翼は静翼と接触して破損するのを有効に防止し得るター
ボ分子ポンプとその動作方法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention is provided in a semiconductor manufacturing apparatus or the like, and includes a moving and stationary blade stage composed of a stationary blade provided in an upper casing and a moving blade provided on a rotating shaft. The present invention relates to a turbo-molecular pump that evacuates the gas to an exhaust port, particularly when an abnormal vibration of a rotor composed of the rotor blades and a rotating shaft or an abnormality of an energization control unit of a magnetic bearing that maintains the rotating shaft in the air occurs. The present invention relates to a turbo-molecular pump capable of effectively preventing the rotor blade from contacting a stationary blade and being damaged due to the abnormality, and a method of operating the turbo-molecular pump.

【0002】[0002]

【従来の技術】図5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5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。
2. Description of the Related Art FIG. 5 shows an example of a turbo molecular pump applied to the present invention. In FIG. 5, reference numerals 1 and 16 denote an upper part integrally assembled via an O-ring 15 by bolts 21. A casing and a lower casing. The upper opening of the upper casing 1 serves as a gas intake port 2, and a plurality of spacers 13 are provided in the inside thereof in the axial direction via a ring-shaped gap. The upper end of the spacer 13 is in contact with the inner end surface of the upper casing 1, and the lower end is fitted into the upper end of the lower casing 16. It is clamped and fixed and provided in a multi-stage shape.

【0003】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、
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。
[0003] Reference numeral 6 denotes a rotor. The rotor 6 is provided with a plurality of moving blades 5 in a multi-stage manner, and the moving blades 5 and the stationary blades 4 are provided so as to mesh with each other alternately to form a blade stage. A thread groove pump stage 8 is provided below the rotor 6. 14 is
A seal ring fixed to the upper surface of the lower casing 16 by bolts 18 is disposed opposite to the outer periphery of the thread groove pump stage 8 with a small gap therebetween, thereby increasing the compression effect.

【0004】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に固定され、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1
9、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1
0、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。
[0004] An exhaust port 3 is opened at the lower side of the lower casing 16, and the fluid that has passed through the thread groove pump stage 8 is sent out from the exhaust port 3 to the outside. Reference numeral 17 denotes a cylindrical support cylinder fixed to the lower casing 16 and protruding upward. The upper protection bearing 1 made of a radial ball bearing is arranged on the inner periphery of the support cylinder 17 in order from the top.
9, upper magnetic bearing 9 as a radial bearing, stator portion 12a of motor 12, lower magnetic bearing 1 as a radial bearing
0, a lower protection bearing 20 composed of a radial ball bearing, and a thrust magnetic bearing 11 provided with a thrust disk 7a at the lower end of the rotating shaft 7 described later interposed therebetween.

【0005】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、前記上部磁気軸受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。
Reference numeral 7 denotes a rotating shaft fixed to the center of the upper portion of the rotor 6. The rotating shaft 7 is suspended in the axial direction from a portion fixed to the rotor 6, and the upper magnetic bearing 9 and the lower magnetic bearing 9 are arranged in order from the upper portion. A radial load is supported by the bearing 10, and a thrust disk 7 a made of a disk-shaped magnetic plate provided at the lower end is sandwiched by the thrust magnetic bearing 11.
Aerial maintenance control in the thrust direction (axial direction) is performed.

【0006】前記ロータ6及び回転軸7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。
A rotor 12b is fixed to the rotor 6 and the rotating shaft 7 so as to face a stator 12a of the motor 12 provided between the upper magnetic bearing 9 and the lower magnetic bearing 10.

【0007】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。
An upper protection bearing 19 is provided above the upper magnetic bearing 9 of the rotary shaft 7, and a radial interval between the rotary shaft 7 and the upper protection bearing 19 is set to a required value. I have. Further, the lower protective bearing 20 is provided below the lower magnetic bearing 10 of the rotating shaft 7, and the radial and thrust intervals between the rotating shaft 7 and the lower protective bearing 20 are set to required values. ing.

【0008】次に上部磁気軸受9及び下部磁気軸受10
は、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(図5(B)参照)。
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。
Next, an upper magnetic bearing 9 and a lower magnetic bearing 10
Is in a plane orthogonal to the axis (Z-axis) of the rotating shaft 7,
A pair is provided in each of the left-right (X-axis) and front-rear (Y-axis) directions, so that the rotary shaft 7 can be maintained in the air on the center axis without falling down (see FIG. 5B). .
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.
The axial center (Z axis) direction is set by the thrust magnetic bearing 11,
That is, the five axis directions are supported in the air, and the rotation is controlled.

【0009】上記のように構成されたターボ分子ポンプ
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がシールリング1
4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段階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。
During operation of the turbo molecular pump constructed as described above, the magnetic bearings 9, 10, and 11 are energized to keep the pump rotating parts such as the rotary shaft 7 and the rotor 6 having the moving blades 5 in the air. In this state, the motor 12 is driven to rotate the pump rotating unit at a high speed of, for example, 10,000 to 100,000 rpm. Due to the high speed rotation of the pump rotating part, the moving blade 5
And the thread pump stage 8 is
After the gas to be evacuated is compressed in the first stage between the moving blades 5 and the stationary blades 4 from the upper gas inlet 2 by rotating while facing the inner peripheral surface of the screw groove 4, the screw groove is formed. The second stage compression takes place in the spiral groove passage of the pump stage 8 and flows in the direction of the outlet 3 via the gas passage in the pump,
The gas inlet 2 side is maintained at a high vacuum.

【0010】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
の回転を補償する。
When the magnetic control of the upper and 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 protection bearing 19 and the lower protection bearing 20 When the outer periphery of the rotating shaft 7 abuts (touch-down), the rotating shaft 7 and the rotor 6
To compensate for rotation.

【0011】[0011]

【発明が解決しようとする課題】さて前記磁気軸受9,
10,11の磁気制御に異常をきたす場合とは、例えば
制御回路の故障、ケーブル断線、コネクタ接触不良等が
あり、そして前記上部保護軸受19と下部保護軸受20
の内径、言換えれば保護軸受19,20と回転軸7との
クリアランスは、前記磁気軸受9,10,11により正
常に空中維持され、そのバラツキの範囲では、回転軸7
は保護軸受19,20に接触することなく、又前記磁気
制御異常により、前記回転軸7が保護軸受19,20に
接触した場合でも動翼5が静翼4に接触しないような設
計ギャップが設定される。
The magnetic bearing 9,
Abnormalities in the magnetic controls 10 and 11 include, for example, control circuit failure, cable disconnection, poor connector contact, and the like.
In other words, the clearance between the protective bearings 19, 20 and the rotating shaft 7 is normally maintained in the air by the magnetic bearings 9, 10, 11 and within the range of variation, the rotating shaft 7
The design gap is set such that the rotor blades 5 do not contact the stationary blades 4 even when the rotating shaft 7 contacts the protective bearings 19 and 20 due to the magnetic control abnormality without contacting the protective bearings 19 and 20. Is done.

【0012】しかしながら前記保護軸受は、上部保護軸
受19と下部保護軸受20により回転軸7を上下に二点
支持する構成を取るが、前記のように回転軸7の上端に
は動翼5が大きく張り出しており、このため回転軸7の
重心が上端側にあるために、前記磁気軸受9,10,1
1の磁気的拘束力が解除された際に、前記クリアランス
内を回転軸7がランダムに揺動し、保護軸受内周との衝
突を繰り返しながら回転することとなる。
However, the protection bearing has a configuration in which the rotating shaft 7 is supported at two points vertically by the upper protecting bearing 19 and the lower protecting bearing 20, but the rotor blade 5 is large at the upper end of the rotating shaft 7 as described above. Since the center of gravity of the rotating shaft 7 is on the upper end side, the magnetic bearings 9, 10, 1
When the magnetic restraining force is released, the rotating shaft 7 randomly swings in the clearance, and rotates while repeatedly colliding with the inner periphery of the protective bearing.

【0013】そして前記衝撃の繰り返しにより、回転軸
7の加振が繰り返され、これに追従して静翼4内に櫛歯
状に嵌合している動翼5が加振且つ共振し、そして前記
動翼5の振れは静翼動翼間のクリアランス(圧縮空間)
より大きくなり、この結果動翼5と静翼4が接触して、
破損に至る恐れがある。又保護軸受側においても、前記
回転軸7の衝突により変形してガタが発生し(前記クリ
アランスの増大)、結果として動翼5と静翼4との設計
ギャップが保証されなくなり、前記と同様に動翼5と静
翼4が接触して、破損に至る恐れがある。
With the repetition of the impact, the vibration of the rotary shaft 7 is repeated, and the moving blade 5 fitted in the comb-like shape in the stationary blade 4 vibrates and resonates following the vibration, and The run-out of the moving blade 5 is a clearance (compression space) between the stationary blade moving blades.
The blade 5 and the stationary blade 4 come into contact with each other,
There is a risk of damage. Also, on the protective bearing side, the bearing is deformed by the collision of the rotating shaft 7 to cause backlash (increase in the clearance). As a result, the design gap between the moving blades 5 and the stationary blades 4 cannot be guaranteed. The moving blades 5 and the stationary blades 4 may come into contact with each other, leading to breakage.

【0014】本発明は、かかる技術的課題に鑑み、動翼
及び回転軸を含むロータの異常振動若しくは磁気軸受の
通電制御部の異常が生じた場合でも、動翼と静翼が接触
して、破損に至る恐れを解消しながらターボ分子ポンプ
の回転を保証し得るターボ分子ポンプの保護動作方法を
提供することを目的とする。
The present invention has been made in view of the above-mentioned technical problems, and even when abnormal vibration of a rotor including a moving blade and a rotating shaft or abnormality of a power supply control unit of a magnetic bearing occurs, the moving blade and the stationary blade come into contact with each other. An object of the present invention is to provide a turbo molecular pump protection operation method capable of guaranteeing rotation of the turbo molecular pump while eliminating the possibility of breakage.

【0015】[0015]

【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、一端に動翼を有する回転
軸を磁気軸受の通電制御により空中維持した状態で、該
回転軸を介して動翼を回転させ、静翼との間で気体の排
気及び圧縮を行なうターボ分子ポンプの保護動作方法に
おいて、前記動翼及び回転軸を含むロータの異常振動若
しくは磁気軸受の通電制御部の異常を検知し、該検知信
号に基づいて前記回転軸をラジアル又は/及びスラスト
方向の一側に強制移動させ、該一側に位置する支持部で
回転軸を回転可能に接触支持させることを特徴とする。
In order to solve the above-mentioned problem, the invention according to the first aspect of the present invention is to provide a rotary shaft having a moving blade at one end while maintaining the rotary shaft in the air by controlling the energization of a magnetic bearing. In the method of protecting a turbo-molecular pump for rotating and moving a moving blade and exhausting and compressing a gas between the moving blade and a stationary blade, an abnormal vibration of a rotor including the moving blade and a rotating shaft or an energization control unit of a magnetic bearing. An abnormality is detected, and the rotary shaft is forcibly moved to one side in the radial or / and thrust direction based on the detection signal, and the rotary shaft is rotatably contacted and supported by a support located on the one side. And

【0016】即ち、本発明は、前記動翼及び回転軸を含
むロータの異常振動若しくは磁気軸受の通電制御部の異
常の場合に、前記回転軸が保護軸受との間のクリアラン
ス内をランダムに揺動するのを阻止するために、前記異
常検知信号に基づいて前記回転軸をラジアル又は/及び
スラスト方向の一側に強制移動させ、該一側に位置する
支持部で回転軸を回転可能に支持させるものであるが、
前記強制移動手段は請求項4に記載のように磁気的吸引
力を用いてもよく、又バネ等の弾性力を利用してもよ
い。又前記片側支持部は請求項4に記載のように保護軸
受を用いてもよく、又磁気軸受を構成する電磁石の表面
にフッ素樹脂加工をして該表面に支持するようにしても
よい。
That is, according to the present invention, in the case of abnormal vibration of the rotor including the rotor blades and the rotating shaft or abnormality of the power supply control section of the magnetic bearing, the rotating shaft randomly fluctuates in the clearance between the rotating shaft and the protective bearing. In order to prevent movement, the rotary shaft is forcibly moved to one side in the radial or / and thrust direction based on the abnormality detection signal, and the rotary shaft is rotatably supported by a support located on the one side. Is to let
The forcible moving means may use a magnetic attraction force as described in claim 4, or may use an elastic force such as a spring. Further, the one-side supporting portion may use a protective bearing as described in claim 4, or the surface of the electromagnet constituting the magnetic bearing may be processed by a fluororesin to support the surface.

【0017】又前記強制移動はラジアル方向のみでもよ
いが、スラスト方向にガタがあると、動翼と静翼が櫛歯
状に配置されているために、両者が接近し、例えラジア
ル方向側で位置固定しても、両者が接触する恐れが出て
くる。このような場合は、請求項3に記載のように、前
記回転軸の支持がスラスト方向で一点、ラジアル方向で
回転軸の上下の二点支持で行ない、いわゆる三点支持で
支持することにより前記欠点の解消が図れる。
The forcible movement may be performed only in the radial direction. However, if there is play in the thrust direction, the moving blades and the stationary blades are arranged in a comb-teeth shape, so that they come close to each other. Even if the positions are fixed, there is a risk that they will come into contact with each other. In such a case, as described in claim 3, the rotation shaft is supported by one point in the thrust direction and two points above and below the rotation axis in the radial direction, and is supported by a so-called three-point support. The disadvantage can be eliminated.

【0018】請求項4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装置に関する発明で、
前記構成のターボ分子ポンプにおいて、前記動翼及び回
転軸を含むロータの異常振動若しくは磁気軸受の通電制
御部の異常を検知する手段と、前記回転軸に対し所定ク
リアランスを以て遊嵌させた保護軸受と、該検知信号に
基づいて前記磁気軸受への通電電圧を前記通電制御部と
は別系統から供給する電圧切換え手段とを具え、前記切
換え手段による磁気軸受の磁気的吸引力により、回転軸
を保護軸受の一側に強制移動させ、該保護軸受で回転軸
を回転可能に接触支持させることを特徴とする。
A fourth aspect of the present invention relates to an apparatus for effectively implementing the first aspect of the present invention.
In the turbo-molecular pump having the above-described configuration, means for detecting abnormal vibration of the rotor including the rotor blades and the rotating shaft or abnormality of the power supply control unit of the magnetic bearing, and a protective bearing loosely fitted with a predetermined clearance to the rotating shaft. Voltage switching means for supplying an energizing voltage to the magnetic bearing based on the detection signal from a system different from the energizing control unit, and protecting the rotating shaft by a magnetic attraction of the magnetic bearing by the switching means. It is characterized in that it is forcibly moved to one side of the bearing, and the rotating shaft is rotatably contacted and supported by the protective bearing.

【0019】請求項2記載の発明は、前記ターボ分子ポ
ンプの保護動作方法において、前記動翼及び回転軸を含
むロータの異常振動若しくは磁気軸受の通電制御部の異
常を振動量と時間との関係において第一の異常と第二の
異常とに判別検知し、第一の異常検知において、前記回
転軸の空中維持状態での回転を継続しながら警報を鳴動
若しくは表示させ、第二の異常検知において、該第二の
異常検知信号に基づいて前記回転軸をラジアル又は/及
びスラスト方向の一側に強制移動させ、該一側に位置す
る支持部で回転軸の回転可能に接触支持させることを特
徴とするターボ分子ポンプの保護動作方法にある。
According to a second aspect of the present invention, in the method for protecting the turbo-molecular pump, the abnormal vibration of the rotor including the rotor blades and the rotating shaft or the abnormality of the power supply control unit of the magnetic bearing is related to the relationship between the amount of vibration and time. In the first abnormality and the second abnormality is detected and determined, and in the first abnormality detection, an alarm is sounded or displayed while the rotation of the rotating shaft in the air-maintaining state is continued, and in the second abnormality detection, The rotary shaft is forcibly moved to one side in a radial or / and thrust direction based on the second abnormality detection signal, and the rotary shaft is rotatably contacted and supported by a support portion located on the one side. The protective operation method of the turbo molecular pump described above.

【0020】かかる発明によれば、前記異常信号があっ
たとき直ちに磁気軸受による空中維持を取り止めて、例
えばラジアル球軸受のような機械的軸受による接触支持
による軸支を行なうと、回転数が大幅に低下し、特に半
導体製造装置においてウエーハにシラン等の反応ガスを
流しながら酸化膜やCVD膜を生成途中に急激な回転ダ
ウンが生じると、そのバッチ工程のウエーハが不良にな
ってしまう。又、前記した請求項1記載の保護動作を取
らずにそのまま放置することは、ポンプの破壊が他の半
導体設備の破損につながるのみならず、シラン等の毒性
ガスが外部に流れ、危険である。更に軽異常信号が発せ
られた場合、必ずしも外部ノイズにより瞬間的な異常と
なる場合もあり、このような誤動作を排除する必要があ
る。一方、重異常の場合は直ちに保護動作に入らない
と、動翼と静翼が接触して、破損に至る恐れがある。
According to this invention, when the air bearing is stopped immediately by the magnetic bearing when the abnormal signal is detected and the bearing is supported by the contact support by a mechanical bearing such as a radial ball bearing, the number of rotations is greatly increased. In particular, if a rapid rotation down occurs during the formation of an oxide film or a CVD film while flowing a reaction gas such as silane through a wafer in a semiconductor manufacturing apparatus, the wafer in the batch process becomes defective. If the pump is left as it is without taking the protective action described in claim 1, the destruction of the pump not only leads to damage to other semiconductor equipment, but also toxic gas such as silane flows to the outside, which is dangerous. . Furthermore, when a light abnormality signal is issued, an instantaneous abnormality may necessarily occur due to external noise, and it is necessary to eliminate such a malfunction. On the other hand, in the case of a heavy abnormality, unless the protection operation is immediately started, the moving blades and the stationary blades may come into contact with each other and may be damaged.

【0021】そこで本発明は前記異常を、動翼と静翼が
接触する恐れのない軽異常と、接触する恐れのある重異
常とに分け、軽異常の場合は振動検知時間を時間との関
係において第一の異常(軽異常)と第二の異常(重異
常)とに判別検知し、軽異常信号が発せられた場合、必
ずしも外部ノイズにより瞬間的な異常となる場合もあ
り、このような誤動作を排除するために、例えば、2秒
程度軽異常信号が続くか否かを判断して、続いた場合に
警報を鳴動若しくは表示させて、操作者に注意を促し、
その時点で圧力を低くするか若しくは予備ポンプに切換
える等の対策を取らせる。
Therefore, the present invention classifies the abnormalities into light abnormalities in which the moving blade and the stationary blade do not come into contact with each other and heavy abnormalities in which the moving blades and the stationary blade may come into contact with each other. In the case where the first abnormality (light abnormality) and the second abnormality (heavy abnormality) are discriminated and detected and a light abnormality signal is issued, an instantaneous abnormality may necessarily be caused by external noise. In order to eliminate a malfunction, for example, it is determined whether or not the light abnormal signal continues for about 2 seconds, and if it continues, an alarm is sounded or displayed to alert the operator,
At that time, take measures such as lowering the pressure or switching to a backup pump.

【0022】そして前記対策を取っても又対策を取る前
に重異常の場合は直ちに保護動作に入らないと、動翼と
静翼が接触して、破損に至る恐れがある。そこで重異常
の場合は直ちに異常と判断し、該第二の異常検知信号に
基づいて前記回転軸をラジアル又は/及びスラスト方向
の一側に強制移動させ、該一側に位置する支持部で回転
軸の回転可能に接触支持させることにより、動翼と静翼
が接触して、破損に至る恐れを解消しながらターボ分子
ポンプの回転を保証し得る。
Even if the above countermeasures are taken, if a serious abnormality occurs before taking the countermeasures, unless the protection operation is immediately started, the moving blades and the stationary blades may come into contact with each other, possibly leading to breakage. Therefore, in the case of a serious abnormality, the abnormality is immediately determined to be abnormal, and the rotary shaft is forcibly moved to one side in the radial or / and thrust direction based on the second abnormality detection signal, and is rotated by the support portion located on the one side. By rotatably contacting the shaft, the rotating blade and the stationary blade come into contact with each other, and rotation of the turbo-molecular pump can be guaranteed while eliminating the possibility of damage.

【0023】請求項5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装置に関する発明で、
前記構成のターボ分子ポンプにおいて、前記動翼及び回
転軸を含むロータの異常振動若しくは磁気軸受の通電制
御部の異常を振動量と時間との関係において第一の異常
と第二の異常とに判別検知する手段と、警報を鳴動若し
くは表示させる手段と、前記回転軸に対し所定クリアラ
ンスを以て遊嵌させた保護軸受と、該検知信号に基づい
て前記磁気軸受への通電電圧を前記通電制御部とは別系
統から供給する電圧切換え手段とを具え、第一の異常検
知において、前記回転軸の空中維持状態での回転を継続
しながら警報を鳴動若しくは表示させ、第二の異常検知
において、該第二の異常検知信号に基づいて前記切換え
手段を動作させ、該切換え手段による磁気軸受の磁気的
吸引力により、回転軸を保護軸受の一側に強制移動さ
せ、該保護軸受で回転軸を回転可能に接触支持させるこ
とを特徴とする。
A fifth aspect of the present invention relates to an apparatus for effectively implementing the first aspect of the present invention.
In the turbo-molecular pump having the above-described configuration, abnormal vibration of the rotor including the rotor blade and the rotating shaft or abnormality of the power supply control unit of the magnetic bearing is determined as a first abnormality and a second abnormality in relation to the amount of vibration and time. Means for detecting, means for sounding or displaying an alarm, a protective bearing loosely fitted with a predetermined clearance to the rotating shaft, and an energizing control unit for applying an energizing voltage to the magnetic bearing based on the detection signal. A voltage switching unit supplied from another system, wherein in the first abnormality detection, an alarm is sounded or displayed while the rotation of the rotary shaft in the air-maintaining state is continued, and in the second abnormality detection, the second abnormality is detected. The switching means is operated on the basis of the abnormality detection signal, and the rotating shaft is forcibly moved to one side of the protection bearing by the magnetic attraction force of the magnetic bearing by the switching means, and is rotated by the protection bearing. And characterized in that rotatably contact support the shaft.

【0024】[0024]

【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。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Preferred embodiments of the present invention will be illustratively described in detail below 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 illustrative examples. Only.

【0025】図1は、本発明の実施形態に係るターボ分
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
ロック構成を示し、振動検知に基づく警報表示と回転軸
の保護動作を設定しているブロック図である。図2は、
本発明の実施形態に係るターボ分子ポンプの要部構成を
示す断面図で、異常検知前の状態を示す。図3(A)は
異常検知後の回転軸の保護動作の要部拡大図で図2の対
応図である、(B)は(A)を上面からみた図、(C)
は(A)の丸部分の拡大図である。図4は振動検知に基
づく警報表示と回転軸の保護動作をの流れを示すブロッ
ク図である。図5は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。
FIG. 1 shows a block diagram of a main part of a pump unit A and a power supply unit B of a turbo-molecular pump according to an embodiment of the present invention, in which an alarm display based on vibration detection and a protection operation of a rotating shaft are set. It is a block diagram. FIG.
FIG. 2 is a cross-sectional view illustrating a main part configuration of the turbo-molecular pump according to the embodiment of the present invention, showing a state before abnormality detection. FIG. 3A is an enlarged view of a main part of the protection operation of the rotating shaft after the abnormality is detected, and is a corresponding view of FIG. 2, FIG. 3B is a view of FIG.
(A) is an enlarged view of a circle portion. FIG. 4 is a block diagram showing a flow of an alarm display based on vibration detection and a protection operation of the rotating shaft. FIG. 5 is an overall sectional view of a turbo-molecular pump to which the present invention is applied.

【0026】先ず本実施形態の理解を容易化する為に、
図2及び図3に従って回転軸7と支持筒17の保護軸受
19,20と磁気軸受9,10,11の構成について概
略的に説明する。17は下部ケーシング16に固定さ
れ、上方に突設された円筒状の支持筒で、該支持筒17
の内周に上部から順に、ラジアル玉軸受からなる上部保
護軸受19、位置センサ24、ラジアル軸受である上部
磁気軸受9の一側左右電磁石部9R 1,9L1、モータ1
2のステータ部12a(図示省略)、ラジアル軸受であ
る下部磁気軸受10の一側左右電磁石部10R1,10
1、ラジアル玉軸受からなる下部保護軸受20、並び
に回転軸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の上下電磁石部11U,1
1Lが配設されている。
First, in order to facilitate understanding of this embodiment,
Protective bearing for the rotating shaft 7 and the support cylinder 17 according to FIGS.
19, 20 and magnetic bearings 9, 10, 11
This will be briefly described. 17 is fixed to the lower casing 16
And a cylindrical support cylinder projecting upward,
In the inner circumference of the upper part, in order from the top,
Protection bearing 19, position sensor 24, upper part which is a radial bearing
One side left and right electromagnet part 9R of the magnetic bearing 9 1, 9L1, Motor 1
2 and a radial bearing (not shown).
Left and right electromagnets 10R on one side of the lower magnetic bearing 101, 10
L1, Lower protective bearing 20 consisting of a radial ball bearing,
Provided with a thrust disk 7a at the lower end of the rotating shaft 7
Upper and lower electromagnet portions 11U, 1 of the separated thrust magnetic bearing 11
1L is provided.

【0027】一方回転軸7は、上部から順に、上部磁気
軸受9の他側左右電磁石部9R2,9L2、下部磁気軸受
10の他側左右電磁石部10R2,10L2及び下端に設
けられた円盤状の磁性板からなるスラストディスク7a
を具え、該スラストディスク7aを前記スラスト磁気軸
受11の上下電磁石部11U,11L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。
On the other hand, the rotating shaft 7 is provided on the other left and right electromagnet portions 9R 2 and 9L 2 on the other side of the upper magnetic bearing 9, the other left and right electromagnet portions 10R 2 and 10L 2 on the other side of the lower magnetic bearing 10 and the lower end in order from the top. Thrust disk 7a made of a disk-shaped magnetic plate
The thrust disk 7a is sandwiched between the upper and lower electromagnets 11U and 11L of the thrust magnetic bearing 11 to perform aerial maintenance control in the thrust direction (axial direction).

【0028】尚、図1及び図5に示すように、上部磁気
軸受9及び下部磁気軸受10は、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、該上部磁気軸受の
一側電磁石部9及び下部磁気軸受の一側電磁石部10に
より左右(X軸)及び前後(Y軸)方向を、前記スラス
ト磁気軸受の一側電磁石部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。
As shown in FIGS. 1 and 5, the upper magnetic bearing 9 and the lower magnetic bearing 10 are provided with an axis (Z
Axis), a pair is provided in each of the left-right (X-axis) and front-rear (Y-axis) directions, so that the rotating shaft 7 can be maintained in the air on the center axis without falling down. I have. Therefore, the rotating shaft 7 is moved in the left-right (X-axis) and front-rear (Y-axis) directions by the one-side electromagnet portion 9 of the upper magnetic bearing and the one-side electromagnet portion 10 of the lower magnetic bearing. The electromagnet section 11 supports the axis (Z axis) direction, that is, the five axis directions, in the air, and rotates in a controlled manner.

【0029】元に戻り、回転軸7の前記上部磁気軸受9
の一側電磁石部9R2、9L2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との間
隔を所要の値α1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の一側電磁石部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との間隔を所要値α1に設定している。
Returning to the original, the upper magnetic bearing 9 of the rotating shaft 7
The upper protection bearings 19 are provided above the one-side electromagnet portions 9R 2 and 9L 2 , and the distance between the rotary shaft 7 and the upper protection bearings 19 is set to a required value α 1 . Further, the rotating shaft 7
The lower protective bearing 20 is provided below the one-side electromagnet section 10 of the lower magnetic bearing 10, and the interval between the rotating shaft 7 and the lower protective bearing 20 is set to a required value α 1 .

【0030】支持筒17と回転軸7間に位置する電磁石
部9R1と9R2,9L1と9L2、10R1と10R2,1
0L1と10L2とのクリアランスβ1を、保護軸受1
9、20との間隔α1より大(β1>α1)に設定し、図
3に示すように、前記回転軸7が保護軸受19,20に
当接した際に、電磁石部9R1と9R2,10R1と10
2が離間(β1−α1)しているように設定する。
The electromagnet portions 9R 1 and 9R 2 , 9L 1 and 9L 2 , 10R 1 and 10R 2 , 1 located between the support cylinder 17 and the rotating shaft 7
The clearance β 1 between 0L 1 and 10L 2 is increased
Than the distance alpha 1 between 9,20 and set to a large (β 1> α 1), as shown in FIG. 3, when the rotary shaft 7 is in contact with the protection bearings 19 and 20, the electromagnet portion 9R 1 9R 2 , 10R 1 and 10
R 2 is set so spaced (β 1 1).

【0031】又、図3に示すように、回転軸7の細径部
7bに位置する保護軸受20上面と細径部7bの上段差
面7c間の距離α2を、前記回転軸7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下面と前
記スラスト磁気軸受の下側電磁石部11Lとのクリアラ
ンスβ2より小に(β2−α2)設定する。
As shown in FIG. 3, the distance α 2 between the upper surface of the protection bearing 20 located at the small diameter portion 7b of the rotary shaft 7 and the upper step surface 7c of the small diameter portion 7b is set at the lower end of the rotary shaft 7. The clearance (β 2 −α 2 ) is set to be smaller than the clearance β 2 between the lower surface of the thrust disk 7 a formed of a disk-shaped magnetic plate and the lower electromagnet portion 11 L of the thrust magnetic bearing.

【0032】かかる実施形態によれば、後記に詳細に説
明するように、前記位置変位センサ等で検知される回転
軸や動翼部の振幅が125μmで、且つ0.5秒以上続
いた場合は磁気軸受の、支持筒17と回転軸7間に位置
する電磁石部の、9R1と10R1が、9R2と10R2
吸引し合うように、又9L1と9L2、10L1と10L2
の吸引が小さくなるように通電することにより、図3に
示すように、回転軸は磁気的吸引力によりラジアル方向
の図上右方向に強制移動し、前記電磁石部9R1と9
2、10R1と10R2のクリアランスβ1が、保護軸受
19、20との間隔α1より大(β1>α1)に設定され
ている為に、前記電磁石部9R1と9R2,10R1と1
0R2が離間(β1−α1)している状態で、前記回転軸
7が保護軸受19,20に当接するために、回転軸7の
回転は保護軸受19,20により円滑に保証される。
According to this embodiment, as will be described later in detail, when the amplitude of the rotating shaft or the moving blade portion detected by the position displacement sensor or the like is 125 μm and continues for 0.5 seconds or more, 9R 1 and 10R 1 of the electromagnet portion of the magnetic bearing located between the support cylinder 17 and the rotating shaft 7 attract 9R 2 and 10R 2 , and 9L 1 and 9L 2 , 10L 1 and 10L 2
As shown in FIG. 3, the rotating shaft is forcibly moved to the right in the radial direction by magnetic attraction force to reduce the attraction of the electromagnets 9R 1 and 9R.
For clearance beta 1 of R 2, 10R 1 and 10R 2 is set to a large (β 1> α 1) than the distance alpha 1 between the protective bearings 19 and 20, the electromagnet portion 9R 1 and 9R 2, 10R 1 and 1
In a state where 0R 2 is separated (β 1 1), to the rotating shaft 7 is in contact with the protection bearings 19 and 20, the rotation of the rotary shaft 7 is smoothly ensured by protective bearings 19, 20 .

【0033】又、図3に示すように、前記スラスト磁気
軸受7aの下側電磁石部11Lのみを通電し、上側電磁
石部11Uの通電を解除することにより、磁気的吸引力
により回転軸7は下側に強制移動し、これによりスラス
トディスク7a下面と前記スラスト磁気軸受の下側電磁
石部11Lとのクリアランス(β2−α2)を維持しつ
つ、回転軸7の細径部7bに位置する保護軸受20上面
と細径部7bの上段差面7cが係合し、回転軸7の回転
は保護軸受20により円滑に保証されながら位置固定さ
れる。この結果、前記回転軸7の支持がスラスト方向で
一点、ラジアル方向で回転軸の上下の二点支持で行な
い、いわゆる三点支持で回転軸7の回転を保証しながら
位置固定されることとなる。
As shown in FIG. 3, by energizing only the lower electromagnet portion 11L of the thrust magnetic bearing 7a and deenergizing the upper electromagnet portion 11U, the rotating shaft 7 is moved downward by magnetic attraction. Side, thereby maintaining a clearance (β 2 −α 2 ) between the lower surface of the thrust disk 7a and the lower electromagnet portion 11L of the thrust magnetic bearing, while protecting the rotary shaft 7 at the small diameter portion 7b. The upper surface of the bearing 20 and the upper step surface 7c of the small diameter portion 7b are engaged, and the position of the rotating shaft 7 is fixed while being smoothly assured by the protective bearing 20. As a result, the rotation shaft 7 is supported at one point in the thrust direction and at two points above and below the rotation shaft in the radial direction, and the position of the rotation shaft 7 is fixed while so-called three-point support ensures rotation of the rotation shaft 7. .

【0034】かかる点を回路構成としてブロック化した
のが図1で、又その動作を説明したのが図4のフローチ
ャート図である。先ずポンプ本体A側より前記した位置
変位センサ若しくは独立した振動センサ30より検知し
た振幅量を比較器31A、31Bに投入する。
FIG. 1 is a block diagram of such a point as a circuit configuration, and FIG. 4 is a flowchart illustrating the operation thereof. First, the amplitude amount detected by the position displacement sensor or the independent vibration sensor 30 from the pump main body A side is input to the comparators 31A and 31B.

【0035】比較器31Aでは基準振幅量50μmに対
応する基準電圧発生器32Aよりの信号と比較し、前記
検知振幅量が50μm以上の場合に比較出力を判定手段
33Aに送付する。(S1)
The comparator 31A compares the signal with a signal from the reference voltage generator 32A corresponding to the reference amplitude of 50 μm, and sends a comparison output to the judging means 33A when the detected amplitude is 50 μm or more. (S1)

【0036】一方比較器31Bでは基準振幅量125μ
mに対応する基準電圧発生器32Bよりの信号と比較
し、前記検知振幅量が125μm以上の場合に比較出力
を判定手段33Bに送付する。(S2) 前記比較器31Bの基準振幅量を125μmに設定した
のは、回転軸7と保護軸受19、20との間隔α1に対
応させたもの(α1:125μm)である。
On the other hand, the comparator 31B has a reference amplitude of 125 μm.
The signal is compared with a signal from the reference voltage generator 32B corresponding to m, and when the detected amplitude is 125 μm or more, a comparison output is sent to the judgment means 33B. (S2) The reference amplitude of the comparator 31B is set to 125 μm in correspondence with the interval α 1 between the rotating shaft 7 and the protective bearings 19 and 20 (α 1 : 125 μm).

【0037】判定手段33Aでは、前記比較器31Aよ
りの比較出力、言換えれば前記検知振幅量50μm以上
が2秒以上続いた場合は(S4)、磁気軸受の通電制御
回路等の故障であると判断して警報を鳴動させるか、表
示35を行なう(S5)。尚34Aはタイマである。
In the determination means 33A, if the comparison output from the comparator 31A, in other words, the detected amplitude amount of 50 μm or more continues for 2 seconds or more (S4), it is determined that the magnetic bearing power supply control circuit or the like is faulty. Judgment is made to sound an alarm or display 35 is performed (S5). 34A is a timer.

【0038】又判定手段33Bでは、前記比較器31B
よりの比較出力、言換えれば前記検知振幅量125μm
以上の場合は、より具体的には0.5秒でも続いた場合
は(S6)、動翼5の破損につながると判断して、前記
磁気軸受9,10,11の駆動電源36の通電制御を行
なう駆動制御回路37内で、通常の回転軸7の空中維持
を行なうインバータ制御から整流回路に切換え(S
7)、ラジアル方向側の磁気軸受についてはY軸方向側
の電磁石9YU1〜9YL2の通電をカットし、Χ軸方向
側の電磁石部の、9ΧR1と、9ΧR2が吸引し合うよう
に、又9L1と9L2の吸引が小さくなるように通電する
こと(下部磁気軸受も同様)により、回転軸は磁気的吸
引力によりラジアル方向の図上右方向に強制移動し、前
記電磁石部9R1と9R2が離間(β1−α1)している状
態で、前記回転軸7が保護軸受19,20に当接するた
めに、回転軸7の回転は保護軸受19,20により円滑
に保証される。尚、34Bはタイマである。
In the judgment means 33B, the comparator 31B
The comparison output, in other words, the detected amplitude amount 125 μm
In the above case, more specifically, when the operation continues for 0.5 seconds (S6), it is determined that the rotor blade 5 is damaged, and the energization control of the drive power supply 36 of the magnetic bearings 9, 10, 11 is performed. In the drive control circuit 37 that performs the operation, the inverter control that normally maintains the rotary shaft 7 in the air is switched to the rectifier circuit (S
7), to cut the power in the Y-axis direction side of the electromagnet 9YU 1 ~9YL 2 for magnetic bearing of the radial direction, of the electromagnet of the Χ axis side, and 9Kaiaru 1, so 9Kaiaru 2 with each other by suction, by also applying a current to the suction of 9 L 1 and 9 L 2 decreases (as well as the lower magnetic bearings), the rotary shaft is moved forcibly in the drawing the right direction in the radial direction by the magnetic attraction force, the electromagnet portion 9R 1 and in a state where 9R 2 is separated (β 1 1), to the rotating shaft 7 is in contact with the protection bearings 19 and 20, the rotation of the rotary shaft 7 is smoothly ensured by protective bearings 19, 20 You. 34B is a timer.

【0039】又、前記スラスト磁気軸受11においても
下側電磁石部11Lのみを通電し、上側電磁石部11U
の通電を解除することにより、磁気的吸引力により回転
軸7は下側に強制移動し、これにより前記クリアランス
(β2−α2)を維持しつつ、回転軸7の細径部7bに位
置する保護軸受20上面と細径部7bの上段差面7cが
係合し、回転軸7の回転は保護軸受20により円滑に保
証されながら位置固定される。
In the thrust magnetic bearing 11, only the lower electromagnet portion 11L is energized, and the upper electromagnet portion 11U
, The rotating shaft 7 is forcibly moved downward by the magnetic attraction force, thereby maintaining the clearance (β 2 −α 2 ) while maintaining the clearance (β 2 −α 2 ) at the small diameter portion 7 b of the rotating shaft 7. The upper surface of the protective bearing 20 and the upper step surface 7c of the small-diameter portion 7b engage with each other, and the rotation of the rotating shaft 7 is fixed by the protective bearing 20 while being smoothly assured.

【0040】この結果、前記回転軸の支持がスラスト方
向で一点、ラジアル方向で回転軸の上下の二点支持で行
ない、いわゆる三点支持で回転軸7の回転を保証しなが
ら位置固定されることとなる。
As a result, the rotation shaft is supported at one point in the thrust direction and at two points above and below the rotation shaft in the radial direction. Becomes

【0041】[0041]

【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、前記ロータの異常振動検知信号に基づい
て前記回転軸をラジアル又は/及びスラスト方向の一側
に強制移動させ、該一側に位置する支持部で回転軸を回
転可能に支持させる為に、動翼及び回転軸を含むロータ
の異常振動若しくは磁気軸受の通電制御部の異常が生じ
た場合でも、動翼と静翼が接触して、破損に至る恐れを
解消しながらターボ分子ポンプの回転を保証し得る。
As described above, according to the first and third aspects of the present invention, the rotary shaft is forcibly moved to one side in the radial or / and thrust direction based on the abnormal vibration detection signal of the rotor. In order to rotatably support the rotating shaft with the support located on one side, even if abnormal vibration of the rotor including the moving blade and the rotating shaft or abnormality of the power supply control unit of the magnetic bearing occurs, the moving blade and the stationary blade Contact with each other to ensure the rotation of the turbo-molecular pump while eliminating the risk of breakage.

【0042】又前記強制移動はラジアル方向のみでもよ
いが、スラスト方向にガタがあると、動翼と静翼が櫛歯
状に配置されているために、両者が接近し、例えラジア
ル方向側で位置固定しても、両者が接触する恐れが出て
くる。このような場合は、請求項3に記載のように、前
記回転軸の支持がスラスト方向で一点、ラジアル方向で
回転軸の上下の二点支持で行ない、いわゆる三点支持で
支持することにより前記欠点の解消が図れる。
The forcible movement may be performed only in the radial direction. However, if there is backlash in the thrust direction, the moving blades and the stationary blades are arranged in a comb shape, so that they come close to each other. Even if the positions are fixed, there is a risk that they will come into contact with each other. In such a case, as described in claim 3, the rotation shaft is supported by one point in the thrust direction and two points above and below the rotation axis in the radial direction, and is supported by a so-called three-point support. The disadvantage can be eliminated.

【0043】請求項2及び5記載の発明によれば、本発
明は前記異常を、動翼と静翼が接触する恐れのない軽異
常と、接触する恐れのある重異常とに分け、軽異常の場
合は振動検知時間を時間との関係において第一の異常
(軽異常)と第二の異常(重異常)とに判別検知し、軽
異常信号が発せられた場合、必ずしも外部ノイズにより
瞬間的な異常となる場合もあり、このような誤動作を排
除するために、2秒程度軽異常信号が続くか否かを判断
して、続いた場合に警報を鳴動若しくは表示させて、操
作者に注意を促し、又重異常の場合は直ちに異常と判断
し、該第二の異常検知信号に基づいて前記回転軸をラジ
アル又は/及びスラスト方向の一側に強制移動させ、該
一側に位置する支持部で回転軸の回転可能に接触支持さ
せることにより、動翼と静翼が接触して、破損に至る恐
れを解消しながらターボ分子ポンプの回転を保証し得
る。
According to the second and fifth aspects of the present invention, the present invention classifies the abnormalities into light abnormalities in which the moving blade and the stationary blade do not come into contact with each other and heavy abnormalities in which the moving blade and the stationary blade may come into contact with each other. In the case of, the vibration detection time is discriminated and detected as a first abnormality (light abnormality) and a second abnormality (heavy abnormality) in relation to time, and when a light abnormality signal is issued, it is not necessarily instantaneous due to external noise. In order to eliminate such a malfunction, it is determined whether or not the light abnormality signal continues for about 2 seconds, and if so, an alarm is sounded or displayed, and attention is paid to the operator. In the case of a heavy abnormality, the abnormality is immediately judged to be abnormal, and the rotary shaft is forcibly moved to one side in the radial or / and thrust direction based on the second abnormality detection signal, and the support located on the one side is The rotation of the rotating shaft is supported by the And stationary vanes in contact, may guarantee the rotation of the turbo-molecular pump while eliminating the risk to failure.

【図面の簡単な説明】[Brief description of the drawings]

【図1】 本発明の実施形態に係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
を示し、振動検知に基づく警報表示と回転軸の保護動作
を設定しているブロック図である。
FIG. 1 is a block diagram showing a main part block configuration of a pump unit A and a power supply unit B of a turbo-molecular pump according to an embodiment of the present invention, in which an alarm display based on vibration detection and a rotation axis protection operation are set. is there.

【図2】 本発明の実施形態に係るターボ分子ポンプの
要部構成を示す断面図で、異常検知前の状態を示す。
FIG. 2 is a cross-sectional view showing a configuration of a main part of the turbo-molecular pump according to the embodiment of the present invention, showing a state before abnormality detection.

【図3】 (A)は異常検知後の回転軸の保護動作の要
部拡大図で図2の対応図であり、(B)は(A)を上面
からみた図、(C)は(A)の丸部分の拡大図である。
3A is an enlarged view of a main part of the operation of protecting the rotating shaft after detecting an abnormality, and is a corresponding view of FIG. 2, FIG. 3B is a view of FIG. 2A as viewed from above, and FIG. It is an enlarged view of the circle part of ().

【図4】 振動検知に基づく警報表示と回転軸の保護動
作をの流れを示すブロック図である。
FIG. 4 is a block diagram showing a flow of an alarm display based on vibration detection and a protection operation of a rotating shaft.

【図5】 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。
FIG. 5 is an overall sectional view of a turbo-molecular pump to which the present invention is applied.

【符号の説明】[Explanation of symbols]

A ポンプ本体 B 電源ユニット 5 動翼 7 回転軸 7b 回転軸の細径部 7c 細径部の上段差面 9 上部磁気軸受 10 下部磁気軸受 11 スラスト磁気軸受(電磁石) 19,20 保護軸受 30 振動センサ 31A、31B 比較器 32A、32B 基準電圧発生器 33A、33B 判定手段 36 駆動電源 37 駆動制御回路 Reference Signs List A pump main body B power supply unit 5 rotor blade 7 rotating shaft 7b small-diameter portion of rotating shaft 7c upper step surface of small-diameter portion 9 upper magnetic bearing 10 lower magnetic bearing 11 thrust magnetic bearing (electromagnet) 19, 20 protective bearing 30 vibration sensor 31A, 31B Comparator 32A, 32B Reference voltage generator 33A, 33B Judging means 36 Drive power supply 37 Drive control circuit

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】 一端に動翼を有する回転軸を磁気軸受の
通電制御により空中維持した状態で、該回転軸を介して
動翼を回転させ、静翼との間で気体の排気及び圧縮を行
なうターボ分子ポンプの保護動作方法において、 前記動翼及び回転軸を含むロータの異常振動若しくは磁
気軸受の通電制御部の異常を検知し、該検知信号に基づ
いて前記回転軸をラジアル又は/及びスラスト方向の一
側に強制移動させ、該一側に位置する支持部で回転軸を
回転可能に接触支持させることを特徴とするターボ分子
ポンプの保護動作方法。
In a state where a rotating shaft having a moving blade at one end is maintained in the air by energizing control of a magnetic bearing, the moving blade is rotated through the rotating shaft to exhaust and compress gas with the stationary blade. In the method for performing a protective operation of a turbo-molecular pump to be performed, abnormal vibration of a rotor including the rotor blades and the rotating shaft or abnormality of a power supply control unit of a magnetic bearing is detected, and the rotating shaft is radially and / or thrusted based on the detection signal. A protective operation method for a turbo-molecular pump, comprising: forcibly moving the rotary shaft in one side in the direction, and rotatably contacting and supporting the rotation shaft by a support portion located on the one side.
【請求項2】 一端に動翼を有する回転軸を磁気軸受の
通電制御により空中維持した状態で、該回転軸を介して
動翼を回転させ、静翼との間で気体の排気及び圧縮を行
なうターボ分子ポンプの保護動作方法において、 前記動翼及び回転軸を含むロータの異常振動若しくは磁
気軸受の通電制御部の異常を、振動量と時間との関係に
おいて第一の異常と第二の異常とに判別検知し、 第一の異常検知において、前記回転軸の空中維持状態で
の回転を継続しながら警報を鳴動若しくは表示させ、 第二の異常検知において、該第二の異常検知信号に基づ
いて前記回転軸をラジアル又は/及びスラスト方向の一
側に強制移動させ、該一側に位置する支持部で回転軸の
回転可能に接触支持させることを特徴とするターボ分子
ポンプの保護動作方法。
In a state where a rotating shaft having a moving blade at one end is maintained in the air by energizing control of a magnetic bearing, the moving blade is rotated through the rotating shaft to exhaust and compress gas with the stationary blade. In the protection operation method of the turbo-molecular pump to be performed, the abnormal vibration of the rotor including the rotor blade and the rotating shaft or the abnormality of the power supply control unit of the magnetic bearing, the first abnormality and the second abnormality in relation to the amount of vibration and time. In the first abnormality detection, an alarm is sounded or displayed while the rotation shaft keeps rotating in the air-maintaining state, and the second abnormality detection is performed based on the second abnormality detection signal. Wherein the rotating shaft is forcibly moved to one side in a radial or / and thrust direction, and the rotating shaft is rotatably contacted and supported by a support located on the one side.
【請求項3】 前記回転軸の支持がスラスト方向で一
点、ラジアル方向で回転軸の上下で二点支持であること
を特徴とする請求項1若しくは2記載のターボ分子ポン
プの保護動作方法。
3. The method according to claim 1, wherein the rotary shaft is supported at one point in the thrust direction and at two points above and below the rotary shaft in the radial direction.
【請求項4】 一端に動翼を有する回転軸を磁気軸受の
通電制御により空中維持した状態で、該回転軸を介して
動翼を回転させ、静翼との間で気体の排気及び圧縮を行
なうターボ分子ポンプにおいて、 前記動翼及び回転軸を含むロータの異常振動若しくは磁
気軸受の通電制御部の異常を検知する手段と、 前記回転軸に対し所定クリアランスを以て遊嵌させた保
護軸受と、 該検知信号に基づいて前記磁気軸受への通電電圧を前記
通電制御部とは別系統から供給する電圧切換え手段とを
具え、 前記切換え手段による磁気軸受の磁気的吸引力により、
回転軸を保護軸受の一側に強制移動させ、該保護軸受で
回転軸を回転可能に接触支持させることを特徴とするタ
ーボ分子ポンプ。
4. A rotating shaft having a moving blade at one end thereof is maintained in the air by energizing control of a magnetic bearing, and the moving blade is rotated via the rotating shaft to exhaust and compress gas with the stationary blade. In the turbo-molecular pump to be performed, means for detecting abnormal vibration of the rotor including the rotor blades and the rotating shaft or abnormality of the power supply control unit of the magnetic bearing; and a protective bearing loosely fitted with a predetermined clearance to the rotating shaft; A voltage switching means for supplying an energizing voltage to the magnetic bearing based on a detection signal from a different system from the energizing control unit, and a magnetic attraction force of the magnetic bearing by the switching means.
A turbo-molecular pump wherein a rotating shaft is forcibly moved to one side of a protective bearing, and the rotating shaft is rotatably contacted and supported by the protective bearing.
【請求項5】 一端に動翼を有する回転軸を磁気軸受の
通電制御により空中維持した状態で、該回転軸を介して
動翼を回転させ、静翼との間で気体の排気及び圧縮を行
なうターボ分子ポンプにおいて、 前記動翼及び回転軸を含むロータの異常振動若しくは磁
気軸受の通電制御部の異常を振動量と時間との関係にお
いて第一の異常と第二の異常とに判別検知する手段と、 警報を鳴動若しくは表示させる手段と、 前記回転軸に対し所定クリアランスを以て遊嵌させた保
護軸受と、 該検知信号に基づいて前記磁気軸受への通電電圧を前記
通電制御部とは別系統から供給する電圧切換え手段とを
具え、 第一の異常検知において、前記回転軸の空中維持状態で
の回転を継続しながら警報を鳴動若しくは表示させ、 第二の異常検知において、該第二の異常検知信号に基づ
いて前記切換え手段を動作させ、該切換え手段による磁
気軸受の磁気的吸引力により、回転軸を保護軸受の一側
に強制移動させ、該保護軸受で回転軸を回転可能に接触
支持させることを特徴とするターボ分子ポンプ。
5. A rotating shaft having a moving blade at one end is maintained in the air by energization control of a magnetic bearing, and the moving blade is rotated via the rotating shaft to exhaust and compress gas with the stationary blade. In the turbo molecular pump to be performed, abnormal vibration of the rotor including the rotor blade and the rotating shaft or abnormality of the power supply control unit of the magnetic bearing is discriminated and detected as a first abnormality and a second abnormality in relation to the amount of vibration and time. Means, a means for sounding or displaying an alarm, a protection bearing loosely fitted with a predetermined clearance to the rotating shaft, and a system different from the conduction control unit for supplying an energizing voltage to the magnetic bearing based on the detection signal. And a voltage switching means supplied from the controller. In the first abnormality detection, an alarm is sounded or displayed while the rotation of the rotary shaft in the air-maintenance state is continued, and the second abnormality is detected in the second abnormality detection. The switching means is operated based on the normal detection signal, and the rotating shaft is forcibly moved to one side of the protection bearing by the magnetic attraction of the magnetic bearing by the switching means, and the rotating shaft is rotatably contacted by the protection bearing. A turbo-molecular pump characterized by being supported.
JP28036198A 1998-10-01 1998-10-01 Turbo molecular pump and its protection operation method Expired - Fee Related JP3546144B2 (en)

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Application Number Priority Date Filing Date Title
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Application Number Priority Date Filing Date Title
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JP3546144B2 JP3546144B2 (en) 2004-07-21

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008208745A (en) * 2007-02-23 2008-09-11 Jtekt Corp Centrifugal air compressor
WO2014192356A1 (en) * 2013-05-31 2014-12-04 エドワーズ株式会社 Maintenance prediction device and prediction method therefor
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008208745A (en) * 2007-02-23 2008-09-11 Jtekt Corp Centrifugal air compressor
WO2014192356A1 (en) * 2013-05-31 2014-12-04 エドワーズ株式会社 Maintenance prediction device and prediction method therefor
CN112943663A (en) * 2019-11-26 2021-06-11 佛山市云米电器科技有限公司 Fan control method, system, fan and computer readable storage medium
CN112943663B (en) * 2019-11-26 2023-02-28 佛山市云米电器科技有限公司 Fan control method, system, fan and computer readable storage medium
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