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JPS6333391B2 - - Google Patents
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JPS6333391B2 - - Google Patents

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Publication number
JPS6333391B2
JPS6333391B2 JP54148934A JP14893479A JPS6333391B2 JP S6333391 B2 JPS6333391 B2 JP S6333391B2 JP 54148934 A JP54148934 A JP 54148934A JP 14893479 A JP14893479 A JP 14893479A JP S6333391 B2 JPS6333391 B2 JP S6333391B2
Authority
JP
Japan
Prior art keywords
current
signal
current component
command
component
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
Application number
JP54148934A
Other languages
Japanese (ja)
Other versions
JPS5674090A (en
Inventor
Hiroshi Nagase
Toshiaki Okuyama
Yuzuru Kubota
Katsunori Suzuki
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP14893479A priority Critical patent/JPS5674090A/en
Publication of JPS5674090A publication Critical patent/JPS5674090A/en
Publication of JPS6333391B2 publication Critical patent/JPS6333391B2/ja
Granted legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P27/00Arrangements or methods for the control of AC motors characterised by the kind of supply voltage
    • H02P27/02Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using supply voltage with constant frequency and variable amplitude
    • H02P27/026Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using supply voltage with constant frequency and variable amplitude whereby the speed is regulated by measuring the motor speed and comparing it with a given physical value

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Control Of Ac Motors In General (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明はかご形誘導電動機をベクトル制御する
誘導電動機の制御装置に関する。 最近、ベクトル制御と呼ばれる誘導機の制御方
式が検討されている。この制御方式は誘導機の1
次電流を磁束をつくる励磁電流成分とそれに直交
する2次電流成分とに分離し、それぞれ独立に制
御するので、速度応答性能を直流機と同等にする
ことが可能である。 第1図はこの制御方式を適用した従来例を示
す。 第1図において、1は交流電流、2は交流電源
1から供給される交流を任意の周波数と電圧の交
流に変換する周波数変換器で、例えばサイクロコ
ンバータやPWMインバータが適用される。3は
かご形誘導電動機、4は誘導機3の回転速度を検
出する速度発電機、5は誘導機3の回転速度を指
令する速度指令回路、6は速度指令回路5と速度
発電機4の出力信号偏差に応じて働く速度制御回
路で、その出力信号は誘導機3の2次電流成分を
指令する信号となる。7は誘導機3の励磁電流成
分を指令する励磁電流指令回路、8は速度制御回
路6の出力信号に比例して誘導機3のすべり周波
数を演算するすべり周波数演算回路、9はすべり
周波数演算回路8と速度発電機4の出力信号の和
をとり、誘導機3の1次周波数を指令する加算
器、10は加算器9の出力信号(1次周波数指令
信号)に比例した周波数の正弦波信号を出力する
発振器で、その出力信号は誘導機3の2次鎖交磁
束の位置基準信号となる。11は発振器10の信
号を基準とし、速度制御回路6からの2次電流成
分指令と励磁電流指令回路7の励磁電流成分指令
に応じて誘導機3の1次電流を指令する電流パタ
ーン回路で、その出力信号は1次電流の瞬時値を
指令する交流の正弦波信号となる。12は誘導機
3の1次電流を検出する電流検出器、13は電流
パターン回路11と電流検出器12の出力信号偏
差に応じて働く電流制御回路、14は電流制御回
路13の出力信号に応じて周波数変換器2のサイ
リスタのゲートを制御するゲート制御回路であ
る。なお、12〜14は1相分だけを示すが他の
相においても同様な回路がある。 この回路は誘導機の2次電流成分と励磁電流成
分をそれぞれ直流機における電機子電流、界磁電
流に対応させて制御することが特徴である。2次
電流成分指令信号と励磁電流成分指令信号から正
弦波の磁束基準信号を基に誘導機の1次電流の瞬
時値指令信号を演算し、この信号に応じて1次電
流の瞬時値を制御する。このように制御すると高
応答で精度のよいトルク制御が可能となる。 しかしながらこの制御回路には次の問題点があ
る。すなわち、電流制御回路13は電流検出器1
2で検出する1次電流の瞬時値が交流の電流指令
信号に一致するように働いている。ところが、こ
のような電流制御には必らず制御上の遅れがある
ために、交流信号を扱うと電流指令信号に対して
実際の電流が比例しなくなり、また、位相も遅れ
るようになる。特に、周波数が高くなる程この傾
向は顕著になる。したがつて実際の2次電流成
分、励磁電流成分はそれぞれの指令信号に比例し
た値にならず、そのためトルク、電圧が所定の値
にならないという問題が生じる。その結果とし
て、トルクの高応答制御ができなくなることにな
る。 本発明は上記欠点に対処してなされたもので、
その目的とするところは2次電流成分と励磁電流
成分の指令値と実際値を常に一致させ、トルク、
電圧を所定の値に保つことのできる誘導電動機の
制御装置を提供することにある。 本発明の特徴は1次電流の検出値から2次電流
成分、励磁電流成分を検出し、それらがそれぞれ
の指令信号と一致するように制御する電流成分制
御機能を電流指令手段に持たせ、この電流指令手
段の発生する1次電流を指令する交流信号に基づ
き電流制御手段で1次電流を制御するようにした
ことにある。 第2図は本発明の一実施例を示す。部品番号1
〜14に示すものは第1図と同一物を示す。10′
は1次周波数を指令する加算器9の出力信号に応
じた周波数の正弦波信号を出力する発振器で、後
述する6つの信号を出力する。11′は発振器1
0′の出力信号を基準にし、後述する第1の電流
成分制御回路16と第2の電流成分制御回路17
の出力信号に応じて1次電流の瞬時値を指令する
交流信号を出力する電流パターン回路である。1
5は誘導機3の1次電流の2次電流成分I2fと励
磁電流成分Infを検出する電流成分検出回路、1
6は速度制御回路6の出力信号で2次電流成分を
指令するI2pと電流成分検出回路15によつて検
出した2次電流成分I2fとの偏差に応じて働く第
1の電流成分制御回路、17は励磁電流指令回路
7の出力信号Inpと電流成分検出回路15によつ
て検出した励磁電流成分Infとの偏差に応じて働
く第2の電流成分制御回路である。 この回路の詳細な構成と動作を以下に説明す
る。 第3図は1次電流I1と2次電流成分I2および励
磁電流成分Inの関係を示すベクトル図である。I1
はI2とInのベクトル和で与えられ、I2とInは直交
している。発振器10′の出力信号を基準に2次
電流成分I2と励磁電流成分Inを求める。 まず、速度制御回路6からは速度偏差に応じて
2次電流成分指令信号I2Pが出力される。一方、
励磁電流指令回路7からは励磁電流成分指令信号
Inpが出力される。また、1次角周波数ω1は良く
知られているように次式によつて演算される。 ωs=(R2/M+L2・1/Inp)I2p ……(1) ω1=ωs+ωr ……(2) ここで、ωsはすべり角周波数、ωrは誘導機3
の回転角周波数、R2は2次抵抗、Mは励磁イン
ダクタンス、L2は2次漏れインダクタンスであ
る。 (1)式の演算はすべり周波数演算回路8で実行さ
れ、また(2)式の演算は加算器9で実行される。加
算器9の出力である1次角周波数信号ω1は発振
器10′に入力される。発振器10′は角周波数
ω1の正弦波信号を出力する。 そして、2次電流成分I2と励磁電流成分Inを次
の原理で求める。発振器10′の出力信号は誘導
機3の2次鎖交磁束の基準信号で、次式に示すa
〜fの6つの信号が出力される。 a=Asinω1t ……(3) b=Asin(ω1t+120゜) ……(4) c=Asin(ω1t+240゜) ……(5) d=Asin(ω1t+90゜) ……(6) e=Asin(ω1t+210゜) ……(7) f=Asin(ω1t+330゜) ……(8) で表わすことができる。ここでAは発振器10′
の出力信号の振幅である。 第4図に発振器10′の一例を示す。 第4図において、101は入力信号に比例した
周波数の正弦波信号を出力する可変周波発振器
で、(3)、(6)式で表わされる2つの信号a,dを出
力する。102〜104は演算増幅器で次の演算
をし信号b,c,e,fを出力する。なお、R、
2R、√3R、(3−√3)R、1/2R、
The present invention relates to an induction motor control device that performs vector control of a squirrel cage induction motor. Recently, a control method for induction machines called vector control has been studied. This control method is one of the induction motors.
Since the secondary current is separated into an excitation current component that creates magnetic flux and a secondary current component orthogonal to it and each is controlled independently, it is possible to make the speed response performance equivalent to that of a DC machine. FIG. 1 shows a conventional example to which this control method is applied. In FIG. 1, 1 is an alternating current, and 2 is a frequency converter that converts the alternating current supplied from the alternating current power source 1 into alternating current of arbitrary frequency and voltage, such as a cycloconverter or a PWM inverter. 3 is a squirrel cage induction motor, 4 is a speed generator that detects the rotation speed of the induction machine 3, 5 is a speed command circuit that commands the rotation speed of the induction machine 3, and 6 is the output of the speed command circuit 5 and the speed generator 4. This is a speed control circuit that operates according to the signal deviation, and its output signal becomes a signal that commands the secondary current component of the induction machine 3. 7 is an excitation current command circuit that commands the excitation current component of the induction machine 3; 8 is a slip frequency calculation circuit that calculates the slip frequency of the induction machine 3 in proportion to the output signal of the speed control circuit 6; 9 is a slip frequency calculation circuit 8 and an adder that takes the sum of the output signal of the speed generator 4 and commands the primary frequency of the induction machine 3. 10 is a sine wave signal with a frequency proportional to the output signal of the adder 9 (primary frequency command signal). The output signal serves as a position reference signal for the secondary flux linkage of the induction machine 3. 11 is a current pattern circuit that commands the primary current of the induction machine 3 in accordance with the secondary current component command from the speed control circuit 6 and the excitation current component command from the excitation current command circuit 7, using the signal from the oscillator 10 as a reference; The output signal is an alternating current sinusoidal signal that commands the instantaneous value of the primary current. 12 is a current detector that detects the primary current of the induction machine 3; 13 is a current control circuit that operates according to the output signal deviation between the current pattern circuit 11 and the current detector 12; and 14 is a current control circuit that operates according to the output signal of the current control circuit 13. This is a gate control circuit that controls the gate of the thyristor of the frequency converter 2. Note that 12 to 14 show only one phase, but similar circuits exist for other phases as well. This circuit is characterized in that it controls the secondary current component and excitation current component of the induction machine in correspondence with the armature current and field current in the DC machine, respectively. Calculate the instantaneous value command signal of the primary current of the induction machine based on the sine wave magnetic flux reference signal from the secondary current component command signal and the excitation current component command signal, and control the instantaneous value of the primary current according to this signal. do. Controlling in this manner enables highly responsive and accurate torque control. However, this control circuit has the following problems. That is, the current control circuit 13
It works so that the instantaneous value of the primary current detected in step 2 matches the alternating current command signal. However, since such current control necessarily involves a control delay, when an AC signal is used, the actual current is no longer proportional to the current command signal, and the phase also lags. In particular, this tendency becomes more pronounced as the frequency becomes higher. Therefore, the actual secondary current component and excitation current component do not have values proportional to their respective command signals, which causes a problem that the torque and voltage do not reach predetermined values. As a result, high-response control of torque becomes impossible. The present invention has been made to address the above-mentioned drawbacks.
The purpose is to always match the command values and actual values of the secondary current component and excitation current component, and to
An object of the present invention is to provide a control device for an induction motor that can maintain voltage at a predetermined value. A feature of the present invention is that the current command means has a current component control function that detects the secondary current component and the excitation current component from the detected value of the primary current and controls them so that they match the respective command signals. The primary current is controlled by the current control means based on an alternating current signal that commands the primary current generated by the current command means. FIG. 2 shows an embodiment of the invention. Part number 1
Items 1 to 14 are the same as those shown in FIG. 10'
is an oscillator that outputs a sine wave signal of a frequency corresponding to the output signal of the adder 9 that commands the primary frequency, and outputs six signals to be described later. 11' is oscillator 1
0' as a reference, a first current component control circuit 16 and a second current component control circuit 17, which will be described later.
This is a current pattern circuit that outputs an alternating current signal that commands the instantaneous value of the primary current according to the output signal of the primary current. 1
5 is a current component detection circuit that detects the secondary current component I 2f and the exciting current component I nf of the primary current of the induction machine 3;
Reference numeral 6 denotes a first current component control circuit that operates according to the deviation between I 2p , which commands the secondary current component with the output signal of the speed control circuit 6, and the secondary current component I 2f detected by the current component detection circuit 15. , 17 is a second current component control circuit that operates according to the deviation between the output signal I np of the excitation current command circuit 7 and the excitation current component I nf detected by the current component detection circuit 15. The detailed configuration and operation of this circuit will be explained below. FIG. 3 is a vector diagram showing the relationship between the primary current I 1 , the secondary current component I 2 and the exciting current component I n . I 1
is given by the vector sum of I 2 and I n , and I 2 and I n are orthogonal. A secondary current component I 2 and an excitation current component I n are determined based on the output signal of the oscillator 10'. First, the speed control circuit 6 outputs a secondary current component command signal I 2P according to the speed deviation. on the other hand,
The excitation current command circuit 7 outputs an excitation current component command signal.
I np is output. Furthermore, the primary angular frequency ω 1 is calculated by the following equation, as is well known. ωs=(R 2 /M+L 2・1/I np )I 2p ...(1) ω 1 =ωs+ωr ...(2) Here, ωs is the slip angular frequency, and ωr is the induction machine 3
, R 2 is the secondary resistance, M is the excitation inductance, and L 2 is the secondary leakage inductance. The calculation of equation (1) is executed by the slip frequency calculation circuit 8, and the calculation of equation (2) is executed by the adder 9. The primary angular frequency signal ω 1 which is the output of the adder 9 is input to the oscillator 10'. Oscillator 10' outputs a sinusoidal signal of angular frequency ω 1 . Then, the secondary current component I 2 and the excitation current component I n are determined using the following principle. The output signal of the oscillator 10' is a reference signal of the secondary flux linkage of the induction machine 3, and is expressed by the following formula a
Six signals of ~f are output. a=Asinω 1 t...(3) b=Asin(ω 1 t+120°)...(4) c=Asin(ω 1 t+240°)...(5) d=Asin(ω 1 t+90°)...( 6) e=Asin(ω 1 t+210°) ……(7) f=Asin(ω 1 t+330°) ……(8) It can be expressed as follows. Here A is the oscillator 10'
is the amplitude of the output signal. FIG. 4 shows an example of the oscillator 10'. In FIG. 4, 101 is a variable frequency oscillator that outputs a sine wave signal with a frequency proportional to the input signal, and outputs two signals a and d expressed by equations (3) and (6). Operational amplifiers 102 to 104 perform the following calculations and output signals b, c, e, and f. In addition, R,
2R, √3R, (3-√3)R, 1/2R,

【式】 は抵抗で、それらの抵抗の比は順に1:2:√
3:(3−√3):1/2:
[Formula] is the resistance, and the ratio of those resistances is 1:2:√
3:(3-√3):1/2:

【式】のように選定する。 このような構成により、入力信号に比例した周
波数の6つの信号a〜fが出力される。 これらの信号から、1次電流の2次電流成分I2
と励磁電流成分Inは次のようにして求める。すな
わち、いま電流検出器12によつて検出した1次
電流(3相分)をi1U,i1V,i1Wとすると、それら
は第3図を参照して、 i1U=kI1sin(ω1t+θ) ……(13) i1V=kI1sin(ω1t+θ+120゜) ……(14) i1W=kI1sin(ω1t+θ+240゜) ……(15) と表わされる。ここで、kは電流検出器12の検
出ゲインである。(3)〜(8)式で表わされる磁束位置
基準信号と(13)〜(15)式で表わされる1次電
流検出信号から2次電流成分I2と励磁電流成分In
が求められる。 d・i1U+e・i1V+f・i1W=3/2kAI1sinθ=
(3/2kA)I2……(16) a・i1U+b・i1V+c・i1W=3/2kAI1cosθ=
(3/2kA)In……(17) (16)、(17)式の演算を行えば、それぞれ1次
電流I1の2次電流成分I2と励磁電流成分Inに比例
する信号が検出できる。 第5図に(16)、(17)式の演算を行うための電
流成分検出回路15の具体的回路を示す。第5図
において106〜111は掛算器、112,11
3は演算増幅器、Rは抵抗である。演算増幅器1
12からは2次電流成分I2に比例する信号I2f、演
算増幅器113からは励磁電流成分Inに比例する
信号Infが出力される。 第1の電流成分制御回路16は2次電流成分指
令信号I2Pと検出信号I2fの偏差に応じて働き、両
者が一致するように動作し交流の1次電流指令信
号の振幅を補正する信号xを出力する。第2の電
流成分制御回路17は励磁電流成分指令信号Inp
と検出信号Infの偏差に応じて働き、両者が一致
するように動作し交流の1次電流指令信号の振幅
を補正する信号yを出力する。 電流パターン演算回路11′は信号x,yとか
ら以下の演算によつて1次電流の瞬時値を指令す
る交流信号i1Up,i1Vp,i1Wpを出力する。 i1Up=x・d+y・a=Bsin(ω1t+α)
……(18) i1Vp=x・e+y・b=Bsin(ω1t+α+120゜)
……(19) i1Wp=x・f+y・c=Bsin(ω1t+α+240゜)
……(20) ここで、B=√22tanα=x/yである。 第6図は電流パターン回路11′の構成を示す。
第6図において、114〜119は掛算器、12
0〜122は演算増幅器、Rは抵抗である。 図示の構成により1次電流の指令信号i1Up
i1Vp,i1Wpが出力される。この1次電流指令信号
iiUp,i1Vp,i1Wpと電流検出器12からの電流検出
信号i1U,i1V,i1Wを電流制御回路13に入力す
る。電流制御回路13はこれら各相の電流偏差に
応じて働き、その出力信号によつて周波数変換器
2は制御される。このようにして、誘導機3の1
次電流が制御される。 以上のようにして制御するのであるが、2次電
流成分の指令信号と検出信号、および励磁電流成
分の指令信号と検出信号が常に一致するように電
流成分が制御され、さらに、両電流成分を制御す
るようにして得られた電流指令信号(交流信号)
によつて交流電流を制御する電流制御回路が動作
するので、交流の電流はその指令波形に見合うよ
うに制御されるので、常に精度よく電流が制御さ
れる。この結果、回転速度や負荷状態によらず所
定のトルク、電圧の運転が行える。 なお、上記実施例では2つの電流成分を検出す
る際〔(16)式〜(17)式の演算〕と交流の1次
電流指令信号を演算する際〔(18)式〜(20)式
の演算〕に90度位相の異なる2組の3相信号〔(3)
式〜(8)式〕を用いて行つたが、例えば特公昭50−
34725号公報に示してあるように周知の変換方法、
すなわち2相の正弦波信号と2相−3相変換を用
いて、電流成分と1次電流指令信号を得るように
することもできる。 次に、第3図に示したベクトル図は誘導機の2
次鎖交磁束を基準にしてベクトル図を書いたが、
主磁束を基準にしたベクトル図も書くこともでき
る。第7図は2次漏れインダクタンスがある程度
大きいときにはこれを考慮したときのベクトル図
を示す。2次電流成分I2は磁束と同相成分I2rと90
度位相差成分I2aからなる。I2aがトルクに関係す
る成分でI2rとI2aの関係は I2r=ω2L2/R2I2a ……(21) で表わされる。 第8図は2次漏れインダクタンスを考慮すると
きの電流成分検出回路15の構成を示す。第8図
において、123〜129は掛算器、130〜1
33は演算増幅器、R,Ra,Rb,Rcは抵抗で
2RはRの2倍の抵抗値をもつている。演算増幅
器130の出力信号は第7図のI1の主磁束と90度
位相をもつ成分I2aに比例する信号であり、演算
増幅器131の出力信号は第7図のI1の主磁束と
同位相の成分(I2r+In)に比列する成分である。
演算増幅器132と掛算器129は演算増幅器1
30とすべり周波数演算回路8からの信号によ
り、(21)式の演算を行いI2の磁束と同位相成分
I2rを演算する。I2rに比例する信号が求まればこ
の信号と演算増幅器131の出力信号とから励磁
電流成分Inを求めることができる。 電流成分検出回路15を第8図のように構成す
れば、2次漏れインダクタンスの影響を考慮して
いるので、より精度よく1次電流の成分が検出で
きる。こうすれば2次もれインダクタンスの比較
的大きなモータに対しても所定のトルク、電圧の
運転が行える。 以上述べたように本発明によれば、運転状態に
よらず常に2次電流成分と励磁電流成分が直流信
号を扱う電流成分制御回路の働きによつて設定値
になるように交流の1次電流指令信号の大きさと
位相が決定される。この結果、交流信号を扱う電
流制御回路に遅れがあつても精度のよい電流制御
ができるので、所定のトルク、電圧で運転でき
る。
Select as shown in [Formula]. With this configuration, six signals a to f having frequencies proportional to the input signal are output. From these signals, the secondary current component of the primary current I 2
and excitation current component I n are determined as follows. That is, if the primary currents (three phases) detected by the current detector 12 are i 1U , i 1V , i 1W , then with reference to FIG . 1 t + θ) ... (13) i 1V = kI 1 sin (ω 1 t + θ + 120°) ... (14) i 1W = kI 1 sin (ω 1 t + θ + 240°) ... (15) Here, k is the detection gain of the current detector 12. The secondary current component I 2 and the exciting current component I n are calculated from the magnetic flux position reference signal expressed by equations (3) to (8) and the primary current detection signal expressed by equations (13) to ( 15 ).
is required. d・i 1U +e・i 1V +f・i 1W = 3/2kAI 1 sinθ=
(3/2kA) I 2 ... (16) a・i 1U + b・i 1V +c・i 1W = 3/2kAI 1 cosθ=
(3/2 kA) I n ... (17) By performing the calculations of equations (16) and (17), a signal proportional to the secondary current component I 2 and exciting current component I n of the primary current I 1 is obtained, respectively . Can be detected. FIG. 5 shows a specific circuit of the current component detection circuit 15 for calculating equations (16) and (17). In FIG. 5, 106 to 111 are multipliers, 112, 11
3 is an operational amplifier, and R is a resistor. Operational amplifier 1
12 outputs a signal I 2f proportional to the secondary current component I 2 , and an operational amplifier 113 outputs a signal I nf proportional to the excitation current component I n . The first current component control circuit 16 operates according to the deviation between the secondary current component command signal I 2P and the detection signal I 2f , and operates so that the two match, and is a signal that corrects the amplitude of the AC primary current command signal. Output x. The second current component control circuit 17 uses an excitation current component command signal I np
It operates according to the deviation between the detection signal I nf and the detection signal I nf , and outputs a signal y that corrects the amplitude of the alternating current primary current command signal by operating so that the two coincide. The current pattern calculation circuit 11' outputs AC signals i 1Up , i 1Vp , i 1Wp that command the instantaneous value of the primary current from the signals x and y by the following calculations. i 1Up = x・d+y・a=Bsin(ω 1 t+α)
...(18) i 1Vp = x・e+y・b=Bsin(ω 1 t+α+120°)
...(19) i 1Wp = x・f+y・c=Bsin(ω 1 t+α+240°)
...(20) Here, B=√ 2 + 2 tanα=x/y. FIG. 6 shows the configuration of the current pattern circuit 11'.
In FIG. 6, 114 to 119 are multipliers, 12
0 to 122 are operational amplifiers, and R is a resistor. With the illustrated configuration, the primary current command signal i 1Up ,
i 1Vp and i 1Wp are output. This primary current command signal
i iUp , i 1Vp , i 1Wp and current detection signals i 1U , i 1V , i 1W from the current detector 12 are input to the current control circuit 13 . The current control circuit 13 operates according to the current deviation of each phase, and the frequency converter 2 is controlled by its output signal. In this way, one of the induction machines 3
The next current is controlled. Control is performed as described above, and the current component is controlled so that the command signal and detection signal of the secondary current component and the command signal and detection signal of the excitation current component always match, and furthermore, both current components are Current command signal (AC signal) obtained by controlling
Since the current control circuit that controls the alternating current is operated by, the alternating current is controlled to match the command waveform, so the current is always controlled with high precision. As a result, operation with a predetermined torque and voltage can be achieved regardless of the rotational speed or load condition. In addition, in the above embodiment, when detecting two current components [calculations of equations (16) to (17)] and when calculating the AC primary current command signal [formulas (18) to (20)] [(3)
For example, in the 1970s,
The well-known conversion method as shown in Publication No. 34725,
That is, it is also possible to obtain the current component and the primary current command signal using a two-phase sine wave signal and two-phase to three-phase conversion. Next, the vector diagram shown in Figure 3 is
Next, I drew a vector diagram based on the flux linkage, but
It is also possible to draw a vector diagram based on the main magnetic flux. FIG. 7 shows a vector diagram when considering the secondary leakage inductance when it is large to some extent. The secondary current component I 2 is the magnetic flux and the in-phase component I 2r and 90
It consists of a degree phase difference component I 2a . I 2a is a component related to torque, and the relationship between I 2r and I 2a is expressed as I 2r = ω 2 L 2 /R 2 I 2a (21). FIG. 8 shows the configuration of the current component detection circuit 15 when considering secondary leakage inductance. In FIG. 8, 123-129 are multipliers, 130-1
33 is an operational amplifier, and R, Ra, Rb, and Rc are resistors.
2R has twice the resistance value of R. The output signal of the operational amplifier 130 is a signal proportional to the component I 2a having a phase of 90 degrees with the main magnetic flux of I 1 in FIG. 7, and the output signal of the operational amplifier 131 is the same as the main magnetic flux of I 1 in FIG. This is a component proportional to the phase component (I 2r +I n ).
Operational amplifier 132 and multiplier 129 are operational amplifier 1
30 and the signal from the slip frequency calculation circuit 8, calculate the equation (21) and obtain the same phase component as the magnetic flux of I2 .
Calculate I 2r . If a signal proportional to I 2r is found, the excitation current component I n can be found from this signal and the output signal of the operational amplifier 131. If the current component detection circuit 15 is configured as shown in FIG. 8, the influence of secondary leakage inductance is taken into consideration, so that the primary current component can be detected with higher accuracy. In this way, even a motor with a relatively large secondary leakage inductance can be operated at a predetermined torque and voltage. As described above, according to the present invention, the AC primary current is controlled so that the secondary current component and the excitation current component always reach the set value by the function of the current component control circuit that handles the DC signal, regardless of the operating state. The magnitude and phase of the command signal are determined. As a result, even if there is a delay in the current control circuit that handles AC signals, accurate current control can be performed, allowing operation with predetermined torque and voltage.

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

第1図は従来例を示す図、第2図は本発明の一
実施例を示す図、第3図は第2図の動作説明図、
第4図〜第6図は第2図の部品の詳細図、第7図
は第2図の他の動作説明図、第8図は第2図の部
品の他の詳細図である。 2……周波数変換器、3……誘導機、6……速
度制御回路、7……励磁電流指令回路、8……す
べり周波数演算回路、9……加算器、10……発
振器、11′……電流パターン回路、13……電
流制御回路、15……電流成分検出回路、16,
17……電流成分制御回路。
Fig. 1 is a diagram showing a conventional example, Fig. 2 is a diagram showing an embodiment of the present invention, Fig. 3 is an explanatory diagram of the operation of Fig. 2,
4 to 6 are detailed views of the components shown in FIG. 2, FIG. 7 is another operational explanatory view of the parts shown in FIG. 2, and FIG. 8 is another detailed view of the parts shown in FIG. 2. 2... Frequency converter, 3... Induction machine, 6... Speed control circuit, 7... Excitation current command circuit, 8... Slip frequency calculation circuit, 9... Adder, 10... Oscillator, 11'... ...Current pattern circuit, 13...Current control circuit, 15...Current component detection circuit, 16,
17...Current component control circuit.

Claims (1)

【特許請求の範囲】[Claims] 1 出力電圧と出力周波数を制御できる周波数変
換器と、該周波数変換器によつて駆動される誘導
電動機と、該誘導電動機の1次電流を、磁束と同
相成分である励磁電流成分指令信号および直交成
分である2次電流成分指令信号とに分けて直流信
号で指令する電流成分指令手段と、前記誘導電動
機の1次周波数指令信号に対応して発生する磁束
位置基準信号を出力する信号発生手段と、前記誘
導電動機の1次電流の2次電流成分と励磁電流成
分を前記磁束位置基準信号に基づいて直流信号と
して検出する電流成分検出手段と、前記2次電流
成分指令信号と2次電流成分検出信号の偏差に応
じた信号を出力する第1電流成分制御手段と、前
記励磁電流成分指令信号と励磁電流成分検出信号
の偏差に応じた信号を出力する第2電流成分制御
手段と、前記第1および第2電流成分制御手段の
出力信号に応じて1次電流を指令する交流信号を
発生する電流指令手段と、該電流指令手段の出力
信号によつて前記誘導電動機の1次電流を制御す
る電流制御手段とを具備した誘導電動機の制御装
置。
1 A frequency converter that can control the output voltage and output frequency, an induction motor driven by the frequency converter, and a primary current of the induction motor that is controlled by an excitation current component command signal that is in phase with the magnetic flux and a quadrature component. current component command means for commanding a secondary current component command signal using a direct current signal; and signal generation means for outputting a magnetic flux position reference signal generated in response to the primary frequency command signal of the induction motor. , current component detection means for detecting a secondary current component and an exciting current component of the primary current of the induction motor as DC signals based on the magnetic flux position reference signal; and detection of the secondary current component command signal and the secondary current component. a first current component control means for outputting a signal according to the deviation of the signal; a second current component control means for outputting a signal according to the deviation between the excitation current component command signal and the excitation current component detection signal; and current command means for generating an alternating current signal for commanding the primary current in response to the output signal of the second current component control means, and a current for controlling the primary current of the induction motor based on the output signal of the current command means. A control device for an induction motor, comprising a control means.
JP14893479A 1979-11-19 1979-11-19 Control device for induction motor Granted JPS5674090A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14893479A JPS5674090A (en) 1979-11-19 1979-11-19 Control device for induction motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14893479A JPS5674090A (en) 1979-11-19 1979-11-19 Control device for induction motor

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP61265508A Division JPS62163588A (en) 1986-11-10 1986-11-10 Induction motor control device

Publications (2)

Publication Number Publication Date
JPS5674090A JPS5674090A (en) 1981-06-19
JPS6333391B2 true JPS6333391B2 (en) 1988-07-05

Family

ID=15463920

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14893479A Granted JPS5674090A (en) 1979-11-19 1979-11-19 Control device for induction motor

Country Status (1)

Country Link
JP (1) JPS5674090A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0657093U (en) * 1993-01-08 1994-08-05 三木プーリ株式会社 Control unit for multiple motors

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0828972B2 (en) * 1986-05-12 1996-03-21 三菱電機株式会社 Non-circulating current type cycloconverter control device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5313127A (en) * 1976-07-22 1978-02-06 Toshiba Corp Controller for induction motor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0657093U (en) * 1993-01-08 1994-08-05 三木プーリ株式会社 Control unit for multiple motors

Also Published As

Publication number Publication date
JPS5674090A (en) 1981-06-19

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