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Dynamic Stability- Small Signal+ automaticcontrols (outdated terminology)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