25-Nav-B6 Ocean Engineering and Offshore Structures · May 2013
Question 4 of 8: Industrial Load and Power-Factor Correction
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 4: Industrial Load and Power-Factor Correction (20 marks)
All voltages and currents are rms; the load voltage is held at 250 V in both cases.
Find. [a] $I$, $P$, $Q$, pf; [b] $V_G$ and $P_T$; [c] $I_C$, the new
line current, the new pf, and the phasor diagram; [d] the new $V_G$ and $P_T$; [e] two
advantages of parallel capacitive correction.
Figure 4 — generator, series line impedance $Z_T$, the series $R$–$X_L$ industrial load, and the correction capacitor switched in parallel across the load.
Approach. Solve the load branch by Ohm’s law in phasor form,
take real and reactive power from $S = VI^{*}$, add the capacitor current at the load
terminals (the load voltage is unchanged because the capacitor is in parallel with it),
and re-run the line drop with the reduced current.
[a] Load impedance and current. The load branch is
$$Z_L = R + jX_L = 6 + j8 = 10\angle 53.13^\circ\ \Omega,$$
so
$$I = \frac{V}{Z_L} = \frac{250\angle 0^\circ}{10\angle 53.13^\circ}
= \boxed{\;25\angle -53.13^\circ\ \text{A} = (15 - j20)\ \text{A}\;}$$
The current lags the voltage, as expected for an inductive load.
Powers and power factor. Using $P = I^{2}R$ and $Q = I^{2}X_L$ with
$I = 25$ A:
$$P = 25^{2}(6) = 3750\ \text{W}, \qquad Q = 25^{2}(8) = 5000\ \text{var},$$
$$S = VI = 250 \times 25 = 6250\ \text{VA}, \qquad
\text{pf} = \cos 53.13^\circ = \frac{P}{S} = \frac{3750}{6250} = 0.60\ \text{lagging}.$$
The complex-power route gives the same answer,
$S = VI^{*} = 250(15+j20) = 3750 + j5000$ VA, which is a useful cross-check.
[b] Generator voltage. The line carries the full load current, so
$$V_G = V + I Z_T = 250 + (15 - j20)(1 + j3) = 250 + (75 + j25),$$
$$\boxed{\;V_G = 325 + j25 = 325.96\angle 4.40^\circ\ \text{V}\;}$$
The generator must supply about 76 V more than the load receives — a regulation of
some 30 %.
Transmission loss. Only the resistive part of $Z_T$ dissipates:
$$P_T = I^{2}R_T = 25^{2}(1) = \boxed{\;625\ \text{W}\;}$$
That is 16.7 % of the 3750 W actually delivered to the load.
[c] Capacitor current. The capacitor sits directly across the
250 V load terminals, so
$$I_C = \frac{V}{-jX_C} = \frac{250\angle 0^\circ}{12.5\angle -90^\circ}
= 20\angle 90^\circ\ \text{A} = j20\ \text{A},$$
leading the voltage by 90°.
New line current and power factor. The load branch still draws
$(15 - j20)$ A because its terminal voltage is unchanged; the line now carries the sum:
$$I' = I + I_C = (15 - j20) + j20 = \boxed{\;15\angle 0^\circ\ \text{A}\;}$$
$$\text{pf}' = \cos 0^\circ = 1.00\ \text{(unity)}.$$
The capacitor supplies $V^{2}/X_C = 250^{2}/12.5 = 5000$ var, exactly the load’s
reactive demand, so the correction happens to be complete for this particular
$X_C$.
Phasor diagram for [c] — $I_C$ is added head-to-tail to the lagging load current $I$; its $+j20$ A cancels the load’s $-j20$ A, leaving $I'$ in phase with $V$. (Voltage and current use separate scales.)
[d] New generator voltage and loss. Repeating the line calculation
with the smaller, in-phase current:
$$V_G' = V + I' Z_T = 250 + 15(1 + j3) = 265 + j45
= \boxed{\;268.79\angle 9.64^\circ\ \text{V}\;}$$
$$P_T' = (15)^{2}(1) = \boxed{\;225\ \text{W}\;}$$
The required generator voltage falls from 326 V to 269 V, and the line loss falls from
625 W to 225 W — a reduction of 400 W, or 64 %, while the load still receives
the same 3750 W.
[e] Two advantages. First, reduced line current for the same
delivered real power: the current falls from 25 A to 15 A, so the $I^{2}R$ loss falls
by 64 % and the same conductors can carry more useful load — released capacity
in the cable, the transformer and the switchgear. Second, improved voltage
regulation: the drop across $Z_T$ falls from about 79 V to 47 V, so the generator
voltage needed drops from 326 V to 269 V and the load voltage is far less sensitive to
load changes. A third practical benefit worth stating is the avoidance of the utility
power-factor penalty charge that applies below a typical 0.90 threshold.