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Analysis, Design, and Evaluation of Three-Phase Three-Wire Isolated AC-DC Converter Implemented with Three Single-Phase Converter Modules Laszlo Huber, Misha Kumar, and Milan M. Jovanović Delta Products Corporation P.O. Box 12173 5101 Davis Drive Research Triangle Park, NC 27709, USA Abstract In this paper, a control method for three single-phase isolated ac-dc converter modules employed to implement an isolated three-phase, three-wire ac-dc converter is presented and its detailed design procedure provided. In the described control the input voltages of the Y–connected single-phase modules with floating common Y point are kept within a safe range by equalizing their input admittances. It is shown that for obtaining equal input admittances of the three PFC front stages, the outputs of the PFC voltage controllers should be equal. This is achieved by adjusting the reference currents of the current controllers in the output dc-dc stages. The performance of the presented control with both balanced and unbalanced source voltages, as well as with a phase fault (open or short circuit) is evaluated by Matlab/Simulink simulations and verified experimentally on a 6-kW prototype. I. INTRODUCTION Three-phase isolated ac-dc converters can be implemented either with a direct three-phase PFC rectifier front end such as the Vienna rectifier or the six-switch PFC boost rectifier followed by an isolated dc-dc converter, or with three single- phase isolated ac-dc converters. Generally, the major advantage of the modular implementation with three single- phase converters is its ease of power expandability. To be able to employ single-phase modules designed for 220/277- Vrms phase-to-neutral voltage in three-phase power systems with nominal phase-to-phase voltage of 380/480 Vrms, the three single-phase modules must be connected in star (Y) configuration. The delta (Δ) configuration cannot be used since it would require that single-phase modules be connected across two phases, i.e., to a voltage exceeding their rating. In applications where the neutral point of the three-phase voltage source is available, the common point (Y point) of the single-phase converter modules is connected to the source neutral point and the three single-phase converters operate independently from each other with their input voltages equal to the respective phase-to-neutral voltages of the source. However, in applications where the source neutral point is not provided, such as, for example, in standard telecom power supplies, any unbalance in the three-phase source phase voltages and/or in the three single-phase modules will create a potential difference between the Y point of the single-phase modules and the source neutral point, resulting in oscillations and significant variations of the input voltages of the single- phase converters [1]. For a stable and reliable steady-state operation, i.e., operation where the input voltage always stays within a specified range, a balancing control of the three single-phase modules is necessary. The stable and reliable Dinggang Ping and Gang Liu Shanghai Design Center, Delta Electronics (Shanghai) Company Ltd, Shanghai 201209, People’s Republic of China operation has also to be guaranteed at startup, as well as in case of phase failure (open and short circuit) and load transients. The balancing control between the three single-phase modules can be achieved with additional passive components used to create a virtual (artificial) neutral point and by using balancing control methods [1]-[8], or without additional passive components by using only balancing control methods [9]. In [1]-[3], three auxiliary transformers with Y-connected primaries and Δ-connected secondaries are used to create an artificial neutral point (ANP). The Y point of the modules is connected to the ANP. With the ANP, the three single-phase modules operate similarly as in the case when the source neutral point is available. When the system is unbalanced, a zero-sequence current flows in the auxiliary transformers that can result in significant losses. To suppress the zero- sequence current, a balancing control method can be employed, where the output reference currents of the single- phase modules, which for a balanced system are equal, are adjusted based on the phase angle of the zero-sequence current [1]. The drawback of using auxiliary transformers is the increased size and cost. Typically, the VA rating of the additional magnetic components is 5% of the VA rating of the rectifier [1]. In [4]-[8], a virtual neutral (VN) point is created by a star connection of three equal resistors. When the three-phase voltage source is balanced, the potential of the virtual neutral point v VN is equal to the potential of the source neutral point v 0 and, therefore, the voltage across a star resistor is equal to the corresponding phase voltage of the three-phase source. Generally, the potential difference between the virtual neutral point and the source neutral point is 3 0 0 0 0 0 , c b a VN VN v v v v v v + + = = , (1) where, v a0 , v b0 , and v c0 are the three-phase source phase-to- neutral voltages. Therefore, if the phase voltages of the three-phase source are unbalanced and contain a zero- sequence component v ZS , the zero-sequence component v ZS appears as voltage v VN,0 , i.e., v ZS =v VN,0 , and, consequently, the voltage across the star resistors will not contain the zero- sequence component. The three-phase source phase voltages can be reconstructed from the voltages across the star resistors following the method presented in [11]. It should be noted that in these implementations the Y point of the single- phase modules is not connected to the virtual neutral point. 978-1-4673-9550-2/16/$31.00 ©2016 IEEE 38

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  • Analysis, Design, and Evaluation of Three-Phase Three-Wire Isolated AC-DC Converter Implemented with Three Single-Phase Converter Modules

    Laszlo Huber, Misha Kumar, and Milan M. Jovanović

    Delta Products Corporation P.O. Box 12173

    5101 Davis Drive Research Triangle Park, NC 27709, USA

    Abstract – In this paper, a control method for three single-phase isolated ac-dc converter modules employed to implement an isolated three-phase, three-wire ac-dc converter is presented and its detailed design procedure provided. In the described control the input voltages of the Y–connected single-phase modules with floating common Y point are kept within a safe range by equalizing their input admittances. It is shown that for obtaining equal input admittances of the three PFC front stages, the outputs of the PFC voltage controllers should be equal. This is achieved by adjusting the reference currents of the current controllers in the output dc-dc stages. The performance of the presented control with both balanced and unbalanced source voltages, as well as with a phase fault (open or short circuit) is evaluated by Matlab/Simulink simulations and verified experimentally on a 6-kW prototype.

    I. INTRODUCTION Three-phase isolated ac-dc converters can be implemented

    either with a direct three-phase PFC rectifier front end such as the Vienna rectifier or the six-switch PFC boost rectifier followed by an isolated dc-dc converter, or with three single-phase isolated ac-dc converters. Generally, the major advantage of the modular implementation with three single-phase converters is its ease of power expandability. To be able to employ single-phase modules designed for 220/277-Vrms phase-to-neutral voltage in three-phase power systems with nominal phase-to-phase voltage of 380/480 Vrms, the three single-phase modules must be connected in star (Y) configuration. The delta (Δ) configuration cannot be used since it would require that single-phase modules be connected across two phases, i.e., to a voltage exceeding their rating.

    In applications where the neutral point of the three-phase voltage source is available, the common point (Y point) of the single-phase converter modules is connected to the source neutral point and the three single-phase converters operate independently from each other with their input voltages equal to the respective phase-to-neutral voltages of the source. However, in applications where the source neutral point is not provided, such as, for example, in standard telecom power supplies, any unbalance in the three-phase source phase voltages and/or in the three single-phase modules will create a potential difference between the Y point of the single-phase modules and the source neutral point, resulting in oscillations and significant variations of the input voltages of the single-phase converters [1]. For a stable and reliable steady-state operation, i.e., operation where the input voltage always stays within a specified range, a balancing control of the three single-phase modules is necessary. The stable and reliable

    Dinggang Ping and Gang Liu

    Shanghai Design Center, Delta Electronics (Shanghai) Company Ltd,

    Shanghai 201209, People’s Republic of China

    operation has also to be guaranteed at startup, as well as in case of phase failure (open and short circuit) and load transients.

    The balancing control between the three single-phase modules can be achieved with additional passive components used to create a virtual (artificial) neutral point and by using balancing control methods [1]-[8], or without additional passive components by using only balancing control methods [9]. In [1]-[3], three auxiliary transformers with Y-connected primaries and Δ-connected secondaries are used to create an artificial neutral point (ANP). The Y point of the modules is connected to the ANP. With the ANP, the three single-phase modules operate similarly as in the case when the source neutral point is available. When the system is unbalanced, a zero-sequence current flows in the auxiliary transformers that can result in significant losses. To suppress the zero-sequence current, a balancing control method can be employed, where the output reference currents of the single-phase modules, which for a balanced system are equal, are adjusted based on the phase angle of the zero-sequence current [1]. The drawback of using auxiliary transformers is the increased size and cost. Typically, the VA rating of the additional magnetic components is 5% of the VA rating of the rectifier [1].

    In [4]-[8], a virtual neutral (VN) point is created by a star connection of three equal resistors. When the three-phase voltage source is balanced, the potential of the virtual neutral point vVN is equal to the potential of the source neutral point v0 and, therefore, the voltage across a star resistor is equal to the corresponding phase voltage of the three-phase source. Generally, the potential difference between the virtual neutral point and the source neutral point is

    3

    00000,

    cbaVNVN

    vvvvvv ++=−= , (1)

    where, va0, vb0, and vc0 are the three-phase source phase-to-neutral voltages. Therefore, if the phase voltages of the three-phase source are unbalanced and contain a zero- sequence component vZS, the zero-sequence component vZS appears as voltage vVN,0, i.e., vZS=vVN,0, and, consequently, the voltage across the star resistors will not contain the zero-sequence component. The three-phase source phase voltages can be reconstructed from the voltages across the star resistors following the method presented in [11]. It should be noted that in these implementations the Y point of the single- phase modules is not connected to the virtual neutral point.

    978-1-4673-9550-2/16/$31.00 ©2016 IEEE 38

  • In [4]-[8], the balancing control between the three single-phase modules is achieved by adjusting the output reference current of the single-phase modules. In [4] and [5], the output reference current of the single-phase modules is adjusted based on the potential difference between the Y point of the modules and the virtual neutral point, vY,VN, whereas in [6]-[8], the output reference current of the single-phase modules is adjusted based on the voltages across the star resistors. In addition, in [6]-[8], the amplitude of an input phase reference current (regulated by average current control) is obtained from the sum of three components: 1) output of a PI-type average-voltage controller that regulates the average value of the output voltages of the three single-phase PFC front ends, 2) an output-power feedforward term (used to improve the control dynamics for load transients), and 3) output of a P-type individual-voltage controller that balances the unequal output voltages of the single-phase PFC front ends. In [4]-[8], the phase currents are controlled to follow the waveform of the voltages across the star resistors, i.e., the source phase potentials referenced to the virtual neutral point.

    In [9], the balancing control between the three single-phase modules is achieved by adjusting the output reference current of the single-phase modules based on the output voltages of the voltage controllers of the single-phase PFC stages (employing average current control). Unlike in [4]-[8], in [9] the phase currents are controlled to follow the input voltages of the single-phase modules, i.e. the source potentials referenced to the star point of the modules. Therefore, by using the balancing control method in [9] compared to those in [4]-[8], standard single-phase converter modules can be easier modified for the three-wire three-phase systems. Unfortunately, no control-oriented analysis is provided in [9].

    Finally, in [12] a balancing control method that does not require any load side balancing is described. In this method, only two output voltages of the three single-phase PFC front ends are balanced at the same time, which avoids the coupling between the three single-phase modules. However, it should be noted that in [12] the availability of the source neutral point is required, but the Y point of the single-phase modules is not connected to the source neutral point.

    In this paper, principles of the balancing control method introduced in [9] are explained and a detailed design

    procedure of the balancing controllers is provided. In addition, the operation with unbalanced source voltages is analyzed with respect to the power distribution between the three single-phase modules, amplitude of the input phase currents, and power factor of the modules. Finally, operation and performance of the balancing control when one phase voltage is reduced and when one phase is disconnected are illustrated with Simulink simulations. Experimental results obtained on a 6-kW prototype are also provided.

    II. PRINCIPLES OF BALANCING CONTROL The block diagram of the three single-phase converter

    modules with Y connection at the input and parallel connection at the output is shown in Fig. 1. The PFC stage of the modules is implemented with average current control, as shown in Fig. 2. The dc-dc stages are also implemented with average current control, where the output-voltage controller is common for all three dc-dc stages as shown in Fig. 3.

    The three single-phase converter modules in Fig. 1 can be equivalently represented with their input admittances Yk, kϵ{a,b,c}, as shown in Fig. 4 [10]. Using Kirchhoff’s voltage and current laws in phasor notation, the potential difference between the Y point of the single-phase modules and the source neutral point (neutral displacement voltage) can be obtained as

    cba

    ccbbaaY YYY

    YVYVYVV

    ++++

    = 0000 . (2)

    If by the balancing control, the input admittances are kept equal, i.e., Ya = Yb = Yc, the neutral displacement voltage in

    Vo

    LoadIob

    vbY

    Ioc

    vcY

    vc0

    Y

    vb0 0

    PFC DC/DC

    Ioa

    vaY

    va0

    VoPFCa

    ia

    PFC DC/DC VoPFCb

    ib

    PFC DC/DC VoPFCc

    ic

    Fig. 1 Block diagram of three single-phase rectifier modules with Y connection at input and parallel connection at output.

    PWM

    C

    v EAx

    dx 1- voPFCref

    |v | xY

    DUTY-CYCLEFEEDFORWARD

    Sx

    CURRENTCONTROLLER

    PI

    VOLTAGECONTROLLER|i | x

    Km

    C2AB

    |v | xY

    A

    B

    PI

    voPFCx

    voPFCref

    VOLTAGEFEEDFORWARD

    See (11)

    |v | xY

    xref|i |

    Fig. 2 Block diagram of PFC control circuit.

    VOLTAGECONTROLLER

    PI

    io,ref

    Vo

    Voref

    ioa

    iob

    ioc

    CURRENTCONTROLLER

    PIa

    PI

    CURRENTCONTROLLER

    PIb

    PI

    CURRENTCONTROLLER

    PIc

    PI

    dDC/DCa

    dDC/DCb

    dDC/DCc

    Fig. 3 Block diagram of dc-dc control circuit.

    39

  • (2) is

    3

    0000

    cbaY

    VVVV

    ++= . (3)

    Since for balanced source voltages VY0 = 0, the input voltage of each single-phase PFC module is equal to the corresponding source voltage.

    For unbalanced source voltages where the amplitude of one phase voltage is smaller than the amplitude of the other two phase voltages, i.e., Va0 = mVm, m < 1, and Vb0 = Vc0 = Vm,

    00 31

    aY VmV ⋅−−= , (4)

    i.e., VY0 is collinear with Va0, but it has opposite direction, as shown in the phasor diagram in Fig. 5. It follows from Fig. 5 that the amplitude of the input voltage of all three single phase PFC modules is smaller than Vm, i.e., VkY < Vm, k ϵ{a,b,c}.

    The condition for equal input admittances is derived by recognizing that according to Fig. 2, the reference current of the modules is given as

    },,{,|| 22, cbakCvvK

    CBAKi

    k

    EAkkYm

    k

    kkmrefk ∈

    ⋅=

    ⋅= , (5)

    where, Km is the multiplier constant and Ck is the voltage feedforward term. By the average current control, the current controllers in the PFC stages enforce the input phase currents to follow the reference currents, i.e., ik = ik,ref. Therefore, the

    input admittance Yk can be obtained as

    }{2 c,b,ak,CvK

    |v|

    i

    |v|i

    Yk

    EAkm

    kY

    ref,k

    kY

    kk ∈=== . (6)

    It follows from (6) that for equal input admittances

    incba YYYY === , (7)

    the outputs of the voltage controllers as well as the voltage-feedforward terms in the PFC control circuits should be equal, i.e.,

    EAEAcEAbEAa vvvv === , (8)

    and

    CCCC cba === . (9)

    The voltage feedforward term C is obtained by considering the total input power

    ==

    ⋅=⋅=cbak

    RMSkYincbak

    RMSkYRMSktotin VYVIP,,

    2,

    ,,,,, . (10)

    Then, it follows from (6)-(10), that if

    =

    =cbak

    RMSkYVC,,

    2,

    2 , (11)

    the output voltage of the voltage controllers in the PFC control circuit is obtained as

    m

    totinEA K

    Pv ,= , (12)

    i.e., vEA does not depend on the input voltages, which is the goal of the voltage feedforward control method. In the case, no voltage feedforward is implemented, C = 1.

    With equal input admittances, for balanced source voltages, the total input power is equally distributed between the three single-phase modules. However, for unbalanced source voltages, to achieve equal input admittances, the total input power cannot be equally distributed between the three single-phase modules. In fact, a module connected to a reduced source voltage will draw less input current and, therefore, it will operate at reduced input power. The desired distribution of the total power between the single-phase modules that results in equal input admittances can be achieved by implementing the balancing-control circuit as shown in Fig. 6. In this balancing circuit, reference currents iok,ref, k ϵ{a,b,c} of the current controllers in the dc-dc stages are adjusted by currents iAdj,k, k ϵ{a,b,c} which are obtained at the outputs of the balancing controllers that regulate the difference between the average output-voltage of PFC controllers

    },,{,3

    cbakv

    v kEAk

    EAavg ∈=

    , (13)

    v a0

    v b00

    v c0

    Y

    i a

    i b

    i c

    Y a

    Y b

    Y c

    v Y0 +

    Fig. 4 Simplified equivalent circuit of three single-phase converter modules.

    Vb0

    Vc0

    Va0 ReVb0 Vc0+

    Vc0 VY0_VcY=

    Vb0 VY0_VbY=

    VY0_VY0

    Fig. 5 Phasor diagram of input voltages of single-phase PFC modules when amplitude of phase “a” source voltage is smaller than amplitude of phase “b” and “c” source voltages, i.e., for Va0 = mVm, m < 1, and Vb0 = Vc0 = Vm.

    40

  • and corresponding module PFC control voltage vEAk. The design of the balancing controllers is performed

    through simulations in Simulink and SIMetrix. In order to reduce the simulation time, in the simulation circuit the dc-dc output stages are replaced with current sources ILoad,k, k ϵ{a,b,c}, which represent the load currents of the PFC stages, i.e., the input currents of the dc-dc stages for balanced source voltages, and with controlled current sources iAdj,k, k ϵ{a,b,c}, which are controlled by the output signals of the balancing controllers, as shown in Fig. 7. Instead of adjusting the reference currents of the current controllers in the dc-dc stages, the load currents of the PFC stages are adjusted. However, to keep the total load current constant, the total adjustment current must be zero. Therefore, the balancing control circuit in Fig. 7 is modified so that the adjustment current in phase “c” is generated as the negative sum of the adjustment currents in phases “b” and “c”, i.e.,

    )( ,,, bAdjaAdjcAdj iii +−= . (14)

    To measure the balancing loop transfer function in phase “a”, a perturbation signal is injected at the output of the “a” balancing controller as shown in Fig. 8. This injection current, iInj, is added to adjustment current iAdj,a,

    InjaAdjInjaAdj iii +=+ ,, . (15)

    To keep the total load current constant, injection signal iInj is also injected in phases “b” and “c” with opposite sign and with half of its value. The plant transfer function is defined as

    )(

    )()(

    ,

    ,

    sIsV

    sTInjaAdj

    aRespPL

    += , (16)

    where, VResp,a(s) is the response signal at the input of the balancing controller “a”. Finally, the balancing loop gain is defined as )()()( sTsTsT BCPLLG ⋅= , (17)

    where, TBC(s) is the transfer function of the balancing controller.

    The Bode plots of the plant transfer function, balancing controller transfer function and balancing loop gain are presented in Fig. 9, which were obtained at the zero crossing of source voltage va0. The balancing controller is designed as a PI controller. The crossover frequency of the balancing loop gain is selected at 3.3 Hz to avoid interaction with the PFC voltage loop whose bandwidth is 10 Hz. At the crossover frequency, the magnitude of the balancing controller transfer function is

    v EAa iAdj,a

    v EAb

    Σ 3

    v EAc

    PIa

    BALANCINGCONTROLLER

    PIb

    BALANCINGCONTROLLER

    PIc

    BALANCINGCONTROLLER

    iAdj,b

    iAdj,c

    io,ref

    ioa,ref

    iob,ref

    ioc,ref

    v EAavg

    Fig. 6 Block diagram of balancing control circuit.

    0

    v a0

    PFCa

    v b0

    PFCb

    v c0

    PFCc

    Y

    I Load,a

    I Load,b

    I Load,c

    i Adj,a

    i Adj,b

    i Adj,c

    v aY V oPFCa

    v bY

    v cY

    V oPFCb

    V oPFCc

    Fig. 7 Block diagram of three single-phase PFC modules used in simulations.

    v EAa iAdj,a

    v EAb

    Σ 3v EAc

    iAdj,b

    iAdj,c

    PIa

    BALANCINGCONTROLLER

    PIb

    BALANCINGCONTROLLER

    1

    21

    21

    i Inj SOURCE

    INJECTIONSIGNAL

    iAdj,a+InjvResp,a

    iAdj,b+Inj

    iAdj,c+Inj

    Fig. 8 Block diagram of balancing control circuit with injection signal source used for measuring balancing loop transfer functions.

    -60

    -40

    -20

    0

    20

    40

    60

    80

    100m 200m 400m 1 2 4 10 20 40 100

    -50

    0

    50

    100

    150

    Fig. 9 Bode plots of plant transfer function, balancing controller transfer function, and balancing loop gain.

    TLG

    |T| [dB]

    |TLG

    |

    |TBC

    |

    fC=3.3Hz

    63.2dB

    fz=2Hz

    sKK)s(T ipBC +=

    -63.2dB

    o43PM =

    |TPL

    |

    TPL

    150100

    50

    0

    -50

    1100m 200m 400m 2 10 4 20 40 100

    T [o]

    80

    60

    40

    20

    0-20

    -40

    -60

    TBC

    41

  • .dB2.63][)(1log20][)(2

    =ω=

    ωω+=ω dBTKdBT cPL

    c

    zpcBC

    (18)

    Selecting fz = 2 Hz, it follows from (18) that 41091.5 −⋅=pK . Finally, from

    p

    iz K

    K=ω , (19)

    it is obtained that 31042.7 −⋅=iK .

    III. ANALYSIS OF OPERATION FOR UNBALANCED SOURCE VOLTAGES

    The operation for unbalanced source voltages is analyzed for the case when the amplitude of one phase voltage is smaller than the amplitude of the other two phase voltages i.e., for Va0 = mVm, m < 1, and Vb0 = Vc0 = Vm. The analysis includes the power distribution between the three single-phase modules, the amplitude of the phase currents, and the power factor of the modules.

    The calculated power distribution between the three single-phase modules is shown in Fig. 10. The dashed lines present the input power of the modules, PkY, k ϵ{a,b,c}, whereas, the solid lines present the power delivered by the phase sources, Pk0, k ϵ{a,b,c}. As can be seen in Fig. 10, the input power of module “a”, whose source voltage is reduced, is provided by its own source “a”, but also by sources “b” and “c”. For example, for m = 0.5, module “a” consumes 20.5%, while modules “b” and “c” each consume 39.7% of the total power.

    However, source “a” delivers only 15.4%, while sources “b” and “c” each deliver 42.3% of the total power.

    The calculated amplitude of the phase currents is shown in Fig. 11. It should be noted in Fig. 11 that the amplitude of phase current “a” decreases by only 1% when the amplitude of phase voltage “a” decreases by 20%. It should also be noted in Fig. 11 that at m = 0, the amplitude of phase currents “b” and “c” increases by almost 60%. However, if phase “a” is disconnected, the amplitude of phase currents “b” and “c” increases by 73.2%. In fact, when phase “a” is disconnected and the input admittances of phases “b” and “c” are equal, the neutral displacement voltage VY0 is

    2

    000

    cbY

    VVV

    += . (20)

    As shown by the phasor diagram in Fig. 12, when phase “a” is disconnected, input voltages VbY and VcY, and, consequently, input phase currents Ib = Y·VbY and Ic = Y·VcY are equal with opposite signs and they are phase shifted by 30o versus the respective input source voltages Vb0 and Vc0. If the total power is maintained before and after phase “a” is disconnected, i.e.,

    φφφ

    =⋅=⋅= 2o23

    23)30cos(

    22

    23 mmmmmmtot IV

    IVIVP , (21)

    it is finally obtained that

    φφφ ⋅=⋅= 332 732.13 mmm III . (22)

    The calculated power factor of modules “b” and “c” when the amplitude of phase voltage “a” decreases is shown in Fig. 13. It can be seen in Fig. 13 that the power factor of modules “b” and “c” is greater than 0.99 for m > 0.55. The power factor of module “a” does not decrease when the amplitude of phase voltage “a” decreases as it can be concluded from Fig. 5.

    IV. SIMULATION AND EXPERIMENTAL RESULTS

    Simulink simulation results obtained for 230-Vrms source phase voltages, 400-V output voltage of the PFC stages, and 6-kW output power are presented in Fig. 14. Figure 14 illustrates the operation with balancing control before and after the amplitude of phase voltage “a” drops by 50%. It

    0.1

    0.2

    0.3

    0.4

    0.5

    000.20.40.60.81

    1/3

    0.5

    tot

    0aP

    )m(P

    tot

    0c,0b

    P)m(P

    m

    tot

    cY,bY

    P)m(P

    tot

    aYP

    )m(P

    Fig. 10 Calculated power distribution between three single-phase modules.

    Fig. 11 Calculated amplitude of phase currents.

    1.2

    1.4

    1.6

    0.6

    0.8

    1

    00.20.40.60.81

    )1m(I)m(I

    a

    a=

    m

    )1m(I)m(I

    c,b

    c,b

    =

    VY0

    Vb0

    Vc0

    VY0_

    Re

    Im

    Vc0

    Vb0

    VY0_

    VY0_

    Vb0 Vc0+

    VcY

    VbY

    =

    =

    Fig. 12 Phasor diagram of input voltages of PFC modules when phase “a” is disconnected.

    42

  • should be noted in Fig. 14 that after the amplitude of phase voltage “a” drops by 50%, it takes approximately 0.2 sec for the new steady state to be established. It should also be noted in Fig. 14 that in the new steady state, the adjustment currents are IAdj,a ≈-2A, and IAdj,b ≈ IAdj,c ≈1A. Before the drop of the amplitude of phase voltage “a”, the load current of each PFC stage was 2kW/400V=5A. Therefore, in the new steady state, the adjusted load currents of the PFC stages are ILoad,a,adj ≈ 5-2 = 3A and ILoad,b,adj ≈ ILoad,c,adj ≈ 5+1 = 6A, i.e., the output power of the PFC stages is adjusted as PLoad,a,adj ≈ 1.2 kW and PLoad,b,adj ≈ PLoad,c,adj ≈ 2.4 kW, which means that the output power of PFC stage “a” is reduced to 20% of the total output power, whereas, the output power of each of the PFC stages “b” and “c” is increased to 40% of the total output power. These results are in good agreement with the analytical results for m = 0.5 presented in Fig. 10.

    Simulation waveforms that illustrate the operation when one phase is disconnected and then reconnected are presented in Fig. 15. The waveforms in Fig. 15 are obtained for 230-Vrms source phase voltages, 400-V output voltage of the PFC stages, and 6-kW output power when all three phases are connected, and at reduced output power of 76% (determined by a maximum overcurrent of 32%, i.e., 1.732·0.76 = 1.32, for the single-phase modules) when one phase is disconnected. It should be noted that when one phase is disconnected, the reference voltage of the balancing controllers is obtained as the averaged value of the output voltages of the PFC voltage controllers of the two active modules. In addition, when one phase is disconnected, the balancing loop bandwidth is increased by increasing balancing coefficient Kp five times. As can be seen in Fig. 15, in both cases (after disconnecting and after reconnecting phase “a”), the new steady-state is established in approximately 0.1 sec. The waveforms of the simulated input voltages vkY and input currents ik, kϵ{a,b,c}, are in good agreement with the analytical results in Fig. 12.

    Experimental results obtained on a 6-kW prototype at full load are presented in Figs. 16(a)-(c). Figure 16(a) shows the source phase voltages and input currents for balanced source voltages Va0 =Vb0 =Vc0 = 230 Vrms. Figure 16(b) shows the same waveforms when the RMS value of source voltage “a” is decreased to Va0 = 180 Vrms, i.e., to 78%, whereas, Fig. 16(c) shows the waveforms when the RMS value of source voltage “a” is further decreased to Va0 = 150 Vrms, i.e., to 65%. It should be noted in Figs. 16(a)-(c) that as the RMS

    Fig. 13 Calculated power factor of single-phase modules.

    -400-200

    0200400

    -20-10

    01020

    0

    10

    20

    300350400450

    02,5005,000

    -200-100

    0100200

    -1-0.5

    00.5

    1

    0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.4510

    15

    20

    0.98

    0.99

    1

    00.20.40.60.810.94

    0.97

    0.96

    0.95

    m

    c,bPF

    -400-200

    0200400

    -20

    0

    20

    0

    10

    20

    300350400450

    0

    5000

    10000

    -100-50

    050

    100

    0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45-202

    t[sec]

    (a)

    (b)

    (c)

    (d)

    (e)

    (f)

    (g)

    Fig. 14 Key simulated waveforms for 230Vrms source phase voltages and 6-kW load before and after amplitude of phase “a” source voltage drops by50%: (a) low-pass filtered input phase voltages with respect to Y point [V],(b) input phase currents [A], (c) rectified input phase current references [A],(d) PFC output voltages [V], (e) PFC voltage controller outputs [digital valuein Q12 format], (f) low-pass filtered neutral displacement voltage VY0 [V],and (g) adjustment currents [A].

    vaYvbY

    Ic

    VEAa

    VEAc

    IAdj,a

    vcY

    IAdj,bIAdj,c

    |Icref|

    VY0

    VobVoc

    IaIb

    Voref

    VEAb

    |Iaref||Ibref|

    Voa

    Amplitude of phase “a” voltage drops by 50%

    VEAavg

    t[sec]

    (a)

    (b)

    (c)

    (d)

    (e)

    (f)

    (g)

    (h)

    Fig. 15 Key simulated waveforms for 230Vrms source phase voltages and 6-kW load when phase “a” is disconnected and reconnected: (a) low-passfiltered input phase voltages with respect to Y point [V], (b) input phasecurrents [A], (c) rectified input phase current references [A], (d) PFC outputvoltages [V], (e) PFC voltage controller outputs [digital value in Q12 format],(f) low-pass filtered neutral displacement voltage VY0 [V], (g) adjustmentcurrents [A], and (h) total load current [A].

    ILoad,tot

    Phase “a” disconnected Phase “a” reconnected

    vaYvbY

    Ic

    VEAa

    IAdj,a

    vcY

    IAdj,bIAdj,c

    |Icref|

    VY0

    VobVoc

    VEAc

    IaIb

    VorefV

    EAb

    |Iaref||Ibref|

    Voa

    VEAavg

    43

  • value of source voltage Va0 decreases to 78% and to 65%, the amplitude of the input current of phase “a” is almost constant, whereas, the amplitude of input current of phase “b” increases by approximately 10% and 18%, respectively, which is in good agreement with the analytical results presented in Fig. 11.

    V. SUMMARY In this paper, analysis of the balancing control method for

    three single-phase isolated ac-dc converter modules employed to implement an isolated three-phase, three-wire ac-dc converter, introduced in [9], is presented. The balancing control between the three single-phase modules is achieved by equalizing the input admittances of the PFC front stages, which operate with average current control. It is shown that for equal input admittances, the outputs of the voltage controllers as well as the voltage feedforward terms in the PFC control circuit should be equal.

    With equal input admittances, for balanced source voltages, the total input power is equally distributed between the three single-phase modules. However, for unbalanced source voltages, to achieve equal input admittances, a module

    connected to a reduced source voltage draws less input current and, therefore, it operates at reduced input power. The desired distribution of the total power between the single-phase modules is achieved by adjusting the reference current of the current controllers in the dc-dc stages. The adjustment currents are obtained at the outputs of the balancing controllers, which balance the output voltages of the PFC voltage controllers.

    A detailed design procedure of the balancing controllers performed through simulations in Simulink and SIMetrix is provided.

    The operation with unbalanced source voltages is analyzed with respect to the power distribution between the three single-phase modules, amplitude of the input phase currents, and power factor of the modules. Operation and performance of the balancing control when one phase voltage is reduced and when one phase is disconnected and reconnected are illustrated with Simulink simulations.

    Experimental results obtained on a 6-kW prototype are also provided.

    REFERENCES [1] M. Karlsson, C. Thoren, and T. Wolpert, “A novel approach to

    the design of three-phase AC/DC power converters with unity power factor,” Proc. International Telecommunications Energy Conf. (INTELEC), paper 5-1, Jun. 1999.

    [2] M. Karlsson, C. Thoren, and T. Wolpert, “Practical considerations concerning a novel 6kW three-phase AC/DC power converter with unity power factor,” Proc. International Telecommunications Energy Conf. (INTELEC), pp. 28-33, Sep. 2000.

    [3] M. Karlsson and T. Wolpert, “Stable artificial neutral point in a three phase network of single phase rectifiers,” U.S. Patent 6,466,466, Oct. 15, 2002.

    [4] D. Chapman, D. James, and C.J. Tuck, “A high density 48V 200A rectifier with power factor correction – An engineering overview,” Proc. International Telecommunications Energy Conf. (INTELEC), pp. 118-125, Sep. 1993.

    [5] C.J. Tuck, D.A. James, and D.A. Chapman, “Power converter with star configured modules,” U.S. Patent 5,757,637, May 26, 1998.

    [6] R. Greul, S.D. Round, and J.W. Kolar, “Analysis and control of a three-phase unity power factor Y-rectifier,” IEEE Trans. Power Electronics, vol. 22, no 5, pp. 1900-1911, Sep. 2007.

    [7] R. Greul, U. Drofenik, and J.W. Kolar, “Analysis and comparative evaluation of a three-phase three-level unity power factor Y-rectifier,” Proc. International Telecommunications Energy Conf. (INTELEC), pp. 421-428, Oct. 2003.

    [8] R. Greul, U. Drofenik, and J.W. Kolar, “A novel concept for balancing of the phase modules of a three-phase unity power factor Y-rectifier,” Proc. Power Electronics Specialists Conf. (PESC), pp. 3787-3793, Jun. 2004.

    [9] R. Girod and D. Weida, “High efficiency true 3-phase compact switch-mode rectifier module for telecom power solutions,” Proc. International Telecommunications Energy Conf. (INTELEC), pp. 658-663, Oct. 2013.

    [10] M.L. Heldwein A.F. Souza, and I. Barbi, “A simple control strategy applied to three-phase rectifier units for telecommunication applications using single-phase rectifier modules,” Proc. Power Electronics Specialists Conf. (PESC), pp. 795-800, Jun. 1999.

    Ia[A]

    Vb0

    [V] V

    a0[V]

    Ib[A]

    Ia[A]

    Ib[A]

    Vb0

    [V] V

    a0[V]

    Ia[A]

    Vb0

    [V] V

    a0[V]

    Ib[A]

    4ms/div

    100V/div 5A/div

    4ms/div

    100V/div 5A/div

    4ms/div

    100V/div 5A/div

    (b)

    (c) Fig. 16 Experimental waveforms of source phase voltages and input currents obtained on a 6-kW prototype at full load with: (a) balanced source voltages Va0 = Vb0 = Vc0 = 230 Vrms, (b) unbalanced source voltages Va0 = 180 Vrms, Vb0 = Vc0 = 230 Vrms, and (c) unbalanced source voltages Va0 = 150 Vrms, Vb0 = Vc0 = 230 Vrms.

    (a)

    44

  • [11] T. Atsushi, Y. Itsuo, and O. Tsuyoshi, “The control method of 3-phase PWM converter for 3-phase 3-wired imbalanced ac voltages,” Proc. International Telecommunications Energy Conf. (INTELEC), pp. 1-8, Oct. 2011.

    [12] J. Biela, U. Drofenik, F. Krenn, J. Miniboeck, and J.W. Kolar, “Three-phase Y-rectifier cyclic 2 out of 3 dc output voltage balancing control method,” IEEE Trans. Power Electronics, vol. 24, no 1, pp. 34-44, Jan. 2009.

    45

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