22-Elec-A6 Power Systems and Machines · December 2016
Question 3 of 6: Three-Phase Squirrel-Cage Induction Motor
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: Professional Engineers Ontario — 07-Elec-A6 Power Systems and Machines, December 2016. Closed-book; formula sheet supplied. Six questions of equal value; candidates answer any five. All six are solved here as a study resource. All ac voltages and currents are rms; three-phase voltages are line-to-line unless noted.
Reference texts: S. J. Chapman, Electric Machinery Fundamentals, 5th ed. (transformers, induction/synchronous machines, dc motors); J. D. Glover et al., Power System Analysis and Design, 6th ed. (three-phase power, two-wattmeter method, power-factor correction).
Question 3: Three-Phase Squirrel-Cage Induction Motor (20 marks)
Given. Y-connected, 6-pole, 60 Hz machine at slip $s=0.04$.
Given data (per phase, referred to stator)
R1
X1
R2
X2
Xm
Pcore
Prot
0.082 Ω
0.19 Ω
0.070 Ω
0.18 Ω
7.2 Ω
1400 W
1450 W
Find. Stator and rotor currents; input, air-gap (rotor input), developed and output power; efficiency; and output torque.
Per-phase equivalent circuit; the rotor resistance appears as $R_2/s$.
Approach. Reduce the per-phase circuit ($Z_2=R_2/s+jX_2$ in parallel with $jX_m$, in series with the stator impedance) to find the stator current; step through the power flow $P_{in}\to P_{ag}\to P_{conv}\to P_{out}$; and get torque from $P_{out}/\omega_m$. The magnetizing branch is lossless, so core loss is a rotational loss removed at the shaft.
Phase voltage and input impedance. $V_1=440/\sqrt3=254.0$ V. With $R_2/s=0.070/0.04=1.75\ \Omega$,
$$Z_2=1.75+j0.18,\quad Z_2\parallel jX_m = 1.577+j0.550,\quad Z_{in}=(0.082+j0.19)+(1.577+j0.550)=1.816\angle 24.0^\circ\ \Omega.$$
Stator current (part a).
$$\boxed{I_1=\frac{V_1}{Z_{in}}=\frac{254.0}{1.816\angle24.0^\circ}=139.9\angle{-24.0^\circ}\ \text{A}.}$$
Rotor current (part b). The air-gap voltage is $E=I_1(Z_2\parallel jX_m)=233.6\angle{-4.8^\circ}$ V, so
$$\boxed{I_2=\frac{E}{Z_2}=\frac{233.6\angle{-4.8^\circ}}{1.759\angle 5.9^\circ}=132.8\ \text{A}.}$$
Input power and stator copper loss (parts c, d).
$$P_{in}=3V_1 I_1\cos\theta_1=3(254.0)(139.9)\cos24.0^\circ = 97.35\ \text{kW},$$
$$P_{scl}=3 I_1^{2} R_1 = 3(139.9)^2(0.082)=4812\ \text{W}.$$
Air-gap (rotor input) power (part e). Since $X_m$ is lossless, all real power crossing the gap is dissipated in the rotor branch:
$$\boxed{P_{ag}=3 I_2^{2}\,\frac{R_2}{s}=3(132.8)^2(1.75)=92.54\ \text{kW}}\;=\;P_{in}-P_{scl}\ \checkmark.$$
Developed power (part f). The rotor copper loss is $P_{rcl}=sP_{ag}=3701$ W, so
$$\boxed{P_{conv}=(1-s)P_{ag}=0.96(92.54)=88.84\ \text{kW}.}$$
Output power (part g). Subtract rotational and core losses at the shaft:
$$\boxed{P_{out}=P_{conv}-P_{rot}-P_{core}=88.84-1.45-1.40 = 85.99\ \text{kW}=115.3\ \text{hp}.}$$
Efficiency and output torque (parts h, j). $\eta=P_{out}/P_{in}=85.99/97.35 = 88.3\%$. The synchronous speed is $n_s=120f/P=1200$ rpm, the mechanical speed $n_m=(1-s)n_s=1152$ rpm, $\omega_m=120.6$ rad/s, so
$$\boxed{T_{out}=\frac{P_{out}}{\omega_m}=\frac{85\,990}{120.6}=712.8\ \text{N}\cdot\text{m}.}$$