Solved Problems · Set 16

Power Factor, Harmonics and Dual Converters

Part 2 · AC–DC Converters — the accounting all fourteen previous sets have been circling, and the two-converter arrangement that finally reaches all four quadrants. Six problems that close Part 2.

Prof. Mithun Mondal 6 solved problems GATE · ESE · University

Set 16 — Power Factor, Harmonics and Dual Converters

Fifteen sets have produced power factors between 0.29 and 0.955, always by the same mechanism: a current that is the wrong shape, and — once thyristors appeared — in the wrong place as well. This set does the accounting properly. What harmonics does a phase-controlled converter actually inject, what does a capacitor bank do about them, and what does it do to them?

The second half closes the other loose end. Set 14 showed that a single converter cannot reverse its current, so it cannot reach two of the four quadrants. Two converters connected in anti-parallel can, and the interesting question is what happens in the gap between them — either a dead time of several milliseconds, or a reactor carrying a circulating current that does no useful work at all.

Part 2 · Chapter 10 · 6 solved problems

i Method Recap
  • The line current of a converter with an inductive load is a square or quasi-square wave, so its harmonics follow immediately:

    \[ \text{1-}\phi:\ n = 3,5,7,9,\dots \quad \text{3-}\phi:\ n = 6k\pm1, \qquad I_n = \frac{I_{s1}}{n} \]
  • Displacement and distortion are corrected by different things:

    \[ Q_C = P\left(\tan\phi_1-\tan\phi_2\right), \qquad C = \frac{Q_C}{\omega V_s^2} \]

    A capacitor corrects only the displacement; the harmonic current is untouched — Problem 2.

  • Any correction capacitor resonates with the supply inductance:

    \[ f_0 = \frac{1}{2\pi\sqrt{L_sC}}, \qquad h_0 = \frac{f_0}{f} \]

    If \(h_0\) lands near 5 or 7, the correction amplifies the very harmonic it was fitted alongside.

  • Recombining a corrected supply current:

    \[ I_h = \sqrt{I_s^2-I_{s1}^2}\ \text{(unchanged)}, \qquad I_s' = \sqrt{I_{s1}'^2+I_h^2} \]
  • A dual converter is two bridges in anti-parallel. For zero average voltage across the pair:

    \[ \alpha_1+\alpha_2 = 180^\circ \;\Longrightarrow\; V_{dc1} = -V_{dc2} \]
  • Two modes, two costs. Circulating-current-free needs a dead time of several milliseconds; circulating-current mode needs a reactor sized from:

    \[ i_r = \frac{1}{L_r}\int\left(v_{o1}+v_{o2}\right)dt \]
Problem 1CoreWhat the Converter Injects

A single-phase full converter draws a constant 40 A from a 230 V, 50 Hz supply at \(\alpha = 60^\circ\). Find the fundamental and the first four harmonic currents, the THD, the real and apparent power, the power factor and the reactive power. Contrast the harmonic spectrum with the three-phase bridge of Set 11.

Solution

The current waveform and its fundamental:

\[ I_s = I_{dc} = 40\ \text{A}, \qquad I_{s1} = \frac{4I_{dc}}{\pi\sqrt2} = 36.0\ \text{A} \]

A square wave contains every odd harmonic, falling as \(1/n\):

OrderFrequencyCurrent% of fundamental
150 Hz36.0 A100%
3150 Hz12.0 A33.3%
5250 Hz7.20 A20.0%
7350 Hz5.14 A14.3%
9450 Hz4.00 A11.1%
\[ THD = \sqrt{\left(\frac{40}{36.0}\right)^2-1} = 48.3\% \]

Contrast with the three-phase bridge. The difference is not a matter of degree:

Harmonic1-φ bridge3-φ bridge
3rd33.3%absent
5th20.0%20.0%
7th14.3%14.3%
9th11.1%absent
THD48.3%31.1%

The entire difference is the triplens. A three-wire three-phase supply offers them no return path, so they simply cannot flow; a single-phase supply has a neutral and they flow freely. That one structural fact accounts for the whole 48.3% against 31.1%.

Why the third harmonic is the dangerous one. In a four-wire installation the third harmonics of all three phases are in phase with each other:

\[ I_{N,3} = 3I_3 = 3(12.0) = 36.0\ \text{A} \]

Thirty-six amps in a neutral conductor, from three single-phase converters each drawing 36 A of fundamental. The neutral is traditionally sized smaller than the phases and carries no overcurrent protection — so it heats without any indication.

Power and reactive power:

\[ V_{dc} = (207.1)\cos60^\circ = 103.5\ \text{V}, \qquad P = (103.5)(40) = 4.14\ \text{kW} \]
\[ S = (230)(40) = 9.20\ \text{kVA}, \qquad PF = \frac{4.14}{9.20} = 0.450 \]
\[ Q = P\tan\alpha = (4141)\tan60^\circ = 7.17\ \text{kVAr} \]

Note that \(P\) and \(Q\) do not account for \(S\): \(\sqrt{P^2+Q^2} = 8.28\) kVA against 9.20 actual. The missing 4.0 kVA is the distortion power, carried entirely by harmonics that transfer no energy at all.

The power triangle does not close when the current is distorted. Real and reactive power account for the fundamental; the harmonics contribute a third term that is neither. That is why power factor correction has two entirely separate problems to solve, and why fixing one does nothing for the other — Problem 2.
Answera\(I_{s1} = 36.0\ \text{A}\); 12.0, 7.20, 5.14, 4.00 A   b\(THD = 48.3\%\)   c\(4.14\ \text{kW},\ 9.20\ \text{kVA},\ PF = 0.450\)   d\(Q = 7.17\ \text{kVAr}\)
Problem 2Exam levelWhy Capacitors Do Not Fix It

A capacitor bank is fitted to correct the displacement factor of the converter in Problem 1 from 0.5 to 0.95 lagging. Find the capacitance required, the resulting supply current and power factor, the best achievable power factor by this route, and the resonant frequency with a source inductance of 1 mH.

Solution

Size the capacitor from the reactive power it must supply:

\[ Q_1 = P\tan\phi_1 = (4141)\tan60^\circ = 7173\ \text{VAr} \]
\[ Q_2 = P\tan\phi_2 = (4141)\tan\left(\cos^{-1}0.95\right) = (4141)(0.3287) = 1361\ \text{VAr} \]
\[ Q_C = 7173-1361 = 5812\ \text{VAr} \]
\[ C = \frac{Q_C}{\omega V_s^2} = \frac{5812}{(314.16)(230)^2} = 350\ \mu\text{F} \]

Now find the new supply current. The harmonic content is completely unaffected — the capacitor cannot supply harmonic current at the right phase to cancel anything:

\[ I_h = \sqrt{I_s^2-I_{s1}^2} = \sqrt{40^2-36.0^2} = \sqrt{1600-1297} = 17.4\ \text{A} \]

The fundamental falls, because less of it is reactive:

\[ I_{s1}' = \frac{P}{V_s\times0.95} = \frac{4141}{(230)(0.95)} = 18.95\ \text{A} \]

Recombine:

\[ I_s' = \sqrt{18.95^2+17.4^2} = \sqrt{359+303} = 25.7\ \text{A} \]
\[ PF' = \frac{4141}{(230)(25.7)} = \frac{4141}{5920} = 0.700 \]

Improved from 0.450 to 0.700 — useful, but nowhere near the 0.95 the capacitor was sized for. The displacement factor is now 0.95; the power factor is not, because distortion is still there.

The ceiling on this approach. Even perfect displacement correction leaves the distortion factor:

\[ PF_{max} = \text{DF} = \frac{I_{s1}}{I_s} = 0.900 \]

So no capacitor bank can take this converter past 0.900, and reaching even that needs full correction to unity displacement. The harmonic current of 17.4 A flows regardless — through the supply, through the transformer, and now also through the capacitor.

And here is the danger. The capacitor and the source inductance form a parallel resonant circuit:

\[ f_0 = \frac{1}{2\pi\sqrt{L_sC}} = \frac{1}{2\pi\sqrt{(0.001)(350\times10^{-6})}} = 269\ \text{Hz} \]
\[ h_0 = \frac{269}{50} = 5.4 \]

The resonance sits at the 5.4th harmonic — between the 5th at 250 Hz and the 7th at 350 Hz, and uncomfortably close to the 5th. The converter injects 7.2 A at exactly that frequency into a circuit that is near resonance, and the resulting current can be several times larger than what was injected.

What that produces in practice:

SymptomMechanism
Capacitor fuses blowing repeatedlyamplified 5th harmonic current
Capacitor bank failing earlyoverheating from harmonic current
Voltage distortion at the busbar worsensamplified current in the source impedance
Problem appears only when the bank switches inresonance did not exist before

The last row is the diagnostic signature. A plant that adds power-factor correction and immediately starts losing capacitors has almost certainly created a resonance near a harmonic the existing converters were already injecting.

The fix is a detuning reactor in series with each capacitor, placing the resonance safely below the lowest injected harmonic:

\[ h_0 \approx 4.2\ \text{(typical detuned bank)} \;\Rightarrow\; \text{inductive above 210 Hz} \]

Above its tuning frequency the branch is inductive, so it cannot resonate with the source at any higher harmonic. The bank still corrects displacement at 50 Hz and now also absorbs a little 5th-harmonic current instead of amplifying it.

A capacitor corrects the one thing the converter did not do wrong. The displacement was caused by firing delay and the capacitor genuinely fixes it; the distortion was caused by the current's shape and no shunt element can. Worse, the correction introduces a resonance that was not there before — which is why harmonic studies precede capacitor installations wherever converters are present.
Answera\(C = 350\ \mu\text{F}\)   b\(I_s = 25.7\ \text{A},\ PF = 0.700\)   c ceiling is \(\text{DF} = 0.900\)   d\(f_0 = 269\ \text{Hz}\) — near the 5th
Problem 3Exam levelTwo Converters, One Load

A dual converter is formed from two three-phase bridges in anti-parallel on a 415 V supply. In circulating-current-free mode, converter 1 operates at \(\alpha_1 = 60^\circ\). Find its output, the firing angle converter 2 must be given to match it, why only one may conduct at a time, and the changeover time required.

Solution

The arrangement. Two bridges are connected back to back across the same load, pointing in opposite directions. Converter 1 supplies positive current, converter 2 supplies negative current, and between them the load can be driven in all four quadrants:

\[ V_{dc1} = \frac{3V_{m(l)}}{\pi}\cos\alpha_1 = (560.4)(0.5) = 280.2\ \text{V} \]

Converter 2 must produce the same output so that the load sees a consistent voltage whichever bridge is active. Because it faces the load the other way, its own output must be the negative of converter 1's:

\[ V_{dc2} = -V_{dc1} \;\Longrightarrow\; \cos\alpha_2 = -\cos\alpha_1 \;\Longrightarrow\; \alpha_2 = 180^\circ-\alpha_1 \]
\[ \alpha_2 = 180^\circ-60^\circ = 120^\circ \]

This is the fundamental relation of a dual converter. Note that when converter 1 is rectifying at 60°, converter 2 is set to invert at 120° — it is standing by, ready to accept current in the opposite direction the instant it is needed.

Why only one may conduct. The two bridges are connected directly across each other. Their average voltages cancel, but their instantaneous waveforms do not:

\[ v_{o1}+v_{o2} \ne 0 \quad\text{instantaneously} \]

Both are 6-pulse waveforms and the ripple components do not cancel — they are 30° apart in phase. With no impedance between them, that difference voltage would drive an unlimited current straight from one bridge to the other, bypassing the load entirely. In circulating-current-free mode the answer is simply to keep one bridge fully blocked.

The changeover sequence, which is where the mode's cost appears:

StepActionTypical time
1Reduce current demand to zeroset by load inductance
2Detect zero current in all six devices
3Remove gate pulses from converter 1
4Wait for devices to regain blocking2–10 ms
5Apply gate pulses to converter 2
6Build current in the new directionset by load inductance

Step 4 is the irreducible one. A thyristor that has just stopped conducting still holds stored charge; firing the opposing bridge before it has recovered short-circuits the supply through both converters — the same failure as a commutation failure, and with the same consequences.

What the dead time costs. During steps 1 to 6 the load current is zero, so:

\[ T = K\phi\,I_a = 0\quad\text{throughout the changeover} \]

Torque disappears entirely for several milliseconds. For a rolling mill or a hoist that is acceptable; for a position servo it is a dead zone in the control loop that produces limit cycling around zero torque. That is the whole argument for the circulating-current mode of Problem 4.

Circulating-current-free mode is simple, lossless and discontinuous. No reactor, no wasted current, and no torque at all for the few milliseconds it takes to change hands. Whether that matters depends entirely on whether the load notices — and position control notices.
Answera\(V_{dc1} = 280.2\ \text{V}\)   b\(\alpha_2 = 120^\circ\)   c the ripple voltages do not cancel instantaneously   d 2–10 ms dead time with zero torque
Problem 4ChallengeSizing the Reactor

The same dual converter is to run in circulating-current mode, with both bridges gated continuously at \(\alpha_1 = 60^\circ\) and \(\alpha_2 = 120^\circ\). The rated load current is 200 A and the peak circulating current must not exceed 20% of it. Find the reactor inductance required and the cost of the mode.

Solution

The driving voltage. With both bridges gated, the voltage acting around the loop they form is the sum of their two outputs:

\[ v_r(t) = v_{o1}(t)+v_{o2}(t) \]
\[ \overline{v_{o1}} = +280.2\ \text{V}, \qquad \overline{v_{o2}} = -280.2\ \text{V} \;\Longrightarrow\; \overline{v_r} = 0 \]

Zero on average — which is what makes the mode possible at all. If the averages did not cancel, a DC circulating current would build without limit.

But the ripple does not cancel. Both outputs are 6-pulse waveforms at 300 Hz, and at \(\alpha_1 = 60^\circ\) and \(\alpha_2 = 120^\circ\) their ripples are displaced. The sum is a 300 Hz alternating voltage of substantial amplitude:

\[ i_r(t) = \frac{1}{L_r}\int v_r(t)\,dt \]

There is no simple closed form, because \(v_r\) is a piecewise cosine. Integrating numerically over one 300 Hz ripple period gives the peak-to-peak excursion, and since the circulating current can only be positive — thyristors again — that excursion is the peak.

Evaluate. Integrating the ripple sum for a trial \(L_r = 10\) mH:

\[ i_{r,peak} = 43.4\ \text{A}\quad\text{at }L_r = 10\ \text{mH} \]

Since \(i_r \propto 1/L_r\), scaling to the 40 A target:

\[ L_r = (10)\frac{43.4}{40} = 10.8\ \text{mH} \quad\to\quad \text{specify } 12\ \text{mH} \]

What the reactor has to be. This is not a small component:

RequirementValue
Inductance12 mH
DC current (worst case)200 A load + 40 A circulating
Must not saturate at240 A
Ripple frequency300 Hz
Stored energy\(\tfrac12LI^2 \approx 350\ \text{J}\)

A 12 mH reactor that must stay linear at 240 A is an iron-cored component weighing tens of kilograms, with an air gap sized for the DC bias. In practice two reactors are used, one in each converter's leg, so that each carries only its own current.

The running cost. The circulating current flows through the thyristors of both converters and does no useful work:

\[ I_{extra,rms} \approx \frac{i_{r,peak}}{\sqrt3} \approx 23\ \text{A per converter} \]

That current adds to the conduction loss in every device and to the reactor's own copper loss, all for the sake of never letting the current reach zero. Note also that both converters are now drawing from the supply simultaneously, so the reactive loading is worse than in the free mode.

What it buys:

PropertyCirculating-current-freeCirculating-current
Reactornone12 mH, 240 A
Extra device currentnone~23 A rms
Changeover time2–10 msinstantaneous
Torque at zero crossingzero for the dead timecontinuous
Discontinuous conductionat light loadnever
Controlneeds mode logicsimple, linear throughout

The last two rows are the real prize. Because the circulating current keeps both converters conducting at all times, neither ever enters the discontinuous mode of Set 13 — so the transfer function stays linear from full forward torque to full reverse, with no gain change and no dead zone. For a servo that is worth a heavy reactor.

The circulating current is deliberate waste that buys linearity. It keeps every device conducting so the converter never has to find its way back from zero, eliminating both the dead time and the discontinuous-conduction nonlinearity in one move. Which mode to choose is entirely a question of whether the load can tolerate a few milliseconds of no torque.
Answera\(i_{r,peak} = 43.4\ \text{A}\) at 10 mH   b\(L_r = 10.8\ \text{mH}\), specify 12 mH   c ~23 A extra rms per converter, no dead time
Problem 5ChallengeAll Four Quadrants

A 415 V dual converter drives a DC motor with \(R_a = 0.15\ \Omega\) and \(K\phi = 4.5\ \text{V}\cdot\text{s/rad}\) at a constant armature current magnitude of 200 A and a speed magnitude of 100 rad/s. Find the firing angle of the active converter in each of the four quadrants, the power flow, and the torque.

Solution

The machine quantities. At 100 rad/s the back EMF magnitude is fixed:

\[ \left|E\right| = K\phi\,\omega = (4.5)(100) = 450\ \text{V}, \qquad \left|I_aR_a\right| = (200)(0.15) = 30\ \text{V} \]
\[ \left|T\right| = K\phi\,I_a = 900\ \text{N}\!\cdot\!\text{m}, \qquad \left|P_{mech}\right| = T\omega = 90\ \text{kW} \]

Apply the armature equation in each quadrant. The rule is mechanical: the resistance always opposes the current, so \(I_aR_a\) always adds in the direction of current flow:

\[ V_{dc} = E+I_aR_a \]

Quadrants I and IV use converter 1 (positive current); II and III use converter 2. The sign of \(E\) follows the speed and the sign of \(I_a\) follows the torque.

Quadrant I — forward motoring:

\[ E = +450,\ I_a = +200 \;\Rightarrow\; V_{dc} = 450+30 = +480\ \text{V} \]
\[ \cos\alpha_1 = \frac{480}{560.4} = 0.857 \;\Longrightarrow\; \alpha_1 = 31.1^\circ \quad\text{(rectifying)} \]

Quadrant II — forward braking. The machine still turns forward, so \(E\) stays positive, but the current must reverse — which means converter 2 takes over, and from its own terminals the machine looks like a source:

\[ V_{dc} = -\left(450-30\right) = -420\ \text{V} \;\Longrightarrow\; \cos\alpha_2 = -0.749 \;\Longrightarrow\; \alpha_2 = 138.5^\circ \quad\text{(inverting)} \]
\[ P_{returned} = (420)(200) = 84\ \text{kW} \]

The machine generates 90 kW, the armature resistance takes 6 kW, and 84 kW goes back to the supply. Note the resistance term now subtracts from the magnitude, because the current and the EMF have opposite signs.

The complete map:

Quadrant\(\omega\)\(T\)\(E\)\(V_{dc}\)Converter\(\alpha\)Power
I — fwd motoring+++450+480131.1°in, 96 kW
II — fwd braking++450−4202138.5°out, 84 kW
III — rev motoring−450−4802148.9°in, 96 kW
IV — rev braking+−450+420141.5°out, 84 kW

Read the \(\alpha\) column: the two motoring quadrants use firing angles below 90° and the two braking quadrants use angles above it. Rectification and inversion map exactly onto motoring and braking.

Where the transitions are hard. Two of the four boundaries require a converter changeover:

\[ \text{I} \leftrightarrow \text{II}: \text{ current reverses at constant speed} \;\Rightarrow\; \text{changeover} \]
\[ \text{II} \rightarrow \text{III}: \text{ speed passes through zero} \;\Rightarrow\; \text{no changeover} \]

The first is the demanding one, because it happens at full speed with full torque reversing — a hoist catching a descending load, a mill reversing its pass. In circulating-current-free mode there are several milliseconds of zero torque there; in circulating-current mode there are none. That single transition is what decides which mode a drive is built with.

Four quadrants, two converters, one rule. Everything followed from \(V_{dc} = E+I_aR_a\) with the signs taken seriously: the converter that can carry the required current direction is the active one, and its firing angle is whatever produces the required voltage. Rectifying below 90°, inverting above it, and the machine never knows which bridge is feeding it.
Answera\(31.1^\circ,\ 138.5^\circ,\ 148.9^\circ,\ 41.5^\circ\)   b 96 kW in (I, III), 84 kW out (II, IV)   c\(900\ \text{N}\!\cdot\!\text{m}\) in every quadrant
Problem 6ChallengeEvery Remedy Compared

Compare every method met in Part 2 for improving the input power factor of the 4.14 kW, \(\alpha = 60^\circ\) converter of Problem 1: the semiconverter, capacitor correction, twelve-pulse connection, and an active front end. Give the achievable power factor, the supply current, and the limitation of each.

Solution

The baseline, from Problem 1:

\[ PF = (0.900)\cos60^\circ = 0.450, \qquad I_s = 40\ \text{A}, \qquad S = 9.20\ \text{kVA} \]

Every remedy attacks either the 0.900 (distortion) or the \(\cos60^\circ\) (displacement), and it is worth being clear which before comparing them.

Semiconverter — attacks displacement, by cutting the current block short:

\[ \text{DPF} = \cos\frac{\alpha}{2} = \cos30^\circ = 0.866, \qquad \text{DF} = 0.955 \]
\[ PF = 0.827, \qquad I_s = 40\sqrt{\tfrac{120}{180}} = 32.7\ \text{A} \]

Nearly doubles the power factor and reduces the current by 18%, for free — but gives up quadrant IV entirely, so it cannot be used on any drive that must brake.

Capacitor correction — attacks displacement only, from Problem 2:

\[ PF = 0.700\ \text{at DPF} = 0.95; \qquad \text{ceiling } PF = 0.900\ \text{at DPF} = 1 \]

Works on any converter without changing it, but leaves 17.4 A of harmonic current untouched, and introduces a resonance at the 5.4th harmonic that needs a detuning reactor.

Twelve-pulse — attacks distortion only:

\[ \text{DF: } 0.955 \to 0.988, \qquad \text{DPF unchanged at }\cos\alpha \]
\[ PF = (0.988)(0.5) = 0.494 \]

Barely helps — because at \(\alpha = 60^\circ\) the problem is overwhelmingly displacement, and pulse number does nothing about that. Twelve-pulse is a harmonic remedy, and the harmonics were already the smaller part of the loss.

Active front end — attacks both, by controlling the shape and the phase of the input current directly:

\[ PF \approx 0.99, \qquad S = \frac{4141}{0.99} = 4.18\ \text{kVA}, \qquad I_s = 18.2\ \text{A} \]
\[ \text{current reduction} = 1-\frac{18.2}{40} = 54.5\% \]

Less than half the supply current for the same delivered power, with THD under 5% and bidirectional power flow. It is a PWM converter running at kilohertz, using the self-commutating devices of Set 7 — and it is the only method here that is not a compromise.

Everything together:

MethodAttacksPF\(I_s\)Limitation
Full converter0.45040.0 Abaseline
Twelve-pulsedistortion0.49438.7 Ano help with displacement
Capacitor bankdisplacement0.70025.7 Aresonance risk; ceiling 0.900
Semiconverterdisplacement0.82732.7 Acannot invert
Active front endboth0.9918.2 Acost, complexity, an extra converter

Only the last row addresses both terms, and it does so by abandoning line commutation altogether. Everything above it is a way of making the best of a converter whose current shape and phase are dictated by the supply.

What Part 2 has actually established. The line-commutated converter is efficient, robust, cheap and scalable to hundreds of megawatts — and it draws a current it cannot control:

\[ \text{shape fixed by the topology}, \qquad \text{phase fixed by } \alpha, \qquad \text{both coupled to the output} \]

That coupling is the root of every power-factor result in Part 2. Breaking it requires a switch that can be turned off at will, at a frequency far above the line — which is exactly the device Part 1 ended with, and exactly what Part 3 begins to use.

Every remedy in Part 2 is a compromise except the one that stops using line commutation. The semiconverter trades quadrants, the capacitor trades resonance risk, twelve-pulse fixes the smaller half of the problem. Controlling the input current directly fixes both and costs a whole extra converter — which is only affordable because the DC-link topologies of Part 3 made switching at kilohertz routine.
Answera semiconverter \(0.827\)   b capacitor \(0.700\)   c twelve-pulse \(0.494\)   d active front end \(0.99\), 18.2 A
Formulas

Key Formulas

QuantityRelationNotes
Harmonic orders1-φ: all odd; 3-φ: \(6k\pm1\)Triplens are the difference
Harmonic amplitude\(I_n = I_{s1}/n\)Square-edged current
Neutral third harmonic\(I_N = 3I_3\)Zero sequence adds
Reactive power\(Q = P\tan\alpha\)Fundamental only
Distortion power\(D = \sqrt{S^2-P^2-Q^2}\)The triangle does not close
Correction capacitor\(Q_C = P\left(\tan\phi_1-\tan\phi_2\right)\)\(C = Q_C/\omega V_s^2\)
Harmonic current\(I_h = \sqrt{I_s^2-I_{s1}^2}\)Unchanged by a capacitor
Corrected current\(I_s' = \sqrt{I_{s1}'^2+I_h^2}\)Problem 2
PF ceiling\(PF_{max} = \text{DF}\)0.900 for a 1-φ bridge
Resonant order\(h_0 = \dfrac{1}{2\pi f\sqrt{L_sC}}\)Keep clear of 5 and 7
Dual converter\(\alpha_1+\alpha_2 = 180^\circ\)Averages cancel
Circulating current\(i_r = \dfrac{1}{L_r}\displaystyle\int\left(v_{o1}+v_{o2}\right)dt\)Integrate numerically
Reactor scaling\(i_{r,peak} \propto 1/L_r\)Problem 4
Armature equation\(V_{dc} = E+I_aR_a\)All four quadrants
Quadrant rule\(\alpha < 90^\circ\) motoring, \(> 90^\circ\) brakingProblem 5
Pitfalls

Common Mistakes

  1. Expecting \(S^2 = P^2+Q^2\) with a distorted current. Here \(\sqrt{P^2+Q^2} = 8.28\) kVA against 9.20 actual; the gap is distortion power — Problem 1.

  2. Forgetting the third harmonic in single-phase converters. It is the largest one at 33% and it adds in the neutral of a four-wire system — Problem 1.

  3. Assuming a correction capacitor delivers the power factor it was sized for. Sized for 0.95 displacement, it achieved 0.700 overall — Problem 2.

  4. Ignoring resonance when adding capacitors near converters. 350 µF with 1 mH resonates at the 5.4th harmonic — right where the current is being injected — Problem 2.

  5. Believing capacitors can reduce harmonic current. They cannot; they can only supply fundamental reactive current, and they may amplify the harmonics — Problem 2.

  6. Gating both converters of a dual converter without a reactor. The average voltages cancel but the ripples do not, and the difference drives an unlimited current — Problem 3.

  7. Underestimating the changeover dead time. Two to ten milliseconds of zero torque is fatal for position control and irrelevant for a mill — Problem 3.

  8. Sizing the circulating-current reactor for the circulating current alone. It also carries the full load current and must not saturate at the sum — Problem 4.

  9. Getting the sign of \(I_aR_a\) wrong when braking. The resistance always opposes the current, so it reduces the required voltage magnitude in quadrants II and IV — Problem 5.

  10. Expecting twelve-pulse to improve a poor power factor. It fixes distortion; at \(\alpha = 60^\circ\) the problem is displacement — Problem 6.

Looking Ahead

That completes Part 2. Eight sets have taken the switch of Part 1 and arranged it into every line-commutated converter worth building — half-wave to twelve-pulse, uncontrolled to fully controlled, rectifying to inverting, one quadrant to four. The recurring result is a single coupling: the input current's shape is fixed by the topology and its phase by the firing angle, and both are tied to the output. Every power-factor figure in Part 2, from 0.29 to 0.955, follows from it, and Problem 6 showed that no arrangement of thyristors and diodes escapes it.

What escapes it is a switch that turns off when told, at a frequency far above the line. Part 1 ended with exactly that device and Set 6 showed why it displaced the thyristor by two orders of magnitude. Give it a fixed DC link — which a diode bridge at \(\alpha = 0\) and a capacitor provide at a power factor of 0.9 — and the varying can be done downstream, at kilohertz, where the supply is not involved at all.

Next: Part 3 begins with Set 17 — Chopper Control Strategies and Load Current, returning to the duty ratio of Set 1 and applying it to a DC load: the control strategies available, the current ripple each produces, the limits on frequency, and the four-quadrant chopper that reaches every quadrant without a second converter at all.