Solved Problems · Set 15

Source Inductance and Overlap Angle

Part 2 · AC–DC Converters — current cannot transfer between phases instantly, and everything that follows from that finite transfer is in this set. Six problems on overlap, regulation, notches and the inversion limit.

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

Set 15 — Source Inductance and Overlap Angle

Every result in Sets 9 to 14 assumed that current transfers from one device to the next the instant the gate says so. It does not. The supply and its transformer have inductance, and inductor current cannot step — so for a finite interval called the overlap angle \(\mu\), both the outgoing and incoming devices conduct together and two phases are short-circuited through that inductance.

Three consequences follow, and they are not small. The output voltage falls in proportion to load current, behaving exactly like a series resistance that dissipates no power. The displacement factor worsens beyond \(\cos\alpha\). And the supply voltage itself is momentarily collapsed at the point of common coupling — a notch that every other user of the network sees, and that standards limit.

Part 2 · Chapter 10 · 6 solved problems

i Method Recap
  • The overlap angle follows from the volt-seconds needed to reverse the current in the source inductance:

    \[ \text{1-}\phi:\ \cos(\alpha+\mu) = \cos\alpha-\frac{2\omega L_sI_{dc}}{V_m}; \qquad \text{3-}\phi:\ \cos(\alpha+\mu) = \cos\alpha-\frac{2\omega L_sI_{dc}}{V_{m(line)}} \]
  • The voltage drop is proportional to current and independent of firing angle:

    \[ \text{1-}\phi:\ \Delta V = \frac{2\omega L_sI_{dc}}{\pi}; \qquad \text{3-}\phi:\ \Delta V = \frac{3\omega L_sI_{dc}}{\pi} \]
  • Which is an equivalent resistance that dissipates nothing:

    \[ R_c = \frac{2\omega L_s}{\pi}\ \text{or}\ \frac{3\omega L_s}{\pi}, \qquad V_{dc} = V_{dc0}\cos\alpha-R_cI_{dc} \]
  • The output can also be written symmetrically, which is a useful check:

    \[ V_{dc} = \frac{V_{m}}{\pi}\left[\cos\alpha+\cos(\alpha+\mu)\right]\ \text{(1-}\phi) \]
  • Overlap shifts the fundamental current further, worsening the displacement factor:

    \[ \text{DPF} \approx \cos\left(\alpha+\frac{\mu}{2}\right) \]
  • The supply notch is what other users see. Its depth divides between the source and any converter-side reactor:

    \[ \text{depth at PCC} = v_{comm}\frac{L_{source}}{L_{source}+L_{reactor}}, \qquad \text{area} = 2L_{source}I_{dc} \]
  • In inversion the overlap eats the extinction angle:

    \[ \gamma = 180^\circ-\alpha-\mu \ \ge\ \gamma_{min} \]

    And \(\mu\) grows with current, so a heavier load lowers the maximum firing angle — Problem 5.

Problem 1CoreHow Long the Handover Takes

A single-phase full converter on a 230 V, 50 Hz supply with a source inductance of 2 mH delivers a constant 30 A at \(\alpha = 30^\circ\). Find the overlap angle, the commutation voltage drop and the actual output voltage, and verify the result two ways.

i(in) i(out) 30 A overlap μ vo area lost each commutation
During overlap both devices conduct, the output sits between the two sources, and volt-seconds are lost
Solution

What has to happen during commutation. The load current must transfer from one thyristor pair to the other, which means the source current must change from \(+30\) A to \(-30\) A — a change of \(2I_{dc}\) through \(L_s\):

\[ \int v\,dt = L_s\Delta i = L_s\left(2I_{dc}\right) \]

The supply voltage supplies those volt-seconds, and while it is doing so it is short-circuited through the two conducting pairs — so the load gets nothing.

Integrating the supply over the overlap gives the standard result:

\[ \cos(\alpha+\mu) = \cos\alpha-\frac{2\omega L_sI_{dc}}{V_m} \]
\[ \frac{2\omega L_sI_{dc}}{V_m} = \frac{2(314.16)(0.002)(30)}{325.3} = \frac{37.70}{325.3} = 0.1159 \]
\[ \cos(\alpha+\mu) = 0.866-0.116 = 0.750 \;\Longrightarrow\; \alpha+\mu = 41.4^\circ \;\Longrightarrow\; \mu = 11.4^\circ \]

Eleven degrees is 0.63 ms — not negligible against a 10 ms half cycle. And note what \(\mu\) depends on: the current and the inductance, not the power.

The voltage drop. Averaging the lost area over the half period:

\[ \Delta V = \frac{2\omega L_sI_{dc}}{\pi} = \frac{37.70}{\pi} = 12.0\ \text{V} \]
\[ V_{dc} = \frac{2V_m}{\pi}\cos\alpha-\Delta V = 179.3-12.0 = 167.3\ \text{V} \]

Verify with the symmetric form, which averages the supply over the actual conduction pattern rather than subtracting a correction:

\[ V_{dc} = \frac{V_m}{\pi}\left[\cos\alpha+\cos(\alpha+\mu)\right] = (103.5)(0.866+0.750) \]
\[ = (103.5)(1.616) = 167.3\ \text{V}\ \checkmark \]

Two independent routes agreeing. The second form is the more fundamental — it says the output is the mean of the voltage at the start and end of commutation — and the first is that result rearranged into a drop.

Read the loss of control range. The 12 V drop is 6.7% of the ideal output at this angle, but it is a fixed voltage, so its proportional effect grows as the output is reduced:

\[ \alpha = 30^\circ:\ \frac{12.0}{179.3} = 6.7\%; \qquad \alpha = 75^\circ:\ \frac{12.0}{53.6} = 22.4\% \]

A drive at low speed loses nearly a quarter of its output to commutation. And since the drop is proportional to current, it also means the machine's speed sags with load in a way the cosine law does not predict — which is Problem 2.

Overlap is the price of a real supply, and it is charged per ampere. Nothing about the converter changed; the source simply cannot hand current between phases instantly. What it costs is volt-seconds during every commutation, and there are two commutations per cycle in a single-phase bridge and six in a three-phase one.
Answera\(\mu = 11.4^\circ\)   b\(\Delta V = 12.0\ \text{V}\)   c\(V_{dc} = 167.3\ \text{V}\), confirmed both ways
Problem 2CoreA Resistance That Burns Nothing

For the same converter at \(\alpha = 30^\circ\), find the output voltage and overlap angle at 10, 30 and 60 A, derive the equivalent commutation resistance, compute the load regulation, and explain where the “lost” power goes.

Solution

The drop is linear in current, which is the key structural observation:

\[ \Delta V = \frac{2\omega L_s}{\pi}I_{dc} = R_cI_{dc}, \qquad R_c = \frac{2(314.16)(0.002)}{\pi} = 0.40\ \Omega \]

So the converter behaves exactly as an ideal source \((2V_m/\pi)\cos\alpha\) in series with 0.40 Ω. Every question about regulation reduces to that Thevenin equivalent.

Sweep the load:

\(I_{dc}\)\(\Delta V\)\(V_{dc}\)\(\mu\)
0 A0 V179.3 V
10 A4.0 V175.3 V4.17°
30 A12.0 V167.3 V11.40°
60 A24.0 V155.3 V20.64°

The drop is exactly linear; the overlap angle is not, because the cosine is nonlinear. Doubling the current from 30 to 60 A doubles the drop but raises \(\mu\) by only 81%.

Load regulation from no load to 60 A:

\[ \text{regulation} = \frac{V_{NL}-V_{FL}}{V_{FL}} = \frac{179.3-155.3}{155.3} = 15.5\% \]

Poor for a supply and significant for a drive: the machine's speed will sag by that much between no load and full load at fixed firing angle, on top of the sag from armature resistance. A speed controller has to correct for both.

Now the question that catches people out: where does the power go? Twelve volts at 30 A looks like 360 W, but the source inductance is lossless:

\[ P_{L_s} = 0 \quad\text{(a pure inductance dissipates nothing)} \]

So the 360 W is not dissipated anywhere. It is never drawn from the supply in the first place. The commutation process makes the converter draw less real power and more reactive power — the fundamental current shifts further behind the voltage, so \(V_sI_{s1}\cos\phi_1\) falls by exactly 360 W.

Confirm through the displacement factor. The extra shift is approximately half the overlap angle:

\[ \text{DPF} \approx \cos\left(\alpha+\frac{\mu}{2}\right) = \cos\left(30^\circ+5.7^\circ\right) = 0.812 \]

Against \(\cos30^\circ = 0.866\) without overlap — a 6.2% reduction, matching the 6.7% voltage drop to within the accuracy of the approximation.

This is the resolution: \(R_c\) is a bookkeeping device that correctly predicts the voltage while being physically a phase shift, not a dissipation. Calling it a resistance is convenient and calling it lossy is wrong.

Two practical consequences:

Because \(R_c\) is losslessConsequence
No heat is producedno cooling required, no efficiency penalty in the usual sense
Reactive power rises insteadthe supply must carry it — worse power factor
Effect scales with \(L_s\)a weak supply gives worse regulation
Effect scales with \(I_{dc}\)regulation is a load-dependent error, correctable by feedback
An equivalent resistance that produces no heat is a warning about models. \(R_c = 2\omega L_s/\pi\) predicts the terminal voltage perfectly and predicts the dissipation not at all. Using it in an efficiency calculation — a common error — invents 360 W of loss that does not exist and hides the reactive power that does.
Answera\(175.3,\ 167.3,\ 155.3\ \text{V}\)   b\(R_c = 0.40\ \Omega\)   c regulation 15.5%   d no loss — it appears as reactive power
Problem 3Exam levelOverlap in Three Phases

A 415 V six-pulse converter with a source inductance of 0.2 mH per phase delivers 100 A at \(\alpha = 30^\circ\). Find the overlap angle, the voltage drop, the actual output, and the equivalent commutation resistance. Compare the severity with the single-phase case.

Solution

The three-phase overlap relation has the same form, with the line peak as the commutating voltage:

\[ \cos(\alpha+\mu) = \cos\alpha-\frac{2\omega L_sI_{dc}}{V_{m(line)}} \]
\[ \frac{2(314.16)(0.0002)(100)}{586.9} = \frac{12.57}{586.9} = 0.0214 \]
\[ \cos(\alpha+\mu) = 0.866-0.021 = 0.845 \;\Longrightarrow\; \alpha+\mu = 32.4^\circ \;\Longrightarrow\; \mu = 2.4^\circ \]

The voltage drop carries a factor of three, because there are six commutations per cycle rather than two:

\[ \Delta V = \frac{3\omega L_sI_{dc}}{\pi} = \frac{3(314.16)(0.0002)(100)}{\pi} = \frac{18.85}{\pi} = 6.0\ \text{V} \]
\[ V_{dc} = (560.4)(0.866)-6.0 = 485.4-6.0 = 479.4\ \text{V} \]
\[ R_c = \frac{3\omega L_s}{\pi} = 0.06\ \Omega \]

Compare the two converters:

Quantity1-φ, 2 mH, 30 A3-φ, 0.2 mH, 100 A
Overlap angle11.4°2.4°
Voltage drop12.0 V6.0 V
Ideal output179.3 V485.4 V
Drop as % of output6.7%1.2%
\(R_c\)0.40 Ω0.06 Ω

The three-phase converter is far less affected in relative terms — but that is mostly because its inductance is ten times smaller. The structural advantage is that the drop is compared against an output nearly three times larger.

Read the scaling properly. With the same source inductance the three-phase converter would have a larger absolute drop, since the coefficient is \(3/\pi\) rather than \(2/\pi\):

\[ \frac{R_{c,3\phi}}{R_{c,1\phi}} = \frac{3}{2} = 1.5\quad\text{for equal }L_s \]

More commutations per cycle means more lost volt-seconds. What saves the three-phase converter is the denominator: its output is 2.7 times larger, so the same absolute drop is a much smaller fraction. That is the correct way to state the advantage.

Where the inductance comes from. It is rarely a component; it is the supply itself:

\[ L_s \approx \frac{V_{ph}^2}{\omega S_{sc}}\times \text{(per-unit reactance)} \]

A transformer of 5% impedance feeding this converter would contribute roughly this much inductance. So the overlap angle is a property of how stiff the supply is, and a converter that behaves well on a strong grid can regulate poorly on a generator or at the end of a long cable — a common and confusing field problem.

Overlap is set by the supply's short-circuit strength, not by the converter. The same equipment sees 2.4° on a stiff network and 15° behind a small generator, with all the regulation and power-factor consequences that implies. That is why converter specifications quote a minimum short-circuit ratio.
Answera\(\mu = 2.4^\circ\)   b\(\Delta V = 6.0\ \text{V}\)   c\(V_{dc} = 479.4\ \text{V}\)   d\(R_c = 0.06\ \Omega\), 1.2% against 6.7%
Problem 4ChallengeNotching the Supply

The converter of Problem 3 has 0.2 mH of total commutating inductance, of which 0.05 mH is the utility source and 0.15 mH is a line reactor at the converter. Find the notch depth and area seen at the point of common coupling, compare with IEEE 519 limits of 20% depth and 22,800 V·µs area, and evaluate what happens if the line reactor is removed.

Solution

What a notch is. During overlap two phases are short-circuited through the total commutating inductance. The instantaneous commutating voltage is divided across that inductance in proportion to where it sits — so the voltage at any point in the network collapses by the fraction of inductance upstream of it:

\[ \text{notch depth at PCC} = v_{comm}\frac{L_{utility}}{L_{utility}+L_{reactor}} \]

The full notch depth is the instantaneous line voltage at the commutation instant:

\[ v_{comm} = V_{m(line)}\sin\alpha = (586.9)\sin30^\circ = 293.4\ \text{V} \]

Note that this grows with firing angle: at \(\alpha = 90^\circ\) the full line peak is being short-circuited, which is why notching is worst at low output.

With the line reactor fitted, only a quarter of the inductance is upstream:

\[ \text{depth} = (293.4)\frac{0.05}{0.20} = (293.4)(0.25) = 73.4\ \text{V} \]
\[ \frac{73.4}{586.9} = 12.5\% \;<\; 20\% \quad\checkmark \]

The notch area, which is the other half of the standard. It is the volt-seconds absorbed by the upstream inductance during the two commutations per cycle affecting each line:

\[ \text{area} = 2L_{utility}I_{dc} = 2(0.00005)(100) = 0.010\ \text{V}\!\cdot\!\text{s} = 10{,}000\ \text{V}\!\cdot\!\mu\text{s} \]
\[ 10{,}000 \;<\; 22{,}800\ \text{V}\!\cdot\!\mu\text{s} \quad\checkmark \]

Both limits satisfied with margin. Note that the area depends only on the upstream inductance and the current — not on the firing angle, and not on the reactor. The reactor helps the depth, not the area.

Now remove the line reactor:

\[ \text{depth} = (293.4)\frac{0.05}{0.05} = 293.4\ \text{V} = 50\%\ \text{of peak} \quad\textbf{fails} \]

A 50% notch, two and a half times the limit. Every other load on that busbar sees the supply voltage collapse by half for 2.4° of every 60 — enough to disrupt zero-crossing detectors, misfire other thyristor equipment, and cause audible noise in transformers.

The counter-intuitive part. Adding the line reactor increases the total commutating inductance, which makes the converter's own regulation and overlap worse:

QuantityNo reactor (0.05 mH)With reactor (0.20 mH)
Overlap angle0.6°2.4°
Voltage drop1.5 V6.0 V
Notch depth at PCC50% — fails12.5% — passes
Notch area at PCC10,000 V·µs10,000 V·µs

The converter is made slightly worse so that the network is made much better. That is the whole purpose of a line reactor, and it explains why one is fitted to almost every large drive even though nothing in the converter's own performance calls for it.

A line reactor does not reduce the disturbance — it decides who gets it. The notch area is fixed by the utility inductance and the load current; the reactor merely moves the voltage collapse to the converter's own terminals instead of the shared busbar. The converter pays 4.5 V of extra regulation so that its neighbours see a 12.5% notch rather than 50%.
Answera\(73.4\ \text{V} = 12.5\%\)   b\(10{,}000\ \text{V}\!\cdot\!\mu\text{s}\)   c both pass   d without the reactor, 50% depth — fails
Problem 5ChallengeThe Inversion Ceiling

The 415 V converter with 0.2 mH of source inductance operates in inversion. The thyristor turn-off time requires a minimum extinction angle of 5.4°. Find the maximum firing angle at 100 A, the absolute limit beyond which commutation is impossible at all, and the maximum firing angle at 300 A. Explain the failure mechanism.

Solution

The extinction angle now has two claimants. Set 14 treated \(\gamma = 180^\circ-\alpha\); with overlap the commutation itself consumes \(\mu\) of it:

\[ \gamma = 180^\circ-\alpha-\mu \ \ge\ \gamma_{min} \;\Longleftrightarrow\; \alpha+\mu \le 180^\circ-\gamma_{min} \]

Which is convenient, because \(\alpha+\mu\) is exactly the quantity the overlap equation gives directly.

Apply the overlap relation with \(\gamma_{min} = 5.4^\circ\) at 100 A:

\[ \cos(\alpha+\mu) \le \cos\left(174.6^\circ\right) = -0.9956 \]
\[ \cos\alpha \le -0.9956+\frac{2\omega L_sI_{dc}}{V_{m(line)}} = -0.9956+0.0214 = -0.9742 \]
\[ \alpha_{max} = 167.0^\circ \]

There is also an absolute limit, independent of any turn-off time. The overlap equation requires \(\cos(\alpha+\mu) \ge -1\), since a cosine cannot go below it:

\[ \cos\alpha \ge -1+0.0214 = -0.9786 \;\Longrightarrow\; \alpha \le 168.1^\circ \]

Beyond 168.1° the supply simply cannot deliver the volt-seconds needed to transfer 100 A before its polarity reverses. Commutation does not merely become risky — it becomes impossible.

Now raise the current to 300 A:

\[ \frac{2\omega L_sI_{dc}}{V_{m(line)}} = 3(0.0214) = 0.0642 \]
\[ \cos\alpha \le -0.9956+0.0642 = -0.9313 \;\Longrightarrow\; \alpha_{max} = 158.6^\circ \]

The ceiling has dropped by 8.4°. A converter operating safely at 167° with 100 A will commutation-fail at the same firing angle if the current rises to 300 — and a regenerating drive's current rises exactly when the braking demand increases.

The failure sequence, and why it is self-worsening:

TriggerEffect on \(\mu\)Effect on \(\gamma\)
Load current risesrisesfalls
Supply voltage dipsrises (smaller \(V_m\) in the denominator)falls
Supply frequency fallsfalls (\(\omega t_q\) is an angle)
Any of the abovecommutation failure

Note the second row: a voltage dip is doubly bad, because it both increases the overlap and reduces the margin available. That is why a network fault elsewhere on the system is the classic cause of commutation failure in an HVDC inverter — and why those terminals monitor \(\gamma\) continuously and retard the firing angle the moment it narrows.

What failure costs. The outgoing thyristor never regains its blocking ability, so:

\[ \text{AC supply short-circuited} + \text{DC source driving current} \;\Rightarrow\; \text{fault current from both} \]

The DC-side inductor, which was there to smooth the current, now maintains the fault current at whatever it was. There is no natural zero crossing to clear it, so the protection must act — either a fast fuse or, in HVDC, retarding the firing to bring the converter briefly back into rectification.

The safe inverting range shrinks as the load grows, which is exactly backwards from what a designer wants. A drive braking hard draws the most current at the moment it needs the largest firing angle. Every inverting converter must therefore compute its firing limit from the measured current rather than fixing it once — which is what a modern controller does, and what a fixed-limit design fails to do.
Answera\(\alpha_{max} = 167.0^\circ\) at 100 A   b absolute limit \(168.1^\circ\)   c\(158.6^\circ\) at 300 A
Problem 6ChallengeA Drive, Fully Accounted

A 415 V six-pulse converter with 0.3 mH of source inductance delivers 150 A at \(\alpha = 25^\circ\). Find the overlap angle and actual output, the displacement and power factors with and without overlap, the real and apparent power, and verify the power balance.

Solution

The overlap angle:

\[ \frac{2\omega L_sI_{dc}}{V_{m(line)}} = \frac{2(314.16)(0.0003)(150)}{586.9} = \frac{28.27}{586.9} = 0.0482 \]
\[ \cos(\alpha+\mu) = \cos25^\circ-0.0482 = 0.9063-0.0482 = 0.8581 \]
\[ \alpha+\mu = 30.9^\circ \;\Longrightarrow\; \mu = 5.9^\circ \]

Output voltage:

\[ \Delta V = \frac{3\omega L_sI_{dc}}{\pi} = \frac{42.41}{\pi} = 13.5\ \text{V} \]
\[ V_{dc} = (560.4)(0.9063)-13.5 = 507.9-13.5 = 494.4\ \text{V} \]
\[ P = (494.4)(150) = 74.2\ \text{kW} \]

The displacement factor, both ways:

\[ \text{without overlap: } \cos\alpha = 0.906; \qquad \text{with: } \cos\left(\alpha+\frac{\mu}{2}\right) = \cos27.9^\circ = 0.884 \]
\[ PF = (0.955)(0.884) = 0.844 \qquad\text{against}\qquad (0.955)(0.906) = 0.865 \]

Overlap has cost 2.4% of power factor. Small here, but it scales with current: at 450 A the overlap would be about 18° and the penalty three times larger.

Verify the power balance, which is the check that confirms the lossless claim of Problem 2:

\[ I_s = I_{dc}\sqrt{\frac23} = 122.5\ \text{A}, \qquad S = \sqrt3\,(415)(122.5) = 88.0\ \text{kVA} \]
\[ PF = \frac{P}{S} = \frac{74.2}{88.0} = 0.843 \]

Against 0.844 from the factor product — agreement to 0.1%, which is as close as the \(\mu/2\) approximation allows. The real power drawn from the supply equals the real power delivered to the load; no energy has disappeared into \(R_c\).

Assemble the full accounting:

QuantityIdeal converterWith overlapChange
Output voltage507.9 V494.4 V−2.7%
Output power76.2 kW74.2 kW−2.7%
Displacement factor0.9060.884−2.4%
Power factor0.8650.844−2.4%
Apparent power88.0 kVA88.0 kVAunchanged
Equivalent \(R_c\)0.09 Ωlossless

Read the last two rows together. The apparent power is unchanged because the RMS line current is set by the DC current alone; the real power fell; therefore the reactive power rose by exactly the difference. That is the whole physical content of the commutation drop.

What a controller must do about it. The drop is a load-dependent, firing-angle-independent error:

\[ V_{dc} = V_{dc0}\cos\alpha-R_cI_{dc} \]

So an open-loop drive will run slower under load than its firing angle suggests, by 13.5 V here on top of the armature \(I_aR_a\) drop. A closed-loop speed controller corrects it automatically; an open-loop one needs an \(IR\)-compensation term with \(R_a+R_c\) in place of \(R_a\).

Overlap turns an ideal voltage source into a Thevenin source, and that is the whole model. One number, \(R_c = 3\omega L_s/\pi\), predicts the regulation, the extra displacement, the notch severity and the inversion limit. It is the single most useful consequence of taking the supply seriously.
Answera\(\mu = 5.9^\circ,\ V_{dc} = 494.4\ \text{V}\)   b\(PF = 0.844\) vs \(0.865\)   c\(74.2\ \text{kW},\ 88.0\ \text{kVA}\)   d\(R_c = 0.09\ \Omega\), lossless
Formulas

Key Formulas

QuantitySingle-phaseThree-phase
Overlap relation\(\cos(\alpha+\mu) = \cos\alpha-\dfrac{2\omega L_sI_{dc}}{V_m}\)same, with \(V_{m(line)}\)
Voltage drop\(\dfrac{2\omega L_sI_{dc}}{\pi}\)\(\dfrac{3\omega L_sI_{dc}}{\pi}\)
Commutation resistance\(R_c = \dfrac{2\omega L_s}{\pi}\)\(R_c = \dfrac{3\omega L_s}{\pi}\)
Symmetric output form\(\dfrac{V_m}{\pi}\left[\cos\alpha+\cos(\alpha+\mu)\right]\)\(\dfrac{3V_{m(l)}}{2\pi}\left[\cos\alpha+\cos(\alpha+\mu)\right]\)
QuantityRelationNotes
Thevenin model\(V_{dc} = V_{dc0}\cos\alpha-R_cI_{dc}\)The whole of Problem 2
Load regulation\(\dfrac{V_{NL}-V_{FL}}{V_{FL}}\)15.5% here
Displacement factor\(\text{DPF} \approx \cos\left(\alpha+\dfrac{\mu}{2}\right)\)Worse than \(\cos\alpha\)
Commutating voltage\(v_{comm} = V_{m(line)}\sin\alpha\)Worst at \(\alpha = 90^\circ\)
Notch depth at PCC\(v_{comm}\dfrac{L_{utility}}{L_{total}}\)Reactor divides it — Problem 4
Notch area at PCC\(2L_{utility}I_{dc}\)Reactor does not reduce this
Extinction angle\(\gamma = 180^\circ-\alpha-\mu\)Overlap eats the margin
Inversion limit\(\cos\alpha \le -\cos\gamma_{min}+\dfrac{2\omega L_sI_{dc}}{V_{m(l)}}\)Falls as current rises
Absolute limit\(\cos\alpha \ge -1+\dfrac{2\omega L_sI_{dc}}{V_{m(l)}}\)Commutation impossible beyond
Power balance\(P_{in} = P_{out}\)\(R_c\) dissipates nothing
Pitfalls

Common Mistakes

  1. Treating \(R_c\) as a real resistance in an efficiency calculation. It drops voltage without dissipating a watt; the “lost” power was never drawn — Problem 2.

  2. Using \(2\omega L_s/\pi\) for a three-phase converter. Six commutations per cycle give \(3\omega L_s/\pi\) — Problem 3.

  3. Assuming three-phase converters suffer less overlap. For the same \(L_s\) their drop is 1.5 times larger; what saves them is the bigger output — Problem 3.

  4. Forgetting that \(\mu\) depends on load current. A converter characterised at rated load has a different overlap at every other operating point — Problem 2.

  5. Ignoring overlap in the displacement factor. DPF is \(\cos(\alpha+\mu/2)\), not \(\cos\alpha\) — Problems 2 and 6.

  6. Believing a line reactor reduces the notch area. It reduces the depth at the PCC; the area is fixed by the utility inductance and the current — Problem 4.

  7. Omitting the line reactor because the converter does not need it. The converter is made slightly worse so the network is made much better — Problem 4.

  8. Using \(\gamma = 180^\circ-\alpha\) in inversion. The overlap consumes part of it, so \(\gamma = 180^\circ-\alpha-\mu\) — Problem 5.

  9. Fixing the inverting firing limit once. It falls as the current rises — 167° at 100 A but 158.6° at 300 A — Problem 5.

  10. Forgetting that a voltage dip is doubly dangerous in inversion. It increases the overlap and reduces the available margin at the same time — Problem 5.

Looking Ahead

Six problems on the consequences of one physical fact: inductor current cannot step. The overlap angle followed from the volt-seconds needed to reverse the supply current; the voltage drop turned out to be a resistance that produces no heat, because what it really represents is a phase shift; the supply notch turned out to be shared between the utility and the converter in proportion to their inductances; and the inversion limit turned out to tighten as the load grows, which is precisely backwards from what a braking drive needs.

Part 2 is nearly complete. What remains is the accounting that all fourteen sets have been circling: the line-current harmonics a converter actually injects, why a capacitor bank cannot correct them and may make things worse, and how two converters in anti-parallel finally deliver the four-quadrant operation that Set 14 showed a single bridge cannot reach.

Next: Set 16 — Power Factor, Harmonics and Dual Converters, where the harmonic spectrum of a phase-controlled converter is computed and set against a capacitor correction that resonates with the fifth, the dual converter is worked in both circulating-current modes with its reactor sized, and the four quadrants are reached at last — closing Part 2.