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    EXPERT SYSTEMS AND SOLUTIONS

    Email: [email protected]

    [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.