Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JP4076268B2 - Inverter control device - Google Patents
[go: Go Back, main page]

JP4076268B2 - Inverter control device - Google Patents

Inverter control device Download PDF

Info

Publication number
JP4076268B2
JP4076268B2 JP11439998A JP11439998A JP4076268B2 JP 4076268 B2 JP4076268 B2 JP 4076268B2 JP 11439998 A JP11439998 A JP 11439998A JP 11439998 A JP11439998 A JP 11439998A JP 4076268 B2 JP4076268 B2 JP 4076268B2
Authority
JP
Japan
Prior art keywords
magnetic flux
primary
angular velocity
calculator
information
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
JP11439998A
Other languages
Japanese (ja)
Other versions
JPH11299300A (en
Inventor
宜弘 中村
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.)
Toyo Electric Manufacturing Ltd
Original Assignee
Toyo Electric Manufacturing 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 Toyo Electric Manufacturing Ltd filed Critical Toyo Electric Manufacturing Ltd
Priority to JP11439998A priority Critical patent/JP4076268B2/en
Publication of JPH11299300A publication Critical patent/JPH11299300A/en
Application granted granted Critical
Publication of JP4076268B2 publication Critical patent/JP4076268B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Landscapes

  • Control Of Ac Motors In General (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は,誘導電動機の高速・高精度トルク制御システムに関するもので,誘導電動機の温度変化に伴う二次抵抗値変動によるトルク制御特性劣化に対してロバスト化を行うものである。
【0002】
【従来の技術】
図3に従来技術の一例のブロック線図を示し,以下この図に基づいて説明を行う。誘導電動機2に電力変換器1から電力が供給される。トルク・磁束制御器5は,誘導電動機2のトルクTと磁束φ1が所定のトルク指令値T*と磁束指令値φ1*に追従するように電力変換器1を制御する一次電圧指令値v1*を出力する。トルク・磁束制御器5に入力される誘導電動機2のトルクTと磁束φ1は,トルク・磁束演算器7で演算される。トルク・磁束演算器7には電流検出器4の出力である誘導電動機2の一次電流i1と,二次磁束演算器6の出力である誘導電動機2の二次磁束φ2が入力される。二次磁束φ2は,速度検出器3の出力である誘導電動機2の回転速度ωmと,電流検出器4の出力である誘導電動機2の一次電流i1と,誘導電動機2の二次抵抗値R2を用いて二次磁束演算器6で演算される。
【0003】
【発明が解決しようとする課題】
従来技術のトルク・磁束制御器5では,誘導電動機2のトルクTと磁束φ1を所定のトルク指令値T*と磁束指令値φ1*に追従させるように制御を行なっている。この時,誘導電動機2のトルクTと磁束φ1の演算を行う上で誘導電動機2の二次磁束φ2の情報が必要となる。二次磁束φ2は二次磁束演算器6で演算される。二次磁束演算器6では誘導電動機2の二次抵抗値R2を用いている。二次抵抗値R2は誘導電動機2の温度変化により変動してしまうが,二次磁束演算器6の二次抵抗値R2にはインバータ制御装置の初期運転時の自動計測値が設定される。従って,その後の運転での温度変化による二次抵抗値R2の変動によって二次磁束演算器6の出力である二次磁束φ2に演算誤差を生じる。二次磁束演算器6の出力である二次磁束φ2に生じた演算誤差によって,誘導電動機2のトルクTと磁束φ1の演算にも誤差を生じる。そのため,トルク・磁束制御器5の出力は所定のトルク指令値T*と磁束指令値φ1*に見合ったものではなく,誘導電動機2において所定の出力トルクが得られない。
本発明は上述した点に鑑みて創案されたもので、その目的とするところは、これらの欠点を解決し,所定のトルクが得られるインバータ制御装置を提供することにある。
【0004】
【課題を解決するための手段】
つまり、その目的を達成するための手段は、
1)請求項1において,
電流検出器4の出力である一次電流i1から一次角速度を演算する第一一次角速度演算器と,二次磁束演算器6の出力である二次磁束φ2から一次角速度を演算する第二一次角速度演算器と,第一一次角速度演算器の一次角速度情報と第二一次角速度演算器の一次角速度情報の差が零となるように二次磁束演算器6の二次抵抗値R2を調整する二次抵抗調整器を具備するものである。
【0005】
2)請求項2において、
誘導電動機2の一次電圧を検出または一次電圧指令値v1*から推定する電圧検出器の一次電圧情報から一次角速度を演算する第三一次角速度演算器と,二次磁束演算器6の出力である二次磁束φ2から一次角速度を演算する第二一次角速度演算器と,第三一次角速度演算器の一次角速度情報と第二一次角速度演算器の一次角速度情報の差が零となるように二次磁束演算器6の二次抵抗値R2を調整する二次抵抗調整器を具備するものである。
以下、本発明の一実施例を図面に基づいて詳述する。
【0006】
【発明の実施の形態】
図1は本発明の請求項1記載の一実施例を示すブロック図,図2は本発明の請求項2記載の一実施例を示すブロック図であり,図1においては,第一一次角速度演算器8と第二一次角速度演算器9と二次抵抗調整器10が具備されている点と二次磁束演算器6の二次抵抗値R2に二次抵抗調整器10の出力を用いていることが従来技術と異なる。第一一次角速度演算器8は電流検出器4の一次電流i1を用いて,一次角速度ω11を

Figure 0004076268
により求める。ここでi1dとi1qは一次電流i1の成分であり,p()は()内量の時間微分を表わす。
【0007】
第二一次角速度演算器9は二次磁束演算器6の二次磁束φ2を用いて,一次角速度ω12を
Figure 0004076268
により求める。ここでφ2dとφ2qは二次磁束φ2の成分であり,p()は()内量の時間微分を表わす。
【0008】
二次磁束演算器6は電流検出器4の一次電流i1と速度検出器3の回転速度ωmを用いて,二次磁束φ2を
φ2=∫{(1/L2)
*(M*R2*i1−R2*φ2+j*ωm*L2*φ2)}dt (3)
により求める。ここで二次抵抗値R2に二次抵抗調整器10の出力を用いる。また,Mは相互インダクタンスでL2は二次自己インダクタンスである。
【0009】
二次抵抗調整器10は第一一次角速度演算器8の一次角速度ω11と第二一次角速度演算器9の一次角速度ω12を用いて,
R2=(Ki/s+Kp)*(ω11−ω12) (4)
により二次抵抗値R2を求める。ここでKiは積分ゲインでKpは比例ゲインである。また,1/sは積分を表わす。
【0010】
第一一次角速度演算器8の一次角速度ω11は電流検出器4の一次電流i1の情報のみを用いて求められており,誘導電動機2の温度変化による演算誤差は生じないので真値と考えることができる。第二一次角速度演算器9の一次角速度ω12の演算には二次抵抗値R2の情報を用いるので誘導電動機2の温度変化による二次抵抗値R2の変動によって演算誤差を生じる。一次角速度ω12がその真値と考える一次角速度ω11と等しくなるように二次抵抗調整器10によって二次磁束演算器6の二次抵抗値R2を調整することで誘導電動機2の温度変化によって生じる演算誤差をなくし,トルク・磁束制御器5による高精度なトルク制御を実現する。
【0011】
次に,本発明の請求項2記載の実施例を図2に基づいて説明する。
図2においては,第一一次角速度演算器8に代わって第三一次角速度演算器11と電圧検出器12が具備されている点が実施例1と異なる。電圧検出器12は誘導電動機2の一次電圧v1を検出または一次電圧指令値v1*から推定する。第三一次角速度演算器11は電圧検出器12の一次電圧v1を用いて,一次角速度ω13を,
Figure 0004076268
により求める。ここでv1dとv1qは一次電圧v1の成分であり,p()は()内量の時間微分を表わす。二次磁束演算器6と第二一次角速度演算器9と二次抵抗調整器10のアルゴリズムは図1で説明した通りである。
【0012】
第三一次角速度演算器11の一次角速度ω13は電圧検出器12の一次電圧v1の情報のみを用いて求められており,誘導電動機2の温度変化による演算誤差は生じないので真値と考えることができる。
図1で述べたように,第二一次角速度演算器9の一次角速度ω12の演算には二次抵抗値R2の情報を用いるので誘導電動機2の温度変化による二次抵抗値R2の変動によって演算誤差を生じる。一次角速度ω12がその真値と考える一次角速度ω13と等しくなるように二次抵抗調整器10によって二次磁束演算器6の二次抵抗値R2を調整することで誘導電動機2の温度変化によって生じる演算誤差をなくし,実施例1と同様にトルク・磁束制御器5による高精度なトルク制御を実現する。
【0013】
【発明の効果】
以上説明したように本発明によれば、誘導電動機2の温度変化による二次抵抗値R2の変動に対して本発明による補償を行うことで, トルク・磁束制御器5によって誘導電動機2では所定の出力トルクが得られ,高精度なトルク制御が実現でき,実用上、極めて有用性の高いものである。
【図面の簡単な説明】
【図1】本発明のインバータ制御装置の実施例1を示すブロック線図である。
【図2】本発明のインバータ制御装置の実施例2を示すブロック線図である。
【図3】従来技術の一例を示すブロック線図である。
【符号の説明】
1 電力変換器
2 誘導電動機
3 速度検出器
4 電流検出器
5 トルク・磁束制御器
6 二次磁束演算器
7 トルク・磁束演算器
8 第一一次角速度演算器
9 第二一次角速度演算器
10 二次抵抗調整器
11 第三一次角速度演算器
12 電圧検出器[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a high-speed and high-accuracy torque control system for induction motors, and is intended to make robust against torque control characteristic deterioration due to secondary resistance value fluctuation accompanying temperature change of the induction motor.
[0002]
[Prior art]
FIG. 3 shows a block diagram of an example of the prior art, which will be described below with reference to this figure. Electric power is supplied from the power converter 1 to the induction motor 2. The torque / magnetic flux controller 5 generates a primary voltage command value v1 * for controlling the power converter 1 so that the torque T and the magnetic flux φ1 of the induction motor 2 follow a predetermined torque command value T * and a magnetic flux command value φ1 *. Output. The torque T and the magnetic flux φ1 of the induction motor 2 input to the torque / flux controller 5 are calculated by the torque / flux calculator 7. The torque / magnetic flux calculator 7 receives the primary current i1 of the induction motor 2 that is the output of the current detector 4 and the secondary magnetic flux φ2 of the induction motor 2 that is the output of the secondary magnetic flux calculator 6. The secondary magnetic flux φ2 includes the rotation speed ωm of the induction motor 2 that is the output of the speed detector 3, the primary current i1 of the induction motor 2 that is the output of the current detector 4, and the secondary resistance value R2 of the induction motor 2. And is calculated by the secondary magnetic flux calculator 6.
[0003]
[Problems to be solved by the invention]
In the torque / magnetic flux controller 5 of the prior art, control is performed so that the torque T and magnetic flux φ1 of the induction motor 2 follow a predetermined torque command value T * and magnetic flux command value φ1 *. At this time, information on the secondary magnetic flux φ2 of the induction motor 2 is required to calculate the torque T and the magnetic flux φ1 of the induction motor 2. The secondary magnetic flux φ2 is calculated by the secondary magnetic flux calculator 6. The secondary magnetic flux calculator 6 uses the secondary resistance value R2 of the induction motor 2. Although the secondary resistance value R2 varies depending on the temperature change of the induction motor 2, the secondary resistance value R2 of the secondary magnetic flux calculator 6 is set to an automatic measurement value during the initial operation of the inverter control device. Accordingly, a calculation error occurs in the secondary magnetic flux φ2 that is the output of the secondary magnetic flux calculator 6 due to the change in the secondary resistance value R2 due to the temperature change in the subsequent operation. Due to the calculation error generated in the secondary magnetic flux φ2 which is the output of the secondary magnetic flux calculator 6, an error also occurs in the calculation of the torque T and the magnetic flux φ1 of the induction motor 2. Therefore, the output of the torque / magnetic flux controller 5 does not correspond to the predetermined torque command value T * and the magnetic flux command value φ1 *, and the predetermined output torque cannot be obtained in the induction motor 2.
The present invention has been made in view of the above-described points, and an object of the present invention is to provide an inverter control device that can solve these drawbacks and obtain a predetermined torque.
[0004]
[Means for Solving the Problems]
In other words, the means to achieve that purpose is
1) In claim 1,
A first primary angular velocity calculator that calculates the primary angular velocity from the primary current i1 that is the output of the current detector 4, and a secondary primary that calculates the primary angular velocity from the secondary magnetic flux φ2 that is the output of the secondary magnetic flux calculator 6. The secondary resistance value R2 of the secondary magnetic flux calculator 6 is adjusted so that the difference between the primary angular velocity information of the angular velocity calculator and the first primary angular velocity calculator and the primary angular velocity information of the second primary angular velocity calculator is zero. The secondary resistance regulator is provided.
[0005]
2) In claim 2,
These are the outputs of the third primary angular velocity calculator and the secondary magnetic flux calculator 6 that calculate the primary angular velocity from the primary voltage information of the voltage detector that detects or estimates the primary voltage of the induction motor 2 from the primary voltage command value v1 *. The difference between the primary angular velocity information of the second primary angular velocity calculator that calculates the primary angular velocity from the secondary magnetic flux φ2 and the primary angular velocity information of the third primary angular velocity calculator and the primary angular velocity information of the second primary angular velocity calculator is zero. A secondary resistance adjuster for adjusting the secondary resistance value R2 of the secondary magnetic flux calculator 6 is provided.
Hereinafter, an embodiment of the present invention will be described in detail with reference to the drawings.
[0006]
DETAILED DESCRIPTION OF THE INVENTION
FIG. 1 is a block diagram showing an embodiment of the first aspect of the present invention, and FIG. 2 is a block diagram showing an embodiment of the second aspect of the present invention. In FIG. Using the output of the secondary resistance adjuster 10 as the secondary resistance value R2 of the secondary magnetic flux calculator 6 and the point where the calculator 8, the second primary angular velocity calculator 9 and the secondary resistance adjuster 10 are provided. Is different from the prior art. The first primary angular velocity calculator 8 uses the primary current i1 of the current detector 4 to calculate the primary angular velocity ω11.
Figure 0004076268
Ask for. Here, i1d and i1q are components of the primary current i1, and p () represents the time differentiation of the amount in ().
[0007]
The second primary angular velocity calculator 9 uses the secondary magnetic flux φ2 of the secondary magnetic flux calculator 6 to calculate the primary angular velocity ω12.
Figure 0004076268
Ask for. Here, φ2d and φ2q are components of the secondary magnetic flux φ2, and p () represents time differentiation of the amount in parentheses.
[0008]
The secondary magnetic flux calculator 6 uses the primary current i1 of the current detector 4 and the rotational speed ωm of the speed detector 3 to change the secondary magnetic flux φ2 to φ2 = ∫ {(1 / L2)
* (M * R2 * i1-R2 * φ2 + j * ωm * L2 * φ2)} dt (3)
Ask for. Here, the output of the secondary resistance adjuster 10 is used as the secondary resistance value R2. M is a mutual inductance and L2 is a secondary self-inductance.
[0009]
The secondary resistance adjuster 10 uses the primary angular velocity ω11 of the first primary angular velocity calculator 8 and the primary angular velocity ω12 of the second primary angular velocity calculator 9,
R2 = (Ki / s + Kp) * (ω11−ω12) (4)
To obtain the secondary resistance value R2. Here, Ki is an integral gain, and Kp is a proportional gain. 1 / s represents integration.
[0010]
The primary angular velocity ω11 of the first primary angular velocity calculator 8 is obtained using only the information of the primary current i1 of the current detector 4, and no calculation error due to the temperature change of the induction motor 2 occurs. Can do. Since the information of the secondary resistance value R2 is used for the calculation of the primary angular velocity ω12 of the second primary angular velocity calculator 9, a calculation error occurs due to the fluctuation of the secondary resistance value R2 due to the temperature change of the induction motor 2. Calculation caused by temperature change of the induction motor 2 by adjusting the secondary resistance value R2 of the secondary magnetic flux calculator 6 by the secondary resistance adjuster 10 so that the primary angular speed ω12 becomes equal to the primary angular velocity ω11 considered to be the true value. The error is eliminated and high-precision torque control by the torque / flux controller 5 is realized.
[0011]
Next, an embodiment according to claim 2 of the present invention will be described with reference to FIG.
2 is different from the first embodiment in that a third primary angular velocity calculator 11 and a voltage detector 12 are provided in place of the first primary angular velocity calculator 8. The voltage detector 12 detects or estimates the primary voltage v1 of the induction motor 2 from the primary voltage command value v1 *. The third primary angular velocity calculator 11 uses the primary voltage v1 of the voltage detector 12 to calculate the primary angular velocity ω13,
Figure 0004076268
Ask for. Here, v1d and v1q are components of the primary voltage v1, and p () represents the time differentiation of the amount in (). The algorithms of the secondary magnetic flux calculator 6, the second primary angular velocity calculator 9, and the secondary resistance adjuster 10 are as described in FIG.
[0012]
The primary angular velocity ω13 of the third primary angular velocity calculator 11 is obtained by using only the information of the primary voltage v1 of the voltage detector 12, and an arithmetic error due to a temperature change of the induction motor 2 does not occur. Can do.
As described in FIG. 1, since the information of the secondary resistance value R <b> 2 is used for the calculation of the primary angular velocity ω <b> 12 of the second primary angular velocity calculator 9, the calculation is performed by the change of the secondary resistance value R <b> 2 due to the temperature change of the induction motor 2. An error is generated. Calculation caused by temperature change of the induction motor 2 by adjusting the secondary resistance value R2 of the secondary magnetic flux calculator 6 by the secondary resistance adjuster 10 so that the primary angular speed ω12 becomes equal to the primary angular velocity ω13 considered to be the true value. The error is eliminated and high-precision torque control by the torque / flux controller 5 is realized as in the first embodiment.
[0013]
【The invention's effect】
As described above, according to the present invention, the compensation according to the present invention is performed for the fluctuation of the secondary resistance value R2 due to the temperature change of the induction motor 2, so that the torque / flux controller 5 causes the induction motor 2 to have a predetermined value. Output torque can be obtained, high-accuracy torque control can be realized, and it is extremely useful in practice.
[Brief description of the drawings]
FIG. 1 is a block diagram showing Example 1 of an inverter control device of the present invention.
FIG. 2 is a block diagram showing Example 2 of the inverter control device of the present invention.
FIG. 3 is a block diagram showing an example of a prior art.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 Power converter 2 Induction motor 3 Speed detector 4 Current detector 5 Torque / flux controller 6 Secondary flux calculator 7 Torque / flux calculator 8 First primary angular velocity calculator 9 Second primary angular velocity calculator 10 Secondary resistance adjuster 11 Third primary angular velocity calculator 12 Voltage detector

Claims (2)

誘導電動機に電力を供給する電力変換器と,該電動機の回転速度を検出する速度検出器と,該電動機の一次電流を検出する電流検出器と,前記速度検出器の速度情報と前記電流検出器の一次電流情報から前記電動機の二次抵抗値によって二次磁束を演算する二次磁束演算器と,該二次磁束演算器の二次磁束情報と前記電流検出器の一次電流情報から前記電動機のトルクと磁束を演算するトルク・磁束演算器と,該トルク・磁束演算器の演算トルク情報と演算磁束情報が所定のトルク指令値と磁束指令値に追従するように前記電力変換器を制御するトルク・磁束制御器からなるインバータ制御装置において,
前記電流検出器の一次電流情報から一次角速度を演算する第一一次角速度演算器と,前記二次磁束演算器の二次磁束情報から一次角速度を演算する第二一次角速度演算器と,前記第一一次角速度演算器の一次角速度情報と前記第二一次角速度演算器の一次角速度情報の差が零となるように前記二次磁束演算器の二次抵抗値を調整する二次抵抗調整器を具備することを特徴とするインバータ制御装置。
A power converter for supplying power to the induction motor; a speed detector for detecting the rotational speed of the motor; a current detector for detecting a primary current of the motor; speed information of the speed detector; and the current detector A secondary magnetic flux calculator for calculating a secondary magnetic flux from the primary current information of the electric motor according to a secondary resistance value of the motor, a secondary magnetic flux information of the secondary magnetic flux calculator and a primary current information of the current detector from the primary current information of the motor. Torque / magnetic flux calculator for calculating torque and magnetic flux, and torque for controlling the power converter so that the calculated torque information and the calculated magnetic flux information of the torque / flux calculator follow a predetermined torque command value and magnetic flux command value. -In an inverter control device consisting of a magnetic flux controller,
A first primary angular velocity calculator that calculates a primary angular velocity from primary current information of the current detector; a second primary angular velocity calculator that calculates a primary angular velocity from secondary magnetic flux information of the secondary magnetic flux calculator; and Secondary resistance adjustment for adjusting a secondary resistance value of the secondary magnetic flux calculator so that a difference between primary angular velocity information of the first primary angular velocity calculator and primary angular velocity information of the second primary angular velocity calculator becomes zero An inverter control device comprising a device.
前記第一一次角速度演算器に代わって,前記電動機の一次電圧を検出または一次電圧指令値から推定する電圧検出器の一次電圧情報から一次角速度を演算する第三一次角速度演算器を具備することを特徴とする請求項1記載のインバータ制御装置。In place of the first primary angular velocity calculator, a third primary angular velocity calculator that calculates a primary angular velocity from primary voltage information of a voltage detector that detects or estimates a primary voltage of the motor from a primary voltage command value is provided. The inverter control device according to claim 1.
JP11439998A 1998-04-10 1998-04-10 Inverter control device Expired - Lifetime JP4076268B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11439998A JP4076268B2 (en) 1998-04-10 1998-04-10 Inverter control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11439998A JP4076268B2 (en) 1998-04-10 1998-04-10 Inverter control device

Publications (2)

Publication Number Publication Date
JPH11299300A JPH11299300A (en) 1999-10-29
JP4076268B2 true JP4076268B2 (en) 2008-04-16

Family

ID=14636717

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11439998A Expired - Lifetime JP4076268B2 (en) 1998-04-10 1998-04-10 Inverter control device

Country Status (1)

Country Link
JP (1) JP4076268B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20120079169A (en) 2009-12-28 2012-07-11 미쓰비시덴키 가부시키가이샤 Power conversion device for electric vehicle
JP5921031B2 (en) * 2012-02-16 2016-05-24 東洋電機製造株式会社 Induction machine controller

Also Published As

Publication number Publication date
JPH11299300A (en) 1999-10-29

Similar Documents

Publication Publication Date Title
JP3399156B2 (en) Control device for brushless DC motor
JPH08182398A (en) Permanent magnet type synchronous motor drive device
JPH05207767A (en) Motor drive controller
JPH02254987A (en) Method and apparatus for control of induction motor
JPH01103184A (en) Control system for servo motor
JP4076268B2 (en) Inverter control device
JP2005027386A (en) Current sensorless control device for synchronous motor
JP4225657B2 (en) Control device for permanent magnet type synchronous motor
JPH0898600A (en) Motor control device
JPH06284511A (en) Electric vehicle torque control method
CN118369849A (en) Method for automatically setting an angular position sensor
JP3431601B2 (en) Control method and device for sensorless induction machine
JP3454409B2 (en) Induction motor control device
JP2615688B2 (en) Control method of induction motor
JP2625969B2 (en) Vector controller for induction motor
JP2007135281A (en) Speed sensorless vector controller for induction motor
JP2004064926A (en) Electric vehicle control device
JP2000341983A (en) Control device for embedded magnet type synchronous motor
JPH04304184A (en) Vector control method for induction motor
JP4274618B2 (en) Inverter device
JP3957368B2 (en) Induction motor controller
JP2003189687A (en) Variable speed control device for electric motor
JP2003009600A (en) Electric car control device
JPH07303398A (en) Secondary resistance compensating method of induction motor
JPH05168274A (en) Induction motor speed detector

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20041124

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20070110

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20070214

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20080129

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20080129

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110208

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120208

Year of fee payment: 4

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130208

Year of fee payment: 5

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20140208

Year of fee payment: 6

EXPY Cancellation because of completion of term