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Armature reaction at different load power factors

Short answer

Armature reaction is the effect of stator current on the rotor field flux. At unity pf it is cross-magnetizing (slight voltage drop), at lagging pf demagnetizing (large drop, V<E), and at leading pf magnetizing (voltage rise, V>E). It is represented by reactance Xa in the equivalent circuit.

What is meant by armature reaction in a synchronous generator? Explain the effect of armature reaction on the terminal voltage (emf) of an alternator at (i) unity power factor (resistive) load, (ii) lagging power factor (inductive) load and (iii) leading power factor (capacitive) load. Draw relevant phasor diagrams.

Armature reaction is the effect of the magnetic field set up by the armature (stator) current on the main field flux produced by the rotor poles. When the alternator is loaded, the three-phase armature currents produce a rotating mmf that rotates at synchronous speed along with the rotor. This mmf distorts, weakens or strengthens the main flux depending on the power factor of the load, and so changes the terminal voltage.

In the equivalent circuit, armature reaction is represented by a fictitious reactance XaX_a; together with the leakage reactance XlX_l it forms the synchronous reactance Xs=Xa+XlX_s = X_a + X_l, and

Eˉ=Vˉ+Iˉ(Ra+jXs)\bar E = \bar V + \bar I (R_a + jX_s)

(i) Unity power factor (resistive) load

  • The armature current is in phase with the emf, so each conductor carries its maximum current at the instant it is under the centre of a pole (where its emf is maximum). The armature mmf is then at 90° (in quadrature) to the main flux.
  • The effect is cross-magnetising: flux is distorted (crowded at one pole tip, weakened at the other) but its average value changes little.
  • The terminal voltage drops only slightly (mainly due to IRaIR_a and the small quadrature drop). EE is only a little greater than VV.
 (a) Unity pf load
                    E
                  / |
                /   |  j I Xs
              /     |
            O-------+  V
            O------->  I  (in phase with V)

(ii) Lagging power factor (inductive) load

  • For zero pf lagging, the current lags the emf by 90°; armature flux acts directly opposite to the main flux along the pole axis.
  • The effect is demagnetising; the resultant air-gap flux and generated voltage fall.
  • For a practical lagging pf (e.g. 0.8) the effect is partly cross-magnetising and partly demagnetising.
  • The terminal voltage falls considerably with load; V<EV < E, and regulation is large and positive. More field current is needed to keep VV constant.
 (b) Lagging pf load
                      E
                     /|
                   /  |  j I Xs
                 /    |
               O------+ V
                `-.
                   `-. I  (lags V by phi)

(iii) Leading power factor (capacitive) load

  • For zero pf leading, the current leads the emf by 90°; the armature flux acts along the main flux.
  • The effect is magnetising (strengthening); the air-gap flux increases.
  • The terminal voltage rises with load; VV can be greater than EE, so regulation can be negative. Less field current is needed.
 (c) Leading pf load
             I      E
              \    /'.
               \  /   '.  j I Xs
                \/      '.
                O----------+ V
      I leads V by phi;  E < V

Summary

Load pfNature of armature reactionEffect on terminal voltage
UnityCross-magnetising (distorting)Small drop
Zero laggingPurely demagnetisingLarge drop (V<EV < E)
Zero leadingPurely magnetisingRise (V>EV > E)
Practical lag/leadCross + de-/magnetisingDrop / rise

✓ Answer checked by Claude Sonnet 5.5

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