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Handbook of Electrical Engineering For Practitioners in the Oil, Gas ...

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302 HANDBOOK OF ELECTRICAL ENGINEERINGA more detailed treatment <strong>of</strong> this aspect is given <strong>in</strong> sub-section 3.5, however, (11.10) will beused to illustrate <strong>the</strong> stability problem.11.11.1.1 Steady state stability <strong>of</strong> a generator or motorEquation (11.10) applies to any simple form <strong>of</strong> synchronous source and s<strong>in</strong>k where E R and E S and<strong>the</strong> voltages at ei<strong>the</strong>r side <strong>of</strong> <strong>the</strong> l<strong>in</strong>k<strong>in</strong>g reactance X. δ is <strong>the</strong> phase angle between E R and E S .<strong>For</strong><strong>the</strong> generator case, E R and E S may be replaced by V and E g and X by X sg . (<strong>For</strong> <strong>the</strong> synchronousmotor case E R and E S may be replaced by E m and V and X by X sm .)Hence, for <strong>the</strong> generator:P = VE gs<strong>in</strong> δ gX sgNow V is usually kept close to <strong>the</strong> system rated voltage, i.e. 1.0 pu± 0.05 pu and X gs ,<strong>the</strong>synchronous reactance <strong>of</strong> <strong>the</strong> generator may be assumed constant i.e. typically 1.8 pu to 2.9 pu(depend<strong>in</strong>g on <strong>the</strong> generator rat<strong>in</strong>g).E qis <strong>the</strong> <strong>in</strong>ternal emf produced by <strong>the</strong> field w<strong>in</strong>d<strong>in</strong>g on <strong>the</strong> rotor. Hence, for any givenvalue <strong>of</strong> power P supplied by <strong>the</strong> generator <strong>the</strong>re will be a wide range <strong>of</strong> E g and rotor angle δ gvalues.Example:LetV = 1.0 pu,X sg = 2.5 pu and P = 1.0 pu (full load).P = 1.0 = 1.0E g s<strong>in</strong> δ g2.5s<strong>in</strong> δ g = 2.5E g≤ 1.0It can be seen that <strong>the</strong> larger <strong>the</strong> value <strong>of</strong> E g <strong>the</strong> smaller will be <strong>the</strong> value <strong>of</strong> δ g .<strong>For</strong> full-load normal operation δ g is about 50 degrees, which would require E g to be 3.264 pu.Suppose E g is reduced to 2.51 pu, <strong>the</strong>n δ g would be 85 degrees.If E g is reduced aga<strong>in</strong>, to 2.5 pu, <strong>the</strong>n δ g wouldbe90degrees.If E g is reduced below 2.5 pu <strong>the</strong>n <strong>the</strong>re is not a value <strong>of</strong> δ g to satisfy <strong>the</strong> equation and thismeans that <strong>the</strong> power cannot be transferred if δ g is caused to exceed 90 degrees. The generator rotorcan no longer be kept <strong>in</strong> synchronism with <strong>the</strong> term<strong>in</strong>al voltage to which it is connected. δ g canbe caused to exceed 90 degrees by ei<strong>the</strong>r reduc<strong>in</strong>g <strong>the</strong> field excitation, as described above, or byallow<strong>in</strong>g more power to be applied to <strong>the</strong> generator from its prime-mover, e.g. gas turb<strong>in</strong>e. This canhappen at any level <strong>of</strong> power load<strong>in</strong>g on <strong>the</strong> generator (above zero power). When <strong>the</strong> rotor angleδ g exceeds 90 degrees, and <strong>the</strong> generator rotor pulls out <strong>of</strong> synchronism, <strong>the</strong> condition is unstablewhich means <strong>the</strong> limit <strong>of</strong> steady state stability has been exceeded.

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