electric motor based projects
TRANSCRIPT
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EXPERT SYSTEMS AND SOLUTIONS
Email: [email protected]
Cell: 9952749533www.researchprojects.info
PAIYANOOR, OMR, CHENNAI
Call For Research Projects Final
year students of B.E in EEE, ECE, EI,
M.E (Power Systems), M.E (Applied
Electronics), M.E (Power Electronics)
Ph.D Electrical and Electronics.
Students can assemble their hardware in our
Research labs. Experts will be guiding theprojects.
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PRESENTATION ON
SYNCHRONOUS MACHINEMODEL
TANDIN JAMTSHO
STUDENT #3226091
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This presentation shall cover thefollowing topics Introduction
Mathematical model
Circuit based model used for both steady state and transientanalysis
Differential equation model
Conclusion
Discussion at the end of presentation
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The main component of powersystem are
GeneratorStep up
Transformer
Transmission
Line
Step down
TransformerLoad
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Principle of synchronous machine Based on the principle of Faradays
law of electromagnetic induction
Generally the armature winding arelocated on the stator and fieldwinding on the rotor
The field winding is excited by adirect current
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What is mean by synchronous
machine ? A machine that operates at constant
speed and frequency with respect to
time is called the synchronousmachine.
N=120f/P
N=speed of the machine in rev/min
F=frequency in Hz
P=number of poles
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Assumptions made are: The stator windings are sinusoidally
distributed electrically
The effect of the stator slots on thevariation of any rotor inductanceswith rotor angle is neglected
Saturation effect neglected.
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Mathematical model Source of the diagram:
Mohamed E. El-Hawary,Electric Power Systems
Design and Analysis
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By Faradays, the voltage induced in the stator coil
cricpeb
ribpeariape
c
b
a
!
!!
P
PP
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Where
ea = terminal voltage of phase a
P = total flux linkage of phase aia = current in phase a
a,b and c are phases
r = the resistance of each armature winding,
assumed to be same for all three phasesp = the derivative operator d/dt, t is the time
ef = p Pf +rfif
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Inductance
The self inductance of any stator winding phases are given by
U2cos20 aaaaaa LLl !
)120(2cos20 ! Uaaaabb LLl)120(2cos20 ! Uaaaacc LLl
The mutual inductance between any two stator phases are given by
)]30(2cos[ 20 !! Uaaababab LLll
)]90(2cos[ 20 !! Uaaabcbbc LLll)]150(2cos[ 20 !! Uaaabac LLllca
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Elimination of old variable ia ,ib, ic,by introducing
a new variable io
Now I o=1/3(ia+ib+ic )
-
!
3/13/13/1
)120sin(3/2)120sin(3/2sin3/2
)120cos(3/2)120cos(3/2cos3/2
UUU
UUU
-
o
q
q
i
i
i
-
c
b
a
i
i
i
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The new variable for flux linkage
,qP 0P,dPThe equivalent d-axis moving armature coil self
inductance is
The equivalent quadrature-axis moving armature
self inductance is
Zero sequence self inductance is
23/20 aaaboaa LLLL !
23/20 aaaboaaq LLLL !
abaa LLL 200 !
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The armature voltage equation in terms of d,q
and 0 becomes
000 ripe
rippe
rippe
qdqq
dqdd
!
!
!
P
UPP
UPP
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Under steady state operation, flux linkage in per unit along d
and q axis and the voltage relation can be written as
qqq
fdadddd
iL
iLiL
!
!
P
P
dddfdaddq
dqqqd
riixixie
riixrie
q
d
r !
!
!
!
P
P
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On open circuit condition id=iq=0
ed=0 and eq=xadifd Voltage in the q-axis is due to excitation in the
d-axis, lets denote it by E
E= xadifd
ed=xqiq-rid eq=E-xdid-riq
e=ed+jeq
i=id+jiq
Eq=E-(xd-xq)id eq=Eq-xdid-riq
eq=jEq-(r+jxq)I
J Eq=e+(r+jxq)i
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Steady state Vector diagram
H
JO
A
C
D
E
F
B
q-axis
d-axis
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OA=e OD=current, i AC=ir drop CD=jxq OD=e+(r+jxq)i DE=j(xd-xq)id
OE=jE=jEq+j(xd-xq)id If xd=xq, the triangle DEF will vanish
for round rotor machine.
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Determination of xd, xq and xo From slip test
Xd=Max. voltage/Min. current
Xq=Min.voltage/Max current
Xd=open ckt. Voltage/Isc By applying positive sequence current to the armature
and measure the voltage for obtaining Xd and xq.
Xo is measured by connecting the three phasewinding in series and passing single phase current
Xd will be within the range of 0.6 to 2.2
Xq will be within the range of 0.4 to 1.4
X0 will be within the range of 0.01 to 0.25 per unit forall the cases.
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Circuit based models for round rotor and salient
pole synchronous machine are
Reactance of air gap flux is represented xo and the leakage fluxreactance is represented by xl
Xs= xo+xl
Xs
I
E +++
-
V 0
-
+
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D-axis equivalent circuit
dP
fdPd1P
id ifd
i1d
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Q-axis equivalent circuit
dP
qPq1P
iq i1q
q1P
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Transient circuit based model D-axis equivalent circuit for the sub-transient
perioddi(
dP(di(
fdi( di1(
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Q-axis equivalent circuit for the sub-transient period
qi(
dP
qP(qi( qi1(
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Sub-transient and transient reactance The idea of transient for a very short period is called Sub-
transient, the sub-transient direct and quadrature axis aredefined as
Xd= d/id Xq= q/iq
Xd=Ll+ (1/(1/Lad+1/Lfd+1/L1d+---)) Xq=Ll+ (1/(1/Laq+1/L1q+---)) The transient which last for some time around 30 cycles is
termed as transient, the transient reactance of direct andquadrature axis are given by
Xd=Ll+ (1/(1/Lad+1/Lfd))
Xq=Ll+ (1/(1/Laq)) X2=( Xd+ Xq)/2
P
PP
P
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Time constants
Tdo=Xffd/rfd ( direct axis transient open circuit timeconstant, 2 to 11 seconds)
Td=Xd*Tdo/Xd (direct axis transient short circuit
time constant Td=Xd*Tdo/Xd (direct axis sub-transient time
constant Tdo =(x11d-x2f1d/xffd)/r1d (direct axis sub-
transient open circuit time constant) Tqo=x11q/r1q
Tq=xq*Tqo/xq Ta=x2/r (armature short circuit time constant)
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Swing equation of synchronous
machine We know that per unit mechanical acceleration
equation
p2=(Tm
-T
e
)/H
P=d/dt, angle in electrical radians between d-axis and the centre of phase a axis.
H=inertia constant of machine in per unit(KW-rad/kVA)
Tm=mechanical torque input in per unit
Te =electromagnetic torque developed in per
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=t+
the reference axis and the quadrature axis
The equation can be written as =angle between
p2 =(Tm-T
e)/H
By expressing angle in degrees and time in seconds it becomes
p2 =180fb(Tm-T
e)/H
Since p.u electrical torque =p.u air gap power developed
p2 =180fb(Pm-P
e)/H
Swing equation of synchronous
machine
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In literature the quantities involved are expressed in their
natural units without the use of per unit notation
p2 =(Pm-Pe)/M
M=GH/180fb,G is the rating of the machine in kVA,
H in kW-sec/kVA ,Pm and Pe in kW
Swing equation of synchronous
machine
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Conclusion One can get the idea of basic machine parameters
associated with synchronous machine for building models.
After understanding the machine parameters the models
used in MATLAB are built.
This can help in choosing the right model for analysing theperformance of the synchronous machine.
It will be very useful for those working in power stations.
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Reference Mulukutla S.Sarma, Synchronous Machine (Their
Theory, Stability and Excitation Systems).
Charles Concordia, Shycnronous Machines Theory and
Performance.
Mohamed E. El-Hawary, Electric Power SystemsDesign and Analysis
Yao-Nan Yu, Electric Power System Dynamics.