WO2024224659A1 - 電力変換装置 - Google Patents
電力変換装置 Download PDFInfo
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- WO2024224659A1 WO2024224659A1 PCT/JP2023/036163 JP2023036163W WO2024224659A1 WO 2024224659 A1 WO2024224659 A1 WO 2024224659A1 JP 2023036163 W JP2023036163 W JP 2023036163W WO 2024224659 A1 WO2024224659 A1 WO 2024224659A1
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- permanent magnet
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P21/00—Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
- H02P21/12—Stator flux based control involving the use of rotor position or rotor speed sensors
Definitions
- the present invention relates to a power conversion device.
- Patent Document 1 describes a control technology that achieves stable operation in the constant output region of the weakened field.
- Patent document 1 describes a motor output power calculation means and a technology that corrects the speed command value so that the output power is equal to or less than a predetermined value, and that aims to avoid overcurrent when a load torque greater than the torque value of a permanent magnet synchronous motor is applied in the constant output region of the field-weakening region.
- Patent Document 1 Because the purpose of Patent Document 1 is to correct the speed command value, it does not mention how to limit the d-axis (flux axis) current command value calculated in the field-weakening region or the q-axis (torque axis) output current calculated during speed control.
- the speed control input is limited so that the power does not increase above the limit value, but if a large load torque is applied in the constant output region of the weak field magnet region, the primary current may become an overcurrent. If the primary current exceeds the overcurrent, operation may become impossible.
- the object of the present invention is to provide a power conversion device that limits both power and current to achieve highly stable control characteristics.
- the present invention is configured as follows:
- the power conversion device includes a permanent magnet motor, a power converter that supplies power to the permanent magnet motor, and a speed command correction calculation unit that corrects the speed command value based on speed information, a torque command value, and a primary current.
- the speed command correction calculation unit calculates the power limit value so as to limit the current value of the permanent magnet motor to a predetermined limit value or less, and corrects the speed command value so that the power does not increase to the power limit value.
- the present invention provides a power conversion device that limits both power and current and achieves highly stable control characteristics.
- the present invention it is possible to provide a power conversion device that can operate stably without reaching an overcurrent when a load torque greater than the torque value of a permanent magnet motor, which changes depending on the DC voltage of the power converter, is applied in the constant output region of the weak field region.
- FIG. 1 is a schematic configuration diagram of a power conversion device according to a first embodiment
- FIG. 4 is a configuration diagram of a speed command correction calculation unit according to the first embodiment
- FIG. 13 is a diagram showing control characteristics when the first embodiment is not used.
- FIG. 11 is a diagram showing control characteristics when the first embodiment is used.
- FIG. 11 is an explanatory diagram of a verification method when the first embodiment is adopted.
- FIG. 11 is a schematic configuration diagram of a power conversion device according to a second embodiment.
- FIG. 11 is a configuration diagram of a speed command correction calculation unit according to a second embodiment.
- FIG. 11 is a configuration diagram of a power conversion device according to a third embodiment.
- FIG. 11 is a configuration diagram of a speed command correction calculation unit according to a third embodiment.
- FIG. 11 is a configuration diagram of a power conversion device according to a fourth embodiment.
- FIG. 13 is a configuration diagram of a speed command correction calculation unit according to a fourth embodiment.
- FIG. 13 is a configuration diagram of a power conversion device according to a fifth embodiment.
- FIG. 13 is a configuration diagram of a speed command correction calculation unit according to a fifth embodiment.
- FIG. 13 is a configuration diagram of a power conversion device according to a sixth embodiment.
- FIG. 13 is a configuration diagram of a power conversion device according to a seventh embodiment.
- FIG. 13 is a configuration diagram of a power conversion device according to an eighth embodiment.
- FIG. 13 is a configuration diagram of a power conversion device according to a ninth embodiment.
- FIG. 13 is a configuration diagram of a speed command correction calculation unit according to a ninth embodiment.
- each component may be singular or plural.
- the position, size, shape, range, etc. of each component shown in the drawings may not represent the actual position, size, shape, range, etc., in order to facilitate understanding of the invention. Therefore, the present invention is not necessarily limited to the position, size, shape, range, etc. disclosed in the drawings.
- FIG. 1 is a schematic configuration diagram of a power conversion device 100 according to a first embodiment.
- permanent magnet motor 1 outputs a motor torque that combines a torque component due to the magnetic flux of the permanent magnet and a torque component due to the inductance of the armature winding.
- the power converter 2 outputs voltage values proportional to the three-phase AC voltage command values vu * , vv * , vw *, and varies the output voltage and output frequency of the permanent magnet motor 1.
- a controller (such as a microcomputer) of the power converter 2 sets a power limit value Pmax * and a primary current limit value imax * , and calculates the power limit value Pmax ** .
- the DC power supply 3 supplies a DC voltage to the power converter 2.
- the current detector 4 outputs iuc , ivc , and iwc which are detection values of the three-phase AC currents iu , iv , and iw of the permanent magnet motor 1.
- the position detector 5 has the resolution to detect the position of the permanent magnet motor 1 with high precision, and is used to calculate the speed of the permanent magnet motor 1.
- the coordinate conversion unit 6 outputs the d-axis and q-axis current detection values i dc , i qc input to the permanent magnet motor 1 from the detection values i uc , i vc , i wc of the three-phase AC currents i u , iv , i w and the phase detection value ⁇ dc .
- the speed control calculation unit 7 calculates and outputs a q-axis current command value iq * based on a new speed command value ⁇ r** obtained by adding the speed command value ⁇ r* and the speed command value correction value ⁇ r* and a speed detection value ( or a speed estimate value) wrc.
- the speed detection value (or a speed specification value) wrc can be defined as speed information.
- the vector control calculation unit 8 outputs the d-axis and q-axis voltage command values vdc ** , vqc** calculated based on the d-axis and q-axis current command values id*, iq*, current detection values idc, iqc , speed detection value ⁇ rc and the electrical circuit parameters of the permanent magnet motor 1, and outputs the modulation rate Kh *, which is the ratio of the voltage command value V * to the DC voltage value Edc.
- the field-weakening control calculation unit 9 outputs a d-axis current command value i d * based on the modulation factor K h * of the voltage command value.
- the frequency and phase detection and calculation unit 10 converts the position detection value qd detected by the position detector 5 into a phase detection value ⁇ dc that changes from 0 to 2 ⁇ per mechanical angle rotation of the permanent magnet motor 1. It also calculates a speed detection value wrc that changes based on the position detection value qdc .
- the speed command correction calculation unit 11 outputs a correction value ⁇ r * of the speed command value based on the d-axis and q-axis current commands i d * , i q * , the torque command value ⁇ * , and the detected speed value w rc .
- the coordinate conversion unit 12 outputs three-phase AC voltage command values vu * , vv * , vw * based on the dc - axis and qc - axis voltage command values vdc**, vqc ** and the phase detection value ⁇ dc .
- the frequency and phase detection and calculation unit 10 receives an incremental or absolute encoder signal, and generates a phase detection value qdc whose phase value changes from 0 to 2 ⁇ per mechanical rotation. Using this qdc , the speed detection value ⁇ rc is calculated according to the following equation (1).
- the speed control calculation unit 6 calculates a torque command value ⁇ * according to the following equation (2) by proportional control and integral control so that the detected speed value ⁇ rc follows a new speed command value ⁇ r ** , which will be described later.
- Ksp is the proportional gain of the speed control
- Ksi is the integral gain of the speed control
- the q-axis current command value i q * is calculated according to the following equation (3) using the torque command value ⁇ * , the d-axis current command value i d *, and the electrical parameters (L d , L q , K e ) of the permanent magnet motor 1 .
- L d * is the d-axis inductance setting value
- L q * is the q-axis inductance setting value
- K e * is the induced voltage coefficient setting value
- P m is the number of pole pairs.
- the field-weakening control calculation unit 9 calculates a d-axis current command value i d * according to the following equation (4) by integral control so that a modulation factor K h described later does not exceed a modulation factor limit value K h * .
- K p_id is a proportional gain of the field-weakening control
- K i_id is an integral gain of the field-weakening control
- the vector control calculation unit 8 uses the electrical parameters of the permanent magnet motor 1, namely the winding resistance set value R * , the d-axis inductance set value Ld * , the q-axis inductance set value Lq * , the induced voltage coefficient set value Ke * , the dc - axis and qc- axis current command values id * , iq *, and the speed detection value ⁇ rc , to output the dc - axis and qc- axis voltage reference values vdc * , vqc * in accordance with the following equation (5).
- T acr is the response time constant of the current control.
- the voltage correction values ⁇ v dc , ⁇ v qc for the dc axis and qc axis are calculated according to the following equation (6) using proportional control and integral control so that the current detection values i dc , i qc of each component follow the current command values i d * , i q * for the dc axis and qc axis.
- K pd is the proportional gain of the dc axis current control
- K id is the integral gain of the dc axis current control
- K pq is the proportional gain of the qc axis current control
- K iq is the integral gain of the qc axis current control.
- FIG. 2 shows the configuration of the speed command correction calculation unit 11, which is a feature of the first embodiment of the present invention.
- Reference numeral 11_1 denotes a setting unit for a current limit value imax for controlling the permanent magnet motor 1 or the power converter 2 at or below an overcurrent value.
- the current limit value imax is set according to the following equation (8) so as to be equal to or less than the overcurrent level value ioc_lvl of the power converter 2.
- the primary current calculation unit 11_2 calculates a primary current command value i c * by using the d-axis and q-axis current command values i d * , i q * according to the following equation (9).
- the d-axis and q-axis current detection values i dc , i qc of the current command values i d * , i q * may be used to calculate the primary current detection value i c and use it instead of the primary current command value i c * .
- Reference numeral 11_3 denotes a setting section for setting the limit value Pmax of the power of the permanent magnet motor 1 or the power converter 2, and a value at which the permanent magnet motor 1 can be operated may be set.
- the power calculation unit 11_4 uses the detected speed value ⁇ rc and the torque command value ⁇ * to calculate a calculated power value P according to the following equation (10).
- Reference numeral 11_5 denotes a power/current control calculation unit, which inputs the current limit value i max * , primary current command value i c * , power limit value P max * , and power calculation value P, and calculates a correction value ⁇ r * of the speed command value by the following procedure.
- a power correction value ⁇ P max is calculated according to the following equation (11) by proportional and integral calculations so that the primary current command value i c * is equal to or smaller than the current limit value i max * .
- K p_acr is a proportional gain of the command value control of the primary current
- K i_acr is an integral gain of the command value control of the primary current
- a new power limit value P max ** is calculated using the power limit value P max * and the power correction value ⁇ P max according to the following equation (12).
- a correction value ⁇ r * of the speed command value is calculated according to the following equation (13) by proportional and integral calculations so that the calculated power value P becomes equal to or smaller than the new power limit value P max ** .
- K p — ⁇ w is a proportional gain of the power limit value control
- K i — ⁇ w is an integral gain of the power limit value control
- a new speed command value ⁇ r ** is calculated according to the following equation (14) using the speed command value ⁇ r * and the speed command value correction value ⁇ r * .
- Figure 3 shows the control characteristics when a large load torque is applied without using the speed command correction calculation unit 11 according to the present invention. This is the result of a simulation in which the speed command value is increased from zero to the base speed and a load torque is applied.
- the upper part displays the detected speed value ⁇ rc and the calculated power value P of the permanent magnet motor 1
- the lower part displays the detected value i c of the primary current calculated according to the following equation (15).
- the speed command value ⁇ r * is increased from zero to the base speed from time A to B, and a large load torque is applied from time C to D.
- the detected speed value ⁇ rc is decelerated so that the calculated power value P becomes equal to or less than the power limit value Pmax * , but at time F, the detected primary current value ioc increases to the overcurrent level value ioc_lvl , making it impossible to operate the motor from this point on.
- FIG. 4 shows the control characteristics using the speed command correction calculation unit 11 according to the present invention.
- the control characteristics shown in FIG. 4 are the same simulation results as the example shown in FIG. 3.
- the primary current command value i max * is set to a value lower than the overcurrent level value i oc_lvl , and at time F the new power command value P max ** is corrected by the power command value P max * .
- the primary current detection value i c is also controlled by i max * , thereby preventing an overcurrent and enabling stable operation.
- a current detector 21 is attached to the power conversion device 20 that drives the permanent magnet motor 1, and an encoder 22 is attached to the shaft of the permanent magnet motor 1.
- a speed command value ⁇ r * given to a controller (not shown) of the power converter 2 is set to the base speed, and a large torque is applied to the permanent magnet motor 1 .
- the speed and vector current component calculation unit 23 receives the three-phase AC current detection values ( iuc , ivc , iwc ) and the position detection value ⁇ , which is the output of the encoder 22, and calculates the vector current component detection values idcc , iqcc using the following equation (16), the primary current detection value icc using the following equation (17), and the speed detection value ⁇ rcc using the following equation (18).
- a torque estimate value t ⁇ is calculated by the following equation (19) using the electrical parameters (K e * , L d * , L q * ) of the permanent magnet motor 1 and the detected values i dcc and i qcc of the vector current components.
- the detected speed value ⁇ rcc and the estimated torque value t ⁇ are used to calculate the estimated power value P ⁇ according to the following equation (20).
- the first embodiment of the present invention is configured as described above, it is possible to provide a power conversion device 100 that can operate stably without reaching an overcurrent when a load torque greater than the torque value of the permanent magnet motor 1, which changes depending on the DC voltage of the power converter 2, is applied in the constant output region of the weak field region.
- FIG. 6 is a schematic diagram of a power conversion device 100 according to the second embodiment.
- the speed detection value w rc and the torque command value ⁇ * are input to the speed command correction calculation unit 11.
- a DC voltage value E DC and a DC current value I DC are input instead of the speed detection value w rc and the torque command value ⁇ * .
- Reference numerals 1, 2, 5 to 10, and 12 in Fig. 6 denote the same components as those in Fig. 1.
- Reference numeral 13 denotes a current detector for detecting a DC current I DC
- reference numeral 14 denotes a voltage detector for detecting a DC voltage E DC .
- the detected DC current value is IDC
- the detected DC voltage value is EDC .
- FIG. 7 shows the configuration of the speed command correction calculation unit 11a in the second embodiment.
- the reference characters 11a_1, 11a_2, 11a_3, and 11a_5 in FIG. 7 are the same components as the reference characters 11_1, 11_2, 11_3, and 11_5 in FIG. 2.
- Reference numeral 11a_4 denotes a power calculation section which calculates a power calculation value P ⁇ according to the following equation (21) using a detected DC current value I DCc and a detected DC voltage value E DCc .
- the power/current control calculation unit 11a_5 replaces the power calculation value P ⁇ with the power calculation value P to calculate a correction value ⁇ r * of the speed command value.
- Example 2 the same effect as in Example 1 can be obtained.
- FIG. 8 is a configuration diagram of a power conversion device 100 according to the third embodiment.
- the speed detection value w rc and the torque command value ⁇ * are input to the speed command correction calculation unit 11.
- the d-axis and q-axis voltage command values v dc ** , v qc ** are input instead of the speed detection value w rc and the torque command value ⁇ * .
- Figure 9 shows the configuration of speed command correction calculation unit 11b in Example 3.
- Reference numerals 11b_1, 11b_2, 11b_3, and 11b_5 in Figure 9 are the same components as reference numerals 11_1, 11_2, 11_3, and 11_5 in Figure 2.
- Reference numeral 11b_4 is a power calculation unit, which calculates a power calculation value P ⁇ using d-axis and q-axis current command values id * , iq * , voltage command values vdc ** , vqc ** , and a resistance setting value R *, which is an electrical parameter of permanent magnet motor 1, according to the following equation (22).
- the power/current control calculation unit 11b_5 may replace the power calculation value P ⁇ with the power calculation value P to calculate the correction value ⁇ r * of the speed command value.
- stable control characteristics can be achieved similar to those of the first embodiment, even when using the power calculation value of vector control.
- the third embodiment has the advantage that it can be replaced with parts configured using software.
- FIG. 10 is a configuration diagram of a power conversion device 100 according to the fourth embodiment.
- the fourth embodiment is a method for correcting a parameter (power limit value) set in the speed command correction calculation unit 11c with a new speed command value ⁇ r ** (corrected speed command value).
- Reference numerals 1 to 10 and 12 in Fig. 10 indicate the same components as those in Fig. 1.
- Fig. 11 shows the configuration of the speed command correction calculation unit 11c.
- Reference numerals 11c_1, 11c_2, 11b_4 and 11b_5 in Fig. 11 indicate the same components as those in Fig. 2 indicated by reference numerals 11_1, 11_2, 11_4 and 11_5.
- Reference numeral 11c_3 indicates a setting unit for the power limit value P max * .
- the power limit value P max * was a fixed value regardless of the magnitude of the new speed command value ⁇ r ** , but the power limit value P max * may be rewritten according to the speed command value ⁇ r ** .
- it may be a look-up table that outputs the power limit value P max * according to the magnitude of the speed command value ⁇ r ** .
- the fourth embodiment optimizes the power limit value Pmax * in accordance with the operating state, so that the detected value iC of the primary current does not become larger than necessary, the current value is reduced, and more efficient and stable control characteristics can be achieved.
- FIG. 12 is a configuration diagram of a power conversion device 100 according to a fifth embodiment.
- the current command values i d * and i q * of the d-axis and q-axis of the rotating coordinate system are input to the speed command correction calculation unit 11, but in embodiment 5, the detection value i c1 of the primary current in the stationary coordinate system (the current value calculated from the detection value of the current input to the permanent magnet motor 1) is input.
- Reference numerals 1 to 5, 7 to 10, and 12 in Fig. 12 denote the same components as those in Fig. 1.
- Reference numeral 6a denotes a coordinate conversion unit that calculates the current detection values i dc and i qc of the dc and qc axes and the primary current detection value i c1 .
- the coordinate conversion unit 6a calculates the primary current detection value i c1 according to the following equation (23).
- Fig. 13 shows the configuration of the speed command correction calculation unit 11d.
- Reference numerals 11d_1, 11d_3, 11d_4, and 11d_5 in Fig. 13 are the same components as reference numerals 11_1, 11_3, 11_4, and 11_5 in Fig. 2.
- the detected value i c1 of the primary current may be replaced with the detected value i c to calculate a correction value ⁇ r * of the speed command value in 11d_5.
- the same effect as in the first embodiment can be obtained, and in addition, the primary current calculation unit 11_2 in the first embodiment can be omitted, and stable control characteristics can be achieved with fewer control calculations.
- the speed command correction calculation unit 11d of Example 5 omits the primary current calculation unit 11_2 of the speed command correction calculation unit 11 of Example 1 and inputs the detected value i c1 of the primary current, but it is also possible to omit the speed command correction calculation units 11a_2, 11b_2, and 11c_2 of Examples 2 to 4 and input the detected value i c1 of the primary current.
- FIG. 14 is a configuration diagram of a power conversion device 100 according to a sixth embodiment.
- a position detector 5 is attached to the permanent magnet motor 1, but in this embodiment 6, the position detector 5 is omitted.
- Reference numerals 1 to 4 and 6 to 12 in Fig. 14 denote the same components as those in Fig. 1.
- Reference numeral 15 receives as input the voltage command values vdc ** , vqc ** of the dc axis and qc axis of the power converter 2 and the detected current values idc , iqc , and outputs a speed estimate value ⁇ rc and a position estimate value ⁇ dc based on these.
- the frequency and phase estimation/subtraction unit 15 estimates the phase error ⁇ , which is the phase difference between the dq axes, which are the rotating coordinate system of the permanent magnet motor 1 and based on the magnetic flux, and the dc - qc axes, which are based on the control, using the following equation (24).
- the speed estimate ⁇ rc of the permanent magnet motor 1 is calculated according to the following equation (25) using P (proportional) + I (integral) control, and the phase estimate ⁇ dc is calculated according to the following equation (26) using I (integral) control.
- K p_pll is the proportional gain of the PLL control
- K i_pll is the integral gain of the PLL control
- the same effect as in the first embodiment can be obtained, and in addition, the position detector 5 in the first embodiment can be omitted, which has the effect of realizing inexpensive and highly stable control characteristics.
- Example 6 can also be applied to Examples 1 to 5.
- Example 7 Next, a seventh embodiment of the present invention will be described.
- FIG. 15 is a configuration diagram of a power conversion device 100 according to a seventh embodiment.
- the power limit value P max * and the primary current limit value i max * are set in the controller (such as a microcomputer) of the power converter 2, and the power limit value P max ** is calculated.
- the state quantity of the control is fed back to the upper IOT controller 16, and machine learning such as deep learning is performed to reset the above-mentioned power limit value P max * and primary current limit value i max * in the speed command correction calculation unit 11 d.
- the reference numbers 1 to 12 in FIG. 15 indicate the same components as in FIG. 1.
- the voltage command values vdc * , vdc * to the power converter 2, the detected current values idc , iqc input to the permanent magnet motor 1, and the estimated phase error and speed are fed back to an IOT controller 16, which is a higher-level device, for analysis, and parameters related to the predetermined value for the power limit value or the predetermined current value are automatically corrected.
- the power conversion device 100 is equipped with an IOT controller 16 that feeds back and analyzes the voltage command values vdc * , vqc * to the power converter 2, the detected current values idc , iqc input to the permanent magnet motor 1, and the phase error and speed estimated values of the permanent magnet motor 1, and automatically corrects the parameters related to the power limit value or the parameters related to the current.
- Example 7 the same effect as in Example 1 can be obtained.
- feedback is given to the IOT controller 16, and machine learning such as deep learning is performed to reset the above-mentioned power limit value P max * and primary current limit value i max * in the speed command correction calculation unit 11d, so that more stable and efficient control characteristics can be realized without adjustment.
- Example 7 can also be applied to Examples 2 to 6.
- FIG. 16 is a configuration diagram of a power conversion device 100 according to Example 8.
- Example 8 the present invention is applied to a permanent magnet motor drive system.
- the system is equipped with the components indicated by the reference numerals 1 to 12 shown in FIG. 1.
- the permanent magnet motor 1 which has the same components as those shown in FIG. 1, is driven by a power conversion unit 20.
- the power conversion unit 20 is a microcomputer, and the components indicated by reference numerals 6 to 12 in FIG. 1 are software 20a, and the components indicated by reference numerals 2 to 5 in FIG. 1 are implemented as hardware.
- the "power limit value P max * " 30 and the "primary current limit value i max * " 31 of the software 20a can be set or changed by a higher-level device such as the digital operator 20b, the personal computer 32, the tablet 33, or the smartphone 34.
- a higher-level device such as the digital operator 20b, the personal computer 32, the tablet 33, or the smartphone 34.
- the parameters set in the power conversion unit 20 can be set or changed via the digital operator, the personal computer 32, the tablet 33, or the smartphone 34.
- the "power limit value P max * " 30 and the "primary current limit value i max * " 31 may be set on a field bus such as a programmable logic controller, a local area network connected to a computer, or an IOT controller.
- Example 8 an example is shown in which it is applied to Example 1, but it can also be applied to Examples 2 to 7.
- the voltage correction values ⁇ vdc , ⁇ vqc are created from the current command values id * , iq * and the current detection values idc , iqc , and the calculation shown in (equation (7)) is performed in which these voltage correction values ⁇ vdc , ⁇ vqc are added to the voltage reference value for vector control.
- K pd1 is the proportional gain of current control on the dc axis
- K id1 is the integral gain of current control on the dc axis
- K pq1 is the proportional gain of current control on the qc axis
- K iq1 is the integral gain of current control on the qc axis
- T d is the electrical time constant of the d axis (L d /R)
- T q is the electrical time constant of the q axis (L q /R).
- the voltage correction value ⁇ v d_p * of the proportional calculation component on the dc axis, the voltage correction value ⁇ v d_i * of the integral calculation component on the dc axis , the voltage correction value ⁇ v q_p * of the proportional calculation component on the qc axis, and the voltage correction value ⁇ v q_i * of the integral calculation component on the qc axis used for the vector control calculation can be created from the current command values i d*, i q * and the current detection values i dc, i qc according to the following equation (29), and the vector control calculation shown in the following equation (30) can be performed using the speed detection value or speed estimate value ⁇ rc and the electrical circuit parameters of the permanent magnet motor 1.
- K pd2 is the proportional gain of the dc axis current control
- K id2 is the integral gain of the dc axis current control
- K pq2 is the proportional gain of the qc axis current control
- K iq2 is the integral gain of the qc axis current control.
- a vector control calculation shown in the following equation (31) may be performed using the first-order lag signal iqctd of the dc - axis current command value id * and the qc- axis current detection value iqc , the speed estimation value ⁇ rc , and the electrical circuit parameters of the permanent magnet motor 1.
- the switching elements constituting the power converter 2 may be Si (silicon) semiconductor elements or wide band gap semiconductor elements such as SiC (silicon carbide) and GaN (gallium nitride).
- Example 8 the same effects as in Example 1 can be obtained. Furthermore, in Example 8, if it is applied to an AC servo or inverter driven by a permanent magnet motor 1, highly stable and highly efficient control characteristics can be realized even in vector control with or without a position detector 5.
- FIG. 17 is a configuration diagram of a power conversion device 100 according to a ninth embodiment.
- the ninth embodiment is a method in which the parameters set in the speed command correction calculation unit 11e are corrected by the DC voltage detection value E - - DCC .
- Reference numerals 1 to 10 and 12 in Fig. 17 are the same components as those in Fig. 1, and reference numeral 14 is a voltage detector for detecting a DC voltage Edc.
- the detected voltage value of the DC voltage is represented as E DCc .
- Figure 18 shows the configuration of the speed command correction calculation unit 11e.
- Reference numerals 11e_1, 11e_2, 11e_4, and 11e_5 in Figure 18 are the same components as reference numerals 11_1, 11_2, 11_4, and 11_5 in Figure 2.
- Reference numeral 11e_3 in Figure 18 is a setting unit for the power limit value P max * .
- the limit value Pmax * is a fixed value regardless of the magnitude of the detected DC voltage value EDCc , but the power limit value Pmax * may be modified (rewritten) according to the detected value EDCc , or may be a look-up table that outputs the limit value Pmax * according to the magnitude of the detected value EDCc .
- the power limit value P max * is optimized according to the operating state, so that the detected value i c of the primary current does not become larger than necessary, the current value is reduced, and highly efficient and stable control characteristics can be realized.
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Abstract
Description
図1は、実施例1に係る電力変換装置100の概略構成図である。
次に、本発明の実施例2について説明する。
次に、本発明の実施例3について説明する。
次に、本発明の実施例4について説明する。
次に、本発明の実施例5について説明する。
次に、本発明の実施例6について説明する。
次に、本発明の実施例7について説明する。
次に、本発明の実施例8について説明する。
次に、本発明の実施例9について説明する。
Claims (11)
- 永久磁石モータと、
前記永久磁石モータに電力を供給する電力変換器と、
速度情報と、トルク指令値と、一次電流と、に基づき、速度指令値を補正する速度指令補正演算部と、
を備え、
前記速度指令補正演算部は、前記電力変換器の直流電圧により変化する前記永久磁石モータのトルク値よりも大きな負荷トルクが印加された場合、前記永久磁石モータの電流値を所定の制限値以下に制限するように前記電力の制限値を演算し、前記電力が、前記電力の制限値まで増加しないように前記速度指令値を補正することを特徴とする電力変換装置。 - 請求項1に記載の電力変換装置において、
前記速度指令補正演算部は、
前記トルク指令値と前記速度情報により演算した電力が、前記電力の制限値まで増加しないように前記速度指令値を補正することを特徴とする電力変換装置。 - 請求項1に記載の電力変換装置において、
前記速度指令補正演算部は、
前記電力変換器の直流電圧値および直流電流値により演算した電力が、前記電力の制限値まで増加しないように前記速度指令値を補正することを特徴とする電力変換装置。 - 請求項1に記載の電力変換装置において、
前記速度指令補正演算部は、
前記永久磁石モータのd-q軸上の電圧値および電流値により演算した電力が、前記電力の制限値まで増加しないように前記速度指令値を補正することを特徴とする電力変換装置。 - 請求項2から4のうちのいずれか一項に記載の電力変換装置において、
前記一次電流は、前記永久磁石モータに入力される電流の検出値から算出した電流であることを特徴とする電力変換装置。 - 請求項2から4のうちのいずれか一項に記載の電力変換装置において、
前記電力の制限値は、補正された前記速度指令値で修正されることを特徴とする電力変換装置。 - 請求項2から4のうちのいずれか一項に記載の電力変換装置において、
前記永久磁石モータの位置を検出する位置検出器と、前記位置検出器により検出された前記永久磁石モータの位置に基づいて、前記永久磁石モータの速度を演算する周波数および位相の検出演算部と、を備えることを特徴とする電力変換装置。 - 請求項2から4のうちのいずれか一項に記載の電力変換装置において、
前記電力変換器の電圧指令値および電流検出値に基づいて、前記永久磁石モータの位置および速度を推定する周波数および位相の推定演算部を備えることを特徴とする電力変換装置。 - 請求項2から4のうちのいずれか一項に記載の電力変換装置において、
前記電力変換器への電圧指令値vdc *および前記永久磁石モータに入力される電流検出値と、前記永久磁石モータの位相誤差および速度推定値を、フィードバックして解析し、前記電力の制限値に関するパラメータを自動修正するIOTコントローラを備えることを特徴とする電力変換装置。 - 請求項2から4のうちのいずれか一項に記載の電力変換装置において、
前記電力の制限値に関するパラメータまたは前記永久磁石モータの電流に関するパラメータが設定された電力変換部を備え、デジタル・オペレータ、パーソナル・コンピュータ、タブレットまたはスマートフォンを介して、前記電力変換部に設定された前記パラメータを設定または変更されることを特徴とする電力変換装置。 - 請求項2に記載の電力変換装置において、
前記電力変換器の直流電圧を検出する電圧検出器を備え、
前記電力の制限値は、前記電圧検出器が検出した前記直流電圧に従って修正されることを特徴とする電力変換装置。
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006191721A (ja) | 2005-01-05 | 2006-07-20 | Yaskawa Electric Corp | モータ制御装置とその制御方法 |
| WO2010013534A1 (ja) * | 2008-07-31 | 2010-02-04 | アイシン・エィ・ダブリュ株式会社 | 回転電機制御システム及び当該回転電機制御システムを備えた車両駆動システム |
| WO2013108356A1 (ja) * | 2012-01-16 | 2013-07-25 | 三菱電機株式会社 | モータ制御装置 |
| WO2015156003A1 (ja) * | 2014-04-08 | 2015-10-15 | 株式会社日立産機システム | ベクトル制御装置、それを組み込んだインバータ及びそれを組み込んだインバータとモータとのセット装置 |
| WO2022054357A1 (ja) * | 2020-09-09 | 2022-03-17 | 株式会社日立産機システム | 電力変換装置 |
| WO2023276181A1 (ja) * | 2021-06-29 | 2023-01-05 | 株式会社日立産機システム | 電力変換装置 |
-
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- 2023-10-04 CN CN202380092971.0A patent/CN120642203A/zh active Pending
- 2023-10-04 WO PCT/JP2023/036163 patent/WO2024224659A1/ja active Pending
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Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006191721A (ja) | 2005-01-05 | 2006-07-20 | Yaskawa Electric Corp | モータ制御装置とその制御方法 |
| WO2010013534A1 (ja) * | 2008-07-31 | 2010-02-04 | アイシン・エィ・ダブリュ株式会社 | 回転電機制御システム及び当該回転電機制御システムを備えた車両駆動システム |
| WO2013108356A1 (ja) * | 2012-01-16 | 2013-07-25 | 三菱電機株式会社 | モータ制御装置 |
| WO2015156003A1 (ja) * | 2014-04-08 | 2015-10-15 | 株式会社日立産機システム | ベクトル制御装置、それを組み込んだインバータ及びそれを組み込んだインバータとモータとのセット装置 |
| WO2022054357A1 (ja) * | 2020-09-09 | 2022-03-17 | 株式会社日立産機システム | 電力変換装置 |
| WO2023276181A1 (ja) * | 2021-06-29 | 2023-01-05 | 株式会社日立産機システム | 電力変換装置 |
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| TW202444030A (zh) | 2024-11-01 |
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