A Dynamic Magnetic Equivalent Circuit Model for the Design of Wound Rotor Synchronous Machines Research of Xiaoqi (Ron) Wang Advisor: Steve Pekarek Department of Electrical and Computer Engineering Purdue University
WRSM/Rectifier Design +
Ifd ias WRSM
ibs ics
vdc
_
WRSM/active rectifier
WRSM/passive rectifier
design d rc l d rt g d st dbs fwss fhrt fwrt fwrp N s I s N fd I fd Pp
I as I s cos( r )
ftipw ftiph
T
design d rc l d rt g d st dbs fwss fhrt fwrt fwrp N s N fd I fd Pp ftipw ftiph rdt d num dcon Vdc f ( I fd , L"q , L"d ) 2
T
MEC Model for Active Rectification • A steady-state mesh-based MEC model for WRSMs
3
Performance Calculation • Electromagnetic torque P Te , r 2
• Power loss
3 Pres rfd I 2 2 fd
Resistive loss: Core loss:
2
agj Pagj j 1 Pagj r
2 na
2
rs ias2 r dr
0
Pcore Pld ,TVST Pld ,YVSY
where Pld B kh f eq
1
T Bmax ke f dB f 2 dt and B B dt b 0 b 2
Total loss:
Pcond 3Vdrop
T
Eddy Current Loss
Hysteresis Loss
Conduction loss:
2
dB f eq dt 2 2 dt Bmax Bmin 0 2
1 2
2
0
ias r dr
Ploss Pres Pcore Pcond 4
Dynamic MEC Network for Passive Rectification l - axial length of machine
RY
db
d st
h
RSH
rtt
w
rt
h
rp
rp
RTT Rag
d
rc
g
as-axis
h
w st
r
ro
rd
rto
r so
t
Φag1 idp1 Φrp1 RRTO1*
h rsi
rd
RRTE
s
Φag2 RRLO1
w stt
w ss
rs
ics' Φst2
d-a x
is
ics' Φst3
X
X
X
ias Φst4
ias Φst5
ias Φst6
ibs' Φst7
ibs' Φst8
ibs' Φst9
RTL
s q-axi θ rm
d
w
rtb
ics' Φst1
RRFB
RFL
Φag4 λdp,1 RRLO2
Φag6
RRLI1
Φag8 λdp,2 RRLO3
idp2 Φrp2 RRTI1 Φrp3 RRTI2 Φrp4 RRTO2*
RRTO3
ifd'
RRSH1
Φrt1
RRSH2
*
ifd X
RRYP
Φrt2
Φag10
Φag12
Φag15
Φag17
Φag20
λdp,3
RRLO4
idp3
Φrp5 RRTO4
RRTE
*
RRTE RRF
RRFB
RRFB
RRPL RRY
5
Rotor Pole Flux Tubes RRTO1
RRTI1
RRTI2
RRTO3
RRTO4 RRTE2
hRTO1
RRTE1
RRTO2
lRTI1 hrtm lRTE1
lRTO1
lRTO2 RRSH1
RRTO1_1 RRTO1_2 RRTO1_3
fwrto(x)
RRTO1
RRSH2 -x
x
lRTO1 2rdt lhRTO1 2l
2rdt tan 1 ( 2 2 2 2 l hRTO1 4rdt 2 hRTO1 4rdt hRTO1
6
)
Rotor Pole Tip Leakage Flux Tubes
Stator tooth
g
P3 l - axial length of machine dt
d dp dp (hRTO1 2rdt )
r P2
P1: leakage inside the bar. P2: leakage in the steel. P3: leakage in the airgap.
P1
1 hRTO1
ddp
RRLO1
0l l d dp rdt ln( ) 8 2 rdt P1
Leakage path RRLO1
P2
2 g (d dp rdt ) g 2 g d dp rdt 0l ln( ) 2 d dp rdt
Main path RRTO1*
P3
lRTO1
1 * RRTO 1
1 RRTO1
1 RRLO1 7
Damper Bar Placement • Odd number damper bars: one of the bars is located in the center of the most inner two RRTI sections. • Even number damper bars: there is no hole in the center of the most inner two RRTIi sections, but they are symmetrically distributed on the two sides of the rest of the rotor pole sections. • Arbitrary number and radius of damper bars can be applied:
damper_rtip [... rdt 3
rdt 2
rdt1 rdt 2
rdt 3 ...]
• Arbitrary vertical depth of the damper bars can be assigned by adjusting the scaling factor αdp.
8
Steady-State KVL MEC Model A(Rnlnl )φ(lnl1) =Fl(nl1)
System equation: where and
φl st1
stns rt1
rtnr ag1
Fl = Fst(ns1) Frt(nr1) 0(na1) Frp(np1) T
T
Stator and rotor MMF source: Damper winding MMF source: ( npnd ) j, k 1 where Ndp
1 0 (51) Frp = 0 0 0
T
rpnp
T
T
ns3) (31) Fst( ns1) N(abc i abcs , Frt( nr1) N(rtnr1) I fd 1 1 0 Nfd I fd T
( nd 1) Frp( np1) (j )=N(dpnpnd ) (j, k )i dp (k )
, if the kth damper winding current is in the jth rotor pole loop.
N(dpnpnd ) j, k 0
In this case,
T
agna rp1
, otherwise. 0 0 1 0 0
0 0 (31) 0 i dp 0 1 9
Dynamic System Structure KVL MEC Model i
MEC System of Equations
A R (φl ) φl =Fl =Ni
φ
Post-processing l
T λ abcs =PNabc φst
v abcs =f (i,λ )
Dynamic MEC Model
λ (k )
MEC System of Equations
AR W 2
W1 φl I =B fd 0 i λ
i (k )
External Circuit Model (e.g. Passive Rectifier)
v =f (i )
i (k )
v(k ) Numerical Integration
pλ =f (v,i ) λ (k 1)=g(pλ ,λ (k ))
OR: user-input v(k )
10
Restructuring the MEC Model 1) Expand the KVL MEC system: AR φl -Nl,abc i abcs -Nl,dp i dp =Nl,fd Ifd 2) Relate the flux and flux linkage: nd nl ) ( nl 1) nd nd ) φ(l nl1) λ abcs =PNl,abcφst , λ (dpnd 1) =M(l,dp φl 0( nd ( nl nd ) M(l,dp_sub
In this case,
dp ,1 1 1 0 rp1 0 1 1 dp ,2 1 0 1 rp 3 rp 5 dp ,3 M l,dp_sub
3) Dynamic MEC system of equations:
A R -N l,abc -N l,dp φ N 0 0 Ifd NT l l,fd i abcs = 0 I /P 0 λ abcs l,abc 0 M l,dp i dp 0 0 I λ dp 11
Dynamic System with Scaling Apply qd transformation: -1 AR - f scale N l,abc K s T f scale K s N l,abc 0 f M scale l,dp
-f scale N l,dp φl N 0 0 Ifd l,fd i qd0s,scl = 0 f scale I /P 0 λ qd0s 0 f scale I λ dp i dp,scl 0
Adyn
where
i qd0s =f scalei qd0s,scl , i dp =f scalei dp,scl , fscale 103
Compare to the structure block diagram, W1 fscale Nl,abc K s
1
f scale Nl,dp
0 0 N l,fd B 0 f scale I /P 0 0 0 f scale I
T f scale K s N l,abc W2 f M scale l,dp
12
State Equations of Damper Bars re,3
re,1
re,2
re,3
ie idp,1 λdp,3
X
re,3
rdp,1 idp,2 λdp,1 re,1
rdp,2 idp,3 λdp,2 re,2
1 3 i e i dp,k 2 k=1
rdp,3 λdp,3 re,3
From Ohm’s and Faraday’s laws, pλ dp =Tdp i dp
where
rdp ,1 re,1 rdp ,2 re,1 re,1 Tdp re,2 rdp ,2 re,2 rdp ,3 re,2 r r r r r e ,3 dp ,3 e ,3 dp ,1 e,3 13
State Equations of Stator Windings Rearrange the voltage equation:
0 1 0 pλ qd0s =v qd0s -rs i qd0s - -1 0 0 λ qd0s 0 0 0 Calculation of resistive loss:
3 Pres 2
2
0
rs ias2 r d r rfd i 2fd stator field
P 2
nd
2
k 1
0
rdp ,k idp2 ,k r re ,k ie2,k r d r damper
14
C
Hardware Validation
15
Open Circuit Voltage
Field currents:0-10.2 A Rotor speed: 1800 rpm Maximum error: 5% MEC
Hardware 16
Balanced 3-Phase Load Test Conditions: - Rotor speed: 1800 rpm - RMS line-line voltage: 480 V - Power factor: 0.8 lagging (parallel RL load) - Pmech = 303 W - rbrush = 1 Ω - Loss of exciter is not modeled
Average input torque: Tin _ avg
Load
Output power:
Pout Term Pres
Average input torque (Nm)
Output power (kW)
MEC
Test
MEC
Test
MEC
Test
1
4.8
4.5
21.01
19.98
3.1775
2.9858
2
8.0
7.6
33.81
32.26
5.3641
5.0707
3
12.0
11.4
49.95
47.78
7.9783
7.5915
4
15.9
15.2
66.11
64.16
10.4445 10.1030
MEC Load
Test
Ps+f (W)
Pcore (W)
Pdp (W)
Pcore+dp (W)
Ps+f (W)
Pcore+dp (W)
1
235.5
232.3
12.5
244.7
229.5
247.9
2
431.2
241.8
32.9
274.7
414.5
292.8
3
793.2
254.2
86.4
340.6
757.6
354.4
4
1267.4
265.3
181.9
447.2
1211.2
477.0
Term Pmech Pcore
rm
RMS values of Phase current (A)
17
Voltage Waveforms
The error of RMS values is approximately 5%. 18
Standstill Frequency Response -At low frequencies (< 0.4 Hz) Match closely. -At mid frequencies (> 0.4 Hz, 100 Hz) Error between MEC and FEA comes from the modeling of rotor pole tip leakage flux path. Lower test-q due to eddy currents.
Low-frequency asymptote: magnetizing impedances. High-frequency asymptote: subtransient impedances. 19
Different Depth of Damper Bars
αdp=0.5
αdp=0.0001
20
Influence of the Leakage Path Between Poles
21
25 MW WRSM/Rectifier Design +
Ifd ias WRSM
ibs ics
vdc
_
WRSM/active rectifier
WRSM/passive rectifier
θ drc l drt g d st dbs fwss fhrt fwrt fwrp N s I s N fd I fd Pp
ftipw ftiph
θ drc l drt g d st dbs fwss fhrt fwrt T
fwrp N s N fd I fd Pp ftipw ftiph rdt d num dcon
22
T
Pareto Front
23
Genes Distribution
WRSM/active rectifier: larger height of rotor teeth (HRT), airgap length (G), and pole pair (Pp). WRSM/passive rectifier: larger stack length (GLS), stator turns (Ns) and field turns (Nfld). 24
Example Machines
WRSM/active rectifier
WRSM/passive rectifier 25
Conclusions • Developed a voltage-input dynamic MEC model that includes damper bar currents dynamics. – Enables exploration of alternative damper configurations – Enables multi-objective design of machine/passive rectifiers – Readily extended to multi-phase machines
• Initial study utilized to compare Passive/Active designs – Surprising result is that the machine for the passive designs are less massive for a given specified loss
26