22-Elec-B8 Power Electronics and Drives · May 2017
Question 1 of 6: Snubbers, and an a.c. voltage controller driving an inductive motor
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2017 — 16-Elec-B8, Power
Electronics and Drives. Open-book, three hours, six problems of equal value (20 points
each); the rubric states that any five questions constitute a complete paper.
All six problems are worked here, and every sub-part is answered, because this set is a
study resource rather than an exam script.
Reference texts.
M. H. Rashid, Power Electronics: Circuits, Devices and Applications, 4th ed.
— the primary EGBC reference for this exam code.
N. Mohan, T. M. Undeland and W. P. Robbins, Power Electronics: Converters,
Applications and Design, 3rd ed.
B. K. Bose, Modern Power Electronics and AC Drives.
R. Krishnan, Electric Motor Drives: Modeling, Analysis and Control.
C. W. Lander, Power Electronics, 3rd ed.
Question 1: Snubbers, and an a.c. voltage controller driving an inductive motor (20 points)
A snubber is a small auxiliary network fitted around a power semiconductor whose only
purpose is to shape the voltage-and-current trajectory the device follows while it is
switching. It carries no useful load power; it exists so that the switching locus stays
inside the device's safe operating area. Two forms dominate. The turn-off or
dv/dt snubber is a capacitor, usually with a series resistor and a bypass diode
across that resistor, connected directly across the device. As the device turns off, the
capacitor accepts the load current while the device voltage is still low, so voltage and
current never reach their peaks simultaneously and the turn-off energy is transferred out
of the silicon. The turn-on or di/dt snubber is a small series inductor,
often an air-cored or saturable reactor, in the anode lead. It limits the rate of rise of
anode current while the gate-triggered conducting plasma is still spreading laterally
across the junction, so the initially small conduction area is not asked to carry full
current and does not fail by local hot-spotting.
Snubbers are used for four reasons. First, they enforce the manufacturer's
$\mathrm{d}v/\mathrm{d}t$ and $\mathrm{d}i/\mathrm{d}t$ ratings, and for a thyristor
this is not merely a stress question: a reapplied forward $\mathrm{d}v/\mathrm{d}t$
above the rating injects displacement current into the gate-cathode junction and turns the
SCR on spuriously, without any gate signal. Second, they damp the ringing that circuit
stray inductance forms with device capacitance during reverse recovery, which otherwise
produces overvoltage and radiated interference. Third, by moving the switching locus away
from the high-voltage-and-high-current corner they reduce the instantaneous power
dissipated in the die, allowing higher switching frequency for a given junction
temperature. Fourth, in series-connected strings the same RC network equalises the
transient voltage sharing between devices with unequal recovery charge. The cost is real:
the energy $\tfrac{1}{2}CV^{2}$ stored in the snubber capacitor is dissipated in the
snubber resistor once every switching cycle, so an oversized snubber trades device stress
for converter efficiency.
Parts (b) and (c) — The a.c. voltage controller
Given.
Quantity
Symbol
Value
Supply voltage (rms, single-phase)
$V_s$
2300 V
Peak supply voltage
$V_m = \sqrt{2}\,V_s$
3252.69 V
Supply frequency
$f$
60 Hz
Conduction angle
$\gamma$
162.5°
Load power factor (lagging)
$\cos\phi$
0.875
Mean current per thyristor
$I_{T,\mathrm{avg}}$
625 A
Find. The delay angle $\alpha$ that produces the stated conduction angle, and then the equivalent series resistance and inductive reactance of the motor.
Figure 1.1 — The controller fires each thyristor at $\alpha$; because the load is inductive the current runs on past the supply zero and extinguishes at $\beta = \alpha + \gamma$. The stated conduction angle of 162.5° is therefore an indirect statement of the delay angle.
Approach. Fix the load angle from the power factor, read the extinction condition backwards to obtain $\alpha$ from the stated $\gamma$, then use the fact that the current pulse shape depends only on $\alpha$ and $\phi$ to convert the one measured mean device current into the load impedance.
Part (b) — Fix the load angle from the stated power factor. The motor is represented by a series $R + jX$, so the current lags the voltage by $\phi = \arccos(0.875) = 28.955^\circ$, and $\tan\phi = X/R = 0.55328$. This angle is a property of the load alone and is settled before any converter algebra begins.
Write the conduction-interval current and impose extinction. Over $\alpha \le \omega t \le \beta$ the thyristor connects the supply straight to the load, so $$i(\omega t) = \frac{V_m}{Z}\left[\sin(\omega t - \phi) - \sin(\alpha - \phi)\,e^{(\alpha - \omega t)/\tan\phi}\right],$$ the second term being the natural response that forces $i(\alpha) = 0$. The device turns off when the current returns to zero, and with $\beta = \alpha + \gamma$ that condition reads $$\sin(\alpha + \gamma - \phi) = \sin(\alpha - \phi)\,e^{-\gamma/\tan\phi}.$$
Evaluate the damping factor and solve for the delay angle. With $\gamma = 162.5^\circ = 2.83616$ rad, $e^{-\gamma/\tan\phi} = e^{-5.1261} = 5.932\times10^{-3}$. The equation is transcendental in $\alpha$; solving it numerically over the physical range $\phi < \alpha < 180^\circ$ gives $$\boxed{\alpha = 46.353^\circ}\qquad \beta = \alpha + \gamma = 208.853^\circ .$$
Confirm with the closed-form estimate. Because the exponential is only $5.9\times10^{-3}$, the right-hand side is nearly zero and the condition collapses to $\alpha + \gamma - \phi \approx 180^\circ$, i.e. $\alpha \approx 180^\circ + \phi - \gamma = 46.455^\circ$. That is 0.10° above the exact root, so the closed form is a sound sanity check here — but only because $\gamma$ is large and the power factor good; at a poorer power factor the same estimate can be several degrees out.
Part (c) — Normalise the current pulse. The shape of the conduction pulse depends only on $\alpha$ and $\phi$, not on the size of the load, so define the dimensionless waveform $$u(\omega t) = \frac{Z\,i(\omega t)}{V_m} = \sin(\omega t - \phi) - \sin(\alpha - \phi)\,e^{(\alpha-\omega t)/\tan\phi}.$$ Numerical integration over the conduction window gives $\int_{\alpha}^{\beta} u \,\mathrm{d}(\omega t) = 1.78979$.
Convert the measured mean device current into the load impedance. Each thyristor of the back-to-back pair conducts once per supply cycle, so its mean current is averaged over $2\pi$, not over $\pi$: $$I_{T,\mathrm{avg}} = \frac{V_m}{Z}\cdot\frac{1}{2\pi}\int_{\alpha}^{\beta} u\,\mathrm{d}(\omega t).$$ Rearranging, $$Z = \frac{V_m}{I_{T,\mathrm{avg}}}\cdot\frac{1.78979}{2\pi} = \frac{3252.69}{625}\times 0.284847 = \boxed{1.4825\ \Omega}.$$ No power rating, efficiency or line current was needed — one average device current is sufficient because $Z$ is the only free scale factor in the waveform.
Split the impedance into its resistive and reactive parts. The load angle already fixes the split, so $$R = Z\cos\phi = 1.4825 \times 0.875 = \boxed{1.2972\ \Omega},\qquad X = Z\sin\phi = 1.4825 \times 0.48412 = \boxed{0.7177\ \Omega},$$ which at 60 Hz corresponds to a motor inductance $L = X/(2\pi f) = 1.904$ mH.
Cross-check the answer three ways. The rms output voltage over the real conduction window is $$V_{o} = V_s\sqrt{\frac{\gamma - \tfrac{1}{2}\left(\sin 2\beta - \sin 2\alpha\right)}{\pi}} = 2214.7\ \text{V},$$ and the rms load current follows from the same normalised waveform as $I_{rms} = 1452.1$ A. First check: the half-sine device shortcut $\sqrt{2}\,I_{rms}/\pi = 653.7$ A sits 4.6% above the stated 625 A — high and therefore conservative, which is exactly what that approximation should do. Second check: $V_o/I_{rms} = 1.5252\ \Omega$ is 2.9% above $|Z| = 1.4825\ \Omega$, and that gap is physical, not an error: the chopped wave carries harmonics which see $nX$, so the load draws proportionally less harmonic current than harmonic voltage and the ratio of total rms quantities is not the fundamental impedance. Third check: $I_{rms}^{2}R = 2.735$ MW, consistent with a large lagging load drawing 625 A mean per device.
Final results.
Quantity
Symbol
Result
Load (motor) phase angle
$\phi$
28.955°
Delay (firing) angle
$\alpha$
46.353°
Extinction angle
$\beta = \alpha + \gamma$
208.853°
Load impedance magnitude
$Z$
1.4825 Ω
Motor equivalent resistance
$R$
1.2972 Ω
Motor inductive reactance
$X$
0.7177 Ω
Equivalent motor inductance
$L = X/2\pi f$
1.904 mH
rms output voltage
$V_o$
2214.7 V
rms load current
$I_{rms}$
1452.1 A
Check: the printed data describe a genuinely large single-phase load — 1452 A rms drawing 2.74 MW from a 2300 V single-phase source. That is unusual in service (such a machine would normally be three-phase) but it is internally consistent with the 625 A mean thyristor current the question supplies, and no other reading of the data reproduces it. The answers are quoted as the numbers give them.