22-Elec-B8 Power Electronics and Drives · December 2019
Question 4 of 5: Single-phase a.c. voltage controller feeding a motor
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2019 —
16-Elec-B8 Power Electronics and Drives. Three hours; closed book with one
double-sided aid sheet; an approved Casio or Sharp calculator. Five questions
constitute a complete paper and all questions are of equal value, so each carries
20 marks. All a.c. voltages and currents are rms unless noted otherwise; for
three-phase circuits voltages are line-to-line and power is total real power
unless noted otherwise. Every question is solved below, in the exam's own order.
Reference texts.
M. H. Rashid, Power Electronics: Circuits, Devices and Applications,
4th ed. — the primary reference for this exam code (thyristor statics ch. 7,
a.c. voltage controllers ch. 11, d.c. choppers ch. 5).
N. Mohan, T. M. Undeland and W. P. Robbins, Power Electronics: Converters,
Applications and Design, 3rd ed. — switching-converter analysis and
d.c.–d.c. converter waveforms.
C. W. Lander, Power Electronics, 3rd ed. — a compact treatment of
phase control and of the chopper current equations used in Question 5.
B. K. Bose, Modern Power Electronics and AC Drives, and R. Krishnan,
Electric Motor Drives: Modeling, Analysis and Control — for the drive
context behind Questions 3 and 4.
J. J. Grainger and W. D. Stevenson, Power System Analysis — for the
radial-feeder and three-phase load calculations of Questions 1 and 2.
Question 4: Single-phase a.c. voltage controller feeding a motor (20 marks)
Find. (a) confirmation that the firing delay is $\alpha = 40^\circ$; (b) the rms output voltage; (c) the mean current in each thyristor and in the controller as a whole.
Figure 4.1 — The full-wave controller: two thyristors in inverse parallel between the 220 V supply and the motor. T₁ carries the positive half cycle and T₂ the negative one.
Check: two phrases in the printed question are read as follows.
“a 20hp motor whose power factor is 20 degrees” states the load
impedance angle, $\phi = 20^\circ$, so the power factor is
$\cos 20^\circ = 0.940$ lagging — a power factor cannot itself be an angle.
“The corresponding angle 160 degrees” is the conduction angle
$\gamma = 160^\circ$; this is the only reading under which part (a) has anything
to verify, and it reproduces the stated $40^\circ$ to two decimal places, which
confirms it.
Approach. An inductive load holds current past the supply zero, so $\alpha$ and $\gamma$ are tied by the transcendental extinction condition; solve that for $\alpha$, integrate the chopped sine over the real conduction window for the rms output, then get the load current from the motor's power balance and the device current from the shape of the conduction pulse.
Part (a) — write the extinction condition. During
conduction the load current obeys
$$i(\theta) = \frac{V_m}{|Z|}\left[\sin(\theta - \phi)
- \sin(\alpha - \phi)\,e^{(\alpha-\theta)/\tan\phi}\right]$$
Current extinguishes at $\theta = \beta = \alpha + \gamma$, so setting the bracket
to zero gives the condition that links the two angles:
$$\sin(\alpha + \gamma - \phi) = \sin(\alpha - \phi)\,e^{-\gamma/\tan\phi}$$
The load impedance $|Z|$ has cancelled: the conduction window depends on the load
angle alone.
Evaluate the damping factor and solve. With
$\gamma = 160^\circ = 2.7925\ \text{rad}$ and $\tan 20^\circ = 0.36397$,
$$e^{-\gamma/\tan\phi} = e^{-7.672} = 4.655 \times 10^{-4}$$
which is small enough that the right-hand side nearly vanishes and the condition
becomes $\sin(\alpha + 140^\circ) \approx 0$, i.e. $\alpha + \gamma - \phi
\approx 180^\circ$. Solving the full equation numerically over
$21^\circ < \alpha < 89^\circ$ gives
$$\boxed{\,\alpha = 39.99^\circ \approx 40^\circ \quad
(\beta = \alpha + \gamma = 199.99^\circ)\,}$$
The stated delay angle is therefore verified.
Confirm with the closed form, and say when it may be trusted.
Because the exponential term is negligible, the condition collapses to
$$\alpha \approx 180^\circ + \phi - \gamma = 180^\circ + 20^\circ - 160^\circ
= 40^\circ$$
which agrees with the numerical root to $0.01^\circ$. That agreement is a
consequence of the damping factor being $4.7 \times 10^{-4}$: the approximation
degrades rapidly at poorer power factor or smaller conduction angle (at
$\cos\phi = 0.5$ and $\gamma = 135^\circ$ the same estimate is in error by almost nine degrees). Here it is exact enough to be the intended route, and the numerical
solution merely confirms it.
Part (b) — integrate the chopped sine over the real window.
The load voltage is the supply between $\alpha$ and $\beta$ and zero elsewhere, so
over a half period
$$V_o = V_s\sqrt{\frac{1}{\pi}\left[(\beta - \alpha)
- \frac{\sin 2\beta - \sin 2\alpha}{2}\right]}$$
Substituting $\beta - \alpha = \gamma = 2.7925\ \text{rad}$,
$\sin 2\beta = \sin 399.98^\circ = 0.6428$ and
$\sin 2\alpha = \sin 79.98^\circ = 0.9848$,
$$V_o = 220\sqrt{\frac{2.7925 + 0.1710}{\pi}} = 220\sqrt{0.9433}
= 220 \times 0.9713$$
$$\boxed{\,V_o = 213.7\ \text{V (rms)}\,}$$
The controller is delivering 97.1 per cent of the supply voltage, which is
what a $160^\circ$ conduction angle out of a possible $180^\circ$ should give.
Part (c) — get the load current from the motor's power
balance. The motor delivers 20 hp at 87 per cent efficiency and
$\cos\phi = 0.940$, so
$$P_{\text{in}} = \frac{20 \times 745.7}{0.87} = \frac{14\,914}{0.87}
= 17\,142.5\ \text{W}, \qquad
S = \frac{P_{\text{in}}}{\cos\phi} = \frac{17\,142.5}{0.9397} = 18\,242.7\ \text{VA}$$
$$I_{\text{rms}} = \frac{S}{V_o} = \frac{18\,242.7}{213.7} = 85.37\ \text{A}$$
Take the mean-to-rms ratio from the shape of the conduction
pulse. The load impedance is never given and is not needed: define the
normalised pulse $u(\theta) = \sin(\theta-\phi) -
\sin(\alpha-\phi)e^{(\alpha-\theta)/\tan\phi}$ on $[\alpha, \beta]$. Each
thyristor conducts once per cycle, so its mean is taken over $2\pi$ while the load
rms is taken over $\pi$, and the unknown $V_m/|Z|$ cancels in the ratio:
$$\frac{I_{T,\text{avg}}}{I_{\text{rms}}}
= \frac{\dfrac{1}{2\pi}\displaystyle\int_\alpha^\beta u\,d\theta}
{\sqrt{\dfrac{1}{\pi}\displaystyle\int_\alpha^\beta u^2\,d\theta}}
= \frac{1.8154/2\pi}{\sqrt{1.4279/\pi}} = 0.42856$$
$$\boxed{\,I_{T,\text{avg}} = 0.42856 \times 85.37 = 36.59\ \text{A per thyristor}\,}$$
Scale to the controller as a whole. The two devices are in
inverse parallel and each carries one half cycle, so the mean of the rectified
(magnitude) current through the controller is twice the per-device figure:
$$\boxed{\,\overline{|i_o|} = 2 \times 36.59 = 73.18\ \text{A}\,}$$
It is worth stating explicitly that the signed average of the controller's
output current is zero, as it must be for an a.c. waveform; 73.18 A is the
quantity a moving-coil meter behind a bridge, or a thermal rating calculation for
the pair, would use.
Sanity-check the device rating. Approximating the pulse as a
half sine gives $\sqrt{2}I_{\text{rms}}/\pi = \sqrt{2}(85.37)/\pi = 38.43\ \text{A}$,
which is 5 per cent above the exact 36.59 A. The shortcut errs on the
conservative side, so it is a legitimate first pass for selecting a device but not
for reporting an answer.
Figure 4.2 — One cycle of the controller. Each device is fired at α = 40° and conducts for γ = 160°, so the current runs 20° past the supply zero at 180° and the two conduction windows are separated by a 20° dead band.
Final results.
Part
Quantity
Result
(a)
Delay (firing) angle
$39.99^\circ \approx 40^\circ$ — verified
(a)
Extinction angle
$199.99^\circ$
(b)
rms output voltage
$213.7\ \text{V}$ (0.9713 of supply)
(c)
Motor input power / apparent power
$17\,142.5\ \text{W}$ / $18\,242.7\ \text{VA}$
(c)
Load rms current
$85.37\ \text{A}$
(c)
Average current per thyristor
$\mathbf{36.59\ \text{A}}$
(c)
Average current through the controller
$\mathbf{73.18\ \text{A}}$ (mean of $|i_o|$; signed mean is zero)