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16-Mechatronics-B10 · December 2019

Question 4 of 5: Combining a Lagging Load With a Leading Synchronous Motor, and the Effect of Frequency on Power Angle

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. 16-Mex-B10, Power Systems and Machine Drives, National Examinations December 2019 — a three-hour closed-book examination with one double-sided 8½″×11″ aid sheet permitted (no worked solutions or diagrams on it) and an approved Casio or Sharp calculator. The cover page states that FIVE (5) questions constitute a complete exam paper, all of equal value; all five printed questions are worked here. Unless stated otherwise, AC voltages/currents are rms and three-phase quantities are line-to-line voltages with total real power.

Reference texts. S.J. Chapman, Electric Machinery Fundamentals, 5th ed. (Ch. 1 magnetic circuits and reluctance; Ch. 2 transformer equivalent circuits and open/short-circuit testing; Ch. 4 induction motors and power-factor correction; Ch. 6 synchronous-motor power-angle characteristics).

Question 4: Combining a Lagging Load With a Leading Synchronous Motor, and the Effect of Frequency on Power Angle (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

QuantityValue
Existing factory load, S1100 kVA at 0.45 p.f. lagging, 60 Hz
Added synchronous motor input power, P210 kW at 0.2 p.f. leading
Rated power angle (at rated V, f, torque), δrated35°
Frequency change−5%
Load (torque) change−10%

Find. (a) total real power; (b) overall power factor; (c) the new power angle after the frequency and load change.

Check
Part (c) is read as: at rated voltage/frequency/torque the motor's power angle is 35°; find the new power angle when frequency drops 5% and torque (shaft load) drops 10%, holding terminal voltage V and field excitation Ef fixed (no proportional V/f adjustment is stated). This is the only reading consistent with the question's own phrase "for rated voltage, frequency and torque."

Approach. Resolve both loads to real/reactive power (a leading load subtracts vars), sum for (a)/(b); for (c), use the round-rotor power equation P = (VEf/Xs)sinδ with Xs ∝ f and torque T = P/ωs, ωs ∝ f, to get sinδ ∝ Tf².

  1. Existing plant load, resolved. $$P_1=S_1\cos\varphi_1=100(0.45)=45.0\ \text{kW}$$ $$Q_1=S_1\sin\varphi_1=100\sin(\cos^{-1}0.45)=\boxed{89.30\ \text{kVAR (lagging)}}$$
  2. Synchronous-motor contribution (leading ⇒ supplies vars). $$Q_2=-P_2\tan(\cos^{-1}0.2)=-10(4.899)=\boxed{-48.99\ \text{kVAR}}$$
  3. (a) Total real power. $$P_T=P_1+P_2=45.0+10=\boxed{55.0\ \text{kW}}$$
  4. (b) Overall power factor. $$Q_T=Q_1+Q_2=89.30-48.99=40.31\ \text{kVAR (net lagging)}$$ $$S_T=\sqrt{P_T^2+Q_T^2}=\sqrt{55.0^2+40.31^2}=68.19\ \text{kVA}$$ $$\text{pf}_T=\frac{P_T}{S_T}=\boxed{0.807\ \text{lagging}}$$
  5. (c) New power angle after −5% frequency, −10% torque. With Xs=2πfL, V and Ef fixed: $$\sin\delta \propto P\,X_s \propto (T f)f = T f^2$$ $$\frac{\sin\delta_{new}}{\sin\delta_{rated}}=\left(\frac{T_{new}}{T_{rated}}\right)\left(\frac{f_{new}}{f_{rated}}\right)^2=(0.9)(0.95)^2=0.8123$$ $$\sin\delta_{new}=\sin(35^{\circ})(0.8123)=0.5736(0.8123)=\boxed{0.4659}$$ $$\delta_{new}=\sin^{-1}(0.4659)=\boxed{27.8^{\circ}}$$
QuantityValue
(a) Total real power, PT55.0 kW
(b) Overall power factor0.807 lagging
(c) New power angle, δnew27.8° (was 35°)