POWER CONVERSION APPARATUS

Abstract

A power conversion apparatus controls a load apparatus by position sensorless vector control. The power conversion apparatus includes: a current detection unit configured to detect a current passing through the load apparatus; a current detection arithmetic unit configured to calculate a harmonic current component on a dc-axis as a control axis and a harmonic current component on a qc-axis, based on the detected current; a saliency ratio estimation unit configured to output a saliency ratio estimated value based on the harmonic current component on the dc-axis and the harmonic current component on the qc-axis; and a saliency ratio control unit configured to output a current component that increases or decreases a current command value on a d-axis of a rotor coordinate system, based on a deviation between the saliency ratio estimated value and a predetermined saliency ratio.

Description

TECHNICAL FIELD

The present invention relates to a power conversion apparatus, and particularly relates to a power conversion apparatus that enables position sensorless control.

BACKGROUND ART

Examples of a known magnet motor include a surface permanent magnet (SPM) motor in which a permanent magnet is disposed on a surface of a rotor, and an interior permanent magnet (IPM) motor in which a permanent magnet is embedded in a rotor.

Typically, in an SPM motor, since a magnetic resistance is irrelevant to the position of a rotor, a ratio between a d-axis inductance L_d and a q-axis inductance L_q (hereinafter, this ratio L_q/L_d is referred to as a saliency ratio) is approximately 1. Meanwhile, in an IPM motor, a current magnetic flux in a d-axis direction is hard to pass due to the presence of a permanent magnet having a larger magnetic resistance, and a current magnetic flux in a q-axis direction passes through a core of a rotor having a smaller magnetic resistance. As a result, a saliency ratio is equal to or more than 1.

In view of this circumstance, heretofore, position sensorless control by a harmonic superposition method has been applied only to specially designed IPM motors.

PTL 1 discloses a technique premised on an IPM motor. According to this technique, an alternating-current amplitude of a three-phase harmonic current amplitude is obtained by an arithmetic operation, and a ratio between a maximum value and a minimum value of the harmonic current amplitude is estimated as a saliency ratio. According to the technique disclosed in PTL 1, a limit value of a current command as an output from a speed control system is set for preventing the estimated value of the saliency ratio from falling below a predetermined value.

CITATION LIST

Patent Literature

PTL 1: WO 2015/190150 A1

SUMMARY OF INVENTION

Technical Problem

According to the technique disclosed in PTL 1, the limit value of the current command value is set for preventing step-out to be caused since a saliency ratio of a magnet motor approaches 1 when a rotor receives a lowered current.

In the related art, however, lowering a total current including an id current and an iq current prevents an estimated value of a saliency ratio from falling below a predetermined value. It is therefore difficult to enable position sensorless control for stably driving an IPM motor even at a higher torque. It is also difficult to enable position sensorless control for stably driving an SPM motor even at a higher torque.

An object of the present invention is to provide a power conversion apparatus that enables stable position sensorless control even at a higher torque.

Solution to Problem

A preferred example of the present invention is directed to a power conversion apparatus for controlling a load apparatus by position sensorless control, the power conversion apparatus including: a current detection unit configured to detect a current passing through the load apparatus; a current detection arithmetic unit configured to calculate a harmonic current component on a dc-axis as a control axis and a harmonic current component on a qc-axis, based on the detected current; a saliency ratio estimation unit configured to output a saliency ratio estimated value based on the harmonic current component on the dc-axis and the harmonic current component on the qc-axis; and a saliency ratio control unit configured to output a current component that increases or decreases a current command value on a d-axis of a rotor coordinate system, based on a deviation between the saliency ratio estimated value and a predetermined saliency ratio.

Advantageous Effects of Invention

The present invention embodies a power conversion apparatus that enables stable position sensorless control even at a higher torque.

BRIEF DESCRIPTION OF DRAWINGS

FIG. 1 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 1.

FIG. 2 illustrates characteristics of a torque and a phase error in a comparative example.

FIG. 3 illustrates a configuration of a current detection arithmetic unit in Embodiment 1.

FIG. 4 illustrates a configuration of a saliency ratio estimation unit in Embodiment 1.

FIG. 5 illustrates a configuration of a saliency ratio control unit in Embodiment 1.

FIG. 6 illustrates characteristics of a torque and a phase error in Embodiment 1.

FIG. 7 illustrates a verification method adopting Embodiment 1.

FIG. 8 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 2.

FIG. 9 illustrates a configuration of a saliency ratio estimation unit in Embodiment 2.

FIG. 10 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 3.

FIG. 11 illustrates a configuration of a saliency ratio estimation unit 82 in Embodiment 3.

FIG. 12 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 4.

FIG. 13 illustrates a configuration of a saliency ratio control unit 91 in Embodiment 4.

FIG. 14 illustrates a configuration of a system including a power conversion apparatus, a magnet motor, and the like in Embodiment 5.

FIG. 15 illustrates a configuration of a saliency ratio control unit 92 in Embodiment 5.

FIG. 16 illustrates a configuration of a system including a power converter and a magnet motor in Embodiment 6.

DESCRIPTION OF EMBODIMENTS

Embodiments will be described in detail below with reference to the drawings.

Embodiment 1

FIG. 1 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 1. A magnet motor 1 outputs a motor torque as a combination of a torque component from a magnetic flux of a permanent magnet with a torque component from an inductance of an armature coil.

A power converter 2 includes a semiconductor element as a switching element. The power converter 2 receives three-phase alternating-current voltage command values v_u*, v_v, and v_w*, and prepares gate signal (ON, OFF) voltages proportional to the voltage command values v_u*, v_v*, and v_w*. In a case where the power converter 2 includes an insulated gate bipolar transistor (IGBT) as a switching element, the IGBT performs a switching operation based on a gate signal. The power converter 2 also outputs a direct-current voltage E_dc as an output from a direct-current voltage source 2a in addition to the voltages proportional to the three-phase alternating-current voltage command values v_u*, v_v*, and v_w* to make an output voltage and a rotation speed of the magnet motor 1 variable.

A current detector 3 detects three-phase alternating currents i_u, i_v, and i_w passing through the magnet motor 1. With regard to three-phase currents passing through the magnet motor 1, for example, a u-phase current and a w-phase current may be detected first, and then a v-phase current may be obtained from i_v=−(i_u+i_w) based on the alternating current condition (i_u+i_v+i_w=0). In Embodiment 1, the current detector 3 is provided inside the power conversion apparatus. Alternatively, the current detector 3 may be provided outside the power conversion apparatus.

Next, a description will be given of constituent elements of a control unit configured to control the power converter. A coordinate conversion unit 4 outputs a current detected value i_dc on a dc-axis and a current detected value i_qc on a qc-axis, based on detected values i_uc, i_vc, and i_wc of the three-phase alternating currents i_u, i_v, and i_w with respect to a position estimated value θ_dc.

In the following, a description will be given of a rotor coordinate system, a control axis, and others. A dq-axis coordinate system defined with a d-axis and a q-axis is a rotor coordinate system for expressing a magnetic pole position of a rotor. The dq-axis coordinate system rotates in synchronization with a rotor of the magnet motor 1 which is an exemplary load apparatus. In a case where the magnet motor 1 is a permanent magnet synchronous electric motor, the d-axis is typically defined with respect to a phase of a permanent magnet attached to a rotor. The d-axis is also called a magnetic pole axis, and the q-axis is also called a torque axis. A dc-axis and a qc-axis each represent an estimated phase of a magnetic pole position. In other words, the dc-axis and the qc-axis respectively represent a direction along the d-axis and a direction along the q-axis assumed on control by a control unit such as a current detection arithmetic unit 5. The dc-axis is also called a control axis. A dc-qc-axis coordinate system is defined with the dc-axis and the qc-axis perpendicular to the dc-axis.

The current detection arithmetic unit 5 outputs an amplitude value Δi_{dc_ver} of a harmonic current on the dc-axis and an average value i_{dc_ver}, based on a current detected value i_dc on the dc-axis. The current detection arithmetic unit 5 also outputs an amplitude value Δi_{qc_ver} on the qc-axis and an average value i_{qc_ver}, based on a current detected value i_qc on the qc-axis.

A phase error estimation unit 6 outputs a phase error estimated value Δθ_c based on the current detected value i_dc on the dc-axis and the current detected value i_qc on the qc-axis.

A position and speed estimation unit 7 outputs a speed estimated value ω_rc{circumflex over ( )} and a position estimated value θ_dc based on the phase error estimated value Δθ_c.

A saliency ratio estimation unit 8 outputs a saliency ratio estimated value L_dq{circumflex over ( )} based on the amplitude value Δi_{dc_ver} of the harmonic current on the dc-axis and the amplitude value Δi_{qc_ver} of the harmonic current on the qc-axis.

A saliency ratio control unit 9 outputs a corrected value Δi_d* of the direct-current component on the d-axis based on the saliency ratio estimated value L_dq{circumflex over ( )}.

An addition unit 10 adds a current command i_d* on the d-axis to the corrected value Δi_d* of the direct-current component on the d-axis, and outputs a second current command i_d** on the d-axis.

A vector control arithmetic unit 11 outputs a voltage command v_dc* on the dc-axis and a voltage command v_qc* on the qc-axis, based on a deviation between the second current command i_d** on the d-axis and the average value i_{dc_ver}, a deviation between the current command i_q* on the q-axis and the average value i_{qc_ver}, electric constants of the magnet motor 1, and the speed estimated value ω_rc{circumflex over ( )}.

A harmonic voltage generation unit 12 sets a peak value and a frequency for a harmonic voltage, and outputs a harmonic voltage Δv_dc* on the dc-axis and a harmonic voltage Δv_qc* on the qc-axis.

With respect to the position estimated value θ_dc, a coordinate conversion unit 13 outputs three-phase alternating-current voltage commands v_u*, v_v*, and v_w* to the power converter, based on a value v_dc** obtained by adding the voltage command v_dc* to the harmonic voltage Δv_dc* and a value v_qc** obtained by adding the voltage command v_qc* to the harmonic voltage Δv_qc.

Next, a description will be given of a principle of a harmonic superposition method. First, a description will be given of basic operations of voltage control and phase control by vector control.

According to the basic operation of the voltage control, the vector control arithmetic unit 11 calculates a proportional-integral (PI) control output Δv_{dc_pi} for d-axis current control, an integral (I) control output Δv_{dc_i} for d-axis current control, a PI control output Δv_{qc_pi} for q-axis current control, and an I control output Δv_{qc_i} for q-axis current control, based on the deviation between the second current command i_d** on the d-axis and the average value i_{dc_ver} and the deviation between the current command i_q* on the q-axis and the average value i_{qc_ver}.

The vector control arithmetic unit 11 also calculates voltage commands v_dc* and v_qc* in accordance with Equation (1), using a PI control output Δv_{dc_pi} for d-axis current control, an I control output Δv_{dc_i} for d-axis current control, a PI control output Δv_{qc_pi} for q-axis current control, and an I control output Δv_{qc_i} for q-axis current control, as outputs for dc-axis current control and outputs for qc-axis current control, the speed estimated value ω_rc{circumflex over ( )}, and the electric constants (R, L_d, L_q, K_e) of the magnet motor 1.

$\begin{array}{cc}\left[\mathrm{Formula}1\right]& \\ \begin{array}{c}{v}_{dc}^{*}=-{\omega }_{\mathrm{rc}}^{^}·\frac{L_q^{*}}{R*}·\Delta v_{\mathrm{qc\_i}}+\Delta v_{\mathrm{dc\_pi}}\\ v_{\mathrm{qc}}^{*}={\omega }_{\mathrm{rc}}^{^}·\frac{L_d^{*}}{R*}·\Delta v_{\mathrm{dc\_i}}+{\omega }_{\mathrm{rc}}^{^}·K_e^{*}+\Delta v_{\mathrm{qc\_pi}}\end{array}\}& \left(1\right)\end{array}$

The symbols in Equation (1) are defined as follows.

R: Resistance value of entire magnet motor.

L_d: d-Axis inductance value.

L_q: q-Axis inductance value.

K_e: Induced voltage coefficient.

*: Set value.

Δv_{dc_pi}: PI Control output for d-axis current control.

Δv_{dc_i}: I Control output for d-axis current control.

Δv_{qc_pi}: PI Control output for q-axis current control.

Δv_{qc_i}: I Control output for q-axis current control.

The harmonic voltage generation unit 12 outputs rectangular wave or sine wave harmonic voltages Δv_dc* and Δv_qc* each having an amplitude value V_h and a frequency f_h. The harmonic voltage generation unit 12 then calculates a value v_dc** by adding the harmonic voltage Δv_dc* to the voltage command v_dc*, and also calculates a value v_qc** by adding the harmonic voltage Δv_qc* to the voltage command v_qc*, in accordance with Equation (2). The harmonic voltage generation unit 12 thus controls the three-phase voltage commands v_u*, v_v*, and v_v* for controlling the power converter 2.

$\begin{array}{cc}\left[\mathrm{Formula}2\right]& \\ \begin{array}{c}{v}_{dc}^{**}=v_{dc}^{*}+\Delta v_{dc}^{*}\\ v_{\mathrm{qc}}^{**}=v_{\mathrm{qc}}^{*}+\Delta v_{\mathrm{qc}}^{*}\end{array}\}& \left(2\right)\end{array}$

On the other hand, the basic operation of the phase control may be any method as long as the phase error estimation unit 6 is capable of estimating a magnetic pole position. An example of such a method is described in a cited reference “Initial Rotor Position Estimation of Interior Permanent Magnet Synchronous Motor”, the transactions of the Institute of Electrical Engineers of Japan, D (publication of Industry Applications Society), vol. 123(2), pp. 140-148 (2003).

The harmonic voltage generation unit 12 respectively superposes the rectangular wave or sine wave harmonic voltages Δv_dc* and Δv_qc* each having the amplitude value V_h and the frequency f_h on the dc-axis and the qc-axis. The phase error estimation unit 6 calculates the phase error estimated value Δθ_c in accordance with Equation (3).

$\begin{array}{cc}\left[\mathrm{Formula}3\right]& \\ \Delta {\theta }_c=\frac{1}{2}{\tan }^{-1}\left[\frac{2\left\{\left(\mathrm{Ld}+\mathrm{Lq}\right){\mathrm{Vv}}_{dc}^{*}{\mathrm{Vv}}_{\mathrm{qc}}^{*}-\mathrm{Ld}·\mathrm{Lq}\left({\mathrm{Vv}}_{\mathrm{qc}}^{*}{\mathrm{Vi}}_{dc}+{\mathrm{Vv}}_{dc}^{*}{\mathrm{Vi}}_{\mathrm{qc}}\right)\right\}}{\begin{array}{c}2·\mathrm{Ld}·\mathrm{Lq}\left({\mathrm{Vv}}_{dc}^{*}{\mathrm{Vi}}_{dc}-{\mathrm{Vv}}_{\mathrm{qc}}^{*}{\mathrm{Vi}}_{\mathrm{qc}}\right)-\\ \left(\mathrm{Ld}+\mathrm{Lq}\right)\left({\mathrm{Vv}}_{dc}^{*2}-{\mathrm{Vv}}_{\mathrm{qc}}^{*2}\right)\end{array}}\right]& \left(3\right)\end{array}$

The symbols in Equation (3) are defined as follows.

L_d: d-Axis inductance value.

L_q: q-Axis inductance value.

Vv_dc*: Harmonic voltage command superposed on dc-axis.

Vv_qc*: Harmonic voltage command superposed on qc-axis.

V_idc: Harmonic current on dc-axis.

V_iqc: Harmonic current on qc-axis.

The position and speed estimation unit 7 controls the speed estimated value ω_rc{circumflex over ( )} and the position estimated value θ_dc by an arithmetic operation expressed by Equation (4) such that the phase error estimated value Δθ_c becomes “zero”.

$\begin{array}{cc}\left[\mathrm{Formula}4\right]& \\ \begin{array}{c}{\omega }_{\mathrm{rc}}^{^}=0-\Delta {\theta }_c·\left(K_p+\frac{K_i}{s}\right)\\ \theta dc=\frac{1}{s}·{\omega }_{\mathrm{rc}}^{^}\end{array}\}& \left(4\right)\end{array}$

The symbols in Equation (4) are defined as follows.

K_p: Proportional gain.

K_i: Integral gain.

s: Laplacian operator.

Next, a description will be given of control characteristics in a case where the magnet motor 1 has a saliency ratio approximate to 1, and the power conversion apparatus does not include the saliency ratio estimation unit 8 and the saliency ratio control unit 9. FIG. 2 illustrates characteristics of a torque and a phase error in a comparative example on condition that the magnet motor 1 is operated under a load.

In FIG. 2, the upper side illustrates the relationship between a torque and a time, and the lower side illustrates the relationship between a phase error and a time. A ramp-wise load torque T_L is applied to the magnet motor 1 from a point in time (A). As illustrated in the lower side of FIG. 2, the phase error Δθ is lowered by −50 degrees from the state of no load. The magnet motor 1 becomes unstable because of the phase error.

At this time, the power conversion apparatus may reach its overcurrent level to be set based on, for example, a withstand current (maximum current) of the semiconductor switching element in the power converter 2. As a result, the power conversion apparatus fails to drive the magnet motor 1. As described above, the case where the saliency ratio of the magnet motor 1 is approximate to 1 causes a problem in that overcurrent is apt to flow through the power conversion apparatus, which puts the power conversion apparatus out of action.

The use of the current detection arithmetic unit 5, saliency ratio estimation unit 8, and saliency ratio control unit 9, which are the features of Embodiment 1, solves this problem.

Next, a description will be given of control characteristics in the case of using these units. FIG. 3 illustrates a configuration of the current detection arithmetic unit 5.

The current detection arithmetic unit 5 includes a low pass filter 5a and a low pass filter 5b. The low pass filter 5a removes the harmonic current contained in the current detected value i_dc, and outputs the average value i_{dc_ver} of the current detected value. The low pass filter 5b removes the harmonic current contained in the current detected value i_qc, and outputs the average value i_{qc_ver} of the current detected value.

The current detection arithmetic unit 5 calculates the harmonic currents Δi_dc and Δi_qc in accordance with Equation (5), using the current detected values i_dc and i_qc and the average values i_{dc_ver} and i_{qc_ver} of the current detected values.

$\begin{array}{cc}\left[\mathrm{Formula}5\right]& \\ \begin{array}{c}\Delta i_{dc}=i_{dc}-i_{\mathrm{dc\_ver}}\\ \Delta i_{\mathrm{qc}}=i_{\mathrm{qc}}-i_{\mathrm{qc\_ver}}\end{array}\}& \left(5\right)\end{array}$

The current detection arithmetic unit 5 also includes a fast-Fourier-transform (FFT) arithmetic unit 5c. The FFT arithmetic unit 5c outputs the amplitude values Δi_{dc_ver} and Δi_{qc_ver} of the harmonic currents Δi_dc and Δi_qc contained in the current detected values i_dc and i_qc.

FIG. 4 illustrates a configuration of the saliency ratio estimation unit 8. The saliency ratio estimation unit 8 includes a division unit 8a. The division unit 8a outputs a ratio between the amplitude value Δi_{qc_ver} of the harmonic current and the amplitude value Δi_{dc_ver} of the harmonic current. The saliency ratio estimation unit 8 also includes a low pass filter 8b. The low pass filter 8b removes the harmonic component contained in the output from the division unit 8a, and outputs the saliency ratio estimated value L_dq{circumflex over ( )}.

FIG. 5 illustrates a configuration of the saliency ratio control unit 9. The saliency ratio control unit 9 holds a predetermined saliency ratio 9a to be set, that is, a saliency ratio L_{dq_lmt}. The saliency ratio control unit 9 includes a PI control unit 9b. The PI control unit 9b receives a deviation (L_dq{circumflex over ( )}−L_{dq_lmt}) between the predetermined saliency ratio L_{dq_lmt} and the saliency ratio estimated value L_dq{circumflex over ( )}. The PI control unit 9b then calculates and outputs the corrected value Δi_d* of the direct-current component on the d-axis such that the deviation becomes zero. The saliency ratio control unit 9 increases or decreases the d-axis current command i_d* to indirectly control the d-axis inductance. The saliency ratio control unit 9 thus increases the saliency ratio in excess of 1.0.

FIG. 6 illustrates characteristics of a torque and a phase error in Embodiment 1. The saliency ratio L_{dq_lmt} is set at 1.5 under the same condition as that illustrated in FIG. 2. As is obvious from a comparison between the torque-phase error characteristics illustrated in FIG. 2 and those illustrated in FIG. 6, controlling the saliency ratio of the magnet motor 1 effectively enables stable position sensorless control even at a high torque of 200%.

FIG. 7 illustrates a verification method adopting Embodiment 1. A current detector 20 is attached to the power conversion apparatus 22 for driving the magnet motor 1, and an encoder 21 is attached to the shaft of the magnet motor 1.

A harmonic current and saliency ratio calculation unit 23 receives three-phase alternating-current detected values (i_uc, i_vc, i_wc) from the current detector 20, and also receives a position θ from the encoder 21. The harmonic current and saliency ratio calculation unit 23 performs arithmetic operations similar to those of the current detection arithmetic unit 5 and saliency ratio estimation unit 8. The harmonic current and saliency ratio calculation unit 23 thus outputs harmonic currents Δi_dc and Δi_qc or harmonic current amplitude values Δi_{dc_ver} and Δi_{qc_ver} and also outputs a saliency ratio estimated value L_dq{circumflex over ( )}.

A waveform observation unit 24 observes the relationship between the harmonic currents Δi_dc and Δi_qc and the saliency ratio estimated value L_dq{circumflex over ( )} or the relationship between the harmonic current amplitude values Δi_{dc_ver} and Δi_{qc_ver} and the saliency ratio estimated value L_dq{circumflex over ( )}. It is obvious that the present invention is adopted when the saliency ratio estimated value L_dq{circumflex over ( )} is constant. In a case where the encoder 21 cannot be attached to the magnet motor 1, the saliency ratio may be estimated using a current ripple in a case where the three-phase alternating-current detected values (i_uc, i_vc, i_wc) are approximate to zero rather than the harmonic current Δi_dc, an amplitude value of the current ripple rather than the harmonic current amplitude value Δi_{dc_ver}, a current ripple in a case where each current detected value is approximate to its maximum value rather than the harmonic current Δi_qc, and an amplitude value of the current ripple rather than the harmonic current amplitude value Δi_{qc_ver}.

The power conversion apparatus according to Embodiment 1 adjusts the current command value on the d-axis and the current command value on the q-axis independently of each other to increase the saliency ratio of the magnet motor 1. The power conversion apparatus according to Embodiment 1 therefore stabilizes sensorless control to output a higher torque. In other words, the power conversion apparatus according to Embodiment 1 enables stable position sensorless control even at a higher torque. In addition to the IPM motor, the power conversion apparatus according to Embodiment 1 also stably drives an SPM motor having a saliency ratio which is approximately 1, within an enlarged operating range.

Embodiment 2

FIG. 8 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 2.

According to Embodiment 1, a saliency ratio estimated value is calculated from a harmonic current amplitude value. According to Embodiment 2, inductances L_d{circumflex over ( )} and L_q{circumflex over ( )} are calculated from a harmonic current amplitude value, and a saliency ratio estimated value L_dq{circumflex over ( )} is then calculated from a ratio between the inductances L_d{circumflex over ( )} and L_q{circumflex over ( )}.

The configuration illustrated in FIG. 8 is similar to that illustrated in FIG. 1 except a saliency ratio estimation unit 81; therefore, the description thereof will not be given here.

FIG. 9 illustrates a configuration of the saliency ratio estimation unit 81 in Embodiment 2.

The saliency ratio estimation unit 81 holds a constant 81a which is a harmonic voltage amplitude value V_h* and a constant 81b which is a harmonic frequency f_cc. The saliency ratio estimation unit 81 includes a division unit 81c, a division unit 81e, and a low pass filter 81f. The saliency ratio estimation unit 81 calculates an estimated value of an inductance L_d{circumflex over ( )} on a d-axis and an estimated value of an inductance L_q{circumflex over ( )} on a q-axis in accordance with Equation (6).

$\begin{array}{cc}\left[\mathrm{Formula}6\right]& \\ \begin{array}{c}{L}_d^{^}=\frac{1}{2}·\frac{V_h^{*}}{2·f_{\mathrm{cc}}}·\frac{1}{\Delta i_{\mathrm{dc\_ver}}}\\ L_q^{^}=\frac{1}{2}·\frac{V_h^{*}}{2·f_{\mathrm{cc}}}·\frac{1}{\Delta i_{\mathrm{qc\_ver}}}\end{array}\}& \left(6\right)\end{array}$

In Embodiment 2, the harmonic voltage amplitude value V_h* is equal to the amplitude value of the harmonic voltage Δv_dc* on the dc-axis and the amplitude value of the harmonic voltage Δv_qc* on the qc-axis in FIG. 1. The saliency ratio estimation unit 81 also calculates a saliency ratio estimated value L_dq{circumflex over ( )} in accordance with Equation (7).

[Formula 7]

L _dq  =L _q {circumflex over ( )}/L _d{circumflex over ( )}  (7)

This configuration has a merit of reflecting the inductance L_d  on the d-axis and the inductance L_q  on the q-axis, each of which is calculated by the arithmetic operation, on Equation (3) as the phase error estimation arithmetic formula.

Embodiment 3

FIG. 10 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 3. According to Embodiment 1, a saliency ratio estimated value is calculated from a harmonic current amplitude value. According to Embodiment 3, an inductance L_d   on a d-axis and an inductance L_q   on a q-axis are called up by table reference. The configuration illustrated in FIG. 10 is similar to that illustrated in FIG. 1 except a saliency ratio estimation unit 82; therefore, the description thereof will not be given here.

FIG. 11 illustrates the saliency ratio estimation unit 82 in Embodiment 3.

The saliency ratio estimation unit 82 includes a d-axis inductance reference table 82a and a q-axis inductance reference table 82b. The d-axis inductance reference table 82a receives a current command i_d* on the d-axis and a current command i_q* on the q-axis, and outputs an inductance L_d   on the d-axis. The q-axis inductance reference table 82b receives a current command i_d* on the d-axis and the current command i_q* on the q-axis, and outputs an inductance L_q   on the q-axis.

In Embodiment 3, the d-axis inductance reference table 82a holds the inductance L_q   on the d-axis corresponding to the current command i_d* on the d-axis. The q-axis inductance reference table 82b holds the inductance L_q   on the q-axis corresponding to the current command i_q* on the q-axis.

The d-axis inductance reference table 82a and the q-axis inductance reference table 82b may be prepared in offline auto-tuning to be executed upon start-up of a general-purpose inverter. Alternatively, data in each table may be learned during the operation by the method according to Embodiment 1 or 2, and the operation may be switched to the operation by the method according to Embodiment 3 after completion of the learning.

According to Embodiment 3, the inductance on the d-axis is calculated from the current command i_d* on the d-axis, and the inductance on the q-axis is calculated from the current command i_q* on the q-axis. Alternatively, a saliency ratio estimated value L_dq  corresponding to the current command i_d* on the d-axis and the current command i_q* on the q-axis may be obtained in advance by offline auto-tuning or learning during the operation. In other words, the saliency ratio estimated value L_dq  corresponding to the current command i_d* on the d-axis and the current command i_q* on the q-axis may be acquired based on a saliency ratio reference table holding the saliency ratio estimated value L_dq , the current command i_d* on the d-axis, and the current command i_q* on the q-axis.

This configuration produces advantageous effects similar to those described in Embodiment 1 although the method according to Embodiment 3 is implemented in an offline environment.

Embodiment 4

FIG. 12 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 4. According to Embodiment 1, a current command on the d-axis is increased or decreased such that a saliency ratio estimated value follows a predetermined saliency ratio. According to Embodiment 4, a current command on a d-axis is increased when a saliency ratio estimated value L_dq  is lower than a predetermined saliency ratio L_{dq_lmt}.

The configuration illustrated in FIG. 12 is similar to that illustrated in FIG. 1 except a saliency ratio control unit 91; therefore, the description thereof will not be given here.

FIG. 13 illustrates a configuration of the saliency ratio control unit 91 in Embodiment 4.

The saliency ratio control unit 91 holds a predetermined saliency ratio 91a to be set, that is, a saliency ratio L_{dq_lmt}. The saliency ratio control unit 91 includes a proportional-integral (PI) control unit 91b. The PI control unit 91b calculates and outputs a corrected value Δi_d* of a current command on the d-axis such that a deviation between a saliency ratio estimated value L_dq  and the saliency ratio L_{dq_lmt} becomes zero.

The saliency ratio control unit 91 also holds a predetermined limit value 91c to be set, that is, a limit value i_{d_lmt}* of a direct-current component on the d-axis. The saliency ratio control unit 91 also includes a d-axis current command limit unit 91d. The d-axis current command limit unit 91d limits the corrected value Δi_d* of the current command on the d-axis. The d-axis current command limit unit 91d has an upper limit value of i_{d_lmt}* and a lower limit value of 0. The d-axis current command limit unit 91d receives an output from the PI control unit 91b. As a result, the d-axis current command limit unit 91d outputs the corrected value Δi_d* of the current command on the d-axis, the corrected value Δi_d* taking a positive current value.

The predetermined limit value i_{d_lmt}* may be set based on, for example, a withstand current (maximum current) of a semiconductor switching element in a power converter 2.

This configuration does not require a d-axis current more than necessary at a lower torque, and therefore has a merit of improving efficiency.

Embodiment 5

FIG. 14 illustrates a configuration of a system including a power conversion apparatus, a magnet motor, and the like in Embodiment 5. According to Embodiment 1, a current command on the d-axis is increased or decreased such that a saliency ratio estimated value follows a predetermined saliency ratio. According to Embodiment 5, a phase error command is increased or decreased such that a saliency ratio estimated value follows a predetermined saliency ratio.

The configuration illustrated in FIG. 14 is similar to that illustrated in FIG. 1 except a saliency ratio control unit 92 and a position and speed estimation unit 7; therefore, the description thereof will not be given here.

FIG. 15 illustrates a configuration of the saliency ratio control unit 92 in Embodiment 5.

The saliency ratio control unit 92 holds a predetermined saliency ratio 92a to be set, that is, a saliency ratio L_{dq_lmt}. The saliency ratio control unit 92 includes a proportional-integral (PI) control unit 92b. The PI control unit 92b calculates and outputs a phase error command value Δθ_dc* in accordance with Equation (8) such that a deviation between a saliency ratio estimated value L_dq  and the saliency ratio L_{dq_lmt} becomes zero.

$\begin{array}{cc}\left[\mathrm{Formula}8\right]& \\ \Delta {\theta }_{dc}^{*}=\left(K_{p1}+\frac{K_{i1}}{s}\right)\left(L_{\mathrm{dq}}^{^}-L_{\mathrm{dq\_lmt}}\right)& \left(8\right)\end{array}$

The symbols in Equation (8) are defined as follows.

K_p1: Proportional gain.

K_i1: Integral gain.

The position and speed estimation unit 7 outputs a position estimated value θ_dc based on the phase error command value Δθ_dc* so as to eliminate a phase error estimated value Δθ_c.

The power conversion apparatus according to Embodiment 5 stably drives even a magnet motor having a smaller saliency ratio in a manner similar to that described in Embodiment 1.

Embodiment 6

FIG. 16 illustrates a configuration of a system including a power conversion apparatus and a magnet motor in Embodiment 6. Embodiment 6 is an example applied to a magnet motor drive system.

A magnet motor 1 is driven by a power conversion apparatus 16. The power conversion apparatus 16 includes software 16a and hardware. The software 16a provides various functions to be executed by a processor such as a microcomputer in the power conversion apparatus 16.

The coordinate conversion unit 4, the current detection arithmetic unit 5, the phase error estimation unit 6, the position and speed estimation unit 7, the saliency ratio estimation unit 8, the saliency ratio control unit 9, the addition unit 10, the vector control arithmetic unit 11, the harmonic voltage generation unit 12, and the coordinate conversion unit 13 illustrated in FIG. 1 constitute the software 16a illustrated in FIG. 16.

The power converter 2, the direct-current voltage source 2a, and the current detector 3 illustrated in FIG. 1 are implemented as the hardware. A digital operator 16b in the power conversion apparatus 16 or a host apparatus such as a personal computer 17, a digitizer 18 or a smartphone 19 may set a predetermined saliency ratio L_{dq_lmt} in the software 16a and a limit value i_{d_lmt}* of a direct-current component on a d-axis.

Applying Embodiment 6 to the magnet motor drive system allows even a magnet motor having a smaller saliency ratio to be stably driven. The predetermined saliency ratio L_{dq_lmt} and the limit value i_{d_lmt}* of the direct-current component on the d-axis may be set on a local area network connected to a host apparatus such as a programmable logic controller or a computer.

Embodiments 2 to 5 may be applied in place of Embodiment 1.

According to Embodiments 1 to 5, the arithmetic operation expressed by Equation (1) is performed using the current command values i_d** and i_q*, the current detected values i_dc and i_qc, and the circuit constants of the magnet motor 1. Alternatively, an arithmetic operation expressed by Equation (9) may be performed using the current command values i_d** and i_q* and the current detected values i_dc and i_qc to prepare voltage corrected values Δv_dc and Δv_qc. In addition, an arithmetic operation expressed by Equation (11) may be performed to add the voltage corrected values to a voltage reference value for vector control in Equation (10).

$\begin{array}{cc}\left[\mathrm{Formula}9\right]& \\ \begin{array}{c}\Delta v_{dc}=\left(K_{\mathrm{pd}}+\frac{K_{\mathrm{id}}}{s}\right)\left(i_d^{*}-i_{dc}\right)\\ \Delta v_{\mathrm{qc}}=\left(K_{\mathrm{pq}}+\frac{K_{\mathrm{iq}}}{s}\right)\left(i_q^{*}-i_{\mathrm{qc}}\right)\end{array}\}& \left(9\right)\end{array}$

The symbols in Equation (9) are defined as follows.

K_pd: Proportional gain for d-axis current control.

K_id: Integral gain for d-axis current control.

K_pq: Proportional gain for q-axis current control.

K_iq: Integral gain for q-axis current control.

s: Laplacian operator.

$\begin{array}{cc}\left[\mathrm{Formula}10\right]& \\ \begin{array}{c}{v}_{dc0}^{*}=R^{*}i_d^{**}-{\omega }_{\mathrm{rc}}^{^}L_q^{*}\frac{1}{1+\mathrm{Tacr}s}i_q^{*}\\ v_{\mathrm{qc}0}^{*}=R^{*}i_q^{*}+{\omega }_{\mathrm{rc}}^{^}L_q^{*}\frac{1}{1+\mathrm{Tacr}s}i_d^{**}+{\omega }_{\mathrm{rc}}^{^}K_e^{*}\end{array}\}& \left(10\right)\end{array}$

The symbols in Equation (10) are defined as follows.

v_dc0*: d-Axis voltage command.

v_qc0*: q-Axis voltage command.

Tacr: Time constant corresponding to response frequency for current control.

s: Laplacian operator.

K_e: Induced voltage coefficient.

$\begin{array}{cc}\left[\mathrm{Formula}11\right]& \\ \begin{array}{c}{v}_{dc}^{*}=v_{dc0}^{*}+\Delta v_{dc}\\ v_{\mathrm{qc}}^{*}=v_{\mathrm{qc}0}^{*}+\Delta v_{\mathrm{qc}}\end{array}\}& \left(11\right)\end{array}$

In addition, an arithmetic operation expressed by Equation (12) may be performed using the current command values i_d* and i_q* and the current detected values i_dc and i_qc to prepare intermediate current command values i_d** and i_q** for use in a vector control arithmetic operation. Moreover, an arithmetic operation expressed by Equation (13) may be performed using a speed estimated value ω_rc  and the circuit constants of the magnet motor 1.

Above Embodiments may also be applicable to a vector control method of performing an arithmetic operation expressed by Equation (14) using a current command i_d* on the d-axis, a current detected value i_qc on the qc-axis, a speed command value ω_r*, and the circuit constants of the magnet motor 1. Above Embodiments may adopt a vector control method of calculating a voltage command value V_dc* on the dc-axis and a voltage command value v_qc* on the qc-axis.

$\begin{array}{cc}\left[\mathrm{Formula}12\right]& \\ \begin{array}{c}\Delta i_d^{**}=\left(K_{\mathrm{pd}}+\frac{K_{\mathrm{id}}}{s}\right)\left(i_d^{*}-i_{dc}\right)\\ \Delta i_q^{**}=\left(K_{\mathrm{pq}}+\frac{K_{\mathrm{iq}}}{s}\right)\left(i_q^{*}-i_{\mathrm{qc}}\right)\end{array}\}& \left(12\right)\end{array}$

The symbols in Equation (12) are defined as follows.

K_pd: Proportional gain for d-axis current control.

K_id: Integral gain for d-axis current control.

K_pq: Proportional gain for q-axis current control.

K_iq: Integral gain for q-axis current control.

s: Laplacian operator.

$\begin{array}{cc}\left[\mathrm{Formula}13\right]& \\ \begin{array}{c}{v}_{dc}^{*}=R^{*}i_d^{**}-{\omega }_{\mathrm{rc}}^{^}L_q^{*}\frac{1}{1+L_q^{*}/R^{*}s}i_q^{**}\\ v_{\mathrm{qc}}^{*}=R^{*}i_q^{**}+{\omega }_{\mathrm{rc}}^{^}\left(L_d^{*}\frac{1}{1+L_q^{*}/R^{*}s}i_d^{**}+K_e^{*}\right)\end{array}\}& \left(13\right)\\ \left[\mathrm{Formula}14\right]& \\ \begin{array}{c}{v}_{dc}^{*}=R^{*}i_d^{*}-{\omega }_r^{*}L_q^{*}\frac{1}{1+T_ds}i_{\mathrm{qc}}\\ v_{\mathrm{qc}}^{*}=R_1^{*}i_q^{*}+{\omega }_r^{**}\left(L_d^{*}i_d^{*}+K_e^{*}\right)\end{array}\}& \left(14\right)\end{array}$

The symbols in Equation (14) are defined as follows.

R₁: Primary resistance of magnet motor.

Td: Delay time constant of current command i_q* on q-axis.

In Embodiments 1 to 5, the switching element of the power converter 2 may be a Si (silicon) semiconductor element. Alternatively, the switching element may be a SiC (silicon carbide) wide bandgap semiconductor element, a GaN (gallium nitride) wide bandgap semiconductor element or the like.

REFERENCE SIGNS LIST

• 1 magnet motor
• 2 power converter
• 3 current detector
• 5 current detection arithmetic unit
• 6 phase error estimation unit
• 7 position and speed estimation unit
• 8 saliency ratio estimation unit
• 9 saliency ratio control unit
• 11 vector control arithmetic unit

Claims

1. A power conversion apparatus for controlling a load apparatus by position sensorless control, the power conversion apparatus comprising:a current detection unit configured to detect a current passing through the load apparatus;a current detection arithmetic unit configured to calculate a harmonic current component on a dc-axis as a control axis and a harmonic current component on a qc-axis, based on the detected current;a saliency ratio estimation unit configured to output a saliency ratio estimated value based on the harmonic current component on the dc-axis and the harmonic current component on the qc-axis; anda saliency ratio control unit configured to output a current component that increases or decreases a current command value on a d-axis of a rotor coordinate system, based on a deviation between the saliency ratio estimated value and a predetermined saliency ratio.

2. The power conversion apparatus according to claim 1, wherein the current detection arithmetic unit outputs an amplitude value of a harmonic current on the dc-axis based on a current on the dc-axis, and outputs an amplitude value of a harmonic current on the qc-axis based on a current on the qc-axis,the saliency ratio estimation unit outputs the saliency ratio estimated value based on the amplitude value of the harmonic current on the dc-axis and the amplitude value of the harmonic current on the qc-axis, andthe saliency ratio control unit includes a proportional-integral control unit configured to perform proportional-integral control based on the deviation between the saliency ratio estimated value and the predetermined saliency ratio.

3. The power conversion apparatus according to claim 1, wherein the current detection arithmetic unit calculates an amplitude value of a harmonic current on the dc-axis based on a current component on the dc-axis, and calculates an amplitude value of a harmonic current on the qc-axis based on a current component on the qc-axis,the saliency ratio estimation unit calculates an inductance estimated value on the d-axis and an inductance estimated value on the q-axis based on the amplitude value of the harmonic current on the dc-axis and the amplitude value of the harmonic current on the qc-axis, andthe saliency ratio estimation unit outputs the saliency ratio estimated value based on the inductance estimated value on the d-axis and the inductance estimated value on the q-axis.

4. A power conversion apparatus for controlling a load apparatus by position sensorless control, the power conversion apparatus comprising:a saliency ratio estimation unit including a d-axis inductance reference table holding an inductance estimated value on a d-axis of a rotor coordinate system, the inductance estimated value corresponding to a current command on the d-axis, anda q-axis inductance reference table holding an inductance estimated value on a q-axis of the rotor coordinate system, the inductance estimated value corresponding to a current command on the q-axis,the saliency ratio estimation unit being configured to refer to the d-axis inductance reference table and the q-axis inductance reference table based on the current command on the d-axis and the current command on the q-axis to calculate an inductance estimated value on the d-axis and an inductance estimated value on the q-axis,the saliency ratio estimation unit being configured to output a saliency ratio estimated value based on the inductance estimated value on the d-axis and the inductance estimated value on the q-axis; anda saliency ratio control unit configured to output a current component that increases or decreases a current command value on the d-axis, based on a deviation between the saliency ratio estimated value and a predetermined saliency ratio.

5. A power conversion apparatus for controlling a load apparatus by position sensorless control, the power conversion apparatus comprising:a saliency ratio estimation unit including a saliency ratio reference table holding a saliency ratio estimated value corresponding to a current command on a d-axis of a rotor coordinate system and a current command on a q-axis of the rotor coordinate system,the saliency ratio estimation unit being configured to refer to the saliency ratio reference table based on the current command on the d-axis and the current command on the q-axis to output the saliency ratio estimated value; anda saliency ratio control unit configured to output a current component that increases or decreases a current command value on the d-axis, based on a deviation between the saliency ratio estimated value and a predetermined saliency ratio.

6. The power conversion apparatus according to claim 1, wherein the saliency ratio control unit includes:a proportional-integral control unit configured to perform proportional-integral control based on the deviation between the saliency ratio estimated value and the predetermined saliency ratio; anda d-axis current limit unit configured to hold a limit value of the current command value on the d-axis and to limit the current command value on the d-axis based on the limit value.

7. The power conversion apparatus according to claim 1, further comprising: an external apparatus configured to input the predetermined saliency ratio.

8. A power conversion apparatus for controlling a load apparatus by position sensorless control, the power conversion apparatus comprising:a current detection unit configured to detect a current passing through the load apparatus;a current detection arithmetic unit configured to calculate a harmonic current component on a dc-axis as a control axis and a harmonic current component on a qc-axis, based on the detected current;a saliency ratio estimation unit configured to output a saliency ratio estimated value based on the harmonic current component on the dc-axis and the harmonic current component on the qc-axis; anda saliency ratio control unit configured to output a command value of a phase error based on a deviation between the saliency ratio estimated value and a predetermined saliency ratio.

9. The power conversion apparatus according to claim 1, wherein the current detection unit detects three-phase currents,the coordinate conversion unit coordinate-converts the three-phase currents into a current detected value on the dc-axis and a current detected value on the qc-axis, andthe current detection arithmetic unit outputs an amplitude value of a harmonic current on the dc-axis and an average value based on the current detected value on the dc-axis, and also outputs an amplitude value of a harmonic current on the qc-axis and an average value based on the current detected value on the qc-axis.

10. The power conversion apparatus according to claim 1, wherein the load apparatus comprises a magnet motor, andthe magnet motor is selected from a surface permanent magnet motor in which a permanent magnet is disposed on a surface of a rotor and an interior permanent magnet motor in which a permanent magnet is embedded in a rotor.

11. The power conversion apparatus according to claim 1, further comprising: a power converter to be connected to the load apparatus; anda harmonic voltage generation unit configured to output a harmonic voltage on the dc-axis and a harmonic voltage on the qc-axis.

12. The power conversion apparatus according to claim 1, further comprising: a vector control arithmetic unit configured to output a voltage command on the dc-axis and a voltage command on the qc-axis based on a deviation between a second current command value on the d-axis, to which a current component for increasing or decreasing the current command value on the d-axis is added, and an average value of a harmonic current on the dc-axis, a deviation between a current command value on a q-axis and an average value of a harmonic current on the qc-axis, and a speed estimated value.

13. The power conversion apparatus according to claim 12, further comprising: a power converter including a switching element; anda harmonic voltage generation unit configured to generate a harmonic voltage,whereinthe power converter is controlled based on the harmonic voltage and an output from the vector control arithmetic unit.