25-Nav-B6 Ocean Engineering and Offshore Structures · May 2013
Question 6 of 8: DC Test and Slip Behaviour of an Induction Motor
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. PEO National Examinations,
May 2013 — 98-Mar-B6, printed for Electrical & Electronics
Engineering / Mechanical Engineering candidates. Three hours, closed
book, two approved calculators (Casio or Sharp). Eight questions of equal
value; any five constitute a complete paper, and only the first five appearing in
the answer book are marked. Constants supplied on the front page: $\pi = 3.14159$,
$1\ \text{hp} = 746\ \text{W}$, $\mu_0 = 4\pi\times10^{-7}\ \text{H}\,\text{m}^{-1}$.
All eight questions are solved here so the solutions cover whichever five a candidate chooses.
Subject note
This paper, although listed under “Ocean Engineering and Offshore Structures”, is headed 98-Mar-B6 and every question is Electrical & Electronics Engineering content (BJT current mirror, combinational logic, dc machine design, ac power/power-factor correction, op-amp transfer functions, induction-motor dc test and speed-torque, RC-circuit transients, magnetic-circuit impedance) — zero naval-architecture or ocean-engineering content. Solved as the exam actually printed.
Mano & Ciletti, Digital Design, 6th ed. — Boolean algebra and
DeMorgan’s theorems (Ch. 2), NAND/NOR universal gates (Ch. 3).
Chapman, Electric Machinery Fundamentals, 5th ed. — dc machine emf and
torque (Ch. 7–8), induction motors and the dc test (Ch. 6), transformers (Ch. 2).
Sadiku & Alexander, Fundamentals of Electric Circuits, 7th ed. —
ac power and power-factor correction (Ch. 11), first-order transients (Ch. 7),
frequency response (Ch. 14).
Hayt, Kemmerly & Durbin, Engineering Circuit Analysis, 9th ed. —
phasor methods and transfer functions.
Question 6: DC Test and Slip Behaviour of an Induction Motor (20 marks)
$V_{DC} = 3.32$ V, $I_{DC} = 3.1$ A, applied between two line terminals
Operating slip $s$
3.5 % = 0.035
Find. [a] per-phase stator resistance $r_1$; [b] synchronous speed;
[c] rotor speed; [d] rotor electrical frequency; [e] rotor speed at double load; and, in
Part II, the graphical method for the motor–pump operating point.
Part I
Approach. Reduce the delta network seen by the dc source to get
$r_1$, then apply the standard slip relations, which need nothing but $f_e$, $P$ and
$s$.
[a] Resistance seen by the dc source. From Figure 6 the dc supply is
applied between two of the three line terminals:
$$R_{DC} = \frac{V_{DC}}{I_{DC}} = \frac{3.32}{3.1} = 1.0710\ \Omega .$$
Because the test uses dc there is no induced voltage, no rotor current and no reactance
— the reading is pure stator resistance.
Unfold the delta. Between two terminals of a delta winding, one phase
of resistance $r_1$ appears in parallel with the other two in series:
$$R_{DC} = \frac{r_1 \cdot 2r_1}{r_1 + 2r_1} = \frac{2}{3}\,r_1
\quad\Longrightarrow\quad r_1 = \tfrac{3}{2} R_{DC},$$
$$r_1 = 1.5 \times 1.0710 = \boxed{\;r_1 = 1.606\ \Omega\ \text{per phase}\;}$$
(Had the machine been wye connected the two phases would be in series and
$r_1 = R_{DC}/2 = 0.536\ \Omega$ — a factor-of-three difference, which is why the
connection must be read from the nameplate.)
[b] Synchronous speed. The stator field rotates at
$$n_{\text{sync}} = \frac{120 f_e}{P} = \frac{120 \times 60}{6}
= \boxed{\;1200\ \text{r/min}\;}$$
[c] Rotor speed at 3.5 % slip. By definition
$s = (n_{\text{sync}} - n_m)/n_{\text{sync}}$, so
$$n_m = (1-s)\,n_{\text{sync}} = (1 - 0.035)(1200)
= \boxed{\;1158\ \text{r/min}\;}$$
[d] Rotor electrical frequency. The rotor conductors are cut by the
field at the slip speed, so
$$f_r = s\,f_e = 0.035 \times 60 = \boxed{\;2.1\ \text{Hz}\;}$$
Checking through the slip speed: $P(n_{\text{sync}} - n_m)/120 = 6(42)/120 = 2.1$ Hz.
[e] Rotor speed at double load. In the normal low-slip operating
region the torque–slip curve is essentially linear, $T \propto s$, because
$s X_2 \ll R_2$ and the rotor branch is resistance dominated. Doubling the load torque
therefore doubles the slip:
$$s' = 2 \times 0.035 = 0.07, \qquad
n_m' = (1 - 0.07)(1200) = \boxed{\;1116\ \text{r/min}\;}$$
The speed falls by only 42 r/min — 3.5 % — for a doubling of load, which
is the near-constant-speed behaviour that makes the induction motor an industrial
workhorse.
Check: linearity assumption in [e]
Part [e] assumes operation on the linear portion of the torque–slip characteristic,
which holds comfortably at slips of a few percent for a standard design. If the doubled
load pushed the machine towards breakdown torque the relation would no longer be linear
and the slip would rise more than proportionally; the assumption should be stated in the
answer book, as the front-page notes invite.
Part II — graphical determination of the operating point
This part asks for a method, not a number, since neither the motor curve nor $K_P$ is
given numerically. The system is in steady state when the torque the motor develops
equals the torque the pump demands, at a common shaft speed.
Plot both characteristics on one set of axes. Take torque on the
vertical axis and speed $n$ (rev/s, to match the pump law) on the horizontal axis, and
draw the supplied wound-rotor motor characteristic $T_m(n)$: it starts at the locked-rotor
torque at $n = 0$, rises to breakdown torque, then falls steeply to zero at synchronous
speed $n_s$.
Superimpose the load law. On the same axes plot the pump demand
$T_L = K_P n^{2}$ — a parabola through the origin, since a centrifugal pump takes
essentially no torque at standstill and its torque rises with the square of speed.
Read the intersection. Steady operation requires zero net accelerating
torque:
$$T_m(n) = K_P n^{2} \quad\Longrightarrow\quad \boxed{\;n = n_{\text{op}}\;}$$
The abscissa of the intersection is the operating speed; its ordinate is the operating
torque, and the shaft power follows as $P = 2\pi n_{\text{op}} T_{\text{op}}$.
Check that the intersection is stable. The intersection must lie on
the steep, high-speed side of the motor curve, where
$\mathrm{d}T_m/\mathrm{d}n < \mathrm{d}T_L/\mathrm{d}n$. Then a small speed rise makes
the load torque exceed the motor torque and the machine decelerates back to
$n_{\text{op}}$; a small speed drop does the reverse. An intersection on the rising side
of the motor curve, below breakdown, would be unstable and the drive would either stall or
run away to the stable point.
Confirm starting is possible. Finally verify that the motor curve
lies above the parabola over the whole range from standstill to $n_{\text{op}}$;
otherwise the set cannot accelerate from rest. With a wound-rotor machine this is
straightforward — external rotor resistance shifts the peak torque toward standstill
for starting and is then shorted out for running, which also lets the operating speed be
adjusted deliberately by re-inserting resistance.
Part II — the operating point is the intersection of the motor torque–speed characteristic with the pump parabola $T = K_P n^{2}$; a stable point lies on the steep side of the motor curve.
Quantity
Result
Terminal-to-terminal dc resistance
$R_{DC} = 1.071\ \Omega$
[a] Per-phase stator resistance (delta)
$r_1 = 1.606\ \Omega$
[b] Synchronous (field) speed
1200 r/min
[c] Rotor speed at $s = 3.5\%$
1158 r/min
[d] Rotor electrical frequency
2.1 Hz
[e] Rotor speed at double load ($s = 7\%$)
1116 r/min
Part II operating point
intersection of $T_m(n)$ with $K_P n^{2}$, on the steep side