an investigation of dual stator winding induction machines

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in applications where only a fixed speed is required. Although several speed levels can be obtained by changing the connections of the stator winding sets, speed control of induction machines was difficult compared to the DC machines. As a result, DC machines were always used for high performance speed or torque control. The advantage of DC machines lies in the independent regulation of the air-gap field and armature current. The air-gap flux linearly depends on field current while the torque is proportional to the armature current when air gap flux level is fixed. A precise speed control can be achieved by regulating the torque of the machine. However, the torque control of the induction machine is apparently complicated due to the coupling characteristic between air-gap flux and stator currents while electromagnetic torque is the cross-product of them. The development of power electronics provides a novel method of energy conversion such that one kind of electrical energy can be freely converted to another kind of electrical energy with acceptable small losses. The conversions of electrical power can be broadly classified as DC-to-DC, DC-to-AC, AC-to-DC and AC-to-AC and the converters corresponding to each energy conversion are generally called DC-DC converter, inverter, rectifier and AC-AC converters respectively. A diagram of a three-phase Voltage Source Converter (VSC) is shown in Figure 1.1. o Ea Eb Ec Sap Sbp Scp San Sbn Scn 4 Vdc 2 Vdc 2 Figure 1.1 The diagram of a three-phase voltage source converter Vdc + −
It should be noted that at any time the power flowing in the converters could be bi- direction with the same hardware topology. For example, the voltage source converter shown in Figure 1.1 is called as voltage source inverter when power is flowing from dc side to ac side and it can also be called as voltage source rectifier when power is flowing from ac side to dc side. The power direction is dominated by the direction of dc current in the voltage source converter while dc voltage direction is unchanged. Energy conversion in converters is achieved by the Pulse Width Modulation (PWM) technique. The turn on and turn off time of each switching device is calculated from a control scheme and when these PWM pluses are applied, the fundamental voltages embedded in the output PWM voltages are the same as the desired ones. The PWM technique can be generally divided into Carrier-based PWM (CPWM) and Space Vector PWM (SVPWM). In the CPWM method, the modulation signals which contain certain magnitude, frequency and angle information are compared with a high frequency carrier signal to generate the switching pulses. The pulses are “one” when modulation signals are larger than the carrier signal and “zero” when modulation signal are smaller than carrier signal. However, the turn on and turn off times of each device are calculated and then sent to the PWM generator directly in the SVPWM method. The development of fast switching devices in power converters and microcontrollers provides the possibility of implementing complex control schemes to the induction machine. Generally speaking the variable speed control of an induction machine can be classified into two main categories: scalar control and vector control. The scalar control is the first control scheme applied to the induction machine. The constant volts per Hertz (Constant V/Hz) control is the simplest and most robust scalar 5
Page 1 and 2: AN ABSTRACT OF A DISSERTAION AN INV
Page 3 and 4: coupling and interaction terms are
Page 5 and 6: CERTIFICATE OF APPROVAL OF DISSERTA
Page 7 and 8: ACKNOWLEDGEMENTS I would like to ex
Page 9 and 10: vi Page 2.2 Machine Design I.......
Page 11 and 12: viii Page 4.2.3 Self Inductances of
Page 13 and 14: x Page 7.3.4 f = 30 Hz and f = 95 H
Page 15 and 16: xii Page 10.8 D-decomposition Metho
Page 17 and 18: LIST OF FIGURES xiv Page Figure 1.1
Page 19 and 20: Figure 3.10 The simulation of the s
Page 21 and 22: Figure 3.34 Measured flux densities
Page 23 and 24: xx Page Figure 4.8 Self-inductance
Page 25 and 26: Figure 5.2. Simulation results for
Page 27 and 28: Figure 6.8. The dynamic response of
Page 29 and 30: Figure 7.22. Copper losses of the m
Page 31 and 32: Figure 8.7. The dynamic response of
Page 33 and 34: Figure 9.4 Steady state analysis, (
Page 35 and 36: Figure 9.12. The steady state wavef
Page 37 and 38: xxxiv Page Figure 10.16 Pole-zero m
Page 39 and 40: Figure 11.2 Per phase equivalent ci
Page 41 and 42: CHAPTER 1 INTRODUCTION AND LITERATU
Page 43: The last is the recently developed
Page 47 and 48: A. R. Munoz and T.A. Lipo are pione
Page 49 and 50: has to be modified to adapt to thes
Page 51 and 52: circuit model of an induction machi
Page 53 and 54: ωr stator rotor 13 ωr rotor (a) (
Page 55 and 56: 1.2.4 Field Analysis Method In [5.1
Page 57 and 58: separated dc source, etc. From the
Page 59 and 60: in [8.14]. In [8.15-8.17], the stud
Page 61 and 62: [8.22] and the total losses of the
Page 63 and 64: proposed. The switching frequency i
Page 65 and 66: The actual rotor mechanical speed i
Page 67 and 68: 1.2.9 Induction Machine Drive---Vec
Page 69 and 70: stator windings were used as flux s
Page 71 and 72: The rotor flux can be obtained by:
Page 73 and 74: The basic idea of a closed loop flu
Page 75 and 76: estimation. It has been claimed in
Page 77 and 78: { k [ ˆ* ( i iˆ ) ] ( k) [ ˆ* Im
Page 79 and 80: integral and a new stretch-turn ope
Page 81 and 82: The most recent overview paper is g
Page 83 and 84: CHAPTER 2 DUAL STATOR WINDING INDUC
Page 85 and 86: Table 2.1 Parameters of machine des
Page 87 and 88: A C B 2.2.2 Air Gap Flux Density X
Page 89 and 90: where, ω s1 and s2 respectively.
Page 91 and 92: There are two unknown variables in
Page 93 and 94: Since small machines typically have
Page 95 and 96:
N s E = (2.18) 4. 44 fK φ 1 m Flux
Page 97 and 98:
conduct away the heat produced in t
Page 99 and 100:
k cs τ s = 2 2b ⎪ ⎧ ⎡ ⎤⎪
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are: Fts = H ts( ave) d s ( ave) =
Page 103 and 104:
1 2 1 = H o ( ) + H o ( ) + H cr 90
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The skew of the stator winding is n
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0 bs Figure 2.5. Detailed stator sl
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y: The pole pitch at the mid point
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L lsk = L m ( α 2) ⎪⎧ ⎡sin
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2.3.4 Rotor Bar Resistance r b The
Page 115 and 116:
2.3.7 Rotor Resistance Referred to
Page 117 and 118:
Substituting δ = π into (2.97) an
Page 119 and 120:
atio also increases. The air gap fl
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From (2.105-2.108), the ratio of th
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2.5 Conclusions In this chapter, a
Page 125 and 126:
A recently developed dual stator wi
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stator winding induction machine ba
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∫ H ⋅ dl = ∫ J ⋅ ds = N ⋅
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theory itself is correct. The inacc
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( θ ) ⋅ g( θ, θ ) − H ( 0)
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where ( θ ) n A is the average of
Page 137 and 138:
Since the definition of the mutual
Page 139 and 140:
3Cs1 Cs1 − Cs1 − 3Cs1 6Cs1 4Cs1
Page 141 and 142:
3.4.2 Mutual Inductances of the ABC
Page 143 and 144:
where, ( θ ) n is the average of t
Page 145 and 146:
1 0 α 1 − r 2π α − r 2π Fig
Page 147 and 148:
When the skewing factor of the roto
Page 149 and 150:
3.6 Calculation of Stator-Rotor Mut
Page 151 and 152:
dλ v = R ⋅ i + (3.58) dt where,
Page 153 and 154:
3.7.1.3 Stator flux linkage in ABC
Page 155 and 156:
where, r R is the resistance matrix
Page 157 and 158:
Only terms in equation (3.77) which
Page 159 and 160:
119 ( ) ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥
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−1 −1 −1 where, λ qdr = Tr L
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3.16 and Figure 3.17. It is found f
Page 165 and 166:
Figure 3.11 The simulation of the d
Page 167 and 168:
Figure 3.14 The simulation of the s
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Figure 3.16 Rotor bar currents duri
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Phase Y Figure 3.20 Air gap flux de
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Figure 3.24 Total air gap flux dens
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Figure 3.27 The air gap flux densit
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Figure 3.29 Air gap flux density co
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Figure 3.33 Air gap flux density in
Page 181 and 182:
All the waveforms shown above are t
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Figure 3.39 Air gap flux density pr
Page 185 and 186:
Figure 3.42 Normalized spectrum of
Page 187 and 188:
Page 189 and 190:
Page 191 and 192:
Page 193 and 194:
CHAPTER 4 FULL MODEL SIMULATION OF
Page 195 and 196:
Substituting (3.28) and (3.29) into
Page 197 and 198:
Figure 4.3 Self-inductance under 20
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Figure 4.4 Mutual inductance under
Page 201 and 202:
that L AB = L BA , L BC = L CB and
Page 203 and 204:
Page 205 and 206:
Page 207 and 208:
the assumption that the rotor skew
Page 209 and 210:
Page 211 and 212:
Page 213 and 214:
Page 215 and 216:
4.4 Mutual Inductances Calculation
Page 217 and 218:
Figure 4.24 Stator rotor mutual ind
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Figure 4.25 Stator rotor mutual ind
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varying inductances excited by four
Page 223 and 224:
Equations similar to (4.15-4.16) we
Page 225 and 226:
the number of poles for the winding
Page 227 and 228:
Figure 4.29 Dynamic response of dua
Page 229 and 230:
(a) (b) (c) (d) Figure 4.32. Normal
Page 231 and 232:
CHAPTER 5 FIELD ANALYSIS OF DUAL ST
Page 233 and 234:
In the analysis that follows the fu
Page 235 and 236:
where, C s1 is the number of series
Page 237 and 238:
θ , ∂B1 µ 0r = ⋅ J1 θ ∂θ
Page 239 and 240:
C C = k π ⋅ d s2 s2 s2 199 (5.19
Page 241 and 242:
the XYZ winding set is obtained by
Page 243 and 244:
u rpi 2π ' k − jk θ −( i−1)
Page 245 and 246:
The corresponding flux densities in
Page 247 and 248:
The first term in equation (5.55) i
Page 249 and 250:
The second term in (5.64) is zero u
Page 251 and 252:
5.2.2 Torque Equation The calculati
Page 253 and 254:
Re j( ω ) ⎧ 1t− P1θ µ 0r j(
Page 255 and 256:
* ( ) ( ) ( ) ⎛ P1 ⋅ ⋅ ⎞ j
Page 257 and 258:
* Since both ( ) C 2π ∫ 0 2 * Cs
Page 259 and 260:
(A) Induced voltage in the ABC wind
Page 261 and 262:
5.3.3 Equation of Torque Contribute
Page 263 and 264:
winding set works as a generator, w
Page 265 and 266:
possible for the brushless doubly-f
Page 267 and 268:
Since the number of rotor bar is n,
Page 269 and 270:
5.6 Computer Simulation and Experim
Page 271 and 272:
Figure 5.2. Simulation results for
Page 273 and 274:
5.7. Conclusions In this chapter, u
Page 275 and 276:
good steady-state predictions and c
Page 277 and 278:
which are superimposed some space h
Page 279 and 280:
(a) (b) (c) Figure 6.1: Main flux s
Page 281 and 282:
(a) (b) (c) (d) (e) Figure 6.3: Fin
Page 283 and 284:
(a) (b) Figure 6.5: Induced air-gap
Page 285 and 286:
Substituting (6.7) into (6.4-6.6),
Page 287 and 288:
L L L L L L L λ + lr1 m1 ls1 m1 lr
Page 289 and 290:
6.4 Simulation and Experimental Res
Page 291 and 292:
Figure 6.7 . Simulation results for
Page 293 and 294:
Figure 6.9 Experimental results for
Page 295 and 296:
diminish the contribution of the 6-
Page 297 and 298:
CHAPTER 7 STEADY STATE ANALYSIS OF
Page 299 and 300:
where, L L = (7.11) si mi iqdri λq
Page 301 and 302:
Overall efficiency of the dual stat
Page 303 and 304:
Figure 7.2 Stator current speed cha
Page 305 and 306:
Figure 7.6 Power factor speed chara
Page 307 and 308:
Figure 7.9 Power factor speed chara
Page 309 and 310:
7.3.5 f = 35Hz and f = 90 Hz abc xy
Page 311 and 312:
Figure 7.16 Torque speed characteri
Page 313 and 314:
this conclusion is based on the ass
Page 315 and 316:
Figure 7.21. ω s1 vs s2 ω when to
Page 317 and 318:
Figure 7.25 ω s1 vs s2 ω when the
Page 319 and 320:
Figure 7.28. Copper losses of the m
Page 321 and 322:
7.4 Conclusions Based on the steady
Page 323 and 324:
applications and possible use as st
Page 325 and 326:
L pλ + λ = I − = σ (8.3) ( ω
Page 327 and 328:
espectively. The stator q and d axi
Page 329 and 330:
* 3 * ( V I ) V Re( M I ) 3 P p = R
Page 331 and 332:
the modulation index of the rectifi
Page 333 and 334:
Lie derivative and relative order d
Page 335 and 336:
The above algorithm requires that t
Page 337 and 338:
σ = 3 1+ K ( Vqs1iqs1 + Vds1 ds1)
Page 339 and 340:
Butterworth polynomial with the den
Page 341 and 342:
Table 8.1 Parameters of controllers
Page 343 and 344:
generally the case to get a good pe
Page 345 and 346:
Table 8.2 Machine parameters for si
Page 347 and 348:
(a) (b) (c) (d) (e) (f) (g) Figure
Page 349 and 350:
(a) (b) (c) (d) (e) (f) (g) (h) (i)
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(a) (b) (c) (d) (e) (f) (g) (h) (i)
Page 353 and 354:
CHAPTER 9 HIGH PERFORMANCE CONTROL
Page 355 and 356:
The qd0 voltage equations of a dual
Page 357 and 358:
317 ( ) ( ) ( ) ( ) ( ) ⎥ ⎥ ⎥
Page 359 and 360:
If the rotor speed and the rotor fl
Page 361 and 362:
Infeasible region (a) Vdc1 and Vdc2
Page 363 and 364:
The influences of the saturation of
Page 365 and 366:
Figure 9.5(a), by varying the q-axi
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Figure 9.5 Steady state analysis, (
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L1 L3 2 ( 1− K ) Vdc1 3 = ( Vqs1i
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If the PI controllers are used and
Page 373 and 374:
egulation capabilities of the contr
Page 375 and 376:
(a) (b) (c) (d) (e) (f) (g) (h) (k)
Page 377 and 378:
(a) (b) Figure 9.11. The starting p
Page 379 and 380:
9.6 Conclusions The high performanc
Page 381 and 382:
induction machine are applicable to
Page 383 and 384:
In section 10.2, the fundamentals o
Page 385 and 386:
The vector control of an induction
Page 387 and 388:
possibilities for fault conditions,
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where, where, − r r L = (10.18) (
Page 391 and 392:
qsi qsi * ( I I ) σ = K ⋅ − (1
Page 393 and 394:
In the proposed control scheme, rot
Page 395 and 396:
* ωr * ωr + + − ωr k p + ki s
Page 397 and 398:
The value of ω 0 determines the dy
Page 399 and 400:
10.4.4 Stator D-axis Current Contro
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(a) (b) (c) (d) (e) (f) Figure 10.4
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The proposed control scheme has als
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(a) (b) (c) (d) (e) (f) (g) Figure
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10.6 Full-order Flux Observer The c
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while the second three-phase windin
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L r L p ˆ λ ˆ ˆ (10.66) ri si r
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373 [ ] ( ) ( ) ( ) ( ) ( ) ( ) ( )
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t 2bi ⎛ rsiLri K iL ⎞ ⎛ ri K
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ri D i si ri ri si mi ri 2 ( K )
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esults show that the selected obser
Page 421 and 422:
Figure 10.12 The poles of the 6-pol
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383 ( ) ( ) ( ) ( ) ( ) ( ) ( ) ( )
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⎧t s ⎨ ⎩ts 1 2 = t = t 1 2 Th
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Figure 10.15 The poles of the machi
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X i i = X Y = Y i i ( σ , ω) ( σ
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this error is used as the feedback.
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ˆ ω rm The output error is expres
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The expressions of t1 i and t2 i ar
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397 ( ) ( ) ( ) bi ei i bi ei i ai
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The transfer function of rotor spee
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(a) (b) (c) (d) Figure 10.16 Pole-z
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Figure 10.19 Pole-zero maps with di
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Figure 10.22 Pole-zero maps with di
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should ensure the stability under a
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The boundary of the speed controlle
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10.11 Simulation Results for Sensor
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Figure 10.28 Speed estimation for 2
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(a) (b) Figure 10.31 Speed estimati
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(a) (b) (c) (d) (e) (f) Figure 10.3
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Figure 10.34 Actual and estimated v
Page 461 and 462:
CHAPTER 11 HARDWARE IMPLEMENTATION
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esistance for two phase windings. T
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11.2.3 Short Circuit Test The short
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When the input voltages of 2-pole A
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winding set is generating and the o
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11.4 Per Unit Model For the fixed p
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1 = 12 2 0. 0024414 The transformat
Page 475 and 476:
ase values of voltage/current. The
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Start System configuration Initiali
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CHAPTER 12 CONCLUSIONS AND FUTURE W
Page 481 and 482:
Using the rotating-field theory and
Page 483 and 484:
each winding have been clearly show
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voltages of different frequencies,
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REFERENCES 447
Page 489 and 490:
[2.2]. P. C. Roberts, "A Study of B
Page 491 and 492:
[5.3]. R. A. McMahon, P. C. Roberts
Page 493 and 494:
[8.17]. O. Ojo, “Performance of s
Page 495 and 496:
[10.5]. J. C. Moreira, K. T. Hung,
Page 497 and 498:
[10.27]. M. Hinkkanen, “Analysis
Page 499 and 500:
[10.48]. K. Lee and F. Blaabjerg,
Page 501 and 502:
VITA Zhiqiao Wu was born in Shashi,
Page 503:
3. Zhiqiao Wu and O. Ojo, "High Per
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an investigation of dual stator winding induction machines

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