Study of salient poles synchronous generator by finite elements analysis Olivian Chiver, Liviu Neamt, Mircea Horgos and Zoltan Erdei Electrical, Electronics and Computers Engineering Department Technical University of Cluj-Napoca, North University Center Baia Mare, Romania olivian.chiver@ubm.ro Abstract—This paper presents the finite elements analysis (FEA) of a salient poles synchronous generator. The goal of this analysis is to determine the machine parameters in steady-state regime and in transient regime respectively. The used FEA techniques and obtained results for a case study will be presented as well. Finally the FEA results will be compared to the experimental ones and a 2D transient with motion analysis will be performed. Keywords-synchronous; generator; parameters; transients; finite; elements. I. INTRODUCTION Nowadays most of electrical energy is supplied by synchronous generators. These generators have two types of rotors: round rotor in case of turbo-generators, usually with one or two pole pairs, and salient poles rotor, as in case of hydrogenerators, when the pole pairs can reach two figure number. The economic reasons impose a continuous growth of the nominal power of these generators, thus the turbo-generators reach the values of 1200 MW and 700MW in case of hydrogenerators. These excessively high power values determine considerable prices, thus the design phase is very important. The analytical relations used in design computation are quite accurate, but considering the importance of these machines, the design results have to be confirmed by numerical method. It is well known that, in design phase, one of the most powerful instruments is finite elements analysis (FEA) because of its accuracy. The main purpose of the present paper is to estimate the salient poles wound rotor synchronous generator parameters by FEA. Although many papers deal with the parameter determination of salient poles synchronous generator by FEA, [1]-[3], this paper presents several analysis techniques that allow transient parameters determination as well. These parameters impose the transient currents in case of a threephase sudden short circuit regime. As the salient poles generator has a variable air-gap, the direct axis parameters differ from the quadrature axis parameters. II. THE SALIENT POLES GENERATOR PARAMETERS A. Steady-state Parameters In steady-state regime, the salient poles generator parameters are in accordance with equivalent electrical diagrams of the machine, fig.1. Thus the generator behavior is influenced by the stator winding resistance, R, the direct axis synchronous reactance, Xd=ωLd and the quadrature axis synchronous reactance, Xq=ωLq. The direct axis synchronous reactance is the sum of the leakage reactance of the stator winding, Xσ=ωLσ, and the direct axis reaction reactance, Xad=ωLad. Also, the quadrature axis reactance is the sum of the stator winding leakage reactance and the quadrature axis reaction reactance, Xaq=ωLaq. Ue0 is the field winding voltage and Z is the phase load impedance. B. Transients parameters During the transient regime, the reactances change in terms of the transient currents that occur in field excitation winding and in damper winding, respectively. Because the time constant of the dumper winding is smaller than the time constant of field excitation winding, the dumper winding currents extinguish before the excitation winding overcurrent. As long as the transient currents exist in the dumper winding, reactances are so called subtransient reactances, Xd”, Xq”. After the currents in the dumper winding have extinguished and until the extinction of the overcurrent in the field winding, reactance is so called direct axis transient reactance, Xd’. After that, reactances become the synchronous reactances. C. The parameters determination by FEA In case of salient poles synchronous machine, the direct axis reactance corresponds to the magnetic flux that closes through rotor poles axis, Fig. 2. In order to shorten the analysis time, a 2D numerical analysis will be performed, and end winding inductance and resistance will be added in electrical circuits of the generator. The above mentioned parameters can be obtained either by 3D FEA, or analytically. a. Direct axis parameters b. Quadrature axis parameters Figure 1. Equivalent circuit of salient poles generator in steady-state regime Figure 2. Direct axis magnetic flux Figure 3. Quadrature axis magnetic field In order to compute the direct axis inductance, Ld, the excitation current is set to be zero and the stator winding is fed in such a way as to obtain the magnetic flux with maximum value coincident with the direct axis of the rotor. If it is chosen the moment when the currents satisfy relation, On the other hand, the saturated and unsaturated values of these inductances are determined experimentally as well. I a = -2I b = -2Ic , (1) the magnetic field axis is the same as the a phase axis, and the direct axis of the rotor must be lined with this one. Performing a 2D magnetostatic analysis, the 2D direct axis synchronous inductance, Ld-2D, can be computed in several ways. In case of linear magnetic circuit, this inductance can be determined in terms of the stored magnetic energy, Wm, with relation, 2 L d − 2D = 4Wm /(3I a ) . (2) Another possibility to compute this inductance, regardless of the magnetic circuit linearity, is in terms of the linkage magnetic flux. In our case, the direct axis flux is quite the a phase linkage flux, Φa , and the inductance is, Ld −2D = Φa /I a . (3) Of course, it could have been chosen the moment when Ia=0, and Ib=-Ic, Ic=Imcos30, respectively, but in this case the angle between magnetic field and direct axis is 90 electrical degrees. So the rotor has to be rotated with the same angle. In terms of the magnetic energy, the inductance is computed as in (2). In terms of magnetic fluxes, this inductance is, Ld − 2D = Φ b /I b = Φ c /I c . (4) The results obtained in this case differ from the previous ones because of the different harmonics in the two cases [4]. Quadrature axis inductance, Lq-2D, corresponds to the quadrature axis magnetic flux (Fig. 3), and this is computed in the same way as the direct axis inductance, but the axis of stator winding magnetic field has to coincide with the quadrature axis of the rotor. Thus the rotor has to be rotated with π/2p (p is the number of pole pairs) relative to previous position. In case of nonlinear magnetic circuits, the inductance values depend on the current value used in simulations. There is also a different way to determine the two inductances: only a single phase is supplied. If in the magnetostatic simulation the current is imposed only in a phase, the a phase linkage flux is obtained. If the direct axis coincides with the a phase axis, the linkage flux has the maximum value, and the direct axis inductance can be computed. If the a phase axis coincides with the quadrature axis, the linkage flux has the minimum value, and the quadrature axis inductance can be obtained. The calculus relation is, L d,q − 2D = 3Φ a /(2I a ) . (5) It can be noticed that in order to determine synchronous inductances, some particular cases were considered, namely either quadrature magnetic field or direct magnetic field was removed. There also is a possibility to determine these inductances for a certain rotor position relative to stator winding magnetic field. Considering the angle between direct axis and the a phase axis to be α, the direct and quadrature axis (d,q) currents and fluxes can be computed in terms of the three-phase (a,b,c) currents and fluxes, with the following relations [4], I d = (2/3)[I a cos α + I b cos(α − 2π / 3) + I c cos(α − 4π / 3)] I q = (-2/3)[I a sin α + I b sin(α − 2π / 3) + I c sin(α − 4π / 3)] Φ d = (2/3)[Φ a cos α + Φ b cos(α − 2π / 3) + Φ c cos(α − 4π / 3)] (6) Φ q = (-2/3)[Φ a sin α + Φ b sin(α − 2π / 3) + Φ c sin(α − 4π / 3)] The two inductances are, L d − 2D = Φ d /I d , L q − 2D = Φq /I q . (7) It has to be mentioned that regardless of the used method, the value of the end winding inductance, Lew must be added to the 2D inductance values, in order to determine the real synchronous inductances of the generator. Ld = Ld − 2D + Lew , Lq = Lq − 2D + Lew . (8) The determination methods of the end winding inductance are presented in the scientific literature [5]-[8] and it is not the object of this paper. The methods presented in this paper allow the direct computation of the 2D synchronous inductances. But the direct and quadrature axis reaction inductances, Lad, and Laq respectively, are the first to be determined, and then the synchronous inductances by adding the stator winding leakage inductance, Lσ. L d = L ad + L σ = L ad + L σ − 2D + L ew L q = L aq + L σ = L aq + L σ − 2D + L ew . (9) The reaction inductances can be determined based on the magnetic vector potential, A. For instance, from the numerical analysis performed in order to determine the direct axis synchronous inductance, the magnetic vector potential distribution on the circular surface placed in the middle of the air-gap, Fig. 4, can be obtained. From this curve the fundamental component of the magnetic vector potential, A1 [Wb/m], is determined, and then the magnitude of the magnetic flux, Φ ad , can be obtained, Φ ad = 2A 1l . a. Direct axis b. Quadrature axis Figure 5. Subtransient inductances determination Figure 6. Generator windings in case of subtransient inductances determination by FEA (10) In (10) l is the stator core length [m]. The direct axis reaction inductance is, L ad = k w NΦ ad /I a , (11) a. Direct axis subtransient inductance determination kw is the winding factor and N is the series number of turns per phase. In the same way the quadrature axis reaction inductance is computed, certainly the rotor being in the adequate position. Subtransient inductances were determined as in the experimental way. Two phases of the stator winding were supplied from a voltage source with industrial frequency. The rotor position was chosen so that the axis of the resulted magnetic field was the same as the direct axis, when the direct axis transient inductance was determined, Fig. 5a, and the axis of the resulted magnetic field was the same as the quadrature axis, when the quadrature axis inductance was determined, Fig. 5b. A 2D time harmonic analysis was performed. The stator winding resistance was set to be the analytically-computed one (or the measured one), and the stator end winding inductance was included in the phase circuit. The field winding is shortcircuited, Fig. 6. b. Quadrature axis subtransient inductance determination Figure 7. Flux lines and current density From the numerical analysis, the current in the energized phases and the linkage flux are obtained. The phase linkage flux on the current ratio is the subtransient inductance. Fig. 7a and 7b present the flux lines and the current density in all the windings in case of direct axis subtransient inductance determination and quadrature axis, respectively. Another possibility to compute these inductances is to determine the phase angle between voltage and current, and thus to determine the reactive power, Q. The inductances are determined with relation, L”d, q = Q/ (ω2I 2 ) . Figure 4. Magnetic vector potential distribution in air-gap (12) The direct axis transient inductance can be computed in the same way as the subtransient inductance, but the dumper winding must be removed. In FEA the dumper winding was open-circuited. The stator winding magnetic flux induces a current in the field excitation winding. On its turn, this current produces an opposite magnetic field. Fig. 8a presents the magnetic flux lines and current density in case of determination the direct axis transient inductance. Because the quadrature axis magnetic field does not interact with the field excitation winding (the angle between these is 90 degrees), quadrature axis transient inductance is in fact quadrature axis inductance. Indeed, it can be noticed, Fig. 8b, that current density in field excitation winding is zero when reaction field axis is quadrature axis. The path of flux lines is the same as the path of quadrature axis flux lines. III. Figure 9. No-load voltage and short circuit current characteristics THE CASE STUDY. RESULTS In the case study, a salient poles three-phase synchronous generator with DC excitation winding was considered. The main data are: outer diameter of the stator core, 106.5 mm, inner diameter, 70 mm , length, 75 mm, outer diameter of the rotor, 67.3 mm, pole pairs number, 2, stator slots number, 36, stator tooth width, 2.75 mm, turns coil number 133, phase voltage, 230 V, phase current, 0.7 A, rated power 0.37 kW. The synchronous reactances were determined experimentally by the “small slips” method [9]. The minimum and maximum value of the line voltage, the minimum and maximum value of the current were registered. Results: Umin, 35 V, Umax, 35.2 V, Imin, 0.04 A, Imax, 0.06 A. With these values the unsaturated inductances were determined, Ld = Lq = U max 3ωI min U min 3ωI max (13) From the no-load voltage characteristic and short-circuit current characteristic (reported to nominal value), Fig. 9, the unsaturated and saturated value of the direct axis reactance (in p.u.) were obtained. These values are, x d = 1 / 0.65 = 1.54 (14) x d = 1.15 (15) In table I the experimental and FEA results are presented comparatively. TABLE I. Method Inductances [mH] Ldunsatured Ld-satured Lqunsatured Lad-satured Laq-satured Ld’’ Lq’’ Ld’ COMPUTED INDUCTANCES Measured (1) Small Character slip istics 1617 1617.2 FEA (2) (1)/(2) [%] 1612.3 100.3 1072 1225.5 1046.5 98.5 102.4 1129.8 950 155.2 189 210 106.6 95.97 - 165.5 181.4 - 1207.7 - Finally, a 2D transient with motion analysis was performed in order to simulate the sudden short circuit regime. The rotor is imposed the synchronous speed and the stator windings are separated by three opened switches, the generator operating in a no-load regime. After 50 ms the three switches close suddenly and simultaneously and a three-phase short-circuit occurs. It is worth mentioning that the field winding must be supplied by a DC voltage source (not by a current source) in order to enable the occurrence of the overcurrent in the transient regime. The induced line voltages and sudden short circuit currents are presented in Fig. 9 and Fig. 10. In Fig.11 the transient torque is shown. The value of the voltage and that of the torque must be multiplied by 2 because the length of the model machine is only half of the real one. a. Direct axis transient inductance determination b. Quadrature axis transient inductance determination Figure 8. Flux lines and current density Figure 9. Induced line voltages Figure 11. Transient torque a. The stator winding currents It is also to be noticed that the value of the quadrature axis subtransient inductance is higher than the direct axis subtransient inductance. However, it must be taken into account that this is a particular, low-power type of machine, with only two pole pairs. In fact, as it results from Fig 7a and 7b the flux lines have a lower reluctance way in case b than in case a. This is due to the reaction currents from the dumper and field windings that prevent the stator winding flux from closing through the rotor direct axis. The nominal torque of this generator is 2.35 Nm and the maximum torque in transient regime is about 13 Nm, which is a torque 5.5 bigger than the nominal one. The great advantage of using FEA is that it enables the accurate parameters estimation even in the design phase. Also some transient quantities, such as sudden short circuit currents or transient torque are determined directly. 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