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    Precise Method for Measuring Xd andXq Based on S l i p Testo f Synchronous Machines

    Osamu. SUGIURADept. of Elect. and Comp. Science.University of YamanashiYamanashi, Japan

    ABSTRACTAn experimental method for measuring the direct

    and quadrature axis synchronous reactances (Xd andxq) of polyphase synchronous machines with salientpole is newly developed. It is based on a measuringmethod of slip test. It can be applied to all thesynchronous machines, but primarily it is developedand proved for reluctance motors. Precise measuringmethod was derived by the use of tensor analysismethod, and was introduced to minimize measurementerrors due to the stator resistance (Rs) as well asthe machine losses. Detailed results are presentedin case of one reluctance motor which has a highlyvariable Rs. In fact, correlation with othermethods is proved to be quite good, The effects ofRs are observed in the tested motor.

    I . INTRODUCTION

    The various methods to measure Xd and xa of thesynchronous machines have been used in many ways inthe past, as in [l ] - [6] . The slip test haswidely been used to measure Xd and xq. By thissimple experimental test, he proper measured valuesof Xd and x4 can be obtained. But, this measuringmethod takes no account of R3 when the values of Xdand xq are computed, However, Rs can not be ignoredin small motors because the resistance is larger insmall motors than in medium and large motors.

    In this paper, the authors made a try to take R3into consideration. The measuring method of Xd andxq was to make the theoretical analysis at synchro-nous speed of the reluctance motor. This method isobtained by applying the analytical results, and isexperimentally proved.

    List of principal symbols

    0-7803- 462-x/93$03.OOQ lW3IEEE

    Yu i. AKIYAMAYember IEEEDept. of Elect. Engrg.Kanagawa Institute of TechnologyKanagawa, Japan

    R, :resistance of stator winding.LMX IXo

    Xd :direct axis synchronous reactance.xq :quadrature axis synchronous reactance.0

    a

    o : supply frequency, rad/s.o r :rotating speed, rad/s.p :differential operator.

    t : instantaneous torque.t :mean torque.7 :pulsating torque.

    :self inductance of stator winding.:mutual inductance between the stator windings.:mean value in self reactance of stator winding.:maximum value of variation in self reactanceof stator winding.

    :angle between stator winding of a-phase and d-axis of rotor.

    :angle between stator winding of a-phase and d-axis of rotor at time t=o.

    Subscripts

    s :stator.d :direct axis.q :quadrature axis.a, b, c :symbols of 3-phase.

    II. ANALYSIS OF RELUCTANCE YOTOR

    Applications of the theory of tensor to analyzerotating machines were developed by G.Kron, as in

    This Krons method is expedient to analyzetwo phase machines, because the two hypotheticalwindings are assumed to be two phase windings ofthe machine under consideration. But, for the threephase machine, it is necessary to transform thethree phase actual windings into the hypotheticalwindings of the primitive machine with the aid ofconnection matrix, which will make the resultantimpedance matrix rather complicated.

    To avoid such complicated manipulation, Poly AxisMatrix Yethod developed by T.Takeuchi as in [8] is

    [71 .

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    Fig. 1. Winding model of RI.

    L

    I-*/2 7~ -e

    h L

    - ? - - - -

    Fig. 3. Variation of Y a b with 6 .

    I cos20 1

    And, the mutual inductance ?dab between the statorwindings changes sinusoidally as in Fig. 3. Then,the mutual inductance between the stator windingsis written as

    The voltage equations of stator windings are shownas a matrix formula as in (3 ) .

    Fig. 2. Variation of La with 8 . Rs+PLo t $Mob, P n & c

    [ ]= [DMbaj R s + P L ,I .Mbc][:! j (3 )used in this paper. This method analyzes matrix uC PfiIcm PMcb, Rs+PLc

    equations on the actual axes of windings and fa-cilitates the analysis without any confusion. Transforming (3 ) by the three phase sequence trans-

    formation matrix A 3 , we have the voltage equationA. Voltage Equation of (4) based on the symmetrical co-ordinates axis

    Fig. 1 shows the winding model of the reluctancemotor(R.'d) in which ai, bl and CI are three windingsspaced by 120" each other on the stator. La, L b andLc are the self inductance of the stator windings,and M a t , , l b c and M c a are the mutual inductancebetween the stator windings. The salient pole rotoris rotating with an angular speed of w in theclockwise direction as shown by an arrow wt in theFig. 1.

    The self inductance La of the stator windingchanges sinusoidally as in Fig. 2. Then, the selfinductance of the stator windings may be written as

    as

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    were B. Stator Current

    The zero sequence elements are putted aside from(41, because the grounding fault do not consider.

    Then, the resultant voltage equation of (5 ) iswritten as

    The impedance matrix of (5) is a function of timet. To eliminate 8 from the elements of thisimpedance matrix, we define the commutation matrixK as

    which can be chosen by inspecting (51, as in [8] .Transforming (5 ) by the commutation matrix K

    minding that

    The impedance matrix of (7) is the stationaryimpedance matrix. Thus, we can get the inversionof (7) as

    where

    B I I - . R s + ( L + M ) ( p - j w ) - ( 9 ) p - t j o )

    The instantaneous three phase voltages are writtenas

    Then, the voltages based on the symmetrical co-ordinates will be written as

    Substituting (9) in (8) obtains (10).

    where

    The impedance matrix of (7) is the stationaryimpedance matrix which is no more function of time8 = w t + a . And, the currents based on the symmetrical co-

    ordinates will be written as

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    (20) rr =-. xovz s in2(3 =-. (zt%-dV2 s in 6 (25)w x + - x o 2 w 2xdxq

    In the right hand side of the above (201, thefirst term is the power expended in heating theconductors. And the second term is the rate atwhich energy is being stored in the magnetic field,that do not contribute mechanical output. Also notethat in the above (20)

    1K=$i] c[L.][i]

    is the instantaneous stored energy in the magneticfield.

    Therefore, the third term must represent themechanical power expended by the rotor. And, thepower may be expressed as

    On the other hand, z i is an instantaneous torqueand o is an angular speed of the rotor. Then,o i will be the mechanical power expended by the

    rotor, thus, we have

    (21)

    This is the general expression of torque obtainedfrom output. where

    ~(L0-2Mo)cZ~

    L+M3

    Equation(25) is the general torque expression ofRM.

    IU. DERIVATION OF METHOD FOR MEASURINGxd ANDX g

    Fig. 6 shows the vector diagram of I, at the angleof phase difference d m . In Fig. 6, I m i n is thevector of the minimum stator current with the angleof phase difference d m .

    Fig. 7 shows the variation of W, I and V with thepower angle 6.

    The waveforms of input power, stator current andimpressed voltage are the envelopes of the instan-taneous maximum value. If RN is rotating nearly atsynchronous speed, it is permitted to exchange timet for 6. Accordingly, the variation of I and V isobserved quite the same as experimental data ob-tained by the slip test.

    Then, the impedance 2 i n of RM which is viewedfrom power source is

    I

    (23) Fig. 6. Vector diagram of I,.

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    W

    v

    I

    I'

    4 - - - 4 h Wm ;n I

    Fig. 7. Variation of W, I and V with 6.

    were

    Wm ;

    The tangent of (26) is

    (27)I V / A - X t X m i n

    R s V / A Rs R m i n- - = -a n (6m) =

    Thus, comes the following equation as

    From Fig. 6, two currents of I m i n and I m a , canbe written as

    Then, two currents of 11 and 1 1 2 may be definedas

    I p a x + I m i n

    2I tax- I m i n

    2

    I l l =

    I 1 2 =

    From (14), we have

    I l l - J R s 2 + X i 2 ( V / A >- -r 1 2 x o ( V / A >

    - 4 s 2 + + X 1 *x o

    -

    (30)

    (31)

    Substituting (30) in (31) obtains (32)

    ] (32)I m a x - I m i nI m a x + I m i n

    X o = J R s 2 + X i 2

    Then, the direct and quadrature axis synchronousreactances Xd and xq will be

    X d = X l + X O , x q = x I - x O (33)

    Hence, Xd and xq is derived from three kinds ofmeasurement as follows.(a) The resistance Rs is measured by a simple d,ctest.(b) The machine under test is driven steadily atsynchronous speed, and its impedance Z m i n ismeasured for the rotor angle which gives the mini-mum current at the terminal (see Fig. 6).

    Wm;R m i n = 3 I m i n e 1

    Thus, this test gives value of X I as follows.

    (c) Being used the slip test, I m a x and I m n whichare a maximum and a minimum currents, are measuredto get the value of Xo.

    Fig. 8 shows the oscilloscope waveforms of V and

    I.From the measured data,

    1m a x - I m i n

    I m a x f I m i nX D = J R , ~ + X I ~

    terminal voltageI I

    f stator current I

    Fig. 8. Oscilloscope waveforms of V and I.

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    'KO -w2Fig. 9. Circuit for measuring Xd and xq.

    Then, the value of xd and xq are obtained as

    X d = x l + x O

    xq = X I - xo

    Fig. 9 shows the experimental circuit for measur-ing XI and XC, thus, Xd and xq.

    In Fig. 9, Rg was inserted in the armature circuitfor the experiment to determine whether the preciseslip test for measuring Xd and xq is good or not.

    IV. EXPERINIENTAL RESULTS

    The effect of the stator winding resistance R, onthe computed values of xd and xq is investigated inthe first place. Then, the authors computed ap-proximately how large the calculative error is due

    In the second place, he experimental results basedon the precise slip test are taken into consider-

    ation, and a comparison of the conventional sliptest and the precise slip test with regard to theeffect of R, has been made.

    to Rs.

    A. Calculative Error in the Slip Test

    The authors investigated the effect of Rs on thecomputed values of xd and Xg by using the equiva-lent circuit in Fig. 10.

    It is assumed that xd5 is the direct synchronousreactance which is computed by the slip test. And,Xd is the true direct synchronous reactance of RN.

    Then, X d s will be

    (34)

    Changing the above equation into a more suitableform.

    Where, K is the error factor, and can be writtenas

    K= d 14 - (Rs/Xd)

    '(36)

    Fig. 11 shows the variation of K with (Rs/Xd).Differentiating K with respect to (R,/Xd) to in-

    vestigate the characteristics of the curve in Fig.11.

    d K

    d ( R s / X d )K ' =

    K " = 1 / ( 1 f ( R s / x ~ )} 3'2> 0

    K increases always with (Rs/Xd). WhenK

    is dif-ferentiated twice with respect to (Rs/Xd), it canbe obtained from K " that the curve of Fig. 11 in-creases rapidly with (R~/xd).

    6

    Fig. 10 shows the approximate d- axis equivalentcircuit of RI at power angle 6=0.

    4K

    Fig. 10.of RM.

    Approximate d-axis equivalent circuit

    2

    Fig. 11. Variation of K with (Rs/xd).

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    B. Precise Slip Test 1 A -Precise s l i p t e s tB - s l i p t e s t

    The authors carried out the experiment accordingto the results of the precise slip test which wasdescribed in Chap. NI. Further, the authors carriedout the conventional slip test which is based onthe following assumption; when the rotor i s in thedirect and also in the quadrature axis position, hecurrents drawn by the machine are a minimum and amaximum respectively.

    Fig. 9 shows the circuit for measuring Xd and xq.The test motor is rated 1.0 w, 200 volts, 50 Hz.The additional resistance Rq was connected with thecircuit of stator winding to investigate the effectof the stator winding resistance R 3,and the experi-ments were carried out by changing the values of R q ,

    Fig. 12 shows these results. Test results of Xd

    and Xq obtained by these methods for the test ma-chine are plotted as function 01 ( R 3 t R s ) in Fig. 12.Fig. 12 shows a comparison of the calculated valuesof Xd and xq with the test results obtained by twodifferent tests. An increase in RE I results in anequivalent increase in Xd and xq in the slip test,and the values are almost always constant in theprecise slip test.

    Therefore, the precise slip test confirms the va-lidity of a measuring method for Xd and xq.

    V . CONCLUSIONS

    A new measuring method of x d and Xq which took

    account of the stator winding resistance was pro-posed by the authors. The authors carried out theexperiments according to this measuring method andexamined the results. The method of calculatingthe reactances gives results which agree well withmeasured values of unsaturated state.

    The method described in this paper for themeasurement of salient-pole machine reactances hasmore advantages than the slip test, and the ex-periments of this method are widely acceptable andis easier in comparison with other methods.

    ACKNOWLEDGMENT

    2 0X d

    t

    Fig. 12. Comparison of the calculated values ofXd and Xq with the test resultsobtained by two different tests.

    his helpful advice and the ldachine Shop Group ofYamanashi University for producing experimentaldevices.

    REFERENCES

    P. . Lawrenson, and 1. A. Agu, " Theory and performance ofpoly-phace reluctance machines, P r m . EE, vol. 3, pp. 1435-1445, Aug 1964.V.B. Honsinger, " The inductance L d and Lg of reluctancemachines, IEEE, vol. PAS-90, pp. 298-304, Jan/Feb 1971.R.W. Henzies, R.1. Nathur. and H.1. Lee, a Theory and oper-

    ation of reluctance motors with magnetically anistro picrotors, U -synchronous performance, IEEE, vol. PAS-91, pp.42-45, Jan/Feb 1972.E. A.Klingshirn, " DC standstill torque used to measure Lgof reluctance and synchronous machines, IEEE, vol. PAS-97,pp. 1862-1869, Sep/Oct 1978.A.A. Fock. and P.M.Hart, " New method for measuring xd andXg based on the P-Q diagram of the lossy salient -polemachine," PIEE, Pt.B. vol. 131. pp.259-262. 1984T. Fukao, " Principles and output characteristics of superhigh-speed reluctance generator system, IEEE. vol. IA-22.

    G. Kron, " The application of tensors to the analysi s ofrotating electri cal machinery, Gen. Elec. Rev. Aug 1935.May 1938.T. Takeuchi, " Matrix theory of electrical machinery," The

    pp. 702-707, Jul/Aug 1986.

    OHM-SHA LTD., 1967.The authors would like to thank Dr. H. Kazuno for

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