阅读说明：本技术 控制装置和故障判定方法 (Control device and failure determination method ) 是由 早坂圭介 稻田辽一 重田哲 于 2020-04-03 设计创作，主要内容包括：本发明的控制装置在不设置直流电流传感器的情况下判定交流电流传感器的故障相。本发明的控制装置通过向电动机提供从直流转换成三相交流的电力的逆变器电路来控制所述电动机,在所述逆变器电路的输出设置有用于检测三相交流的各相的交流电流的电流传感器,所述控制装置使用用于控制所述逆变器电路的开关的PWM信号的占空比值、由所述电流传感器检测出的三相中的两相的交流电流值来计算各个推定直流电流值,并基于计算出的各个所述推定直流电流值的变化来判定所述电流传感器的故障。(The control device of the present invention determines a failure phase of an AC current sensor without providing a DC current sensor. The control device of the present invention controls a motor by an inverter circuit that supplies the motor with electric power converted from direct current to three-phase alternating current, wherein a current sensor for detecting alternating current of each phase of the three-phase alternating current is provided at an output of the inverter circuit, and calculates each estimated direct current value using a duty value of a PWM signal for controlling a switch of the inverter circuit and an alternating current value of two phases of the three phases detected by the current sensor, and determines a failure of the current sensor based on a change in the calculated each estimated direct current value.)

1. A control device for controlling an electric motor by an inverter circuit for supplying the electric motor with electric power converted from direct current to three-phase alternating current,

a current sensor for detecting an alternating current of each phase of the three-phase alternating current is provided at an output of the inverter circuit,

the control device calculates three estimated direct current values using a duty value of a PWM signal for controlling switches of the inverter circuit, and an alternating current value of two of the three phases detected by the current sensor,

and determining a failure of the current sensor based on the calculated change in each of the estimated direct current values.

2. The control device of claim 1,

when the tendency of change in one of the three estimated direct current values is different from the other estimated direct current values, a current sensor that detects an alternating current value that is not used in the calculation of the estimated direct current value having the different tendency of change is determined to be malfunctioning.

3. The control device of claim 1,

let the duty ratio of the PWM signal for the U-phase be Du, the duty ratio of the PWM signal for the V-phase be Dv, the duty ratio of the PWM signal for the W-phase be Dw, the ac current value for the U-phase be Ius, the ac current value for the V-phase be Ivs, the ac current value for the W-phase be Iws,

the control means calculates a first estimated direct current value Idce1 using Du, Dv, Dw, Ivs and Iws,

a second estimated direct current value Idce2 is calculated using Du, Dv, Dw, Iws and Ius,

the third estimated direct current value Idce3 is calculated using Du, Dv, Dw, iu and Ivs,

the fourth estimated direct current value Idce4 is calculated using Du, Dv, Dw, iu, Ivs and Iws,

the phase and the kind of fault of the current sensor at which a fault occurs are determined based on the result of comparison between the difference between the three phases and the current value Isum and a prescribed threshold value Ihys, and the values obtained by subtracting the fourth estimated direct current value Idce4 from the first estimated direct current value Idce1, the second estimated direct current value Idce2, and the third estimated direct current value Idce3, respectively.

4. The control device of claim 3,

calculating the first estimated direct current value Idce1, the second estimated direct current value Idce2, the third estimated direct current value Idce3, and the fourth estimated direct current value Idce4 using the following equations,

when the three-phase sum current value Isum is positive and conforms to decision formula 1-1, the decision parameter Njudge1 is increased by 1,

when the three-phase sum current value Isum is negative and conforms to decision formula 1-2, the decision parameter Njudge1 is decreased by 1,

when the three-phase sum current value Isum is positive and conforms to decision formula 2-1, the decision parameter Njudge2 is increased by 1,

when the three-phase sum current value Isum is negative and conforms to decision formula 2-2, the decision parameter Njudge2 is decreased by 1,

when the three-phase sum current value Isum is positive and conforms to decision formula 3-1, the decision parameter Njudge3 is increased by 1,

when the three-phase sum current value Isum is negative and conforms to decision formula 3-2, the decision parameter Njudge3 is decreased by 1,

determining a phase in which the current sensor has failed and a failure type based on the amount of change in the determination parameters Njudge1, Njudge2, Njudge3 over a prescribed time,

Idce1＝(-Ivs-Iws)×Du+Ivs×Dv+Iws×Dw

Idce2＝Ius×Du+(-Ius-Iws)×Dv+Iws×Dw

Idce3＝Ius×Du+Ivs×Dv+(-Ius-Ivs)×Dw

Idce4＝(-Ivs-Iws)×Du+(-Ius-Iws)×Dv+(-Ius-Ivs)×Dw

judgment formula 1-1: idce1-Idce4> Isum + Ihys

The judgment formula is 1-2: idce1-Idce4< Isum-Ihys

Judgment formula 2-1: idce2-Idce4> Isum + Ihys

The judgment formula 2-2: idce2-Idce4< Isum-Ihys

Decision formula 3-1: idce3-Idce4> Isum + Ihys

The judgment formula is 3-2: idce3-Idce4< Isum-Ihys.

5. The control device according to claim 3 or 4,

the control means corrects the prescribed threshold by adding the amount of change in the target direct current to a predetermined value,

determining a phase and a fault type of the current sensor at which a fault has occurred based on a result of comparison between a value obtained by subtracting the fourth estimated direct current value Idce4 from the first estimated direct current value Idce1, the second estimated direct current value Idce2, and the third estimated direct current value Idce3, respectively, and a difference between the three-phase sum current value Isum and the prescribed threshold value after correction.

6. The control device of claim 1,

comparing the calculated change in each estimated DC current value with a first determination table to determine a phase in which the current sensor has failed and a type of failure, that is, to perform a first determination,

when the failure of the current sensor cannot be determined by the first determination, the second determination is performed by comparing the calculated change in each estimated direct current value with a second determination table to determine the phase in which the current sensor has failed and the type of failure.

7. The control device of claim 1,

a third determination of determining a failure of the current sensor based on a change in each of the estimated direct current values calculated over the first period of time,

when it is determined that the failure of the current sensor cannot be determined by the third determination, a fourth determination is made to determine the failure of the current sensor based on a change in the estimated dc current values calculated for a second time period longer than the first time period.

8. The control device of claim 1,

and determining that the current sensor has failed for the phase in which the calculated estimated dc current value has the smallest frequency.

9. The control device of claim 8,

a fifth determination of determining a failure of the current sensor based on the frequency of each of the estimated direct current values calculated during a third period of time,

when it is determined that the failure of the current sensor cannot be determined by the fifth determination, a sixth determination is performed, which is a determination of the failure of the current sensor, based on the frequency of each of the estimated dc current values calculated for a fourth time period longer than the third time period.

10. The control device of claim 1,

and determining that the current sensor has failed for a phase for which the difference between the calculated maximum value and minimum value of the estimated dc current value is smallest.

11. The control device of claim 10,

a seventh determination of determining a failure of the current sensor based on a difference between a maximum value and a minimum value of the respective estimated direct current values calculated in a fifth time,

when it is determined that the failure of the current sensor cannot be determined by the seventh determination, an eighth determination is made, which is a determination of the failure of the current sensor, based on a difference between a maximum value and a minimum value of the estimated dc current values calculated for a sixth time longer than the fifth time.

12. A failure determination method for a current sensor executed by a control device for controlling an electric motor by an inverter circuit for supplying the electric motor with electric power converted from direct current to three-phase alternating current, the method being characterized in that,

a current sensor for detecting an alternating current of each phase of the three-phase alternating current is provided at an output of the inverter circuit,

in the method, the raw material is subjected to a chemical reaction,

the control device calculates each of the estimated direct current values using a duty value of a PWM signal for controlling switches of the inverter circuit, and an alternating current value of two of the three phases detected by the current sensor,

the control device determines a failure of the current sensor based on the calculated change in each of the estimated direct current values.

Technical Field

The present invention relates to a motor control device, and more particularly to failure determination of a current sensor.

Background

As background art in the field, there are the following prior arts. Patent document 1 (japanese patent laid-open No. 2017-208893) describes an inverter control device that controls an inverter circuit, calculates an estimated dc current value from a duty value and an ac current sensor value output from an ac current sensor, and diagnoses the dc current sensor based on the estimated dc current value and the dc current sensor value output from the dc current sensor (see abstract).

Further, patent document 2 (japanese patent laid-open No. 2009-303283) describes a motor control device that determines more appropriately a deviation generated in a sensor that detects a phase current in a moving state and corrects the deviation (see abstract).

Documents of the prior art

Patent document

Patent document 1: japanese patent laid-open publication No. 2017-208893

Patent document 2: japanese patent laid-open publication No. 2009-303283

Disclosure of Invention

Technical problem to be solved by the invention

As described in patent document 1, an ac current sensor and a dc current sensor are mounted on an inverter for controlling a rotating electrical machine, but the dc current sensor is used only for diagnosis and is not used for controlling the rotating electrical machine, and therefore, it is required to reduce the cost by eliminating the dc current sensor. The dc current value can be estimated by using the sensor value of the ac current sensor and the gate signal supplied to the power module instead of the dc current value measured with the dc current sensor. However, when the ac current sensor fails, there is a problem that the ac current sensor value and the dc current estimated value are abnormal values at the same time.

Further, the inverter diagnoses a failure of the alternating current sensor by three phases and diagnosis, range diagnosis, but both ways have difficulty in accurately detecting a gain failure. In order to eliminate the dc current sensor, it is necessary to detect a gain failure of the ac current sensor.

Technical scheme for solving technical problem

As described below, a representative example of the invention disclosed in the present application is shown. That is, a control device for controlling a motor by an inverter circuit for supplying electric power converted from direct current to three-phase alternating current to the motor, wherein a current sensor for detecting alternating current of each phase of the three-phase alternating current is provided at an output of the inverter circuit, and the control device calculates each estimated direct current value using a duty value of a PWM signal for controlling a switch of the inverter circuit and an alternating current value of two phases of the three phases detected by the current sensor, and determines a failure of the current sensor based on a change in the calculated each estimated direct current value.

Effects of the invention

According to one aspect of the present invention, a failed phase of an ac current sensor can be determined without providing a dc current sensor. The problems, structures, and effects other than those described above will be further apparent from the following description of the embodiments.

Drawings

Fig. 1 is a diagram showing a configuration example of a power conversion device and its peripheral devices according to an embodiment of the present invention.

Fig. 2 is a diagram showing an example of the internal configuration of an inverter circuit according to an embodiment of the present invention.

Fig. 3 is a flowchart of an ac current sensor gain failure determination process executed by the ac current sensor gain failure determination section of embodiment 1.

Fig. 4 is a flowchart of data processing 1 of embodiment 1.

Fig. 5 is a flowchart of data processing 2 of embodiment 1.

Fig. 6 is a flowchart of data processing 3 of embodiment 1.

Fig. 7 is a diagram showing a configuration example of the gain failure determination table 1 in embodiment 1.

Fig. 8 is a diagram showing a configuration example of the gain failure determination table 2 in embodiment 1.

Fig. 9 is a diagram showing a configuration example of the gain failure determination table 3 in embodiment 1.

Fig. 10 is a diagram showing a configuration example of the gain failure determination table 4 in embodiment 1.

Fig. 11 is a diagram showing a current waveform when the U-phase ac current sensor fails.

Fig. 12 is a diagram showing a configuration example of the gain failure determination table 5 in embodiment 2.

Fig. 13 is a diagram showing a configuration example of the gain failure determination table 6 in embodiment 3.

Detailed Description

Hereinafter, embodiments will be described with reference to the drawings. In the following embodiments, a rotating electrical machine control system for determining a faulty phase of an alternating current sensor will be described.

< example 1>

Fig. 1 is a diagram showing a configuration example of a power conversion device 1 and its peripheral devices according to an embodiment of the present invention.

The power conversion device 1 converts dc power obtained from a dc power supply 3 into ac power, and drives the motor 2. The power conversion device 1 also has a function of converting the power of the motor 2 into dc power and charging the dc power supply 3. The dc power supply 3 is a power supply such as a battery for driving the motor 2. Of the direct currents supplied from the direct current power supply 3, the direction in which the direct current flows from the positive electrode of the direct current power supply 3 to the power conversion device 1 is positive, and the opposite direction is negative.

The motor 2 is a three-phase motor having three windings inside. An angle sensor (not shown) for measuring a rotation angle is mounted on the motor 2, and the angle sensor outputs the measured rotation angle of the motor 2 to the power conversion device 1 as an angle sensor value.

The power conversion apparatus 1 includes a control apparatus 15, a drive circuit 22, an inverter circuit 9, alternating current sensors 14a to 14c, a voltage sensor 10, and an alternating current sensor gain failure determination section 25.

The voltage sensor 10 is a sensor for measuring the output voltage of the direct-current power supply 3, and outputs the measured voltage value to the control device 15 as a voltage sensor value.

The ac current sensors 14a to 14c are sensors for measuring ac currents flowing through the respective phases (U-phase, V-phase, W-phase) of the motor 2. The ac current sensor 14a measures an ac current value Iu flowing in the U phase, and outputs an ac current sensor value Ius to the control device 15. Likewise, the ac current sensor 14b measures an ac current value Iv flowing in the V phase, and outputs an ac current sensor value Ivs to the control device 15. The ac current sensor 14c measures an ac current value Iw flowing through the W phase, and outputs an ac current sensor value Iws to the control device 15. Of the alternating currents, the direction in which the alternating current flows from the power conversion device 1 to the motor 2 is positive, and the opposite direction is negative.

In the present embodiment, the alternating current sensors 14a to 14c are provided inside the power conversion device 1, but may be provided outside the power conversion device 1 (for example, between the power conversion device 1 and the motor 2 or inside the motor 2).

The control device 15 communicates with an electronic control device (not shown) outside the power conversion device 1, and receives a target torque of the motor 2 from other electronic control devices. The control device 15 controls the inverter circuit 9 via the drive circuit 22 based on the target torque, and drives the motor 2. When it is determined that a failure has occurred in the power conversion device 1, the control device 15 outputs an abnormality notification signal to the external abnormality notification device 4.

The control device 15 has therein a communication circuit (not shown), a motor speed calculation section 23, a target current calculation section 17, a duty ratio calculation section 19, a PWM signal generation section 21, and an alternating current sensor gain failure determination section 25.

The motor speed calculation unit 23 calculates the motor rotation speed from the change in the angle sensor value in the motor, and outputs the calculated motor speed value to the target current calculation unit 17.

The target current calculation portion 17 calculates a current value that should flow to the motor 2 using the target torque, the voltage sensor value, and the motor speed value output by the motor speed calculation portion 23, and outputs the current value as a target current value to the duty ratio calculation portion 19. The target current value includes information of a d-axis target current value and a q-axis target current value.

The duty ratio calculation portion 19 calculates the U-phase duty ratio value Du, the V-phase duty ratio value Dv, and the W-phase duty ratio value Dw based on the target current value and the alternating current sensor values iu, Ivs, Iws output by the target current calculation portion 17, and outputs them to the PWM signal generation portion 21 and the alternating current sensor gain failure determination portion 25. The U-phase duty ratio value Du represents the on-time ratio of the U-phase upper arm power semiconductor 90a, and the on-time ratio of the U-phase lower arm power semiconductor 90b paired with the U-phase upper arm power semiconductor is represented by 1-Du. Similarly, the V-phase duty value Dv represents the on-time ratio of the V-phase upper arm power semiconductor 90c, and the on-time ratio of the V-phase lower arm power semiconductor 90d is represented by 1-Dv. The W-phase duty ratio value Dw indicates the on-time ratio of the W-phase upper arm power semiconductor 90e, and the on-time ratio of the W-phase lower arm power semiconductor 90f is indicated by 1-Dw.

The division of the upper and lower arms is illustrated in fig. 2.

The PWM signal generation section 21 has a timer (not shown) therein, and generates a PWM (pulse width modulation) signal based on the timer value, the U-phase duty value Du, the V-phase duty value Dv, and the W-phase duty value Dw, and outputs it to the drive circuit 22.

Further, the PWM signal generation section 21 controls the PWM signal so that the motor 2 is not driven when the abnormality notification signal is output from the alternating current sensor gain failure determination section 25. The state in which the motor 2 is not driven is, for example, a state in which all six power semiconductors in the inverter circuit 9 are turned off (referred to as a free-wheeling state in the present embodiment). As other examples, there is a state in which three power semiconductors of the upper arm are on and three power semiconductors of the lower arm are off (referred to as an upper arm active short-circuit state in the present embodiment) or, conversely, a state in which three power semiconductors of the upper arm are off and three power semiconductors of the lower arm are on (referred to as a lower arm active short-circuit state in the present embodiment).

The ac current sensor gain failure determination unit 25 determines a failure of the ac current sensors 14a to 14c, and includes an estimated dc current calculation unit 26 and a determination unit 28 therein. The ac current sensor gain failure determination unit 25 is constituted by a computer (microcomputer) including an arithmetic unit, a memory, and an input/output device.

The computing device includes a processor and executes programs stored in memory. The processing performed by the arithmetic device to execute the program may be partially performed by another arithmetic device (e.g., hardware such as an FPGA (Field programmable Gate Array) or an ASIC (Application Specific Integrated Circuit)).

The memory includes ROM and RAM as nonvolatile memory elements. The ROM stores an unchanging program (e.g., BIOS) and the like. The RAM is a high-speed and volatile memory element such as a DRAM (dynamic random access memory) or a nonvolatile memory element such as an SRAM (static random access memory), and stores a program executed by the arithmetic device and data used when executing the program.

The input/output device is an interface for transmitting the processing contents of the ac current sensor gain failure determination unit 25 to the outside or receiving data from the outside according to a predetermined protocol.

The program executed by the arithmetic device is stored in a nonvolatile memory as a non-transitory storage medium of the alternating current sensor gain failure determination section 25.

The estimated dc current calculation unit 26 calculates four estimated dc current values and three-phase sum current values based on the duty values Du, Dv, Dw of the respective phases and the ac current sensor values iu, Ivs, Iws, and outputs them to the determination unit 28. The determination section 28 determines the magnitude/magnitude of gain failure and the failure phase of the ac current sensors 14a to 14c using the four estimated dc current values and the three-phase sum current values, and outputs a failure notification signal to the failure notification device and the PWM signal generation section 21. Specifically, the determination unit 28 calculates the four estimated dc current values Idce1, Idce2, Idce3, Idce4 and the three-phase and current value Isum through the processing shown in fig. 3 to 6, performs data processing 1, 2, and 3 using them, counts the determination parameters Njudg1, Njudg2, and Njudg3, and determines the failure phase, the large-gain failure, or the small-gain failure of the ac current sensors 14a to 14c using the counted determination parameters Njudg1, Njudg2, and Njudg 3.

The drive circuit 22 receives the PWM signal output from the PWM signal generation unit 21 and outputs a drive signal for switching on/off of the power semiconductor of the inverter circuit 9.

Fig. 2 is a diagram showing a configuration example of the inside of the inverter circuit 9 according to the embodiment of the present invention.

The inverter circuit 9 has a smoothing capacitor 92 and six power semiconductors 90a to 90 f.

The power semiconductors 90a to 90f perform switching between on and off in accordance with a drive signal input from the drive circuit 22, thereby converting dc power and ac power. The power semiconductors 90a to 90f are, for example, power MOSFETs (metal oxide semiconductor field effect transistors), IGBTs (insulated gate bipolar transistors), or the like. In the present embodiment, the upper three power semiconductors are collectively referred to as upper arms, and the lower three power semiconductors are collectively referred to as lower arms.

The smoothing capacitor 92 is for smoothing the current generated by turning on/off the power semiconductors 90a to 90f and suppressing the ripple of the dc current supplied from the dc power supply 3 to the power conversion device 1. The filter capacitor 92 is formed of, for example, an electrolytic capacitor or a film capacitor.

Fig. 3 is a flowchart of an alternating current sensor gain failure determination process executed by the alternating current sensor gain failure determination section 25 of embodiment 1. The ac current sensor gain failure determination process shown in fig. 3 is repeatedly executed at predetermined timing (for example, at predetermined time intervals).

First, the ac current sensor gain failure determination unit 25 acquires ac current sensor values iu, Ivs, Iws (S101).

Then, estimated dc current calculation section 26 calculates estimated dc current values Idce1, Idce2, Idce3, Idce4 using the following equations from duty values Du, Dv, Dw of the PWM signals of the respective phases and ac current sensor values iu, Ivs, Iws, and calculates the three-phase sum current value Isum and outputs it to determination section 28 (S102).

Idce1＝(-Ivs-Iws)×Du+Ivs×Dv+Iws×Dw

Idce2＝Ius×Du+(-Ius-Iws)×Dv+Iws×Dw

Idce3＝Ius×Du+Ivs×Dv+(-Ius-Ivs)×Dw

Idce4＝(-Ivs-Iws)×Du+(-Ius-Iws)×Dv+(-Ius-Ivs)×Dw

Isum＝Ius+Ivs+Iws

The determination section 28 performs data processing 1 using the estimated dc current values Idce1, Idce4 and the three-phase sum current value Isum, and calculates a determination parameter 1Njudg1 (S103). Details of the data processing 1 will be described later with reference to fig. 4.

The determination section 28 performs data processing 2 using the estimated direct current values Idce2, Idce4 and the three-phase sum current value Isum, and calculates a determination parameter 2Njudg2 (S104). Details of the data processing 2 will be described later with reference to fig. 5.

The determination section 28 performs data processing 3 using the estimated dc current values Idce3, Idce4 and the three-phase sum current value Isum, and calculates a determination parameter 3Njudg3 (S105). Details of the data processing 3 will be described later with reference to fig. 6.

The determination unit 28 counts the determination parameters Njudg1, Njudg2, and Njudg3 for a certain period of time (S106), and determines the failure phase and the gain failure mode (S107). Various methods may be employed to determine the faulty phase and the gain fault pattern, but by using, for example, a gain fault determination table (refer to fig. 7, 8, 9, 10), the faulty phase and the gain fault pattern can be determined according to the trend of increase/decrease of the determination parameters Njudg1, Njudg2, Njudg 3. Further, the failure phase and the gain failure mode may be determined by using a function having the determination parameters Njudg1, Njudg2, Njudg3 as inputs and outputting the failure phase and the gain failure mode, or may be determined by using an artificial intelligence-based failure determination model.

Fig. 4 is a flowchart of data processing 1 of embodiment 1.

The determination section 28 performs data processing 1 using the estimated direct current values Idce1, Idce4 and the three-phase sum current value Isum. The determination unit 28 first determines whether the three-phase sum current value Isum is positive or negative (S111). When the three-phase sum current value Isum is "positive", it is determined whether or not the determination formula 1-1 is satisfied (S112), when the determination formula 1-1 is satisfied, the determination parameter Njudge1 is increased by 1(S113), and when the determination formula 1-1 is not satisfied, nothing is processed.

Judgment formula 1-1: idce1-Idce4> Isum + Ihys

On the other hand, when the three-phase sum current value Isum is "negative", it is determined whether or not the determination formula 1-2 is satisfied (S114), when the determination formula 1-2 is satisfied, the determination parameter Njudge1 is decreased by 1(S115), and when the determination formula 1-2 is not satisfied, nothing is processed.

The judgment formula is 1-2: idce1-Idce4< Isum-Ihys

The determination threshold Ihys may be a fixed value, or may be a value obtained by calculating the amount of change in the target dc current using the following equation, using the torque command value change amount Δ Tcmd, the motor rotation speed ω, the dc voltage value Vdc, and the power conversion efficiency η as variables, and correcting the calculated value as the determination threshold Ihys. By correcting the determination threshold value using the amount of change in the target direct current, it is possible to follow a sharp change in current caused by the command.

Determination threshold value Ihys + ((Δ Tcmd × ω)/(η × Vdc))

Fig. 5 is a flowchart of data processing 2 of embodiment 1.

The determination section 28 performs data processing 2 using the estimated direct current values Idce2, Idce4 and the three-phase sum current value Isum. The determination unit 28 first determines whether the three-phase sum current value Isum is positive or negative (S121). When the three-phase sum current value Isum is "positive", it is determined whether or not the determination formula 2-1 is satisfied (S122), when the determination formula 2-1 is satisfied, the determination parameter Njudge2 is increased by 1(S123), and when the determination formula 2-1 is not satisfied, nothing is processed.

Judgment formula 2-1: idce2-Idce4> Isum + Ihys

On the other hand, when the three-phase sum current value Isum is "negative", it is determined whether or not the determination formula 2-2 is satisfied (S114), when the determination formula 2-2 is satisfied, the determination parameter Njudge2 is decreased by 1(S115), and when the determination formula 2-2 is not satisfied, nothing is processed.

The judgment formula 2-2: idce2-Idce4< Isum-Ihys

As described above, the determination threshold Ihys may be a fixed value, or a value obtained by calculating the amount of change in the target dc current using the following equation and correcting the calculated value may be used as the determination threshold Ihys, with the torque command value change amount Δ Tcmd, the motor rotation speed ω, the dc voltage value Vdc, and the power conversion efficiency η as variables. By correcting the determination threshold value using the amount of change in the target direct current, it is possible to follow a sharp change in current caused by the command.

Determination threshold value Ihys + ((Δ Tcmd × ω)/(η × Vdc))

Fig. 6 is a flowchart of data processing 3 of embodiment 1.

The determination section 28 performs data processing 3 using the estimated direct current values Idce3, Idce4 and the three-phase sum current value Isum. The determination unit 28 first determines whether the three-phase sum current value Isum is positive or negative (S131). When the three-phase sum current value Isum is "positive", it is determined whether or not the determination formula 3-1 is satisfied (S132), when the determination formula 3-1 is satisfied, the determination parameter Njudge3 is increased by 1(S133), and when the determination formula 3-1 is not satisfied, nothing is processed.

Decision formula 3-1: idce3-Idce4> Isum + Ihys

When the three-phase sum current value Isum is negative, it is determined whether or not the determination formula 3-2 is satisfied (S134), when the determination formula 3-2 is satisfied, the determination parameter Njudge3 is reduced by 1(S135), and when the determination formula 3-2 is not satisfied, nothing is processed.

The judgment formula is 3-2: idce3-Idce4< Isum-Ihys

As described above, the determination threshold Ihys may be a fixed value, or a value obtained by calculating the amount of change in the target dc current using the following equation and correcting the calculated value may be used as the determination threshold Ihys, with the torque command value change amount Δ Tcmd, the motor rotation speed ω, the dc voltage value Vdc, and the power conversion efficiency η as variables. By correcting the determination threshold value using the amount of change in the target direct current, it is possible to follow a sharp change in current caused by the command.

Determination threshold value Ihys + ((Δ Tcmd × ω)/(η × Vdc))

Fig. 7 is a diagram showing a configuration example of the gain failure determination table 1 in embodiment 1.

The gain failure determination table 1 is for power running. In the gain failure determination table 1, the failure phases and gain failure modes of the alternating current sensors 14a to 14c are recorded in correspondence with the increasing/decreasing trends of the determination parameters Njudg1, Njudg2, and Njudg 3. The gain failure mode shows whether the ac current sensors 14a to 14c output a value greater than the true value or a value smaller than the true value, and in the normal state, the gains of the ac current sensors 14a to 14c are 1.0. Determination unit 28 determines the failure phase and gain failure mode of ac current sensors 14a to 14c during power running, based on the increasing/decreasing trends of determination parameters Njudg1, Njudg2, and Njudg3 counted during predetermined time T1, by using gain failure determination table 1. The determination unit 28 determines whether the vehicle is in the power running mode or the regeneration mode based on the target torque. For example, if the target torque is positive, the engine is in the power running state, and if the target torque is negative, the engine is in the regeneration state. The determination unit 28 may determine whether the vehicle is in the power running mode or the regeneration mode by estimating the direct current. For example, when one or more estimated direct currents are positive, the vehicle is in the power running state, and when one or more estimated direct currents are negative, the vehicle is in the regeneration state.

Fig. 8 is a diagram showing a configuration example of the gain failure determination table 2 in embodiment 1.

The gain failure determination table 2 is used in the powering operation in the same manner as the gain failure determination table 1 (fig. 7). In the gain failure determination table 2, the failure phases and gain failure modes of the alternating current sensors 14a to 14c are recorded in correspondence with the increasing/decreasing trends of the determination parameters Njudg1, Njudg2, and Njudg 3. When the failed phase and the gain failure mode cannot be determined by gain failure determination table 1 (fig. 7), determination unit 28 determines the failed phase and the gain failure mode of ac current sensors 14a to 14c during power running, based on the increasing/decreasing trends of determination parameters Njudg1, Njudg2, and Njudg3 counted during predetermined time T2, by using gain failure determination table 2.

That is, although the determination can be made by the gain failure determination table 1 (fig. 7) in the trend of increasing or decreasing the ideal determination parameter, the determination may be made by the gain failure determination table 2 (fig. 8) depending on the threshold value and the processing timing of the data processing 1 to 3, without meeting the conditions specified in the gain failure determination table 1.

Further, the determination conditions of the gain failure determination table 1 and the determination conditions of the gain failure determination table 2 may be integrated to constitute one gain failure determination table.

Fig. 9 is a diagram showing a configuration example of the gain failure determination table 3 in embodiment 1.

In embodiment 1, the determination process can be performed by the same algorithm both in the powering operation and in the regeneration operation. However, since the change tendency of the estimated dc current value is different, it is necessary to use different determination tables at the time of powering and at the time of regeneration.

The gain failure determination table 3 is used for the regeneration. In the gain failure determination table 3, the failure phases and gain failure modes of the alternating current sensors 14a to 14c are recorded in correspondence with the increasing/decreasing trends of the determination parameters Njudg1, Njudg2, and Njudg 3. By using the gain failure determination table 3, the determination unit 28 determines the failure phase and the gain failure mode of the ac current sensors 14a to 14c during regeneration based on the increasing/decreasing tendencies of the determination parameters Njudg1, Njudg2, and Njudg3 counted during the predetermined time T3.

Fig. 10 is a diagram showing a configuration example of the gain failure determination table 4 in embodiment 1.

The gain failure determination table 4 is used for the regeneration time in the same manner as the gain failure determination table 3 (fig. 9). In the gain failure determination table 4, the failure phases and gain failure modes of the alternating current sensors 14a to 14c are recorded in correspondence with the increasing/decreasing trends of the determination parameters Njudg1, Njudg2, and Njudg 3. When the failed phase and the gain failure mode cannot be determined by the gain failure determination table 3 (fig. 9), the determination section 28 determines the failed phase and the gain failure mode of the ac current sensors 14a to 14c in the power running, based on the increasing/decreasing trends of the determination parameters Njudg1, Njudg2, and Njudg3 counted within the predetermined time T4, by using the gain failure determination table 4.

That is, although the determination can be made by the gain failure determination table 3 (fig. 9) in the trend of increasing or decreasing the ideal determination parameter, the determination may be made by the gain failure determination table 4 (fig. 10) depending on the threshold value and the processing timing of the data processing 1 to 3, without meeting the conditions specified in the gain failure determination table 3.

Further, the determination conditions of the gain failure determination table 3 and the determination conditions of the gain failure determination table 4 may be integrated to constitute one gain failure determination table.

In the determination process described above, the prescribed times T1 to T4 for counting the determination parameters Njudg1, Njudg2, and Njudg3 may be different times or the same time as long as T2 is a longer time than T1 and T4 is a longer time than T3.

Fig. 11 is a diagram showing a current waveform when the U-phase ac current sensor 14a fails.

The U-phase electric angle is 360 °, and the three-phase and current values Isum, which are ideally 0, change normally. Although illustration is omitted, Idce1, Idce2, Idce3, and Idce4 also change asynchronously, and thus Idce1-Idce4 indicated by a dotted line, Idce2-Idce4 indicated by a dotted line, and Idce3-Idce4 indicated by a dot-dash line also start changing.

When the U-phase electrical angle is between 360 ° and 540 °, Isum is positive, and therefore Isum + Ihys is the upper-limit determination threshold, Idce1-Idce4 does not exceed the determination threshold (the region within the determination threshold is represented by a dotted graph), but Idce2-Idce4 exceeds the determination threshold at point a, and Idce3-Idce4 exceeds the determination threshold at point B. In addition, since Isum is negative when the U-phase electrical angle is 540 ° to 720 °, Isum — Ihys becomes the lower limit determination threshold, and idc 1-idc 4 is smaller than the determination threshold at point C. Therefore, at the point a (U-phase electrical angle 380 °, 740 °, 1100 °), 1 is added to the determination parameter Njudg2, at the point B (U-phase electrical angle 460 °, 820 °, 1180 °), 1 is added to the determination parameter Njudg3, and at the point C (U-phase electrical angle 580 °, 940 °, 1300 °), 1 is subtracted from the determination parameter Njudg 1.

If the predetermined time for the failure determination is set to 3 cycles, the determination parameter Njudg1 is decremented by 3, the determination parameter Njudg2 is incremented by 3, and the determination parameter Njudg3 is incremented by 3, so that it can be seen that the gain of the U-phase is large, if the gain failure determination table 1 (fig. 7) is referred to.

When the ac current sensors 14a to 14c have a gain failure, it is estimated that the dc current value and the three-phase sum current value change. In embodiment 1, the increase/decrease tendency of the estimated dc current value is determined by using four estimated dc currents (idc 1 to idc 4) and three phases sum current values Isum, which are calculated with one phase or all of the three phases as estimated ac current values, based on the principle that the three phases sum current values are zero, whereby the magnitude/magnitude of the gain fault and the faulty phase can be determined.

That is, when the U-phase alternating current sensor 14a fails, Idce1, which is calculated without using Ius, becomes a true value. Idce2, Idce3, and Idce4 vary in waveforms other than the true values. Therefore, the differences (Idce2-Idce4, Idce3-Idce4) between Idce1-Idec4 and the other estimated DC current values vary in different trends. By determining the change by the amount of deviation from the three phases and the current value Isum, it is possible to determine a failure of the alternating current sensor 14 a.

As described above, in embodiment 1 of the present invention, a failure of the alternating current sensors 14a to 14c is determined based on a change in each estimated direct current value. Specifically, the difference between the estimated dc current values (for example, Idce1-Idec4) and the amount of deviation between the three phases and the current value Isum are compared with a prescribed threshold value Ihys. Further, when the trend of change of one estimated dc current value (for example, Idce1) of the three estimated dc currents is different from the other estimated dc current values (for example, Idce2 and Idce3), the U ac current sensor 14a that detects the ac current sensor value Ius that is not used in the calculation of the estimated dc current value Idce1 having the different trend of change is determined as having a failure, and therefore, the failure of the ac current sensors 14a to 14c can be accurately determined. Even if the degree of failure (gain difference) of the ac current sensors 14a to 14c is small, the failure of the ac current sensors can be detected. Further, even if the degree of gain failure of the ac current sensors 14a to 14c changes, the relative relationship between each estimated dc current value and the three phases and the current value does not change, and therefore, determination can be made by the same algorithm.

< example 2>

Next, example 2 of the present invention will be explained. In example 2, in step S107 in fig. 3, the fluctuation frequencies of the estimated dc currents are compared, and the failure phase of the ac current sensors 14a to 14c is determined. In embodiment 2, a failed phase is determined, but a gain failure mode is not determined. In the following description of embodiment 2, the points different from embodiment 1 are mainly described, the same reference numerals are given to the structures having the same functions as embodiment 1, and the description thereof is omitted.

For example, when a U-phase gain fault occurs, the estimated dc current value Idce1 calculated without using the ac current sensor value Ius of the U-phase ac current sensor 14a is not affected by the frequency variation of the ac current, but the amplitudes of the estimated dc current values Idce2, Idce3 calculated using the ac current sensor value Ius of the U-phase ac current sensor 14a vary in proportion to the frequency of the ac current. That is, the estimated dc current value Idce1 has a different frequency of variation from the estimated dc current values Idce2 and Idce 3. Therefore, the changes in the estimated dc current values Idce1, Idce2, Idce3 are determined from the frequencies, and the failure phases of the ac current sensors 14a to 14c are determined.

Determination unit 28 measures estimated dc current values Idce1, Idce2, and Idce3 for a predetermined time T5, calculates variation frequencies F1, F2, and F3 of the estimated dc currents, compares the magnitudes of variation frequencies F1, F2, and F3 of the estimated dc currents, and determines the failure phase of ac current sensors 14a to 14c using gain failure determination table 5 (see fig. 12).

If the measurement result of predetermined time T5 does not satisfy the condition even if gain failure determination table 5 (see fig. 12) is used, determination unit 28 may measure estimated dc current values Idce1, Idce2, and Idce3 for predetermined time T6, recalculate estimated dc current fluctuation frequencies F1, F2, and F3, and use the result to perform re-determination.

Fig. 12 is a diagram showing a configuration example of the gain failure determination table 5 in embodiment 2.

In the gain failure determination table 5, the failure phases of the ac current sensors 14a to 14c are recorded in association with the magnitude relationship among the estimated dc current fluctuation frequencies F1, F2, and F3. Using gain failure determination table 5, determination unit 28 compares the magnitudes of fluctuation frequencies F1, F2, and F3 of estimated dc current values Idce1, Idce2, and Idce3 during predetermined time T5, and determines that ac current sensors 14a to 14c having the lowest fluctuation frequencies have failed.

As described above, according to embodiment 2 of the present invention, the failure phase of the alternating current sensors 14a to 14c can be determined by a simple operation.

< example 3>

Next, example 3 of the present invention will be explained. In example 3, in step S107 in fig. 3, the calculated differences (peak-to-peak values) between the maximum values and the minimum values of the estimated dc current values Idce1, Idce2, Idce3 are compared, and the failure phase of the ac current sensors 14a to 14c is determined. In embodiment 3, a failed phase is determined, but a gain failure mode is not determined. In the following description of embodiment 23, the points different from embodiment 1 are mainly described, the same reference numerals are given to the structures having the same functions as embodiment 1, and the description thereof is omitted.

For example, when a U-phase gain fault occurs, the peak-to-peak values of the estimated direct current values Idce1 calculated without using the alternating current sensor values Ius of the U-phase alternating current sensor 14a are not affected by the gain fault, but the peak-to-peak values of the estimated direct current values Idce1, Idce2, Idce3 calculated using the alternating current sensor values Ius of the U-phase alternating current sensor 14a increase in proportion to the degree of the gain fault. That is, when the ac current sensors 14a to 14c fail, the calculated estimated dc current values differ in peak-to-peak value. Therefore, the changes in the estimated dc current values Idce1, Idce2, Idce3 are determined from the peak-to-peak values, and the failed phases of the ac current sensors 14a to 14c are determined.

The determination unit 28 measures the estimated dc current values Idce1, Idce2, Idce3 for a predetermined time T7, calculates peak-to-peak values Idce1p-p, Idce2p-p, Idce3p-p of the estimated dc currents, compares the magnitudes of the peak-to-peak values Idce1p-p, Idce2p-p, Idce3p-p of the estimated dc currents, and determines the failure phases of the ac current sensors 14a to 14c using the gain failure determination table 6 (see fig. 13).

If the measurement result of predetermined time T7 does not satisfy the condition even if gain failure determination table 6 (see fig. 13) is used, determination unit 28 may further measure estimated dc current values Idce1, Idce2, and Idce3 for predetermined time T8, recalculate peak-to-peak values Idce1p-p, Idce2p-p, and Idce3p-p of the estimated dc currents, and perform re-determination using the result.

Fig. 13 is a diagram showing a configuration example of the gain failure determination table 6 in embodiment 3.

In the gain failure determination table 6, the failure phases of the alternating current sensors 14a to 14c are recorded in correspondence with the magnitude relationships among the peak-to-peak values Idce1p-p, Idce2p-p, Idce3p-p of the estimated direct currents. The determination unit 28 compares the magnitudes of the peak-to-peak values Idce1p-p, Idce2p-p, and Idce3p-p of the estimated dc current values Idce1, Idce2, and Idce3 for the predetermined time T7 using the gain failure determination table 6, and determines that the ac current sensors 14a to 14c having the smallest peak-to-peak values have failed.

As described above, according to embodiment 3 of the present invention, the failed phase of the alternating current sensors 14a to 14c can be determined by a simple operation.

As described above, the control device 15 of the power conversion device 1 according to the embodiment of the present invention is a control device that controls the motor 2 by the inverter circuit 9 that supplies the motor 2 with the electric power converted from direct current to three-phase alternating current, ac current sensors 14a to 14c for detecting ac currents of respective phases of three-phase ac are provided at an output of the inverter circuit 9, the control device 15 (ac current sensor gain failure determination unit 25) calculates three estimated dc current values idc 1 to idc 3 using a duty value of a PWM signal for controlling switches of the inverter circuit and ac current values (any two of iu, Ivs, Iws) of two of the three phases detected by the current sensors, and determines a failure of the alternating current sensors 14a to 14c based on the calculated change in the respective estimated direct current values, it is therefore possible to determine the failed phase and gain failure mode of the alternating current sensor without providing a direct current sensor. Even if the degree of failure (gain difference) of the ac current sensor is small, the failure of the ac current sensor can be detected.

Further, the ac current sensor gain failure determination section 25 determines the phase and the failure type of the failure of the ac current sensors 14a to 14c based on the comparison result between the difference between the three-phase and current value Isum and the predetermined threshold value corrected, and the value obtained by subtracting the estimated dc current value Idce4 from each of the estimated dc current values Idce1, Idce2, and Idce3, as the predetermined threshold value, by adding the amount of change of the target dc current to a predetermined value, and therefore, by correcting the determination threshold value using the amount of change of the target dc current, it is possible to follow the rapid change of the current by the command.

In addition, the ac current sensor gain failure determination unit 25 checks the calculated changes in the estimated dc current values against the first determination table (gain failure determination table 1, gain failure determination table 3) to determine the phase in which the ac current sensors 14a to 14c have failed and the type of failure, that is, to perform the first determination, and when it is not possible to determine the failure of the ac current sensors 14a to 14c by the first determination, checks the calculated changes in the estimated dc current values against the second determination table (gain failure determination table 2, gain failure determination table 4) to determine the phase in which the ac current sensors 14a to 14c have failed and the type of failure, that is, to perform the second determination, so that it is possible to accurately determine the failure of the ac current sensors regardless of the influence of noise and the degree of gain failure (gain difference).

Further, the ac current sensor gain failure determination unit 25 determines that the ac current sensors 14a to 14c have failed, that is, performs the third determination, based on the change in the estimated dc current values calculated at the first time, and determines that the ac current sensors 14a to 14c have failed, that is, performs the fourth determination, based on the change in the estimated dc current values calculated at the second time longer than the first time, when the ac current sensors 14a to 14c cannot be determined to have failed by the third determination, and therefore, the ac current sensors can be accurately determined to have failed in a short time, regardless of the influence of noise or the degree of gain failure (gain difference).

In addition, since the ac current sensor gain failure determination unit 25 determines that the ac current sensors 14a to 14c have failed for the phase in which the frequency of the calculated estimated dc current value is the smallest, the failed phase of the ac current sensors 14a to 14c can be determined by a simple calculation.

In addition, since the ac current sensor gain failure determination unit 25 determines that the current sensor has failed for the phase in which the difference between the maximum value and the minimum value of the calculated estimated dc current value is minimum, it is possible to determine the failed phase of the ac current sensors 14a to 14c by simple calculation.

Further, the ac current sensor gain failure determination unit 25 determines that the ac current sensors 14a to 14c have failed, that is, performs the fifth determination, based on the frequencies of the estimated dc current values calculated during the third time period, and determines that the ac current sensors 14a to 14c have failed, that is, performs the sixth determination, based on the frequencies of the estimated dc current values calculated during the fourth time period, which is longer than the third time period, when the ac current sensors 14a to 14c have failed by the fifth determination, and thus can accurately determine the failure of the ac current sensors in a short time period, regardless of the influence of noise or the degree (gain difference) of the gain failure.

The present invention is not limited to the above-described embodiments, and includes various modifications and equivalent arrangements within the spirit and scope of the appended claims. For example, the embodiments are described in detail to facilitate understanding of the present invention, and are not limited to having all the structures described. In addition, a part of the structure of a certain embodiment may be replaced with the structure of another embodiment. In addition, the structures of other embodiments may be added to the structure of a certain embodiment.

Further, some of the configurations of the embodiments may be added, deleted, or replaced with other configurations.

The above-described respective structures, functions, processing units, and the like may be partially or entirely realized by hardware, for example, by integrated circuit design or the like, or may be realized by software by interpreting and executing programs for realizing the respective functions by a processor.

Information of programs, tables, files, and the like that realize the respective functions may be stored in a memory, a hard disk, a storage device such as an SSD (Solid State Drive), or a recording medium such as an IC card, an SD card, or a DVD.

The control lines and information lines necessary for the description are shown, but the present invention is not limited to the control lines and information lines all necessary for mounting. Virtually all structures can be considered interconnected.

Description of the reference symbols

1 power conversion device, 2 motor, 3 dc power supply, 4 abnormality notification device, 7 angle sensor value, 9 inverter circuit, 10 voltage sensor, 14a to 14c ac current sensor, 15 control device, 17 target current calculation section, 19 duty ratio calculation section, 21PWM signal generation section, 22 drive circuit, 23 motor speed calculation section, 25 ac current sensor gain failure determination section, 26 estimated dc current calculation section, 28 determination section, 90a to 90f power semiconductor, 92 filter capacitor.