## Experiment - 8

To determine the sub-transient (x_{d}″), transient (x_{d}′) and steady state reactance (x_{d}) of a synchronous machine.

- Three phase alternator Rating: 400V, 5kVA, 1500 rpm.
- Dimmer stat, single phase input 230V.
- Output: 0 to 270V, 10A.
- Ammeter: 0 to 10A.a.c. one
- 0 to 0.5/1A.a.c. one
- Voltmeter: 0 to 30V a.c. one.

_{d}″ and X

_{q}″

To understand the behavior of an alternator under transient conditions, the armature and field resistance is assumed to be negligibly small.
Thus, constant flux linkage theorem can be applied. As per this theorem, in purely inductive circuit, the total flux linkage cannot be changed
instantneously at the time of any disturbance. Now, if all the three phases of unloaded alternator with normal excitation are suddenly short circuited
there will be short- circuit current flows in the armature. As the resistance is assumed to be zero, this current will lag behind the voltage by
90^{o} and the m.m.f. produced by this current will be along the d-axis. First conclusion is that this current will be affected by d-axis
parameters X_{d} , X_{d}′ and X_{d}″ only.

Further, there will be demagnetizing effect of this current, but as the flux linkage with field cannot change the effect of demagnetizing armature
m.m.f. must be counterbalanced by a proportional increase in the field current. This additional induced component of field current gives rise to
greater excitation under transient state and results in more short circuits as compared to the steady state short circuit current.

If field poles are provided with damper bars, then at the instant of three phase short circuit, the demagnetizing armature m.m.f. induces currents
in damper bars, which, in turn, produces field in the same direction as the main field and hence at this instant, the excitation further increases
and gives rise to further increase in short circuit armature current. This is for a very short duration, normally 3 to 4 cycles and this period is known as
sub-transient period. Since the field voltage is constant, there is no additional voltage to sustain these increased excitations during sub transient
or transient period. Consequently the effect of increased field current decreases with a time constant determined by the field and armature parameters and
accordingly the short circuit armature current also decays with the same time constant.

In the above figure a symmetrical wave from for armature short circuit current of phase - A. The d.c. component is zero in this phase.

The reactances offered by the machine during sub transient period are known as sub transient reactances. Along the direct axis, it is direct axis sub transient reactance, X″_{d} and along the quadrature axis, it is quadrature axis sub-transient reactance, X″_{q}. As these reactances are due to the fact that flux linkages in field circuit during sudden disturbance remain constant, the sub transient reactances X_{d}″ and X_{q}″ can also be defined as below:

_{c},

_{d}″)

The armature flux linkage per ampere under these conditions is known as direct axis sub transient inductance L_{d}″.

_{q})

_{q}″

This also is defined in a manner similar to X_{d}″, but in this case, armature currents are applied in such time phase that the peak of varying armature m.m.f. wave is along the quadrature axis. The damper bars in the quadrature axis force the field of the varying armature m.m.f. to follow the leakage path as shown Fig. 8.4.

As before, the flux linkage with q-axis damper bars must remain constant i.e. zero before and after the sudden application of armature m.m.f. Under these
conditions, the armature flux linkages per ampere is known as q-axis sub transient inductance Lq″ and X_{q}″=ωL_{q}″.

To determine X_{d}″ and Xq″ in laboratory, the above mentioned conditions are created there. Two phases of the three phase alternator are connected in series and the combination is connected to a low voltage single phase supply. Field winding is short circuited. The rotor is rotated and brought along the d-axis once. X_{d}″ can be calculated from the armature current and voltage per phase of armature in this position. Next, rotor is brought along the q-axis position and X_{q}″ is determined.

- Connect as shown in Fig. 8.1.
- Set the variac output to zero and switch on the supply.
- Gradually increase the variac output and set armature – current to a suitable value.
- Slowly rotate the armature and see the field current and armature current readings. Note the values of applied voltage and armature current when field current is maximum and also when it is zero.
- Repeat step (4) for other applied voltages. Take care that armature current does not exceed its rated value while performing this experiment.