power system stability_unit 4 psoc

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    Power System Stability

    Unit-IV

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    What is Stability

    Ability of the system to return to normal or

    stable operation after having been subjected

    to some disturbance

    Rotor Angle Stability-ABILITY OF SYSTEM TO

    REMAIN IN SYNCHRONISM EVEN AFTER

    DISTURBANCE

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    Disturbance

    Load Changes

    Faults

    Structural Changes due to isolation of somefaulted elements

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    Non-linear , dynamiccontinuously changing

    PS

    Stability dependent on initial operating

    conditions and nature of disturbance

    PS maybe stable for some (large ) disturbances

    and maynot be stable for another

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    Types of Stability

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    Rotor Angle Stability

    ability of system to remain in synchronism

    even after disturbance

    Some generators accelerate while others

    decelerate losing synchronism

    Small signal rotor angle stability, large signal

    rotor angle stability

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    Small signal rotor angle stability

    Maintain synch under small disturbances

    Linearized around initial operating conditions

    Stability depends only on operating cond andnot disturbance

    Instability- non oscillatory periodic inc in rotor

    angle or increceasing amplitude of rotoroscillations due to insufficient damping

    10-20 sec time frame

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    Large signal rotor angle stability

    Large disturbance

    Instability- large excursions from generator rotorangles

    Dependent of initial operating cond ANDdisturbance parameters like type,magnitude,location etc

    3-5 sec time frame

    Dynamic Stability- Small Signal+ automaticcontrols (outdated terminology)

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    Swing Equation

    NORMAL-Relative position of the rotor axis andresultant magnetic field axis is FIXED-POWERANGLE or TORQUE ANGLE

    DISTURBANCE-rotor will deccelerate or acc w r tsynch rotating air gap mmf

    Equation describing relative motion of rotor-SWING EQUATION

    No power changerotor angle remains sameotherwise rotor comes to new operating powerangle relative to synch revolving field

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    Swing Equation -Derivation

    E- no load generated emf

    V-terminal voltage

    -power angle

    Te-electromagnetic torque developed

    sm-Synchronous Speed

    Tm-Driving Mechanical Torque

    J-combined moment of inertia of gen and prime mover m-angular displacement of rotor wrt stationary ref

    frame

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    Derivation-Begins

    Under Steady State cond

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    Modeling of Synchronous Machines-

    Cylindrical Rotor

    Constant voltage, E` and transient reactance

    Xd`

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    Real Power at node 1

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    Power angle curve(Pe vs )

    Maximum Power is referred to as Steady State StabilityLimit (SSSL)

    Gen o/p can be inc till SSSL

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    Modeling of Synchronous Machines-

    Considering Saliency

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    Under transient conditions

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    Steady State Stability

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    Transient StabilityEqual Area Control

    Equal Area Criteria to analyse stability

    Graphical method based on energy stored in

    rotating mass.

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    Must be zero for stability

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    Application of EAC-Sudden increase in

    Power Input

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    Unit-IV contd

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    Application of EAC-three phase fault

    Bolted fault at F- no power transfer to infinite

    bus,Pe=0( Power angle curve is horizontal axis)

    M/c takes total power input,Pm to accelerateand store KE

    Fault at sending end

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    Fault cleared

    at del1

    Critical clearing angle: A2>A1 : loss of stability

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    Critical Clearing time which is the time taken by the machine to swing from

    its initial position to its critical

    clearing angle

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    Fault in between

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    Step by Step solution of swing

    equation

    the period of interest is divided into several shortintervals

    The change in the angular position of the rotorduring a short interval of time is computed by

    making the following assumptions1. The accelerating power Pa computed at the

    beginning of an interval is constant from themiddle of the proceeding interval to the middle

    of the interval considered.2. d/dtis constant throughout any interval at the

    value computed at the middle of the interval.

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    Factors affecting transient stability

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    Auto reclosures

    80-90% faults are temporary

    Auto reclosing improves transient stability

    when done for temporary faults

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    Method of improving thetransient stability limit of a power system

    Increase of system voltages, use of AVR

    Use of high speed excitation system

    Reduction in system transfer reactance

    Use of high speed reclosing breakers

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    Voltage Stability

    voltage stability is concerned with the ability of apower system to maintain acceptable voltages at allbuses in the system under normal conditions and afterbeing subjected to a disturbance

    voltage instability when a disturbance results in aprogressive and uncontrollable decline in voltage

    Following voltage instability, a power systemundergoes voltage collapse if thepost-disturbance

    equilibrium voltages near loads are below acceptablelimits.

    Voltage collapse may be total (blackout) or partial

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    MATHEMATICAL FORMULATION OF VOLTAGE

    STABILITY PROBLEM

    slower forms of voltage instability are

    normally analysed as steady state problems

    using power flow simulation

    PV curves and QV curves- give steady-state

    loadability limits which are related to voltage

    stability

    Consider the radial two bus system

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    V is a double-valued function

    P for a particular pf which determines Q interms of P

    For each value of pf, the higher voltagesolution indicates stable voltage case, whilethe lower voltage lies in the unstable voltageoperation zone

    the changeover occurs at Vcr(critical) andPmax

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    Increase beyond Pmax, V(dec), I (inc), drop(inc)

    and V further decreases

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    QV curve

    Consider once again the simple radial system

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    Automatic Voltage Restorer

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    Reactive Power and Voltage Control

    Generator Excitation System-maintains genvoltage and controls reactive power

    AVR- to maintain constant terminal voltage

    Voltage mag is sensed using PT on a phase

    Voltage rectified and compared with the dcsetpoint

    Amplified error signal control exciter field and incexciter terminal voltage

    Gen field current is inc and then gen emfincreases

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    Amplifier model

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    Exciter model

    Generator model

    Sensor Model

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    Modified AVR

    With stabilizer to improve response