22-Elec-B8 Power Electronics and Drives · December 2019
Question 5 of 5: Basic chopper — completing the design table
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.
Throughout, $V_i = 24\ \text{V}$ and the peak load current is held at its allowed
maximum, $I_{\max} = 20\ \text{A}$. The load has no back e.m.f.
Find. The one missing entry in each row, with each row screened for feasibility before it is solved.
Approach. Every row is the same steady-state relation between $I_{\max}$, $V_i/R$, $T$, $T_{on}$ and $\tau$, inverted for a different unknown; derive it once, then apply it three times.
Derive the master relation once. During the on-interval the
supply drives the R–L load, so the current climbs from $I_{\min}$ towards
$V_i/R$; during the off-interval the free-wheel diode carries it and it decays
towards zero:
$$I_{\max} = \frac{V_i}{R}\left(1 - e^{-T_{on}/\tau}\right) + I_{\min}e^{-T_{on}/\tau},
\qquad I_{\min} = I_{\max}e^{-T_{off}/\tau}$$
Substituting the second into the first and using $T_{on} + T_{off} = T$ eliminates
$I_{\min}$ and gives the relation that governs all three rows:
$$\boxed{\;I_{\max} = \frac{V_i}{R}\cdot
\frac{1 - e^{-T_{on}/\tau}}{1 - e^{-T/\tau}}\;}$$
Two facts follow immediately and are used as screens below. Because
$T_{on} < T$, the fraction is always less than one, so
$I_{\max}$ can never exceed $V_i/R$; and any row solved for the
period must return a $T$ greater than its own $T_{on}$.
Case 1 — solve for the load resistance. Rearranging the
master relation for $R$ with $T = 2.4$, $T_{on} = 1.8$ and $\tau = 1.5\ \text{ms}$:
$$R = \frac{V_i}{I_{\max}}\cdot\frac{1 - e^{-T_{on}/\tau}}{1 - e^{-T/\tau}}
= \frac{24}{20}\cdot\frac{1 - e^{-1.2}}{1 - e^{-1.6}}
= 1.2 \times \frac{0.6988}{0.7981}$$
$$\boxed{\,R_1 = 1.051\ \Omega\,}$$
Back-substitution returns exactly 20.00 A, and the ceiling
$V_i/R = 22.84\ \text{A}$ sits comfortably above the 20 A limit, so the row is
consistent. The corresponding inductance is $L = R\tau = 1.58\ \text{mH}$.
Describe the resulting waveform. The duty ratio is
$\delta = 1.8/2.4 = 0.75$, the minimum current is
$I_{\min} = I_{\max}e^{-T_{off}/\tau} = 20e^{-0.4} = 13.41\ \text{A}$, and the mean
current is $\delta V_i/R = 0.75(22.84) = 17.13\ \text{A}$ — which lies between
$I_{\min}$ and $I_{\max}$ as it must. The ripple is 6.59 A, a third of the mean,
because $\tau$ and $T$ are of the same order and the exponentials are visibly
curved rather than straight.
Figure 5.1 — Two periods of the case-1 load current: exponential rise towards V/R = 22.84 A during Tₔₙ, exponential free-wheel decay towards zero during Tₒ₌₌. The vertical axis is broken to show the ripple band at scale.
Case 2 — screen the row before solving it. Here
$R = 1.25\ \Omega$ is given, so the steady-state ceiling is
$$\frac{V_i}{R} = \frac{24}{1.25} = 19.2\ \text{A}$$
which is below the required peak of 20 A. By the screen established in
step 1, no chopper period can produce a 20 A peak into this load: even at
$\delta \to 1$, which is continuous d.c. and not chopping at all, the current only
approaches 19.2 A.
Confirm the infeasibility algebraically. Inverting the master
relation for $T$ gives
$$T = -\tau\ln\!\left[1 - \frac{V_i}{R\,I_{\max}}\left(1 - e^{-T_{on}/\tau}\right)\right]
= -1.45\ln\left[1 - 0.9600(0.8089)\right] = -1.45\ln(0.2234) = 2.173\ \text{ms}$$
The bracket does lie in $(0,1)$, so the logarithm exists and a careless solution
would stop here — but the answer, 2.173 ms, is less than the row's
own on-time of 2.4 ms. A period shorter than its on-time is impossible, so this
root must be rejected. The row is solvable only if
$R < V_i/I_{\max} = 24/20 = 1.20\ \Omega$; the printed 1.25 Ω exceeds
that bound.
Figure 5.2 — Peak current against chopper period for the case-2 data. The curve rises towards the asymptote V/R = 19.2 A as the period shortens towards Tₔₙ, and never reaches the required 20 A (shaded band).
Case 3 — solve for the on-time. With $T = 1.8$,
$\tau = 1.5\ \text{ms}$ and $R = 0.9\ \Omega$ the ceiling is
$V_i/R = 26.67\ \text{A} > 20\ \text{A}$, so the row passes the screen. Inverting
the master relation for $T_{on}$:
$$T_{on} = -\tau\ln\!\left[1 - \frac{I_{\max}R}{V_i}\left(1 - e^{-T/\tau}\right)\right]
= -1.5\ln\left[1 - 0.7500(0.6988)\right] = -1.5\ln(0.4759)$$
$$\boxed{\,T_{on,3} = 1.114\ \text{ms}\,}$$
This is comfortably less than the 1.8 ms period, giving a duty ratio of
$\delta = 0.619$.
Check case 3 the same way as case 1. Back-substitution
returns 20.00 A exactly. The extremes are
$I_{\min} = 20e^{-(1.8-1.114)/1.5} = 12.66\ \text{A}$ and
$I_{\max} = 20\ \text{A}$, and the mean $\delta V_i/R = 0.619(26.67)
= 16.50\ \text{A}$ lies between them. The ripple, 7.34 A, is larger than case
1's despite the shorter period, because the lower resistance raises the ceiling
the current is chasing.
Check: case 2 of the printed table has no solution, and is reported
rather than patched. With $V_i = 24\ \text{V}$ and $R = 1.25\ \Omega$ the
load can never carry more than $V_i/R = 19.2\ \text{A}$ in the steady state, so the
row's requirement of a 20 A peak is unattainable at any chopper period; the
formal root, 2.173 ms, is shorter than the row's own 2.4 ms on-time and is
therefore not a period at all. The row becomes solvable for any
$R < 1.20\ \Omega$. As the nearest defensible repair, carrying case 1's
resistance $R = 1.051\ \Omega$ into case 2 gives
$T = 3.74\ \text{ms}$ at a duty ratio of 0.643 — a physically sensible design
point — and that figure is offered only as an illustration of the method, not
as the examiner's intended answer. In the examination hall the correct response is
to state the inconsistency, quote the bound $R < V_i/I_{\max}$, and complete the
two rows that are consistent; a candidate who silently reports 2.173 ms has
missed the point the row now tests.
Final results — the completed table.
Case
$T$ (ms)
$T_{on}$ (ms)
$\tau$ (ms)
$R$ ($\Omega$)
$\delta$
$I_{\min}$ (A)
$I_{\text{avg}}$ (A)
1
2.4
1.8
1.5
1.051
0.750
13.41
17.13
2
no solution
2.4
1.45
1.25
—
—
—
3
1.8
1.114
1.5
0.9
0.619
12.66
16.50
Case 2 requires $R < V_i/I_{\max} = 1.20\ \Omega$; at the printed
$1.25\ \Omega$ the peak current cannot reach 20 A. Taking $R = 1.051\ \Omega$
instead would give $T = 3.74\ \text{ms}$.