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JPH0315050B2 - - Google Patents
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JPH0315050B2 - - Google Patents

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Publication number
JPH0315050B2
JPH0315050B2 JP57184885A JP18488582A JPH0315050B2 JP H0315050 B2 JPH0315050 B2 JP H0315050B2 JP 57184885 A JP57184885 A JP 57184885A JP 18488582 A JP18488582 A JP 18488582A JP H0315050 B2 JPH0315050 B2 JP H0315050B2
Authority
JP
Japan
Prior art keywords
radial
rotor
electromagnet
spring constant
control signal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP57184885A
Other languages
Japanese (ja)
Other versions
JPS5977126A (en
Inventor
Masaharu Miki
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.)
Seiko Instruments Inc
Original Assignee
Seiko Instruments Inc
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 Seiko Instruments Inc filed Critical Seiko Instruments Inc
Priority to JP18488582A priority Critical patent/JPS5977126A/en
Publication of JPS5977126A publication Critical patent/JPS5977126A/en
Publication of JPH0315050B2 publication Critical patent/JPH0315050B2/ja
Granted 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Mechanical Engineering (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Description

【発明の詳細な説明】 本発明は、高速回転機における、制御型径方向
磁気軸受に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a controlled radial magnetic bearing for high speed rotating machines.

従来の制御型径方向磁気軸受は、第1図に示す
ように、径方向変位センサー1によりロータ2の
平衡点からの径方向変位を検出し、その信号を制
御回路3により適当な位相とゲインの補償を行な
い、更にその補償された信号に従つて、電磁石駆
動回路4によつて径方向電磁石5を駆動し、ロー
タを平衡点に引き戻し保持する。
As shown in FIG. 1, the conventional controlled radial magnetic bearing detects the radial displacement of the rotor 2 from its equilibrium point using a radial displacement sensor 1, and then sends the signal to a control circuit 3 to adjust the phase and gain to an appropriate level. Further, in accordance with the compensated signal, the electromagnet drive circuit 4 drives the radial electromagnet 5 to return and hold the rotor to the equilibrium point.

ここでは結果のみを述べるが、理論的に以下の
ような事が示される。
Only the results will be described here, but the following can be shown theoretically.

第2図に示すように、ロータ2の幾何学的中心
をS、重心をG、そのSとG間の距離をεとする
と、系の共振点ω0を越えて回転させた場合、ロ
ータは第3図に示すように、重心Gを内側、幾何
学的中心Sを外側にして、回転数ω(ω>ω0)で
回転する。そして回転数ωの上昇に従つて、重心
Gは回転中心Oに近づき、回転数ωの無限大の極
限において、OとGは一致する。従つて十分に回
転数ωが高い場合(ω≫ω0)、ロータは重心Gを
中心に回転していると考えれる事ができる。同様
に、第4図に示すように、幾何学的回転軸をR、
慣性主軸をI、RとI間の角度をτとした場合
も、十分に回転数ωが高い場合(ω≫ω0)、ロー
タは慣性主軸Iを回転軸として回転していると考
える事ができる。
As shown in Fig. 2, if the geometric center of the rotor 2 is S, the center of gravity is G, and the distance between S and G is ε, then when the system is rotated beyond the resonance point ω 0 , the rotor As shown in FIG. 3, it rotates at a rotational speed ω (ω>ω 0 ) with the center of gravity G on the inside and the geometric center S on the outside. As the rotational speed ω increases, the center of gravity G approaches the rotational center O, and at the infinite limit of the rotational speed ω, O and G coincide. Therefore, when the rotational speed ω is sufficiently high (ω≫ω 0 ), the rotor can be considered to be rotating around the center of gravity G. Similarly, as shown in Fig. 4, the geometric rotation axis is R,
Even if the principal axis of inertia is I and the angle between R and I is τ, if the rotational speed ω is sufficiently high (ω≫ω 0 ), the rotor can be considered to be rotating with the principal axis of inertia I as the rotation axis. can.

今、簡単のために、τ=0、ε≠0として、ロ
ータを高速で(ε≫ω0)を回転させた場合の第
1図6に示す外筒へ伝わる振動を考える。ロータ
は重心Gを中心に回転するので、第5図、第6図
に示すように、系方向変位センサー1は、常に回
転数に同期した±εの変位を検出する。その信号
に対応して、径方向電磁石5に回転数に同期した
制御電流が流れるため、径方向磁気軸受の等価バ
ネ定数をkとすると、ほぼ±kεの力が、径方向
電磁石5を介して、外筒6に回転数と同期して伝
わる。τ≠0の場合もほぼ同様である。
For simplicity, let us consider the vibration transmitted to the outer cylinder shown in FIG. 1 when the rotor is rotated at high speed (ε≫ω 0 ) with τ=0 and ε≠0. Since the rotor rotates around the center of gravity G, as shown in FIGS. 5 and 6, the system direction displacement sensor 1 always detects a displacement of ±ε in synchronization with the rotation speed. Corresponding to that signal, a control current synchronized with the rotation speed flows through the radial electromagnet 5, so if the equivalent spring constant of the radial magnetic bearing is k, a force of approximately ±kε flows through the radial electromagnet 5. , is transmitted to the outer cylinder 6 in synchronization with the rotation speed. The same applies to the case where τ≠0.

上に述べた理由により、従来の制御型径方向磁
気軸受の場合、ロータバランスを十分に取つて、
ε,τを極少にしなければ、外部へ伝わる振動を
小さくできず、また径方向電磁石に流れる制御電
流による消費電力も低くする事ができない等の欠
点があつた。
For the reasons stated above, in the case of conventional controlled radial magnetic bearings, the rotor must be sufficiently balanced.
Unless ε and τ are minimized, the vibrations transmitted to the outside cannot be reduced, and the power consumption due to the control current flowing through the radial electromagnets cannot be reduced.

本発明は、上記欠点を解決するためのもので、
径方向電磁石と、径方向変位センサーと、径方向
電磁石を径方向変位センサー信号で制御する制御
回路と電磁石駆動回路とからなる径方向磁気軸受
において、制御回路内に関数発生器を挿入する事
により、平衡点近傍のバネ定数を零または微少に
する事により、ε,τがある程度の大きさの値で
あつても、外部への振動伝達、径方向電磁石の消
費電力を低くする事を目的としたものである。
The present invention is intended to solve the above drawbacks,
In a radial magnetic bearing consisting of a radial electromagnet, a radial displacement sensor, a control circuit that controls the radial electromagnet using a radial displacement sensor signal, and an electromagnet drive circuit, by inserting a function generator into the control circuit. By reducing the spring constant near the equilibrium point to zero or very small, the purpose is to reduce the vibration transmission to the outside and the power consumption of the radial electromagnet even if ε and τ are large values to a certain extent. This is what I did.

本発明の動作原理を第7図を用いて説明する。 The operating principle of the present invention will be explained using FIG. 7.

第1図と共通する部分は、同様の符号で示して
ある。
Parts common to those in FIG. 1 are designated by the same reference numerals.

今、系の共振点より十分に高い回転数(ω≫
ω0)で定数回転しているとすると、前述したよ
うに、回転数ωに同期した径方向変位±εに対応
した出力が、径方向変位センサー1から出力され
る。その出力を、第8図に示すような入力が±
ΔV0までは、入力・出力変換係数が1/f(f>
0)、ΔV0以上、−ΔV0以下では入力・出力変換係
数が1となるような関数発生器7を通して、従来
の制御回路と同様な働きの、位相、ゲイン補償回
路8を通す。更にその補償された信号に従つて、
電磁石駆動回路4により、径方向電磁石5を駆動
する。
Now, the rotational speed (ω≫
ω 0 ), the radial displacement sensor 1 outputs an output corresponding to the radial displacement ±ε synchronized with the rotational speed ω, as described above. The output is inputted as shown in Figure 8 by ±
Up to ΔV 0 , the input/output conversion coefficient is 1/f (f>
0), ΔV 0 or more and −ΔV 0 or less, the signal is passed through a function generator 7 whose input/output conversion coefficient is 1, and then passed through a phase and gain compensation circuit 8 which functions similarly to a conventional control circuit. Further, according to the compensated signal,
The electromagnet drive circuit 4 drives the radial electromagnet 5.

ここで、径方向変位センサー1から出力される
信号をS0sin(wt+)とすると、ΔVpSpとなる
ように関数発生器7を設定すると、等価バネ定数
が1/fになるので、外筒6へ回転数と同期して
伝わる振動は、1/fになる。また径方向電磁石
の消費電力も、それに応じて低くなる。また何か
外乱の影響で、回転軸、重心が振れて、径方向変
位センサー1からの出力が、ΔV0以上から−ΔV0
以下になつた場合は、通常のバネ定数kで中心に
引き戻される。また、定常回転に達する間も従来
とほとんど同様(S0=ΔV0の場合は従来よりεだ
け増加する程度)にロータの振れ回りを押える事
ができる。つまり共振点通過時、大きな外乱等の
ような、εに比べて大きな振れ回りの起る場合に
対しては、従来通りの制御特性を維持できるので
ある。
Here, if the signal output from the radial displacement sensor 1 is S 0 sin (wt+), then if the function generator 7 is set so that it becomes ΔV p S p , the equivalent spring constant becomes 1/f, so The vibration transmitted to the outer cylinder 6 in synchronization with the rotational speed is 1/f. Also, the power consumption of the radial electromagnet is correspondingly lower. Also, due to the influence of some disturbance, the rotation axis and center of gravity swing, and the output from radial displacement sensor 1 changes from ΔV 0 or more to −ΔV 0.
If it falls below, it will be pulled back to the center by the normal spring constant k. Further, even while reaching steady rotation, the whirling of the rotor can be suppressed almost in the same way as in the conventional case (if S 0 =ΔV 0 , it increases by ε compared to the conventional one). In other words, the conventional control characteristics can be maintained even when a swing larger than ε occurs, such as when a large disturbance occurs when passing through the resonance point.

fを大きくすればするほど、外筒6へ伝達され
る振動、径方向電磁石消費電力が低くなるので、
fをできる限り大きくすれば良いのだが、平衡点
近傍においても、この径方向磁気軸受は安定でな
ければならないと言う事から、fの上限が決定さ
れる。極端な例として、径方向磁気軸受の不安定
バネ定数が零の場合(径方向電磁石へのバイアス
電流が零、モータ、重力、その他による不安定性
が零の場合)は、fを無限大にでき、外筒へ伝達
される振動及び径方向電磁石の消費電力は零とな
る。
The larger f is, the lower the vibration transmitted to the outer cylinder 6 and the lower the power consumption of the radial electromagnet.
Although f should be made as large as possible, the upper limit of f is determined because this radial magnetic bearing must be stable even near the equilibrium point. As an extreme example, if the unstable spring constant of the radial magnetic bearing is zero (the bias current to the radial electromagnet is zero, and the instability caused by the motor, gravity, etc. is zero), f can be made infinite. , the vibration transmitted to the outer cylinder and the power consumption of the radial electromagnet become zero.

以上のように、制御回路内に前述したような関
数発生器を挿入する事により、平衡点近傍のバネ
定数を零または微少にして、制御特性をおとす事
なく、定常回転時の外筒へ伝達される振動と径方
向電磁石の消費電力を、従来の場合に比べて著し
く小さくできる。
As described above, by inserting the function generator as described above into the control circuit, the spring constant near the equilibrium point can be made zero or very small, and the spring constant can be transmitted to the outer cylinder during steady rotation without compromising the control characteristics. The generated vibrations and the power consumption of the radial electromagnet can be significantly reduced compared to the conventional case.

このように低振動低消費電力制御型方向磁気軸
受は、高速で低振動な回転を要求し、しかも長時
間運転をする場合の多い軸流分子ポンプなどに適
している。
In this way, the low-vibration, low-power-consumption controlled directional magnetic bearing is suitable for applications such as axial flow molecular pumps that require high-speed, low-vibration rotation and are often operated for long periods of time.

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

第1図は、従来の制御型径方向磁気軸受の構成
図で、第2図は、ロータの幾何学的中心と重心の
関係を示した回転軸に垂直な断面図で、第3図
は、系の共振点を越えて、ロータを回転させた場
合のロータの振れ回りの状況を模式的に示した図
で、第4図は、ロータの幾何学的回転軸と慣性主
軸の関係を示した回転軸に平行な断面図で、第5
図と第6図は、ロータを共振点より十分高く回転
させた場合の状況を示す回転軸に垂直なロータの
断面図で、第7図は、本発明の一実施例を示す構
成図で、第8図は、関数発生器の特性を示す特性
図である。 1……径方向変位センサー、2……ロータ、3
……制御回路、4……電磁石駆動回路、5……径
方向電磁石、6……外筒、7……関数発生器、8
……位相、ゲイン補償器、S……ロータの幾何学
的中心、G……ロータの重心、ε……SG間の距
離、O……回転中心、ω……ロータ回転数、R…
…ロータの幾何学的回転数、I……ロータの回転
主軸、τ……RI間のなす角、±ΔV0……関数発生
器の折れ点。
Fig. 1 is a configuration diagram of a conventional controlled radial magnetic bearing, Fig. 2 is a sectional view perpendicular to the rotation axis showing the relationship between the geometric center of the rotor and the center of gravity, and Fig. 3 is a diagram showing the structure of a conventional controlled radial magnetic bearing. This diagram schematically shows the whirling situation of the rotor when the rotor is rotated beyond the resonance point of the system. Figure 4 shows the relationship between the rotor's geometric axis of rotation and the principal axis of inertia. In the cross-sectional view parallel to the rotation axis, the fifth
6 and 6 are cross-sectional views of the rotor perpendicular to the axis of rotation showing the situation when the rotor is rotated sufficiently above the resonance point, and FIG. 7 is a configuration diagram showing an embodiment of the present invention. FIG. 8 is a characteristic diagram showing the characteristics of the function generator. 1... Radial displacement sensor, 2... Rotor, 3
... Control circuit, 4 ... Electromagnet drive circuit, 5 ... Radial electromagnet, 6 ... Outer cylinder, 7 ... Function generator, 8
... Phase, gain compensator, S ... Geometric center of rotor, G ... Center of gravity of rotor, ε ... Distance between SG, O ... Center of rotation, ω ... Rotor rotation speed, R ...
...Geometric rotation speed of the rotor, I...Rotor's rotational axis, τ...Angle formed between RI, ±ΔV 0 ...Break point of the function generator.

Claims (1)

【特許請求の範囲】[Claims] 1 高速回転機のロータを支持する径方向電磁石
と、前記ロータの径方向の変位を検出する径方向
変位センサーと、前記径方向変位センサーの変位
出力信号に応答して前記径方向電磁石の制御信号
を発生する制御回路と、前記制御信号に基づいて
前記径方向電磁石を駆動する電磁石駆動回路から
なる径方向磁気軸受において、前記制御回路は前
記変位出力信号に基づき、前記ロータの径方向の
変位の絶対値が所定の値より大きい時は通常のバ
ネ定数を呈する制御信号を発生し、前記ロータの
径方向の変位の絶対値が所定の値より小さい時は
前記通常のバネ定数よりも小さいバネ定数を呈す
る制御信号を発生する関数発生器を有することを
特徴とする低振動低消費電力制御型径方向磁気軸
受。
1. A radial electromagnet that supports a rotor of a high-speed rotating machine, a radial displacement sensor that detects radial displacement of the rotor, and a control signal for the radial electromagnet in response to a displacement output signal of the radial displacement sensor. and an electromagnet drive circuit that drives the radial electromagnet based on the control signal, the control circuit controls the radial displacement of the rotor based on the displacement output signal. When the absolute value is larger than a predetermined value, a control signal exhibiting a normal spring constant is generated, and when the absolute value of the radial displacement of the rotor is smaller than a predetermined value, a spring constant is smaller than the normal spring constant. A low-vibration, low-power consumption control type radial magnetic bearing characterized by having a function generator that generates a control signal exhibiting the following characteristics.
JP18488582A 1982-10-21 1982-10-21 Low vibration and low power consumption control type diametrical magnetic bearing Granted JPS5977126A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18488582A JPS5977126A (en) 1982-10-21 1982-10-21 Low vibration and low power consumption control type diametrical magnetic bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18488582A JPS5977126A (en) 1982-10-21 1982-10-21 Low vibration and low power consumption control type diametrical magnetic bearing

Publications (2)

Publication Number Publication Date
JPS5977126A JPS5977126A (en) 1984-05-02
JPH0315050B2 true JPH0315050B2 (en) 1991-02-28

Family

ID=16161013

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18488582A Granted JPS5977126A (en) 1982-10-21 1982-10-21 Low vibration and low power consumption control type diametrical magnetic bearing

Country Status (1)

Country Link
JP (1) JPS5977126A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6261703A (en) * 1985-09-11 1987-03-18 Kawasaki Steel Corp Method and apparatus for supporting plug bar of cross helical rolling mill
JPH07101051B2 (en) * 1987-12-15 1995-11-01 石川島播磨重工業株式会社 Magnetic bearing control method

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5182846A (en) * 1975-01-17 1976-07-20 Mitsubishi Electric Corp JIKIJIKUKE SOCHI

Also Published As

Publication number Publication date
JPS5977126A (en) 1984-05-02

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