Question 6 of 6: Three-Phase Induction Motor Performance
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: Closed-book written exam, 3 hours. Six questions of equal value (20 marks each); five constitute a complete paper. All six are solved here as a study resource. AC quantities are rms; three-phase voltages are line-to-line and power is total power unless noted.
Reference texts: S. J. Chapman, Electric Machinery Fundamentals, 5th ed. (McGraw-Hill); B. S. Guru & H. R. Hiziroglu, Electric Machinery and Transformers, 3rd ed. (Oxford); P. C. Sen, Principles of Electric Machines and Power Electronics; T. Wildi, Electrical Machines, Drives, and Power Systems.
Question 6: Three-Phase Induction Motor Performance (20 marks)
Given. Y-connected, $V_L=440$ V so $V_1=254$ V/phase; stator $R_1=0.1$, $X_1=0.35\ \Omega$; rotor $R_2'=0.12$, $X_2'=0.4\ \Omega$; $P_{rot}=2150$ W; no-load 18 A at 0.089 pf; running speed 1755 rpm.
Given data
V1
R1, X1
R2′, X2′
Prot
No-load
n
254 V
0.1, 0.35 Ω
0.12, 0.4 Ω
2150 W
18 A, 0.089 pf
1755 rpm
Find. (a) line current, (b) developed torque, (c) output power, (d) efficiency at 1755 rpm.
Per-phase approximate equivalent circuit; the magnetizing branch is taken as a lossless $jX_m$ (core loss lumped into the rotational losses).
Check: No core-loss resistor is given, so the magnetizing branch is modelled as a lossless $jX_m$ obtained from the no-load reactive current; core loss is carried within the stated rotational loss and removed at the shaft. For a 60 Hz motor near 1755 rpm the synchronous speed is 1800 rpm (4 poles).
Approach. Find slip and the magnetizing reactance, compute the rotor-branch current and the air-gap power, then developed and output power and efficiency.
Slip and magnetizing reactance.$n_s=1800$ rpm, $s=(1800-1755)/1800=0.025$. From the no-load test the magnetizing current is $I_m=18\sin(\cos^{-1}0.089)=17.9$ A, so
$$X_m=\frac{V_1}{I_m}=\frac{254}{17.9}=14.2\ \Omega.$$
(a) Line current. Adding the magnetizing current $I_m=17.9\angle{-90^\circ}$ A,
$$I_1=I_2'+I_m = 56.8\angle{-26.9^\circ}\ \text{A}\ \Rightarrow\ \boxed{I_L=56.8\ \text{A}.}$$
(b) Developed torque. Air-gap power $P_{ag}=3I_2'^2\dfrac{R_2'}{s}=3(51.2)^2(4.8)=37.8$ kW, and with $\omega_s=188.5$ rad/s,
$$T_{dev}=\frac{P_{ag}}{\omega_s}=\frac{37\,818}{188.5}=\boxed{200.6\ \text{N}\!\cdot\!\text{m}.}$$
(c) Output power.$P_{dev}=(1-s)P_{ag}=0.975(37\,818)=36.9$ kW, so
$$P_{out}=P_{dev}-P_{rot}=36\,872-2150=\boxed{34.7\ \text{kW}\ (46.5\ \text{hp}).}$$