JPH047674Y2 - - Google Patents

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Publication number
JPH047674Y2
JPH047674Y2 JP1984044568U JP4456884U JPH047674Y2 JP H047674 Y2 JPH047674 Y2 JP H047674Y2 JP 1984044568 U JP1984044568 U JP 1984044568U JP 4456884 U JP4456884 U JP 4456884U JP H047674 Y2 JPH047674 Y2 JP H047674Y2
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Japan
Prior art keywords
signal
command signal
magnetic flux
amplifier
current
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JPS60156896U (en
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Description

【考案の詳細な説明】 〔考案の技術分野〕 この考案は、交流電動機の回転速度をフイード
バツク制御する制御回路に関する。
[Detailed Description of the Invention] [Technical Field of the Invention] This invention relates to a control circuit that performs feedback control of the rotational speed of an AC motor.

〔従来技術〕[Prior art]

従来、この種の制御回路として第1図に示すも
のがあつた。第1図において、1は基準速度信号
ωr *と、フイードバツクされる速度信号ωnとを入
力し、トルク成分電流の指令信号i1q *を発生する
演算器、2は基準磁束信号φ2 *を入力し、磁束成
分電流の指令信号i1d *を発生する演算器で、伝達
関数(1+sL2/R2)/Mを有する。ただし、Sは 微分演算子、M,L2,R2はそれぞれ一次及び二
次巻線間の相互インダクタンス、二次巻線の自己
インダクタンス、二次巻線の抵抗である。3は指
令信号i1qを基準磁束信号φ2 *により割算する割算
器、4は割算器3の出力を入力し、伝達関数
MR2/L2を有し、すべり周波数の指令信号ωs *を出 力する演算器、5は指令信号ωs *と速度信号ωn
を加算して補正した指令信号ωp *を発生する加算
器、6は指令信号i1q *,i1d *,ωp *を入力し、各相
別の交流電流の指令信号iu,iv,iwを発生する変
換器、7は指令信号iu,iv,iwと駆動電流iub,ivb
iwbの偏差を求め、これに従い、かつこれを零と
する極性で制御した指令信号iua,iva,iwaを出力
する増幅器、8は指令信号iua,iva,iwaにより制
御された3相交流の駆動電流iub,ivb,iwbを出力
する電力変換装置、9は駆動電流iub,ivb,iwb
より駆動される誘導電動機、10は誘導電動機9
の回転を検出し、速度信号ωnを出力する検出器
である。
Conventionally, there has been a control circuit of this type as shown in FIG. In FIG. 1, numeral 1 is an arithmetic unit which inputs the reference speed signal ω r * and the speed signal ω n to be fed back and generates the torque component current command signal i 1q * , and 2 is the reference magnetic flux signal φ 2 *. is input and generates a command signal i 1d * of magnetic flux component current, and has a transfer function (1+sL 2 /R 2 )/M. However, S is a differential operator, and M, L 2 , and R 2 are the mutual inductance between the primary and secondary windings, the self-inductance of the secondary winding, and the resistance of the secondary winding, respectively. 3 is a divider that divides the command signal i 1q by the reference magnetic flux signal φ 2 * , 4 is the input of the output of divider 3, and the transfer function
an arithmetic unit having MR 2 /L 2 and outputting a command signal ω s * of the slip frequency; 5 generates a corrected command signal ω p * by adding the command signal ω s * and the speed signal ω n ; adder; 6 is a converter that inputs command signals i 1q * , i 1d * , ω p * and generates AC current command signals i u , i v , i w for each phase; 7 is a command signal i u , i v , i w and drive current i ub , i vb ,
An amplifier 8 outputs command signals i ua , i va , i wa which are controlled by determining the deviation of i wb and have a polarity that makes this deviation zero . 9 is an induction motor driven by the drive currents i ub , i vb , i wb ; 10 is an induction motor 9;
This is a detector that detects the rotation of the motor and outputs a speed signal ω n .

次に動作について説明する。誘導電動機9は駆
動電流iub,ivb,iwbにより駆動され、その回転が
検出器10により検出され、速度信号ωnとなつ
て演算器1に入力される。演算器1は基準速度信
号ωr *と速度信号ωnとの偏差を求め、これに従
い、かつこれを零とする極性で制御した指令信号
i1q *を出力する。演算器2は基準磁束信号φ2 *
入力し、伝達関数(1+sL2/R2)/Mにより指令 信号i1d *を発生する。指令信号i1q *は割算器3に
おいて基準磁束信号φ2 *により割算され、更に伝
達関数MR2/L2をもつ演算器4により指令信号ωs * となる。加算器5は指令信号ωs *と速度信号ωn
の加算により指令信号ωp *を求める。変換器6は
このようにして求めた指令信号i1q *,i1d *及びωp *
により、各相別の指令信号iu,iv,iwを出力する。
指令信号iu,iv,iwは増幅器7及び電力変換装置
8を介して誘導電動機9に駆動電流iub,ivb,iwb
となつて供給される。
Next, the operation will be explained. The induction motor 9 is driven by drive currents i ub , i vb , i wb , and its rotation is detected by a detector 10 and inputted to the calculator 1 as a speed signal ω n . Arithmetic unit 1 calculates the deviation between the reference speed signal ω r * and the speed signal ω n , and generates a command signal according to this and controlled with a polarity that makes this deviation zero.
Print i 1q * . The calculator 2 receives the reference magnetic flux signal φ 2 * and generates the command signal i 1d * based on the transfer function (1+sL 2 /R 2 )/M. The command signal i 1q * is divided by the reference magnetic flux signal φ 2 * in the divider 3, and then becomes the command signal ω s * by the arithmetic unit 4 having the transfer function MR 2 /L 2 . The adder 5 obtains the command signal ω p * by adding the command signal ω s * and the speed signal ω n . The converter 6 receives the command signals i 1q * , i 1d * and ω p * obtained in this way.
command signals i u , i v , i w for each phase are output.
The command signals i u , i v , i w are applied to the induction motor 9 via the amplifier 7 and the power converter 8 to drive currents i ub , i vb , i wb
It is supplied as follows.

増幅器7で前述のように電流制御が行われるの
で、誘導電動機9にはトルク成分電流の指令信号
i1q *、磁束成分電流の指令信号i1d *に一致した電
流が供給される。このとき、誘導電動機9の二次
磁束φ2と指令信号i1d *との間には次式が成り立
つ。(参考文献 ニユードライブエレクトロニク
ス 電気書院発行 pp196) φ2=M/1+sL2/R2i1d * …(1) 演算器2は、誘導電動機9に基準磁束信号φ2 *
に等しい二次磁束φ2を発生させるために、(1)式
の逆関数である次式により、基準磁束信号φ2 *
ら指令信号i1d *を演算し出力する。
Since the amplifier 7 performs current control as described above, the induction motor 9 receives a torque component current command signal.
i 1q * and a current that matches the command signal i 1d * of the magnetic flux component current is supplied. At this time, the following equation holds between the secondary magnetic flux φ 2 of the induction motor 9 and the command signal i 1d * . (Reference: New Drive Electronics, published by Denki Shoin, pp196) φ 2 = M/1 + sL 2 /R 2 i 1d * …(1) The calculator 2 sends a reference magnetic flux signal φ 2 * to the induction motor 9.
In order to generate a secondary magnetic flux φ 2 equal to , a command signal i 1d * is calculated and output from a reference magnetic flux signal φ 2 * using the following equation, which is an inverse function of equation (1).

i1d *=1+sL2/R2/Mφ2 * …(2) 従来の制御回路は、以上のように構成され、誘
導電動機の発生トルクTMをトルク成分電流の指
令信号i1q *と基準磁束信号φ2 *との積に比例した
もの、すなわち、 TM−αφ2 *i1q * …(3) とし、直流電動機の速度制御の如く電流とトルク
との間に線形な関係を考えることで、誘導電動機
の良好な速度制御を実現しようとするものであ
る。このような制御方式は、いわゆる誘導電動機
のすべり周波数形ベクトル制御と呼ばれている
(前記文献pp205参照)。
i 1d * = 1 + sL 2 /R 2 /Mφ 2 * ...(2) The conventional control circuit is configured as described above, and combines the generated torque T M of the induction motor with the command signal i 1q * of the torque component current and the reference magnetic flux. It is proportional to the product of signal φ 2 * , that is, T M −αφ 2 * i 1q * …(3), and by considering the linear relationship between current and torque as in the speed control of a DC motor, , which attempts to realize good speed control of an induction motor. Such a control method is called slip frequency type vector control of an induction motor (see the above-mentioned document pp. 205).

しかし、従来の制御回路において、基準磁束信
号φ2 *から指令信号i1d *を演算する演算器2に微
分要素を含むため以下のような欠点がある。これ
を図を用いて説明する。
However, in the conventional control circuit, since the arithmetic unit 2 that calculates the command signal i 1d * from the reference magnetic flux signal φ 2 * includes a differential element, there are the following drawbacks. This will be explained using a diagram.

誘導電動機9を起動するとき、図3−aのよう
に基準磁束信号φ2 *は0からある値までステツプ
的に与えられる。このとき演算器2は、誘導電動
機9に基準磁束信号φ2 *に一致した二次磁束を発
生させるのに必要な指令信号i1d *を出力するもの
であるが、式(2)で表される伝達関数に微分要素を
含むため、指令信号i1d *は、ステツプ的信号のよ
うに急激に変化する入力に対して図3−bの実線
のように演算器2の出力の上限値に達し飽和して
しまう。
When starting the induction motor 9, the reference magnetic flux signal φ 2 * is given stepwise from 0 to a certain value as shown in FIG. 3-a. At this time, the computing unit 2 outputs a command signal i 1d * necessary to cause the induction motor 9 to generate a secondary magnetic flux that matches the reference magnetic flux signal φ 2 * , which is expressed by equation (2). Since the transfer function includes a differential element, the command signal i 1d * reaches the upper limit of the output of the calculator 2 as shown by the solid line in Figure 3-b for inputs that change rapidly, such as step signals. I get saturated.

したがつて、図3−a,cに示すように基準磁
束信号φ2 *と誘導電動機9の二次磁束φ2が一致し
ない。そして、図1において、すべり周波数の指
令信号ωsを求める際に基準磁束信号φ2 *を用いて
いるが、前述のようにφ2 *は二次磁束φ2に一致し
ていないので、ここで得られる指令ωs *も適当で
はない。
Therefore, as shown in FIGS. 3-a and 3-c, the reference magnetic flux signal φ 2 * and the secondary magnetic flux φ 2 of the induction motor 9 do not match. In Fig. 1, the reference magnetic flux signal φ 2 * is used to obtain the command signal ω s of the slip frequency, but as mentioned above, φ 2 * does not match the secondary magnetic flux φ 2 , so here The command ω s * obtained by is also not appropriate.

以上の理由から、従来の制御回路では誘導電動
機9の発生トルクは指令信号i1q *と基準磁束信号
φ2 *との積に比例せず制御の線形性が悪化し良好
な速度制御が行えない場合があるという欠点があ
つた。
For the above reasons, in the conventional control circuit, the torque generated by the induction motor 9 is not proportional to the product of the command signal i 1q * and the reference magnetic flux signal φ 2 * , resulting in poor control linearity and poor speed control. There is a drawback that there are cases.

一方、演算器2の上限値は電力変換器の電流容
量によつて決まるので、飽和させないようにする
には極めて大きな電流容量の電力変換器が必要と
なり、装置の大型化は、コストアツプになる。ま
た、アナログ回路で演算器2を構成しようとする
場合、微分要素を含むためパルス性のノイズの影
響を受けやすく制御が不安定になるといつた欠点
もあつた。
On the other hand, since the upper limit value of the arithmetic unit 2 is determined by the current capacity of the power converter, a power converter with an extremely large current capacity is required to prevent saturation, and increasing the size of the device increases costs. Further, when the arithmetic unit 2 is configured with an analog circuit, there is a drawback that since it includes a differential element, it is susceptible to pulse noise and control becomes unstable.

〔考案の概要〕[Summary of the idea]

この考案は、上記のような従来のものの欠点を
除去するためになされたもので、基準磁束信号を
処理する回路部分に一次遅れ要素を含む伝達関数
をもたせることにより、この回路部分の出力の飽
和による基準磁束信号と二次磁束との不一致を防
止し、良好な制御特性が得られるとともに、パル
ス性のノイズの影響を受けにくい交流電動機の制
御回路を提供することを目的とする。
This invention was made to eliminate the drawbacks of the conventional ones as described above. By providing a transfer function that includes a first-order delay element to the circuit section that processes the reference magnetic flux signal, it is possible to eliminate the saturation of the output of this circuit section. It is an object of the present invention to provide a control circuit for an AC motor that prevents mismatch between a reference magnetic flux signal and a secondary magnetic flux caused by the oscilloscope, provides good control characteristics, and is less susceptible to pulse noise.

〔考案の実施例〕[Example of idea]

以下、この考案の一実施例を図について説明す
る。第2図において、第1図と同一符号は同一部
分を示す。基準磁束信号φ2 *は、ゲインKの増幅
器11を介して減算器12の正入力に供給される
と共に、一次遅れの伝達関数 1/1+sL2/KR2(K>1の定数) …(4) をもつ演算器13に供給され、この演算器13の
出力である信号φ2 *はゲインK−1の増幅器14
を介して減算器12の負入力に供給される。減算
器12は増幅器11の出力から増幅器14の出力
を減算した出力をゲイン1/Mの増幅器15を介す ることにより補正された指令信号i1d *を出力す
る。この指令信号i1d *は変換器6に入力される。
An embodiment of this invention will be described below with reference to the drawings. In FIG. 2, the same symbols as in FIG. 1 indicate the same parts. The reference magnetic flux signal φ 2 * is supplied to the positive input of the subtracter 12 via the amplifier 11 with a gain of K, and the first-order lag transfer function 1/1+sL 2 /KR 2 (constant of K>1)...(4 ), and the signal φ 2 * , which is the output of this calculator 13, is sent to an amplifier 14 with a gain of K-1.
is supplied to the negative input of the subtractor 12 via the subtracter 12. The subtracter 12 subtracts the output of the amplifier 14 from the output of the amplifier 11 and outputs the corrected command signal i 1d * by passing the output through the amplifier 15 with a gain of 1/M. This command signal i 1d * is input to the converter 6.

演算器13の出力である信号φ2′は割算器16
に入力され、演算部1から出力された指令信号
i1q *を割算し、ゲインMR2/L2の増幅器17を介す ることにより、補正された指令信号ωs *を出力す
る。指令信号ωs *は速度信号ωnと加算器5で加算
し、この加算器5から補正した指令信号ωp *を変
換器6に入力する。
The signal φ 2 ', which is the output of the arithmetic unit 13, is sent to the divider 16.
The command signal inputted to and outputted from the calculation unit 1
A corrected command signal ω s * is output by dividing i 1q * and passing it through an amplifier 17 with a gain MR 2 /L 2 . The command signal ω s * is added to the speed signal ω n in an adder 5 , and the corrected command signal ω p * is input from the adder 5 to a converter 6 .

上記実施例の構成により、基準磁束信号φ2 *
指令信号i1d *までの伝達関数は、次式のようにな
る。
With the configuration of the above embodiment, the transfer function from the reference magnetic flux signal φ 2 * to the command signal i 1d * is as shown in the following equation.

i1d *(s)/φ2 *(s)−1/M〔K+K−1/1+
s(L2/KR2)〕=1/M・1+s(L2/R2)/1+s
(L2/KR2)…(5) 磁束成分電流の指令信号i1d *から、誘導電動機
9の実際の二次磁束φ2までの伝達関数は、 φ2(s)/i1d *(s)=1/1+s(L2/R2)…(6) また、基準磁束信号φ2 *から二次磁束φ2までの
伝達関数は、(5)式を(6)式で辺辺割ると次式のよう
になる。
i 1d * (s)/φ 2 * (s)-1/M[K+K-1/1+
s(L 2 /KR 2 )]=1/M・1+s(L 2 /R 2 )/1+s
(L 2 /KR 2 )...(5) The transfer function from the command signal i 1d * of the magnetic flux component current to the actual secondary magnetic flux φ 2 of the induction motor 9 is φ 2 (s)/i 1d * (s )=1/1+s(L 2 /R 2 )...(6) Also, the transfer function from the reference magnetic flux signal φ 2 * to the secondary magnetic flux φ 2 is obtained by dividing equation (5) by equation (6). It becomes as follows.

φ2(s)/φ2 *(s)=1/1+s(L2/KR2) …(7) また、基準磁束φ2 *から、すべり周波数の指令
信号ωsを求めるために用いるφ2′までの伝達関数
は、図2より次式のようになる。
φ 2 (s) / φ 2 * (s) = 1/1 + s (L 2 /KR 2 )...(7) Also, φ 2 used to obtain the command signal ω s of the slip frequency from the reference magnetic flux φ 2 *. According to FIG. 2, the transfer function up to ' is given by the following equation.

φ2′(s)/φ2 *(s)=1/1+s(L2/KR2)…(8
) 以上から、誘導電動機9を起動するときの各部
の波形を第4図に示す。
φ 2 ′ (s) / φ 2 * (s) = 1/1 + s (L 2 /KR 2 )…(8
) From the above, the waveforms of each part when starting the induction motor 9 are shown in FIG.

基準磁束信号φ2 *がステツプ的に与えられた
時、指令信号i1d *図4−aのように、式(5)より最
大値がK・φ2 */Mである図4−bのような波形
となることがわかる。また、式(7),(8)から二次磁
束φ2、信号φ2′の応答波形は図4−cのように同
じものになる。
When the reference magnetic flux signal φ 2 * is given in a stepwise manner, the command signal i 1d * as shown in FIG. It can be seen that the waveform is as follows. Furthermore, from equations (7) and (8), the response waveforms of the secondary magnetic flux φ 2 and the signal φ 2 ' are the same as shown in FIG. 4-c.

ところで基準磁束信号φ2 *は誘導電動機9の二
次磁束φ2に対して電気的時定数L2/R2の1/K
の時定数の一次遅れで応答する。
By the way, the reference magnetic flux signal φ 2 * is 1/K of the electrical time constant L 2 /R 2 with respect to the secondary magnetic flux φ 2 of the induction motor 9.
It responds with a first-order delay with a time constant of .

従つて、演算器13、増幅器11および14に
含まれるゲインKを大きくするほど応答は速くな
る。
Therefore, the response becomes faster as the gains K included in the arithmetic unit 13 and amplifiers 11 and 14 are increased.

しかし、ゲインKを大きくしすぎると、指令信
号i1d *を出力する増幅器15の出力が飽和するの
で、ある一定値以下に設定する必要がある。増幅
器15の出力の上限値i1dmaxおよび基準磁束信
号φ2 *の大きさはあらかじめわかつているので、
次式が成立するようにゲインKを調整すれば、増
幅器15の出力が次式の上限値i1dmaxを超えて
飽和させない範囲で高速な二次磁束φ2の応答が
得られる。
However, if the gain K is made too large, the output of the amplifier 15 that outputs the command signal i 1d * will be saturated, so it is necessary to set it below a certain value. Since the upper limit value i 1d max of the output of the amplifier 15 and the magnitude of the reference magnetic flux signal φ 2 * are known in advance,
If the gain K is adjusted so that the following equation holds true, a fast response of the secondary magnetic flux φ 2 can be obtained within a range where the output of the amplifier 15 does not exceed the upper limit value i 1d max of the following equation and is not saturated.

i1dmax≧K・φ2 */M …(9) また、前述のようにすべり周波数の指令信号
ωsを求めるために用いる信号φ2′と誘導電動機9
の二次磁束φ2の基準磁束信号φ2 *に対する応答は
等しいので、最適な指令信号ωs *が得られること
がわかる。
i 1d max≧K・φ 2 * /M (9) In addition, as mentioned above, the signal φ 2 ' used to obtain the command signal ω s of the slip frequency and the induction motor 9
Since the responses of the secondary magnetic flux φ 2 to the reference magnetic flux signal φ 2 * are equal, it can be seen that the optimal command signal ω s * can be obtained.

さらに、基準磁束信号φ2 *から磁束分電流の指
令信号i1d *までの信号伝達経路に微分要素が含ま
れないので、パルス性のノイズに影響されにく
い。
Furthermore, since no differential element is included in the signal transmission path from the reference magnetic flux signal φ 2 * to the magnetic flux current command signal i 1d * , it is less susceptible to pulse noise.

〔考案の効果〕[Effect of idea]

以上のようにこの考案によれば、基準磁束信号
を処理する回路部分に一次遅れ要素を含む伝達関
数をもたせるようにしたので、二次磁束に対する
応答性及び雑音に対する特性を改善できる効果が
ある。
As described above, according to this invention, since the circuit portion that processes the reference magnetic flux signal has a transfer function that includes a first-order delay element, it is possible to improve the response to the secondary magnetic flux and the characteristics against noise.

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

第1図は従来の交流電動機の制御回路を示すブ
ロツク図、第2図はこの発明の一実施例による交
流電動機の制御回路を示すブロツク図、第3図は
従来の制御回路による交流電動機起動時の各部の
信号波形図、第4図はこの発明の制御回路による
交流電動機起動時の各部の信号波形図である。 1,2,4,13……演算部、3,16……割
算器、5……加算器、6……変換器、8……電力
変換装置、7,11,14,15,17……増幅
器、8……誘導電動機。なお、図中、同一符号は
同一部分を示す。
Fig. 1 is a block diagram showing a conventional control circuit for an AC motor, Fig. 2 is a block diagram showing a control circuit for an AC motor according to an embodiment of the present invention, and Fig. 3 is a block diagram showing a control circuit for an AC motor according to an embodiment of the present invention. FIG. 4 is a signal waveform diagram of each part when the AC motor is started by the control circuit of the present invention. 1, 2, 4, 13... Arithmetic unit, 3, 16... Divider, 5... Adder, 6... Converter, 8... Power converter, 7, 11, 14, 15, 17... ...Amplifier, 8...Induction motor. Note that in the figures, the same reference numerals indicate the same parts.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 基準速度信号と回転する交流電動機から検出さ
れた速度信号とを比較し、この比較の結果により
トルク成分電流の指定信号を発生する第1演算器
と、一次及び二次巻線間の相互インダクタンス
M、二次巻線の自己インダクタンスL2、二次巻
線の抵抗R2、微分演算子Sを構成要素とし、一
次遅れの伝達関数を有し基準磁束信号を入力する
第2演算器と、前記基準磁束信号をゲインKの第
1増幅器を介して正入力とし前記第2演算器の出
力信号をゲインK−1の第2増幅器を介して負入
力とする減算器と、前記減算器の出力信号をゲイ
ン1/Mで増幅して磁束成分電流の指令信号を出
力する第3増幅器と、前記トルク成分の電流の指
令信号を前記第2演算器の出力信号で割算する割
算器と、前記割算器の出力信号をゲインMR2
L2の第4増幅器を介して入力し前記速度信号と
加算してすべり周波数の指定信号を発生する加算
器と、前記トルク成分電流の指令信号と前記磁束
成分電流の指令信号および前記すべり周波数の指
令信号を入力して各相別の交流電流の指令信号を
発生する変換器と、前記各相別の交流電流の指令
信号と前記交流電動機に流れる駆動電流とを各相
毎に比較して各相毎の交流電圧の指令信号を出力
する第5増幅器と、前記各相毎の交流電圧の指令
信号により制御され前記交流電動機の各相に対し
駆動電流を供給する電力変換装置とを備えた交流
電動機の制御回路。
a first computing unit that compares a reference speed signal with a speed signal detected from a rotating AC motor and generates a designated signal for a torque component current based on the comparison result; and a mutual inductance M between the primary and secondary windings. , a secondary winding self-inductance L 2 , a secondary winding resistance R 2 , and a differential operator S as constituent elements, having a first-order lag transfer function and inputting a reference magnetic flux signal; a subtracter having a reference magnetic flux signal as a positive input via a first amplifier with a gain K and an output signal of the second arithmetic unit as a negative input via a second amplifier with a gain K-1; and an output signal of the subtracter. a third amplifier that amplifies with a gain of 1/M and outputs a command signal of the magnetic flux component current; a divider that divides the command signal of the torque component current by the output signal of the second arithmetic unit; The output signal of the divider is given the gain MR 2 /
an adder that inputs the signal through the fourth amplifier of L2 and adds it to the speed signal to generate a designated signal of the slip frequency; a command signal of the torque component current, a command signal of the magnetic flux component current, and a command signal of the slip frequency; A converter inputs a command signal and generates a command signal for AC current for each phase, and compares the command signal for AC current for each phase with the drive current flowing to the AC motor for each phase. an AC power conversion device that is controlled by the AC voltage command signal for each phase and supplies a drive current to each phase of the AC motor; Electric motor control circuit.
JP1984044568U 1984-03-28 1984-03-28 AC motor control circuit Granted JPS60156896U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1984044568U JPS60156896U (en) 1984-03-28 1984-03-28 AC motor control circuit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1984044568U JPS60156896U (en) 1984-03-28 1984-03-28 AC motor control circuit

Publications (2)

Publication Number Publication Date
JPS60156896U JPS60156896U (en) 1985-10-18
JPH047674Y2 true JPH047674Y2 (en) 1992-02-27

Family

ID=30557259

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1984044568U Granted JPS60156896U (en) 1984-03-28 1984-03-28 AC motor control circuit

Country Status (1)

Country Link
JP (1) JPS60156896U (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0767318B2 (en) * 1985-10-31 1995-07-19 株式会社明電舍 Vector control method of induction motor
JPH084399B2 (en) * 1988-10-06 1996-01-17 富士電機株式会社 Induction motor controller

Also Published As

Publication number Publication date
JPS60156896U (en) 1985-10-18

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