25-Nav-B6 Ocean Engineering and Offshore Structures · Undated paper
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 2019 — 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: $\pi = 3.14159$,
$1\ \text{hp} = 746\ \text{W}$. All eight questions are solved here so the solutions cover whichever five a candidate chooses.
Subject note
This paper is listed under 25-Nav-B6 “Ocean Engineering and Offshore Structures”, but the printed paper is headed 98-Mar-B6 (front page: 98-Elec-B6) and every question is Electrical & Electronics Engineering content (BJT current-mirror analysis, combinational logic, a linear dc machine, a gapped/parallel-path transformer magnetic circuit, a three-op-amp instrumentation amplifier, an induction-motor dc test and slip calculation, an RC transient/frequency-response network, and industrial power-factor correction) — zero naval-architecture or ocean-engineering content. Solved as the exam actually printed.
Mano & Ciletti, Digital Design, 6th ed. — Boolean algebra and
De Morgan’s theorems (Ch. 2), NAND/NOR universal gates (Ch. 3).
Fitzgerald, Kingsley & Umans, Electric Machinery, 7th ed. —
elementary electromechanical energy conversion / the linear dc machine (Ch. 3).
Chapman, Electric Machinery Fundamentals, 5th ed. — transformers
(Ch. 2), induction motors and the dc test (Ch. 6).
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).
Question 6: DC Test and Slip Behaviour of an Induction Motor (equal value)
$V_{dc}=3.32$ 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 motor–pump operating point.
Figure 6 — dc resistance test between two delta line
terminals.
Part I
Approach. Reduce the delta network seen by the dc source to
get $r_1$, then apply the standard slip relations, which need only $f_e$, $P$
and $s$.
(a) Unfold the delta. Between two terminals of a delta
winding, one phase of resistance $r_1$ is in parallel with the other two in
series:
$$R_{dc}=\frac{V_{dc}}{I_{dc}}=\frac{3.32}{3.1}=1.071\ \Omega,\qquad
R_{dc}=\frac{r_1\cdot2r_1}{r_1+2r_1}=\frac{2}{3}r_1
\;\Longrightarrow\;r_1=\tfrac{3}{2}R_{dc}=\boxed{1.606\ \Omega\text{ per phase}}.$$
(e) Rotor speed at double load. Near synchronous speed the
torque–slip curve is essentially linear ($T\propto s$, since $sX_2\ll R_2$
there), so doubling the load torque doubles the slip:
$$s'=2\times0.035=0.07,\qquad n_m'=(1-0.07)(1200)=\boxed{1116\ \text{r/min}}$$
— only a 42 r/min (3.5%) drop for a doubling of load, the near-constant-speed
behaviour that makes the induction motor an industrial workhorse.
Part II — graphical operating point
This part asks for a method, since neither the motor curve nor $K$ is given
numerically ($K_p$ is symbolic). Steady operation occurs where the torque the motor develops equals
the torque the pump demands, at a common shaft speed.
Plot both characteristics. Torque on the vertical axis,
speed $n$ (rev/s) on the horizontal axis; draw the wound-rotor motor curve
$T_m(n)$ from the supplied graph, converting its speed axis to rev/s if it is given in r/min, which rises from locked-rotor torque to a breakdown peak and then
falls steeply toward zero at synchronous speed.
Superimpose the load law. Plot $T_L=K_pn^{2}$, a parabola
through the origin (a centrifugal-type load takes negligible torque at standstill,
rising with the square of speed).
Read the intersection.
$$T_m(n)=K_pn^{2}\;\Longrightarrow\;\boxed{n=n_{op}}$$
gives the operating speed (in r/min, $60\,n_{op}$); the shaft power follows as $P=2\pi n_{op}T_{op}$.
Check stability. The intersection must lie where
$dT_m/dn \lt dT_L/dn$ (the steep, high-speed side of the motor curve), so
that a small speed excursion is self-correcting.
Quantity
Result
(a) $r_1$
1.606 Ω per phase
(b) Synchronous speed
1200 r/min
(c) Rotor speed
1158 r/min
(d) Rotor frequency
2.1 Hz
(e) Rotor speed at 2× load
1116 r/min
Part II
operating point = intersection of $T_m(n)$ and $K_pn^2$, on the falling side of $T_m$