KR101905478B1 - Compressor driving apparatus and chiller including the same - Google Patents

Abstract

The present invention relates to a chiller. A compressor driving apparatus according to an embodiment of the present invention includes a compressor having a compressor motor, a magnetic bearing, and a switching element, and applies a current to a bearing coil of the magnetic bearing in accordance with a switching operation, And a compressor motor driving unit for rotating the compressor motor. The compressor motor driving unit includes an inverter for outputting an AC power to the compressor motor, And an inverter control section for controlling the inverter based on the output current detected by the output current detection section. The inverter control section determines whether or not the motor is eccentric or not based on the output current, And if it is eccentric, generates a compensation current command value based on the output current, Based on the command value, control is performed to control the inverter so that the compressor motor rotates. Thus, when the eccentricity of the compressor motor occurs in the magnetic levitation mode, it is possible to prevent the output power reduction and the pulsation of the compressor motor.

Description

[0001] The present invention relates to a compressor driving apparatus and a chiller having the same,

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a compressor driving apparatus and a chiller having the same, and more particularly, to a chiller capable of preventing output power reduction and pulsation of a compressor motor when an eccentricity of a compressor motor occurs in a magnetic levitation system.

The air conditioner is a device that discharges cold air into the room to create a pleasant indoor environment. This air conditioner is installed to provide a more comfortable indoor environment to humans by adjusting the room temperature and purifying the room temperature.

Generally, the air conditioner includes an indoor unit that is configured as a heat exchanger and installed in a room, and an outdoor unit that is composed of a compressor, a heat exchanger, and the like and supplies the refrigerant to the indoor unit.

On the other hand, among the air conditioners, a chiller used in a business place or a building larger than the home generally includes a cooling tower installed on the outdoor roof and a heat exchange unit for circulating the refrigerant and exchanging heat with the cooling water sent from the cooling tower. Further, the heat exchange unit includes a compressor, a condenser, and an evaporator.

On the other hand, when chiller is driven by a compressor motor, a magnetic force is generated by flowing a current through a bearing coil to make the rotor of the compressor motor magnetic levitation, do. This method is referred to as a magnetic bearing method or a magnetic levitation method.
Japanese Unexamined Patent Application Publication No. 2008-301671 discloses an air cycle refrigeration cooling turbine unit 5 having a motor 28 and a magnetic bearing device 17, a controller 19 for a magnetic bearing, a phase detector 40 The calculating unit 38 calculates a coil current application timing for generating a rotating magnetic field by the motor coil 28ba and outputs a power control signal A motor controller (29) for controlling the coil current to be applied to each phase motor coil from the circuit (39) is disclosed.

However, according to this method, when the eccentricity of the compressor motor occurs at the time of rotation of the compressor motor after the compressor rotor is floated, the line-to-line voltage imbalance of the compressor motor and the output of the compressor motor are pulsated or the output of the compressor motor is lowered Lt; / RTI >

An object of the present invention is to provide a compressor driving apparatus and a chiller having the compressor driving apparatus capable of preventing output power reduction and pulsation of a compressor motor when an eccentricity of a compressor motor occurs in a magnetic levitation system.

Another object of the present invention is to provide a compressor driving apparatus capable of smoothly landing a rotor of a compressor motor when the compressor motor is stopped in a magnetic floating system, and a chiller having the same.

According to an aspect of the present invention, there is provided a compressor driving apparatus including: a compressor having a compressor motor, a magnetic bearing, and a switching element, and applying a current to a bearing coil of the magnetic bearing, A bearing drive section for levitation or landing the rotor of the compressor motor from the magnetic bearing and a compressor motor drive section for rotating the compressor motor, wherein the compressor motor drive section drives the compressor motor with an AC power source And an inverter control unit for controlling the inverter based on the output current detected by the output current detection unit. The inverter control unit controls the inverter based on the output current based on the output current, And determines whether or not the motor is eccentric. If the eccentricity is detected, And controls the inverter so as to rotate the compressor motor based on the compensation current command value.

According to an aspect of the present invention, there is provided a chiller including a compressor including a compressor motor, a magnetic bearing, and a compressor driver for driving the compressor, wherein the compressor driver includes a switching element, A bearing driving part for levitation or landing the rotor of the compressor motor from the magnetic bearing by applying a current to the bearing coil of the magnetic bearing and a compressor motor driving part for rotating the compressor motor The compressor motor drive unit includes an inverter for outputting AC power to the compressor motor, an output current detection unit for detecting an output current flowing to the compressor motor, and an inverter control unit for controlling the inverter based on the output current detected by the output current detection unit. And the inverter control unit determines whether the motor is eccentric or not based on the output current, And, if the eccentricity, generates a compensation current command value based on the output current and, on the basis of the compensation current command value, and controls the compressor motor so as to control the inverter, so as to rotate.

In a compressor driving apparatus and a chiller having the same according to the present invention, the compressor driving apparatus includes a compressor motor having a compressor motor and a magnetic bearing, and a switching element. A bearing drive part for applying a current to levitate or land the rotor of the compressor motor from the magnetic bearing and a compressor motor drive part for rotating the compressor motor, And an inverter control unit for controlling the inverter on the basis of an output current detected by the output current detection unit, wherein the inverter control unit includes: Based on the output current, it is determined whether or not the motor is eccentric. If it is eccentric, By controlling the inverter to control the compressor so as to rotate the compressor motor based on the compensation current command value, it is possible to prevent reduction of the output power and pulse of the compressor motor at the time of occurrence of eccentricity of the compressor motor in the magnetic floating system do.

Particularly, when the eccentricity of the compressor motor is generated in the magnetic levitation system, the compressor motor is rotated through compensation control for the eccentricity, thereby reducing the output power and pulsation of the compressor motor.

On the other hand, when the rotor of the compressor motor is landed, by controlling the current flowing through the bearing coil to fall stepwise, it is possible to prevent the rotor of the compressor motor from being damaged when the compressor motor is stopped in the magnetic levitation system.

Particularly, when the rotor of the compressor motor is landed, by controlling the first mode in which the electric current stored in the bearing coil is discharged and the second mode in which the electric current flows in the bearing coil by the electric power stored in the capacitor, When the compressor motor stops, the rotor of the compressor motor can be soft lanfed, thus preventing damage to the rotor of the compressor motor. In addition, damage to the magnetic bearing can be prevented. Accordingly, the stability and reliability of the compressor driving apparatus and the chiller having the compressor driving apparatus are improved.

FIG. 1 is a view showing a configuration of a chiller according to an embodiment of the present invention.
Fig. 2 is a view showing the air conditioning unit of Fig. 1 in more detail.
3 is an example of an internal block diagram of the chiller of Fig.
Fig. 4 illustrates an example of an internal block diagram of the motor drive apparatus of Fig.
5 is an example of an internal circuit diagram of the motor driving apparatus of Fig.
6 is an internal block diagram of the inverter control unit of FIG.
7A is a view showing an example of the structure of the compressor of FIG.
7B is a cross-sectional view taken along line I-I 'of FIG. 7A.
Figure 7c is a side view of the compressor of Figure 7a.
Figures 8A-8C are diagrams that are referenced to illustrate the lifting and landing of the rotor in a bearing.
FIG. 9A is an example of an internal block diagram of the bearing drive unit of FIG.
FIG. 9B is an example of an internal block diagram of the bearing control unit of FIG. 9A.
10 is a view showing a current waveform applied to the bearing coil.
11 is a diagram showing an example of a current waveform applied to a bearing coil according to an embodiment of the present invention.
12A to 12C are circuit diagrams related to the current waveform of FIG.
13A to 13C are drawings referred to the eccentric description of the rotor of the compressor motor.
14 is an example of an internal block diagram of the inverter control unit according to the embodiment of the present invention.
15A to 15B are drawings referred to in the description of FIG.
16 is an example of an internal block diagram of an inverter control unit according to another embodiment of the present invention.
17 is a diagram referred to in the description of Figs. 14 and 16. Fig.
18 is a flowchart showing an operation method of the motor driving apparatus according to the embodiment of the present invention.

Hereinafter, the present invention will be described in detail with reference to the drawings.

The suffix "module" and " part "for components used in the following description are given merely for convenience of description, and do not give special significance or role in themselves. Accordingly, the terms "module" and "part" may be used interchangeably.

FIG. 1 is a view showing a configuration of a chiller according to an embodiment of the present invention.

Referring to the drawings, a chiller 100 includes an air conditioning unit 10 in which a refrigeration cycle is formed, a cooling tower 20 for supplying cooling water to the air conditioning unit 10, And a cold water consumer 30 through which cold water to be heat-exchanged circulates. The cold water consumer 30 corresponds to a device or a space for performing air conditioning using cold water.

Between the air conditioning unit 10 and the cooling tower 20 is provided a circulation flow passage 40 through which cooling water flows so that cooling water is circulated between the air conditioning unit 10 and the cooling tower 20.

The cooling water circulating flow path 40 is provided with a cooling water intake flow path 42 for guiding the cooling water to flow into the condenser 12 and a cooling water outflow path 42 for guiding the cooling water heated in the air conditioning unit 10 to the cooling tower 20 And includes a flow path 44.

At least one of the cooling water intake flow path 42 and the cooling water outflow flow path 44 may further include a cooling water pump 46 for flowing cooling water. As an example, FIG. 2 illustrates a state in which a cooling water pump 46 is installed in the cooling water intake flow path 42.

An outflow temperature sensor 47 for sensing the temperature of the cooling water flowing into the cooling tower 20 can be installed in the cooling water outflow passage 44. The outflow temperature sensor 47 for detecting the temperature of the cooling water An intake temperature sensor 48 for measuring the temperature can be provided.

A cold water circulation passage (50) is provided between the air conditioning unit (10) and the cold water consumer (30) so that cooling water can be circulated between the two. The cold water circulation passage 50 is connected to the cold water supply passage 52 and the cold water supply unit 10 so that the cold water can circulate between the cold water consumer 30 and the air conditioning unit 10. [ 30 to guide the cold water outflow passage 54 to the outside.

A cold water pump (56) for circulating cold water is provided in at least one of the cold water inlet flow path (52) and the cold water outlet flow path (54). FIG. 2 illustrates a state in which the cold water supply passage 52 is provided with the cold water pump 56.

In the present embodiment, the cold water consumer 30 is described as a water-cooled air conditioner for exchanging air with cold water. For example, the cold water consumer 30 includes an air handling unit (AHU, Air Handling Unit) that mixes indoor air and outdoor air, then exchanges the mixed air with cold water to introduce it into the room, And a bottom pipe unit embedded in the floor of the indoor unit. FIG. 2 is a side view of the cold water consumer 30, Respectively.

The cold water consumer 30 includes a casing 61, a cold water coil 62 installed inside the casing 61 and through which cold water passes, and a cooling water pipe 62 provided on both sides of the cold water coil 62, And blowers 63 and 64 for blowing air into the room. The blower includes a first blower 63 for allowing indoor air and outdoor air to be sucked into the casing 61 and a second blower 64 for blowing out air to the outside of the casing 61 .

The casing 61 includes an indoor air suction portion 65, an indoor air discharge portion 66, an ambient air suction portion 67, and an air conditioning air discharge portion.

When the blowers 63 and 64 are driven, a part of the air introduced through the indoor air suction part 65 is discharged to the indoor air discharge part 66 and the rest is discharged to the outdoor air suction part 67 And then passes through the cold water coil 62 to perform heat exchange. Thereafter, the heat exchanged mixed air flows into the room through the air conditioning air discharge unit 68.

Fig. 2 is a view showing the air conditioning unit of Fig. 1 in more detail.

Referring to the drawings, the air conditioning unit 10 includes a compressor 11 for compressing refrigerant, a condenser 12 for introducing high-temperature and high-pressure refrigerant compressed by the compressor 11, a refrigerant condensed in the condenser 12, And an evaporator 14 for evaporating the refrigerant decompressed in the inflator 13 and a driving unit 220 for operating the compressor 11.

The air conditioning unit 10 includes a suction pipe 101 installed at the inlet side of the compressor 11 and guiding the refrigerant from the evaporator 14 to the compressor 11 and a suction pipe 101 provided at the outlet side of the compressor 11, And a discharge pipe 102 for guiding the refrigerant from the evaporator 11 to the condenser 12.

The condenser (12) and the evaporator (14) can be constituted by a shell tubular heat exchanger so as to enable heat exchange between the refrigerant and water.

The condenser 12 includes a shell 121 forming an outer shell, an inlet 122 through which the refrigerant compressed by the plurality of compressors 11a, 11b and 11c installed on one side of the shell 121 flows, a shell 121, And an outlet 123 through which the refrigerant condensed in the condenser 12 flows out.

The condenser 12 is provided with a cooling water pipe 125 for guiding the flow of the cooling water in the shell 121 and a cooling water pipe 125 installed at the end of the shell 121 to supply the cooling water supplied from the cooling tower 20 to the water- And an outlet 128 for discharging the cooling water from the condenser 12 to the cooling tower 20 through the inlet 127 and the outlet channel 44.

In the condenser 12, the cooling water flows through the cooling water pipe 125, and heat exchange is performed with the refrigerant in the shell 121 flowing into the condenser 12 through the refrigerant inlet port 122.

The evaporator 14 includes a shell 141 that forms an outer appearance, an inlet 142 that is installed on one side of the shell 141 and through which the refrigerant expanded in the inflator 13 is supplied, And an outlet 143 through which the refrigerant evaporated in the evaporator 14 flows out to the compressor 11. The outlet 143 is connected to the suction pipe 101 and the evaporated refrigerant is transferred from the evaporator 14 to the compressor 11.

Also. The evaporator 14 includes a cold water pipe 145 installed inside the shell 141 for guiding the flow of cold water, an inlet 141 installed at one side of the shell 141 for introducing cold water into the cold water pipe 145 And an outlet 148 for discharging cold water circulated in the evaporator.

The inlet channel 52 and the outlet channel 54 are connected to the inlet 141 and the outlet 148 so that the cold water can circulate between the cold water coils 62 of the consumer 30.

Meanwhile, the plurality of drivers 220a, 220b, and 220c can drive the plurality of compressors 11a, 11b, and 11c, respectively.

On the other hand, each of the plurality of drivers 220a, 220b, and 220c may include a converter, an inverter, and the like.

3 is an example of an internal block diagram of the chiller of Fig.

The chiller 100 may include an input unit 120, a communication unit 130, a memory 140, a control unit 170, and a driving unit 220.

The input unit 120 may include an operation button, a key, and the like, and may output an input signal for turning on / off the chiller 100, setting an operation, and the like.

In particular, the input unit 120 may include a plurality of switches to which an ID is assigned corresponding to the plurality of drivers 220a, 220b, and 220c, according to the embodiment of the present invention.

The plurality of switches at this time may be a hardware switch, a dip switch, and a tact switch.

For example, the plurality of switches may be first to third switches 122P1, 122P2, and 122P3 to which IDs are assigned corresponding to the plurality of drivers 220a, 220b, and 220c.

The communication unit 130 can exchange data with a peripheral device, for example, a remote control device or the mobile terminal 600 by wire or wirelessly. For example, infrared (IR) communication, RF communication, Bluetooth communication, Zigbee communication, WiFi communication, and the like can be performed.

The memory 140 of the chiller 100 may store data necessary for the operation of the chiller 100. For example, data on operation time, operation mode, and the like at the time of operation of the driving unit 220 can be stored.

In addition, the memory 140 of the chiller 100 may store management data including power consumption information of the chiller, recommended operation information, current operation information, and product management information.

In addition, the memory 140 of the chiller 100 may store diagnostic data including operation information, operation information, and error information of the chiller.

The control unit 170 can control each unit in the chiller 100. For example, the control unit 170 can control the input unit 120, the communication unit 130, the memory 140, the driving unit 220, and the like.

At this time, as shown in FIG. 2, the driving unit 220 may include a plurality of driving units 220a, 220b, and 220c.

Each of the plurality of driving units 220a, 220b and 220c includes an inverter 420, an inverter control unit 430, and an inverter control unit 430 shown in FIG. 4 for driving the plurality of compressors 11a, 11b, A motor 230 may be provided.

The controller 170 may control the plurality of drivers 220a, 220b, and 220c to selectively operate according to the magnitude of the demand load.

Specifically, the controller 170 may control the inverters 420a, 420b, and 420c in the plurality of drivers 220a, 220b, and 220c to selectively operate according to the magnitude of the demand load.

On the other hand, the control unit 170 can control the corresponding plurality of driving units to operate in accordance with the turn-on states of the plurality of switches.

In particular, the control unit 170 can control the plurality of drivers to selectively operate according to the turn-on state of the plurality of switches and the size of the demand load.

Meanwhile, the compressor motor driving unit described in the present specification can be applied to a motorless motor driven by a sensorless method in which a position sensing unit such as a hall sensor for sensing a rotor position of a motor is provided, It can be a motor drive device that can be estimated.

Meanwhile, the compressor motor driving unit 220 according to the embodiment of the present invention may also be referred to as a compressor compressor motor driving unit 220.

Fig. 4 illustrates an example of an internal block diagram of the compressor driving unit of Fig.

Referring to the drawings, the compressor 11 may include a motor 230 and a bearing coil RB.

Accordingly, the compressor driving unit 220 may include a compressor motor driving unit 220a for driving the compressor motor, and a bearing driving unit 221a for driving the bearing coil RB. Meanwhile, in this specification, the compressor driving unit 220 may be referred to as a compressor driving apparatus.

The bearing drive unit 221a controls the rotor (not shown) of the motor for driving the impeller in the compressor 11 to float or land.

To this end, the bearing drive unit 221a may include a bearing control unit 435, a coil drive unit 437, and a bearing coil RB.

The bearing control unit 435 detects gap information from a gap sensor (CB in FIG. 9A) disposed around the bearing coil and current information (hereinafter referred to as " gap information ") from the bearing coil current detection unit And outputs the switching control signal Sci for controlling the coil driver 437 based on the received gap information and the current information IB.

Then, the coil driver 437 can turn on / off the switching element based on the switching control signal Sci. A magnetic field or the like is generated or extinguished in the bearing coil RB due to the turn-on or turn-off of the switching element in the coil driving unit 437 so that the rotor (not shown) of the motor is lifted or landed .

The compressor motor driving unit 220a in the compressor driving unit 220 of FIG. 4 may include a memory 270, an inverter control unit 430, an inverter 430, and the like.

The detailed operation of the compressor motor driving unit 220a will be described in more detail with reference to Fig.

5 is an example of an internal circuit diagram of the compressor motor driving unit of Fig.

The compressor motor driving unit 220a according to the embodiment of the present invention drives the motor in a sensorless manner and may include an inverter 420 and an inverter control unit 430 have.

The compressor motor driving unit 220a according to the embodiment of the present invention may include a converter 410, a dc voltage detection unit B, a smoothing capacitor C, and an output current detection unit E. The driving unit 220 may further include an input current detection unit A, a reactor L, and the like.

The inverter control unit 430 according to the embodiment of the present invention stores the diagnostic data including the time of occurrence of the error, the operation information at the occurrence of the error, and the status information in the memory 140 or the memory 270 Can be controlled.

Meanwhile, the inverter control unit 430 periodically controls operation information and state information to be temporarily stored in the memory 140 or the memory 270, and when the error occurs, the inverter control unit 430 periodically stores operation information, , And finally store the final state information in the memory 140 or the memory 270. [

On the other hand, when an error occurs, the inverter control unit 430 controls the memory 140 or the memory 270 to store operation information at the time of occurrence of an error, and stores operation information or state information after a predetermined time from the occurrence of the error, (140) or the memory (270).

The amount of data of the last operation information and the final state information stored in the memory 140 or the memory 270 is smaller than the amount of data of the operation information at the time of error occurrence or the amount of data of the operation information or state information after a predetermined time A larger one is preferable.

The reactor L is disposed between the commercial AC power source 405, etc. and the converter 410 to perform a power factor correcting or boosting operation. The reactor L may also function to limit the harmonic current due to the fast switching of the converter 410.

The input current detection section A can detect the input current is inputted from the commercial AC power source 405. [ To this end, a current transformer (CT), a shunt resistor, or the like may be used as the input current detector A. The detected input current is may be input to the inverter control unit 430 as a discrete signal in the form of a pulse.

The converter 410 converts the commercial AC power source 405, which has passed through the reactor L, into DC power and outputs the DC power. Although the commercial AC power source 405 is shown as a single-phase AC power source in the figure, it may be a three-phase AC power source. The internal structure of the converter 410 also changes depending on the type of the commercial AC power source 405.

Meanwhile, the converter 410 may include a diode without a switching element, and may perform a rectifying operation without a separate switching operation.

For example, in the case of a single-phase AC power source, four diodes may be used in the form of a bridge, and in the case of a three-phase AC power source, six diodes may be used in the form of a bridge.

On the other hand, the converter 410 may be, for example, a half-bridge type converter in which two switching elements and four diodes are connected, and in the case of a three-phase AC power source, six switching elements and six diodes may be used .

When the converter 410 includes a switching element, the boosting operation, the power factor correction, and the DC power conversion can be performed by the switching operation of the switching element.

The smoothing capacitor C smoothes the input power supply and stores it. In the drawing, one element is exemplified by the smoothing capacitor C, but a plurality of elements are provided so that the element stability can be ensured.

For example, when a direct current power from the solar cell is supplied to the smoothing capacitor C (not shown), the direct current power is supplied to the smoothing capacitor C It may be input directly or may be DC / DC converted and input. Hereinafter, the portions illustrated in the drawings are mainly described.

On the other hand, both ends of the smoothing capacitor C are referred to as a dc stage or a dc stage because the dc power source is stored.

The dc voltage detection unit B can detect the dc voltage Vdc at both ends of the smoothing capacitor C. [ For this purpose, the dc voltage detection unit B may include a resistance element, an amplifier, and the like. The detected dc voltage source Vdc can be input to the inverter control unit 430 as a discrete signal in the form of a pulse.

The inverter 420 includes a plurality of inverter switching elements and converts the smoothed DC power supply Vdc into a three-phase AC power supply va, vb, vc having a predetermined frequency by on / off operation of the switching element, And outputs it to the synchronous motor 230.

The inverter 420 includes a pair of upper arm switching elements Sa, Sb and Sc and lower arm switching elements S'a, S'b and S'c serially connected to each other, The switching elements are connected to each other in parallel (Sa & S a, Sb & S'b, Sc & S'c). Diodes are connected in anti-parallel to each switching element Sa, S'a, Sb, S'b, Sc, S'c.

The switching elements in the inverter 420 perform ON / OFF operations of the respective switching elements based on the inverter switching control signal Sic from the inverter controller 430. [ Thus, three-phase AC power having a predetermined frequency is output to the three-phase synchronous motor 230.

The inverter control unit 430 can control the switching operation of the inverter 420 based on the sensorless method. For this, the inverter control unit 430 can receive the output current io detected by the output current detection unit E.

The inverter control unit 430 outputs the inverter switching control signal Sic to the inverter 420 to control the switching operation of the inverter 420. [ The inverter switching control signal Sic is generated and output based on the output current io detected by the output current detection section E as a switching control signal of the pulse width modulation method (PWM). Detailed operation of the output of the inverter switching control signal Sic in the inverter control unit 430 will be described later with reference to Fig.

The output current detecting section E detects the output current io flowing between the inverter 420 and the three-phase motor 230. [ That is, the current flowing in the motor 230 is detected. The output current detection unit E can detect all of the output currents ia, ib, ic of each phase or can detect the output currents of two phases using the three-phase balance.

The output current detection unit E may be located between the inverter 420 and the motor 230. For current detection, a current transformer (CT), a shunt resistor, or the like may be used.

Three shunt resistors are placed between the inverter 420 and the synchronous motor 230 or the three lower arm switching elements S'a, S'b, S'c To be connected to each other. On the other hand, it is also possible to use two shunt resistors using three phase equilibrium. On the other hand, when one shunt resistor is used, the shunt resistor may be disposed between the capacitor C and the inverter 420 described above.

The detected output current io can be applied to the inverter control unit 430 as a pulse discrete signal and the inverter switching control signal Sic is generated based on the detected output current io do. Hereinafter, the detected output current io may be described as being three-phase output currents (ia, ib, ic).

On the other hand, the three-phase motor 230 has a stator and a rotor, and each phase alternating current power of a predetermined frequency is applied to a coil of a stator of each phase (a, b, c) .

The motor 230 may be, for example, a Surface Mounted Permanent Magnet Synchronous Motor (SMPMSM), an Interior Permanent Magnet Synchronous Motor (IPMSM) A synchronous motor (Synchronous Reluctance Motor; Synrm), and the like. Among them, SMPMSM and IPMSM are permanent magnet applied Permanent Magnet Synchronous Motor (PMSM), and Synrm is characterized by having no permanent magnet.

6 is an internal block diagram of the inverter control unit of FIG.

6, the inverter control unit 430 includes an axis conversion unit 310, a speed calculation unit 320, a current command generation unit 330, a voltage command generation unit 340, an axis conversion unit 350, And a switching control signal output unit 360.

The axial conversion unit 310 receives the three-phase output currents ia, ib, ic detected by the output current detection unit E and converts the three-phase output currents ia, ib, ic into the two-phase currents iα, iβ in the stationary coordinate system.

On the other hand, the axis converting unit 310 can convert the two-phase current i ?, i? Of the still coordinate system into the two-phase current id, iq of the rotating coordinate system.

)와 연산된 속도(

)를 출력할 수 있다.Based on the two-phase current (i?, I?) Of the stationary coordinate system changed in the axis by the axis converting unit 310, the speed calculating unit 320 calculates the speed

) And the calculated speed (

Can be output.

)와 속도 지령치(ω^* _r)에 기초하여, 전류 지령치(i^* _q)를 생성한다. 예를 들어, 전류 지령 생성부(330)는, 연산 속도(

)와 속도 지령치(ω^* _r)의 차이에 기초하여, PI 제어기(335)에서 PI 제어를 수행하며, 전류 지령치(i^* _q)를 생성할 수 있다. 도면에서는, 전류 지령치로, q축 전류 지령치(i^* _q)를 예시하나, 도면과 달리, d축 전류 지령치(i^* _d)를 함께 생성하는 것도 가능하다. 한편, d축 전류 지령치(i^* _d)의 값은 0으로 설정될 수도 있다. On the other hand, the current command generation unit 330 generates the current command

(I ^* _q ) on the basis of the speed command value? ^* _R and the speed command value? ^* _R. For example, the current command generation section 330 generates the current command

The PI controller 335 performs the PI control based on the difference between the speed command value? ^* _R and the speed command value? ^* _R , and generates the current command value i ^* _q . In the figure, the q-axis current command value (i ^* _q ) is exemplified by the current command value, but it is also possible to generate the d-axis current command value (i ^* _d ) unlike the figure. On the other hand, the value of the d-axis current command value i ^* _d may be set to zero.

On the other hand, the current command generation section 330 may further include a limiter (not shown) for limiting the current command value (i ^* _q ) so that the current command value (i ^* _q ) does not exceed the allowable range.

Next, the voltage command generating unit 340 generates the voltage command generating unit 340 with the d-axis and q-axis currents (i _d , i _q ) axially transformed into the two-phase rotational coordinate system in the axial converting unit and the current command value based on ^{_{i * d, i * q)}} , and generates a d-axis, q-axis voltage command value ^{_{(v * d, v * q}} ). For example, the voltage command generation unit 340 performs PI control in the PI controller 344 based on the difference between the q-axis current (i _q ) and the q-axis current command value (i ^* _q ) It is possible to generate the axial voltage command value v ^* _q . The voltage command generation unit 340 performs PI control in the PI controller 348 based on the difference between the d-axis current i _d and the d-axis current command value i ^* _d , It is possible to generate the command value v ^* _d . The voltage command generator 340 may further include a limiter (not shown) for limiting the level of the d-axis and q-axis voltage command values v ^* _d and v ^* _q so as not to exceed the permissible range .

On the other hand, the generated d-axis and q-axis voltage command values (v ^* _d and v ^* _q ) are input to the axial conversion unit 350.

)와, d축, q축 전압 지령치(v^* _d,v^* _q)를 입력받아, 축변환을 수행한다.The axis transforming unit 350 transforms the position calculated by the velocity calculating unit 320

) And the d-axis and q-axis voltage command values (v ^* _d , v ^* _q ).

)가 사용될 수 있다.First, the axis converting unit 350 performs conversion from a two-phase rotating coordinate system to a two-phase stationary coordinate system. At this time, the position calculated by the speed calculator 320 (

) Can be used.

Then, the axial conversion unit 350 performs conversion from the two-phase stationary coordinate system to the three-phase stationary coordinate system. Through this conversion, the axial conversion unit 1050 outputs the three-phase output voltage instruction values v ^* a, v ^* b, v ^* c.

The switching control signal output section 360 generates the switching control signal Sic for inverter according to the pulse width modulation (PWM) method based on the three-phase output voltage instruction values v ^* a, v ^* b and v ^* And outputs it.

The output inverter switching control signal Sic may be converted into a gate driving signal in a gate driving unit (not shown) and input to the gate of each switching element in the inverter 420. As a result, the switching elements Sa, S'a, Sb, S'b, Sc, and S'c in the inverter 420 perform the switching operation.

7A is a view showing an example of the structure of the compressor of FIG.

Referring to the drawings, an impeller 701 and a rotor 702 may be disposed inside the compressor 11. [ The rotor 702 of the compressor motor can be connected to the impeller 701 disposed at one side of the inside of the compressor 11. [

On the other hand, the rotor 702 extends in the z-axis direction, and a T-shaped trust plate 706 can be formed near the end of the rotor 702.

A frame 704 is disposed in the case CS of the compressor 11 and a plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4 and RBC1 to RBC2 may be disposed in the frame 704. [

The plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4 and RBC1 to RBC2 may include a bobbin (not shown) and a bearing coil (not shown) wound around the bobbin.

When a current does not flow through the bearing coils of the plurality of magnetic bearings (RBa1 to RBa4, RBb1 to RBb4, RBC1 to RBC2), the surface of some of the magnetic bearings contacts the rotor 702, Magnetic levitation occurs from the surface of some of the magnetic bearings.

After the magnetic levitation, the rotor 702 of the compressor motor 230 rotates. Particularly, the rotation speed of the rotor 702 can be varied by the control of the inverter control unit 430 shown in Figs. .

The magnetic bearings RBa1 to RBa4 and RBb1 to RBb4 of the plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4 and RBC1 to RBC2 are radial magnetic bearings, The rotation can be controlled. That is, the x and y axes can be controlled.

On the other hand, the magnetic bearings RBa1 to RBa4 and RBb1 to RBb4 of the plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4 and RBC1 to RBC2 are disposed apart from the rotor 702 in the z- .

On the other hand, the magnetic bearings RBC1 to RBC2 among the plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4 and RBC1 to RBC2 are axial magnetic bearings and can control the rotation of the rotor in the axial direction have. That is, the z-axis can be controlled.

On the other hand, the magnetic bearings RBC1 to RBC2 among the plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4 and RBC1 to RBC2 may be disposed apart from a trust plate extending in the y-axis direction.

On the other hand, a plurality of gap sensors (CBa1 to CBa4, CBb1 to CBb4) for sensing the gap between the magnetic bearing and the rotor 702 are provided around the plurality of magnetic bearings (RBa1 to RBa4, RBb1 to RBb4, RBC1 to RBC2) CBb4, CBC1 to CBC2) can be arranged.

Some of the gap sensors CBC1 to CBC2 among the plurality of gap sensors CBa1 to CBa4, CBb1 to CBb4 and CBC1 to CBC2 are radial gap sensors that sense the position of the x, .

Some of the gap sensors CBC1 to CBC2 among the plurality of gap sensors CBa1 to CBa4, CBb1 to CBb4 and CBC1 to CBC2 can sense the position of the z-axis rotor as an axial gap sensor.

Meanwhile, the plurality of gap sensors CBa1 to CBa4, CBb1 to CBb4, and CBC1 to CBC2 may be implemented as hall sensors.

The bearing control unit 435 controls the plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4 and RBC1 to RBC2 based on the gap information from the plurality of gap sensors CBa1 to CBa4, CBb1 to CBb4 and CBC1 to CBC2 , In particular, the currents applied to the bearing coils of the plurality of magnetic bearings (RBa1 to RBa4, RBb1 to RBb4, RBC1 to RBC2) can be controlled.

7B is a cross-sectional view taken along line I-I 'of FIG. 7A.

Referring to FIG. 7A, RBb1 to RBb, which are radial magnetic bearings, may be disposed apart from each other according to a cross section taken along the line I-I 'in FIG. 7A.

The rotor 702 is disposed apart from the inner surface BR of the radial magnetic bearings RBb1 to RBb4. The rotor 702 of Fig. 7B shows floating.

Figure 7c is a side view of the compressor of Figure 7a.

Referring to the drawings, axial magnetic bearings RBC1 to RBC2 may be disposed on both sides of a trust plate 706 near the end of the rotor 702. [

On the other hand, a rotor 702 can be disposed at the lower end of the rust plate 706.

Figures 8A-8C are diagrams that are referenced to illustrate the lifting and landing of the rotor in a bearing.

First, FIG. 8A shows a state in which the current is not applied to the bearing coils of the plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4, RBC1 to RBC2, and the current is not applied to the inner surfaces BR of the radial magnetic bearings RBb1 to RBb4 The case where the rotor 702 is brought into contact is exemplified.

Next, FIG. 8B shows a state in which the current is applied to the bearing coils of the plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4, RBC1 to RBC2, and the current is applied from the inner surface BR of the radial magnetic bearings RBb1 to RBb4 The electrons 702 are shown floating.

On the other hand, the bearing control unit 435 can control the gap between the inner surface BR of the radial magnetic bearings RBb1 to RBb4 and the rotor 702 to be constant.

Next, FIG. 8C shows a state in which the current is not applied to the bearing coils of the plurality of magnetic bearings RBa1 to RBa4, RBb1 to RBb4, RBC1 to RBC2, and the current is not applied to the inner surfaces BR of the radial magnetic bearings RBb1 to RBb4 , And a case where the rotor 702 lands.

On the other hand, the inner surface BR of the radial magnetic bearings RBb1 to RBb4 in Figs. 8A to 8C may be the inner surface of the frame 704 in Fig. 7A.

FIG. 9A is an example of an internal block diagram of the bearing drive unit of FIG.

Referring to the drawing, the bearing driving unit 221a includes a bearing coil RB, a coil driving unit 439 for applying a current to the bearing coil RB, a bearing coil current detecting unit for detecting a current applied to the bearing coil RB, A gap sensor CB for sensing a gap between the bearing coil RB and the rotor 702, gap information Gp from the gap sensor CB, a bearing coil current detector M And a bearing control section 435 for outputting a switching control signal Sci to the coil driving section 439 based on the current IB from the control section 431. [

FIG. 9B is an example of an internal block diagram of the bearing control unit of FIG. 9A.

Referring to the drawing, the bearing control unit 435 may include a current command generation unit 910 and a duty generation unit 920.

The current command generation section 910 generates the current command value I ^* B based on the gap information Gp from the gap sensor CB and the gap command value Gp *. For example, the current command generation section 330 performs PI control in the PI controller 914 based on the difference between the gap information Gp and the gap command value Gp *, and outputs the current command value I ^* B, Lt; / RTI >

On the other hand, the current command generation section 910 may further include a limiter (not shown) for limiting the current command value I ^* B so that the current command value I ^* B does not exceed the allowable range.

The duty generating unit 920 generates the current command value I ^* B based on the current information IB from the bearing coil current detecting unit M and the current command value I ^* B. For example, the duty generator 920 performs PI control in the PI controller 924 based on the difference between the current information IB and the current command value I ^* B, and performs switching control including the duty command It is possible to generate the signal Sci.

Meanwhile, the duty generator 920 may further include a limiter (not shown) for limiting the level so that the duty command value does not exceed the permissible range.

For example, when the gap between the magnetic bearing and the rotor 702 is smaller than the gap command value Gp *, the bearing control unit 435 sets the switching control signal Sci whose duty increases to increase the gap Can be output.

At this time, the switching control signal Sci whose duty increases may mean that the switching period is increased and the duty is increased within the increased switching period.

Alternatively, the switching control signal Sci whose duty increases may mean that the duty increases within a constant switching period.

As another example, when the gap between the magnetic bearing and the rotor 702 is larger than the gap command value Gp *, the bearing control section 435 outputs the switching control signal Sci whose duty is decreased so that the gap is reduced can do.

According to the operation of the bearing control unit 435, the gap can be maintained constant when the rotor rotates.

On the other hand, the bearing control unit 435 can output a switching control signal Sci whose duty increases as the gap between the magnetic bearing and the rotor 702 increases stepwise when the rotor is floated.

On the other hand, the bearing control unit 435 can output a switching control signal Sci whose duty decreases when the rotor is landed, such that the gap between the magnetic bearing and the rotor 702 decreases stepwise.

10 is a view showing a current waveform applied to the bearing coil.

Referring to the drawing, the current waveform Ibrx represents the current waveform applied to the bearing coil.

The Pa period represents the rotor lifetime, the Pb period represents the rotor rotation period since the rotor floats, and the Pc period represents the rotor landing period.

On the other hand, when the current applied to the bearing coil is stopped in the rotor landing period Pc, the current applied to the bearing coil is rapidly lowered as shown in the drawing.

In this case, the flying rotor 702 is landed as shown in FIG. 8C. At this time, a physical collision occurs between the rotor 702 and the bearing BR due to the rapid current fall. As a result, a physical abrasion phenomenon occurs between the rotor 702 and the bearing BR, and furthermore, the possibility of failure of the gap sensor also increases.

In order to solve such a problem, the present invention proposes a method for preventing the rotor of the compressor motor from being damaged when the compressor motor is stopped in the magnetic floating system. This will be described with reference to FIG. 11 and the following figures.

11 is a diagram showing an example of a current waveform applied to a bearing coil according to an embodiment of the present invention, and Figs. 12A to 12C are circuit diagrams related to the current waveform of Fig.

First, referring to Fig. 11, the current waveform Ibrm1 shows an example of a current waveform applied to the bearing coil according to the embodiment of the present invention.

The P1 period represents the rotor lifting period, the P2 period represents the rotor rotation period since the rotor floats, and the P3 period represents the rotor landing period.

According to the embodiment of the present invention, during the rotor landing period P3 of the compressor motor 230, the bearing control unit 435 controls the current flowing in the bearing coil RB to be stepwise lowered .

In particular, when the rotor 702 of the compressor motor 230 is landed, the bearing control unit 435 controls the first mode in which the electric current stored in the bearing coil RB is discharged and the electric power stored in the capacitor Cbs, The second mode in which the current flows through the coil RB can be controlled to be repeated.

Referring to the drawing, during a rotor landing period P3, a period P3b in which a first mode in which a current stored in the bearing coil RB is discharged is performed, and a second mode in which a current flows in the bearing coil RB And the period P3a is repeated.

In particular, during the rotor landing period P3, the period P3b during which the first mode is performed is preferably longer than the period P3a during which the second mode is performed. Thereby, it is possible to control so that the current flowing through the bearing coil RB is stepwise lowered.

Accordingly, when the compressor motor is stopped in the magnetic levitation mode, the rotor of the compressor motor can be soft lanfed, and thus the rotor of the compressor motor can be prevented from being damaged. In addition, damage to the magnetic bearing, the gap sensor, and the like can be prevented. Further, stability and reliability of the compressor driving apparatus 220 and the chiller 100 having the compressor driving apparatus 220 are improved.

11, the period P3b in which the first mode is performed and the period P3a in which the second mode is performed are all constant during the rotor landing period P3, but the present invention is not limited thereto .

The bearing control unit 435 controls the second mode and the first mode to be repeated when the rotor 702 of the compressor motor 230 is lifted. When the rotor 702 of the compressor motor 230 is landed, The first period in which the first mode is performed and the second period in which the second mode is performed are respectively a third period in which the first mode is performed when the rotor 702 of the compressor motor 230 is floated, 2 mode is performed in the fourth period.

In the drawing, during a rotor lifting period P1, a period P1a during which a second mode in which current flows through the bearing coil RB and a first mode during which the current stored in the bearing coil RB is discharged are performed (P1b) is repeated.

In particular, during the rotor lifting period P1, the period P1a during which the second mode is performed is preferably longer than the period P1b during which the first mode is performed. Thereby, it is possible to control so that the current flowing through the bearing coil RB is stepped up.

On the other hand, for quick floating and soft landing, during the rotor landing period P3, the period P3a during which the second mode is performed, during the rotor lifting period P1, Is shorter than the period P1a.

On the other hand, for the quick floating and soft landing, the period P3b during which the first mode is performed during the rotor landing period P3 is the same as the period during which the first mode is performed during the rotor lifting period P1 Is shorter than the period P1b.

Accordingly, when the compressor motor is stopped in the magnetic levitation mode, the rotor of the compressor motor can be stably and softly landed.

The bearing control unit 435 repeats the first mode and the second mode when the compressor motor 230 floats and rotates. When the rotor 702 of the compressor motor 230 is landed, The first period in which the first mode is performed and the second period in which the second mode is carried out are respectively a fifth period in which the first mode is performed and a sixth period in which the second mode is performed, , It can be controlled to be longer. Accordingly, when the compressor motor is stopped in the magnetic levitation mode, the rotor of the compressor motor can be stably and softly landed.

In the figure, a period P2a in which a second mode in which a current flows in the bearing coil RB is performed during the rotor rotation period P2, and a first mode in which the current stored in the bearing coil RB is discharged The period P2b is repeated.

Particularly, during the rotor rotation period P2, the period P2a in which the second mode is performed and the period P2b in which the first mode is performed may be substantially the same. Thereby, the current flowing through the bearing coil RB can be controlled to maintain a constant level, and as a result, the gap between the rotor 702 and the magnetic bearing can be kept constant.

On the other hand, for soft landing, a period P3a during which the second mode is performed during the rotor landing period P3 corresponds to a period P2a during which the second mode is performed during the rotor rotation period P2 ). ≪ / RTI >

On the other hand, for soft landing, a period P3b during which the first mode is performed during the rotor landing period P3 is shorter than a period P2b during which the first mode is performed during the rotor lifting period P1 ). ≪ / RTI >

Accordingly, when the compressor motor is stopped in the magnetic levitation mode, the rotor of the compressor motor can be stably and softly landed.

Since the period P2a during which the second mode is performed during the rotor rotation period P2 is shorter than the period P3a during which the second mode is performed during the rotor landing period P3, ) And the magnetic bearing can be stably and constantly maintained.

Since the period P2b during which the first mode is performed during the rotor rotation period P2 is shorter than the period P3b during which the first mode is performed during the rotor landing period P3, ) And the magnetic bearing can be stably and constantly maintained.

12A, the coil driver 1200 includes a capacitor Cbs for storing a DC power supply Vbs, a first switching element Sb1 connected between both ends of the capacitor Cbs, A second diode element Db2 connected between the first switching element Sb1 and the first diode element Db1 in parallel between the diode element Db1 and the capacitor Cbs, (Sb2).

The bearing coil RB can be connected between the first switching element Sb1 and the first diode element Db1 and between the second diode element Db2 and the second switching element Sb2 have.

That is, the DC power source Vbs from the DC power supply unit 805 is stored in the capacitor Cbs, and the first switching device Sb1 is connected between one end of the capacitor Cbs and one end of the bearing coil RB Can be connected.

The first diode element Db1 may be connected between the other end of the capacitor Cbs and one end of the bearing coil RB.

The second diode element Db2 may be connected between one end of the capacitor Cbs and the other end of the bearing coil RB.

The second switching element Sb2 can be connected between the other end of the capacitor Cbs and the other end of the bearing coil RB.

The bearing control unit 435 controls the first switching device Sb1 and the second switching device Sb2 so that the second mode in which the current flows to the bearing coil RB is performed by the power source stored in the capacitor Cbs, (Sb2) can be simultaneously turned on. Such a second mode may be referred to as a magnetization mode. Thereby, energy can be accumulated in the bearing coil RB.

12B, the capacitor Cbs, the first switching element Sb1, the bearing coil RB, the second switching element Sb1, and the second switching element Sb2 are turned on by simultaneously turning on the first switching element Sb1 and the second switching element Sb2. Sb2) of the first current path Ipath1.

On the other hand, as shown in FIG. 12C, only one of the first switching device Sb1 and the second switching device Sb2 is operated so that the first mode in which the current stored in the bearing coil RB is performed is performed by the bearing control section 435 Can be turned on. In the figure, it is illustrated that the first switching element Sb1 is turned off and the second switching element Sb2 is turned on. Such a first mode may be referred to as a freewheeling mode. Thereby, the energy stored in the bearing coil RB can be discharged.

12C, the second switching element Sb2, the bearing coil RB, and the second current path Ipath2, which sequentially flow along the first diode element Db1, are turned on by the second switching element Sb2 being turned on. ).

On the other hand, the first mode is performed by the second current path Ipath2 in Fig. 12C, and the current flowing in the bearing coil RB is lowered. By the first current path Ipath1 in Fig. 12B, So that the current flowing in the bearing coil RB rises.

On the other hand, in the current waveform Ibrm1 of Fig. 11, the solid line region is a region in which the second mode is performed, as shown in Fig. 12B, and the dotted line region is a region in which the first mode is performed, as shown in Fig.

Hereinafter, with reference to Figs. 12B and 12C, the operation when the rotor 702 of the compressor motor 230 is lifted, rotated, and landed will be described again.

The bearing control unit 435 controls the first mode in which one of the first switching device Sb1 and the second switching device Sb2 is turned on during the period P3 when the rotor 702 of the compressor motor 230 is landed, And a second mode in which both the first switching device Sb1 and the second switching device Sb2 are turned on by the power source stored in the capacitor Cbs.

The bearing control unit 435 controls the second mode and the first mode to be repeated during the P1 period when the rotor 702 of the compressor motor 230 is lifted and the rotor 702 A first period during which one of the first switching device Sb1 and the second switching device Sb2 is turned on and a second period during which the first switching device Sb1 and the second switching device Sb2 are both turned on The third period in which the first mode is performed and the second period in which both the first switching device Sb1 and the second switching device Sb2 are both on the rotor 702 side of the compressor motor 230, It is preferable that the second period is shorter than the fourth period, which is turned on.

On the other hand, when the compressor motor 230 floats and rotates, the first mode and the second mode are repeated. When the rotor 702 of the compressor motor 230 is landed, the first switching device Sb1 and the second The first period in which any one of the switching elements Sb2 is turned on and the second period in which both the first switching element Sb1 and the second switching element Sb2 are turned on are the same During the fifth period in which one of the first switching device Sb1 and the second switching device Sb2 is turned on during the rotation and when the first switching device Sb1 and the second switching device Sb2 are both turned on The sixth period is preferably longer.

On the other hand, there is a case where eccentricity occurs when the rotor of the compressor motor 230 rotates after the rotor portion of the compressor motor 230 is rotated. This will be described with reference to FIG. 13A and the like.

13A to 13C are drawings referred to the eccentric description of the rotor of the compressor motor.

13A illustrates an example in which the eccentricity occurs when the compressor motor 230 rotates the rotor 702 after the compressor motor 230 moves on the rotor 702 and the rotor 702 is irregularly positioned do.

In the figure, it is illustrated that the rotor 702 moves around the inner surface BR of the magnetic bearing while moving irregularly. The eccentricity as shown in FIG. 13A can be called dynamic eccentricity.

13B shows a state in which the eccentricity occurs when the compressor motor 230 rotates the rotor 702 after the compressor motor 230 moves on the rotor 702 and the rotor 702 is eccentrically rotated .

As shown in the drawing, the position of the rotor 702 is hardly changed, but it can be located at a specific position on the inner surface BR of the magnetic bearing. The eccentricity as shown in Fig. 13B can be called static eccentricity.

On the other hand, according to the dynamic eccentricity of Fig. 13A or the static eccentricity of Fig. 13B, an unbalance occurs in the three-phase line voltages Vabx, Vbcx, Vcax of the compressor motor 230 as shown in Fig. .

According to the dynamic eccentricity of Fig. 13A or the static eccentricity of Fig. 13B, pulsation occurs in the output power Px of the compressor motor 230 as shown in Fig. 13C, the output power is not constant, Further, the output power is lowered.

Accordingly, the present invention proposes a method for preventing the output power reduction and the pulsation of the compressor motor 230 by the dynamic eccentricity of FIG. 13A or the static eccentricity of FIG. 13B. This will be described with reference to FIG.

FIG. 14 is an internal block diagram of an inverter control unit according to an embodiment of the present invention, and FIGS. 15A to 15B are views referencing the description of FIG.

Referring to the drawings, a compressor motor driving unit 220a according to an embodiment of the present invention includes an inverter 420 for outputting an AC power to a compressor motor 230, an inverter 420 for detecting an output current flowing to the compressor motor 230, An inverter control unit 1400 for controlling the inverter 420 based on the output current detected by the output current detection unit.

The inverter control unit 1400 according to the embodiment of the present invention determines whether or not the motor 230 is eccentric based on the output current io or ia, ib, ic from the output current detection unit E, In the case of eccentricity, a compensation current instruction value based on the output current (io or ia, ib, ic) is generated and based on the compensation current instruction value icp, the inverter 420 is controlled so as to rotate the compressor motor 230 . Thus, when the eccentricity of the compressor motor occurs in the magnetic levitation mode, the output power of the compressor motor 230 can be reduced and pulsation can be prevented.

On the other hand, the inverter control unit 1400 determines the imbalance of the phase currents flowing through the compressor motors 230 and 230 based on the output currents (io or ia, ib, ic) It is possible to extract a reverse phase current and generate a compensation current instruction value icp based on the normal phase current and the reverse phase current.

The inverter control unit 1400 includes a position estimating unit 315 that estimates the rotor position of the compressor motor 230 based on the output current and a position estimating unit 315 that estimates the rotor position of the compressor motor 230 based on the estimated rotor position. A constant velocity compensation unit 317 for generating a compensation current instruction value icp based on the output current, and a current command value generating unit 325 for generating a current command value based on the calculated speed and the speed command value A voltage command generator 340 for generating a voltage command value based on the generated current command value and the compensation current command value icp from the constant-current compensation unit 317; And a switching control signal output unit 360 for outputting an inverter switching control signal Sic for controlling the inverter 420. [

The speed calculator 320, the current command generator 330, the voltage command generator 340 and the switching control signal output unit 360 of FIG. 14 correspond to the speed calculator 320, the current command generator 330, a voltage command generation unit 340, and a switching control signal output unit 360. [

On the other hand, the normal / reverse compensation unit 317 includes a normal phase current calculation unit 1510 for extracting a normal phase current and a reverse phase current based on the output current (io or ia, ib, ic) And a compensation current command output unit 1520 for generating a compensation current instruction value icp based on the minute current and the reverse phase current.

The normal phase current calculation unit 1510 calculates the phase difference between the normal partial vectors IAP, IBP and ICP based on the output current io or ia, ib, , IBN and ICN) and extract the normal and negative phase currents based on the separated normal fraction vectors (IAP, IBP, ICP) and the inverse phase distribution vectors (IAN, IBN, ICN).

Specifically, the normal-phase-current calculator 1510 determines whether the current is unbalanced based on the output current (io or ia, ib, ic) and determines whether the output current io or ia, ib, Is outside the allowable range, it can be judged as a current imbalance.

On the other hand, the compensation current command output section 1520 outputs the compensated current command output section 1520 based on the separated normal fraction vectors IAP, IBP, ICP and the inverse phase distribution vectors IAN, IBN, ICN as shown in FIG. To generate the compensation vector IA, IB, IC.

Then, the compensation current command output unit 1520 can generate the compensation current instruction value icp based on the eccentricity compensation vectors IA, IB, IC.

15A is a circuit diagram of the compensation current command output section 1520. The compensation current command output section 1520 includes a compensation controller 1522 for performing compensation control based on the normal and negative phase currents outputted from the normal phase current calculation section 1510, And a calculator 1525 for calculating the output current io or ia, ib, ic from the compensation controller 1522 and outputting the compensation current instruction value icp.

As described above, when the eccentricity of the compressor motor 230 is generated in the magnetic levitation mode, the compressor motor 230 is rotated through compensation control for the eccentricity, thereby preventing reduction and pulsation of the output power of the compressor motor 230 .

16 is an example of an internal block diagram of an inverter control unit according to another embodiment of the present invention.

The inverter control unit 1600 of FIG. 16 is similar to the inverter control unit 1400 of FIG. 14 except that the normal / reverse compensation unit 317 is provided in the speed calculation unit 320.

The inverter control unit 1600 according to another embodiment of the present invention includes a position estimating unit 1600 for estimating the rotor position of the compressor motors 230 and 230 based on the output currents io or ia, (Io or ia, ib, ic) based on the estimated rotor position and the compensation current command value icp based on the output current (io or ia, ib, ic) A current command generation unit 330 for generating a current command value based on the calculated speed and the speed command value, a current command value generating unit 330 for generating a current command value, and a compensation current command value icp, And a switching control signal output unit 360 for outputting an inverter switching control signal Sic for controlling the inverter 420 based on the voltage command value.

Thus, when the eccentricity of the compressor motor occurs in the magnetic levitation mode, the output power of the compressor motor 230 can be reduced and pulsation can be prevented.

17 is a diagram referred to in the description of Figs. 14 and 16. Fig.

Referring to the drawing, when the dynamic eccentricity of FIG. 13A or the static eccentricity of FIG. 13B occurs, an unbalance is applied to the three-phase line voltage Vabx, Vbcx, Vcax of the compressor motor 230 as shown in FIG. .

As shown in FIG. 17B, pulsation occurs in the output power Px of the compressor motor 230, the output power becomes unstable, and further the output power decreases.

Accordingly, in the present invention, the inverter control unit 1400 of Fig. 14 or the inverter control unit 1600 of Fig. 16 is used to generate the compensation current command value icp for the eccentricity of the rotor, and the compensation current command value icp to control the inverter 420 so that the compressor motor 230 rotates.

Thus, the three-phase line voltages Vab, Vbc and Vca of the compressor motor 230, which are eccentrically compensated, can be irregularly pulsated as shown in FIG. 17 (c) , The output power P of the output signal Ss is kept at a constant level without substantially pulsing as shown in Fig. 17 (d).

That is, according to the present invention, the inverter control unit 1400 of FIG. 14 or the inverter control unit 1600 of FIG. 16 can reduce the output power and pulsation of the compressor motor 230 at the time of eccentricity of the compressor motor in the magnetic floating system .

18 is a flowchart showing an operation method of the motor driving apparatus according to the embodiment of the present invention.

Referring to the drawings, an inverter control unit 1400 or 1600 in a compressor motor driving apparatus 220a generates a current command value and a voltage command value based on a speed command value w ^* and generates an inverter switching control signal (S1810).

In accordance with the inverter switching control signal, the inverter 420 switches, and thus the motor 230 is driven (S1815).

Next, the output current detecting section E detects the output current flowing to the motor 230, that is, the three-phase current (S1820).

The detected output current (io or ia, ib, ic) is input to the inverter control unit 1400 or 1600, and the normal / reverse compensation unit 317 determines whether the current is unbalanced (S1825).

For example, the normal-phase-phase current calculation unit 1510 in the in-phase-compensation unit 317 determines whether the current is unbalanced based on the output current (io or ia, ib, ic) (io or ia, ib, ic) is out of the allowable range, the current imbalance can be determined.

When a current imbalance occurs, the normal-phase-phase current arithmetic section 1510 in the in-phase-compensator 317 decomposes the normal-current and the reverse-phase currents from the detected output current io or ia, ib, ic (S1830 ).

Then, the compensation current command output unit 1520 in the normal / reverse compensation unit 317 generates the compensation current instruction value icp based on the normal normal current and the reverse phase current detected (S1835).

The voltage command generation unit 340 generates a voltage command value based on the compensation current command value icp and the current command value from the current command generation unit 330. [ The switching control signal output unit 360 outputs the switching control signal Sic to the inverter 420 based on the voltage command value and drives the motor 230 accordingly (S1840).

In this way, by controlling the inverter 420 so as to rotate the compressor motor 230 on the basis of the compensation current instruction value icp, the compressor motor 230 can be operated at the eccentricity of the compressor motor 230 in the magnetic levitation mode, It is possible to prevent output power reduction and pulsation of the output power of the inverter.

Particularly, when the eccentricity of the compressor motor 230 is generated in the magnetic levitation mode, the output of the compressor motor 230 can be prevented from being reduced and pulsated by rotating the compressor motor 230 through compensation control for eccentricity.

Therefore, even when the eccentricity occurs, the stability at the time of rotation of the compressor motor 230 is improved. As a result, the stability of the compressor driving apparatus 220 and the chiller 100 having the compressor driving apparatus 220 can be improved.

The compressor driving apparatus and the chiller having the compressor driving apparatus according to the embodiment of the present invention are not limited to the configuration and method of the embodiments described above but the embodiments can be applied to various implementations All or some of the examples may be selectively combined.

The compressor driving apparatus of the present invention and the operating method of the chiller having the compressor driving apparatus of the present invention can be implemented as a processor readable code on a recording medium readable by a processor provided in a compressor driving apparatus and a chiller having the same. The processor-readable recording medium includes all kinds of recording apparatuses in which data that can be read by the processor is stored.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is to be understood that the invention is not limited to the disclosed exemplary embodiments, but, on the contrary, It will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the present invention.

Claims (10)

A compressor having a compressor motor and a magnetic bearing;
A bearing driver having a switching element and applying a current to a bearing coil of the magnetic bearing in accordance with a switching operation to levitate or land the rotor of the compressor motor from the magnetic bearing;
And a compressor motor driving unit for rotating the compressor motor,
The compressor motor driving unit includes:
An inverter for outputting AC power to the compressor motor;
An output current detector for detecting an output current flowing to the compressor motor;
And an inverter control unit for controlling the inverter based on the output current detected by the output current detection unit,
The inverter control unit includes:
Wherein the control unit determines whether or not the motor is eccentric based on the output current, generates a compensation current command value based on the output current when the motor is eccentric, Control,
The bearing drive unit includes:
A first mode in which a current stored in the bearing coil is discharged when the rotor of the compressor motor is landed and a second mode in which a current flows in the bearing coil by a power source stored in the capacitor,
Wherein the control unit controls the period during which the first mode is performed to be longer than the period during which the second mode is performed when the rotor of the compressor motor is landed. The method according to claim 1,
The inverter control unit includes:
Wherein the controller is configured to determine an unbalance of a phase current flowing through the compressor motor based on the output current, extract a normal current and a reverse phase current when the imbalance is determined, And generates a current command value. The method according to claim 1,
The inverter control unit includes:
A position estimator for estimating a rotor position of the compressor motor based on the output current;
A speed calculator for calculating a speed of the compressor motor based on the estimated rotor position;
A forward / reverse compensation unit for generating the compensation current command value based on the output current;
A current command generator for generating a current command value based on the calculated speed and the speed command value;
A voltage command generator for generating a voltage command value based on the generated current command value and the compensation current command value from the constant /
And a switching control signal output unit for outputting an inverter switching control signal for controlling the inverter based on the voltage command value. The method of claim 3,
Wherein the normal /
A normal phase current calculation unit for extracting a normal phase current and a reverse phase phase current based on the output current;
And a compensated current command output unit for generating the compensated current command value based on the normal current and the inverse phase current. The method according to claim 1,
The inverter control unit includes:
A position estimator for estimating a rotor position of the compressor motor based on the output current;
A speed calculating unit that calculates a speed of the compressor motor based on the estimated rotor position and generates the compensation current command value based on the output current;
A current command generator for generating a current command value based on the calculated speed and the speed command value;
A voltage command generator for generating a voltage command value based on the generated current command value and the compensation current command value;
And a switching control signal output unit for outputting an inverter switching control signal for controlling the inverter based on the voltage command value. The method according to claim 1,
The inverter control unit includes:
And controls the output power of the compressor motor so as not to pulsate when a voltage unbalance occurs in a line-to-line voltage of the compressor motor. delete delete A chiller comprising the compressor drive apparatus according to any one of claims 1 to 6. 10. The method of claim 9,
An air conditioning unit;
A cooling tower for supplying cooling water to the air conditioning unit;
And a cold water consumer where the cold water to be heat-exchanged with the air conditioning unit is circulated,
The air conditioning unit includes:
An evaporator for performing heat exchange;
The compressor compressing the refrigerant from the evaporator;
And a condenser for condensing the refrigerant discharged from the compressor.

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