Solved Problems · Set 14

Three-Phase Controlled Converters and Inverter Mode

Part 2 · AC–DC Converters — the six-pulse bridge with a firing angle, at the power levels where it earns its keep. Six problems on control, ripple, regeneration and the limit beyond which commutation fails.

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

Set 14 — Three-Phase Controlled Converters and Inverter Mode

Set 11 built the six-pulse bridge and found it delivering 95.5% of the line peak with 4.2% ripple. Set 12 added a firing angle to the single-phase bridge and found the output following \(\cos\alpha\). This set combines them, which is the arrangement that actually gets built: virtually every industrial DC drive, electrochemical rectifier and HVDC terminal is a phase-controlled six-pulse bridge or a multiple of one.

Two things change at three phases. The ripple frequency is 300 Hz rather than 100, so the smoothing reactor shrinks and continuous conduction is far easier to hold. And the power levels are large enough that inversion stops being a curiosity and becomes the point — but it brings a hard ceiling on the firing angle, because a line-commutated converter that fails to commutate places a short circuit across the supply.

Part 2 · Chapter 9 · 6 solved problems

i Method Recap
  • The cosine law, on the six-pulse bridge:

    \[ V_{dc} = \frac{3V_{m(line)}}{\pi}\cos\alpha = \frac{3\sqrt3}{\pi}V_{m(ph)}\cos\alpha \]

    And \((3\sqrt3/2\pi)V_{m(ph)}\cos\alpha\) for the three-pulse circuit — exactly half.

  • Device and line currents are unchanged from the diode bridge, because the firing angle moves the conduction window without changing its 120° width:

    \[ I_{T,avg} = \frac{I_{dc}}{3}, \quad I_{T,rms} = \frac{I_{dc}}{\sqrt3}, \quad I_s = I_{dc}\sqrt{\frac23}, \quad I_{s1} = \frac{\sqrt6}{\pi}I_{dc} \]
  • Power factor is the distortion factor times the cosine of the firing angle:

    \[ PF = \frac{3}{\pi}\cos\alpha = 0.955\cos\alpha \]
  • Output ripple grows sharply with \(\alpha\):

    \[ V_{rms} = V_{m(line)}\sqrt{\frac12+\frac{3\sqrt3}{4\pi}\cos2\alpha} \]

    4.2% at \(\alpha = 0\), 53.5% at 60° — Problem 4.

  • Inversion needs \(\alpha > 90^\circ\), and the extinction angle must leave time to commutate:

    \[ \gamma = 180^\circ-\alpha-\mu \ \ge\ \omega t_q+\text{margin} \]
  • Four quadrants need two converters or a reversible field, because thyristor current is always positive:

    \[ V_{dc} = E+I_aR_a\ \text{always}, \qquad \text{power flow set by the sign of } V_{dc} \]
Problem 1CoreThe Six-Pulse Cosine Law

A three-phase full converter on a 415 V, 50 Hz supply feeds a highly inductive load drawing a constant 50 A at \(\alpha = 30^\circ\). Find the output voltage and power, the thyristor currents, the line currents, and the power factor. Confirm the power factor independently.

Vdc 485 587 V α = 30° delay
The firing angle slides the whole envelope later — the average falls and the ripple deepens
Solution

The output. Each conduction interval is delayed by \(\alpha\) from its natural commutation point, and averaging over the 60° window gives the cosine law:

\[ V_{dc} = \frac{3V_{m(line)}}{\pi}\cos\alpha = (560.4)\cos30^\circ = (560.4)(0.866) = 485.4\ \text{V} \]
\[ P = (485.4)(50) = 24.27\ \text{kW} \]

Device currents are unchanged from Set 11. Each thyristor still conducts for 120°, just later:

\[ I_{T,avg} = \frac{50}{3} = 16.7\ \text{A}, \qquad I_{T,rms} = \frac{50}{\sqrt3} = 28.9\ \text{A} \]

Independent of \(\alpha\) — so the devices are rated once for the maximum load current and the firing angle never enters. That simplicity is one of the reasons the full converter, rather than a semiconverter arrangement, dominates at high power.

Line currents, the same 120° quasi-square wave:

\[ I_s = I_{dc}\sqrt{\frac23} = 40.8\ \text{A}, \qquad I_{s1} = \frac{\sqrt6}{\pi}I_{dc} = 39.0\ \text{A} \]
\[ \text{DF} = \frac{39.0}{40.8} = 0.955 = \frac{3}{\pi} \]

The power factor now carries a displacement term:

\[ \text{DPF} = \cos\alpha = 0.866, \qquad PF = (0.955)(0.866) = 0.827 \]
\[ \text{check:}\quad S = \sqrt3\,(415)(40.8) = 29.3\ \text{kVA}, \qquad PF = \frac{24.27}{29.3} = 0.827\ \checkmark \]

Compare the single-phase full converter at the same 30°: 0.780. The three-phase bridge is better because its distortion factor is 0.955 rather than 0.900 — the 60° gaps in the line current make it closer to a sinusoid.

How the control range looks:

\(\alpha\)\(V_{dc}\)PFMode
560.4 V0.955full rectification
30°485.4 V0.827rectifying
60°280.2 V0.477rectifying
90°0 V0no power transfer
150°−485.4 V−0.827inverting

A single gate signal spans \(+560\) to \(-560\) V. Note that the line current is 40.8 A at every one of these points — the converter loads the supply identically whether it is delivering 28 kW or none.

Adding phase control to the six-pulse bridge costs nothing in device rating and everything in displacement. The thyristors carry exactly what the diodes did, the line current keeps its 0.955 distortion factor, and the entire penalty appears as \(\cos\alpha\) — which at 60° has already halved the power factor.
Answera\(485.4\ \text{V},\ 24.27\ \text{kW}\)   b\(16.7\ \text{A},\ 28.9\ \text{A}\)   c\(I_s = 40.8,\ I_{s1} = 39.0\ \text{A}\)   d\(PF = 0.827\)
Problem 2CoreThree Pulses Controlled

The same 415 V supply feeds a three-phase half-wave controlled rectifier with the same 50 A inductive load at \(\alpha = 30^\circ\). Find the output, the device currents, and explain both why the output is exactly half the bridge value and why this circuit is rarely used.

Solution

The three-pulse cosine law, working on phase voltages:

\[ V_{dc} = \frac{3\sqrt3}{2\pi}V_{m(ph)}\cos\alpha = (280.2)(0.866) = 242.7\ \text{V} \]
\[ P = (242.7)(50) = 12.1\ \text{kW} \]

Exactly half the bridge's 485.4 V, and for a structural reason: the bridge stacks an upper group and a lower group in series, each doing the job of one three-pulse converter. Their outputs add.

Device currents are the same as the bridge's, since each thyristor still conducts 120°:

\[ I_{T,avg} = 16.7\ \text{A}, \qquad I_{T,rms} = 28.9\ \text{A} \]

Three devices instead of six — but each carries the same current while delivering half the power. The devices are used half as effectively, which is the first strike against the circuit.

The DC in the supply is the second. Each phase carries current in one direction only:

\[ I_{ph,dc} = \frac{I_{dc}}{3} = 16.7\ \text{A} \]

That DC magnetises the supply transformer's core toward saturation, so the transformer must be oversized or specially connected (zig-zag). The bridge draws symmetric positive and negative blocks and has no such problem.

A third limitation: the control range. With an inductive load the cosine law holds to 90°, but the ripple becomes severe long before that, and the ripple frequency is only 150 Hz:

Property3-pulse6-pulse bridge
\(V_{dc}\) at \(\alpha = 0\)280.2 V560.4 V
Thyristors36
Power per device4.0 kW4.0 kW
Ripple factor at \(\alpha = 0\)18.3%4.2%
Ripple frequency150 Hz300 Hz
Transformer DCyesno
PIV587 V587 V

Same PIV, same power per device, twice the ripple frequency and no core DC — the bridge wins on everything except device count, and device count is the cheapest axis. That is why the three-pulse circuit survives mainly as a teaching step and as half of a bridge.

Where it does appear. Two places, both for specific reasons:

\[ \text{(i) interphase-transformer double-star: two 3-pulse groups in parallel} \]

This doubles the current capability rather than the voltage, which suits very high current, low voltage rectifiers such as electrolysis cells. And (ii) as the upper or lower half of a bridge in fault analysis, where the two groups are treated separately.

A bridge is two three-pulse converters in series. That single observation explains the factor of two in the output, the identical device currents, the identical PIV, and why the DC in the supply cancels — the two groups draw it in opposite directions. Most six-pulse results can be derived by doubling a three-pulse one.
Answera\(242.7\ \text{V},\ 12.1\ \text{kW}\)   b\(16.7\ \text{A},\ 28.9\ \text{A}\)   c half the bridge because a bridge is two such groups in series   d transformer DC and 18.3% ripple
Problem 3Exam levelInverting Into the Grid

A three-phase full converter on the 415 V supply returns 30 kW to the network from a DC source, at a current of 60 A. Find the required output voltage and firing angle, the extinction angle, and check the margin against a thyristor turn-off time of 150 µs. Find the maximum output voltage obtainable if the extinction angle must never fall below 15°.

Solution

Power flows out, so the voltage must reverse. The current is fixed positive by the thyristors:

\[ V_{dc} = -\frac{P}{I_{dc}} = -\frac{30{,}000}{60} = -500\ \text{V} \]

The firing angle:

\[ \cos\alpha = \frac{-500}{560.4} = -0.892 \;\Longrightarrow\; \alpha = 153.1^\circ \]
\[ \gamma = 180^\circ-\alpha = 26.9^\circ \]

The extinction angle \(\gamma\) is the interval between the last firing and the point at which the commutating voltage reverses. It is the time the outgoing thyristor has to regain its blocking ability.

Convert the device requirement into an angle:

\[ \omega t_q = (314.16)\left(150\times10^{-6}\right) = 0.0471\ \text{rad} = 2.70^\circ \]
\[ 26.9^\circ \;\gg\; 2.70^\circ \quad\text{— comfortable} \]

A margin of nearly ten to one. But \(\gamma\) must also cover the commutation overlap angle \(\mu\), which source inductance produces and which Set 15 quantifies — typically 5 to 10° at full load. Even so, 26.9° leaves room.

The maximum inverting voltage, if the control is limited to \(\gamma_{min} = 15^\circ\):

\[ \alpha_{max} = 180^\circ-15^\circ = 165^\circ \]
\[ V_{dc,max} = (560.4)\cos165^\circ = (560.4)(-0.966) = -541.3\ \text{V} \]

So 96.6% of the full DC voltage is available in inversion — the extinction-angle limit costs only 3.4%. That is the usual outcome: the constraint bites hard on the angle but gently on the voltage, because the cosine is flat near 180°.

What commutation failure looks like. If \(\gamma\) falls below the requirement, the outgoing thyristor is still conducting when the supply drives it forward again:

StepWhat happens
1Outgoing device fails to regain blocking
2Two devices in the same leg conduct together
3AC supply is short-circuited through them
4DC source also drives current into the fault — both add
5Fuse operates, or the devices are destroyed

And the failure is self-worsening. A momentary supply dip increases the overlap angle \(\mu\), reducing \(\gamma\) at exactly the moment the margin was already thin. This is why inverting converters are always given a generous \(\gamma_{min}\), and why HVDC terminals monitor it continuously.

The asymmetry worth noticing. Rectification has no equivalent limit:

\[ \text{rectifying: } 0 \le \alpha \le 90^\circ \ \text{— no constraint} \]
\[ \text{inverting: } 90^\circ < \alpha \le 180^\circ-\gamma_{min} \ \text{— hard ceiling} \]

Firing early is always safe; firing late risks the converter. A line-commutated converter is therefore fundamentally safer as a rectifier than as an inverter — and that asymmetry disappears entirely once the switches can turn themselves off, which is the argument for the active front ends of Set 24.

Inversion is limited by the supply, not by the devices. The thyristor needs 2.7° and the design allows 15°, and the difference is entirely margin against overlap and supply disturbance. What the converter is really relying on is that the AC line will reverse on schedule to turn its devices off — which is exactly what a weak or disturbed supply may fail to do.
Answera\(V_{dc} = -500\ \text{V}\)   b\(\alpha = 153.1^\circ,\ \gamma = 26.9^\circ\)   c\(\omega t_q = 2.7^\circ\) — ample   d\(-541.3\ \text{V}\) at \(\alpha = 165^\circ\)
Problem 4Exam levelRipple Against Firing Angle

For the 415 V six-pulse bridge, find the RMS output voltage and the ripple factor at \(\alpha = 0\), 30° and 60°, and explain the consequences for the smoothing reactor of a drive that must operate over that whole range.

Solution

The RMS output as a function of firing angle. Integrating \(v^2\) over one 60° conduction window, delayed by \(\alpha\):

\[ V_{rms} = V_{m(line)}\sqrt{\frac12+\frac{3\sqrt3}{4\pi}\cos2\alpha} \]

Note the \(\cos2\alpha\): the RMS falls much more slowly than the average, which falls as \(\cos\alpha\). That divergence is the whole result.

Evaluate at the three angles:

\(\alpha\)\(V_{dc}\)\(V_{rms}\)Form factorRipple factor
560.4 V560.9 V1.00094.2%
30°485.4 V493.4 V1.016718.3%
60°280.2 V317.8 V1.134153.5%
90°0 V172.6 V
\[ RF = \sqrt{\left(\frac{V_{rms}}{V_{dc}}\right)^2-1} \]

From 4.2% to 53.5% over a firing range of 60°. At \(\alpha = 90^\circ\) the average is zero while the RMS is still 172.6 V — the output is pure ripple.

Why the ripple grows so fast. Two effects compound. The conducting segments are taken from a steeper part of the sine wave, so each is more curved; and the average they are ripple about is falling. The first raises the numerator, the second lowers the denominator:

\[ V_{ac,rms} = \sqrt{V_{rms}^2-V_{dc}^2}: \quad 25.4\ \text{V at }0^\circ, \ 88.7\ \text{V at }30^\circ, \ 149.9\ \text{V at }60^\circ \]

The absolute ripple voltage rises six-fold while the average falls by half — hence the twelve-fold worsening of the ratio.

What this does to the smoothing reactor. The current ripple is the ripple voltage divided by the reactor impedance at 300 Hz:

\[ \Delta I \approx \frac{V_{ac,rms}}{6\omega L} \]

So a reactor sized for acceptable ripple at \(\alpha = 0\) gives six times the ripple at 60°. And since the critical current for continuous conduction rises with ripple — Set 13 — the drive is most likely to go discontinuous at exactly the large firing angles where the ripple is worst.

The design implication:

Size the reactor atConsequence
\(\alpha = 0\) (rated speed)badly undersized at low speed — DCM, poor regulation
Maximum working \(\alpha\)correct, but a larger and costlier reactor
Compromiseaccept DCM at light load, gain-schedule the controller

The middle row is right and the third is what is usually done, because the reactor for \(\alpha = 60^\circ\) is six times the inductance of the one for \(\alpha = 0\). Note that the 300 Hz ripple frequency helps enormously here: the same job in a single-phase drive, at 100 Hz, would need three times the reactance again.

Phase control degrades the output ripple as fast as it degrades the power factor. Both are consequences of the same thing — taking the conducting segments from a steeper part of the waveform — and both are worst at large firing angles, which is where a drive runs when it is doing the least useful work.
Answera\(560.9\ \text{V},\ RF = 4.2\%\)   b\(493.4\ \text{V},\ RF = 18.3\%\)   c\(317.8\ \text{V},\ RF = 53.5\%\)   d reactor must be sized at the largest \(\alpha\)
Problem 5ChallengeA Four-Quadrant Drive

A 415 V six-pulse converter drives a DC motor with \(R_a = 0.2\ \Omega\) and \(K\phi = 4.5\ \text{V}\cdot\text{s/rad}\) at a constant armature current of 100 A. Find the firing angle, speed, torque and power for motoring, then for regenerative braking at the same speed achieved by field reversal, and state what a single converter cannot do.

Solution

Motoring at 500 V output:

\[ \cos\alpha = \frac{500}{560.4} = 0.892 \;\Longrightarrow\; \alpha = 26.9^\circ \]
\[ E = V_{dc}-I_aR_a = 500-(100)(0.2) = 480\ \text{V} \]
\[ \omega = \frac{480}{4.5} = 106.7\ \text{rad/s} = 1019\ \text{rpm} \]

Torque and power:

\[ T = K\phi\,I_a = (4.5)(100) = 450\ \text{N}\!\cdot\!\text{m}, \qquad P_{mech} = T\omega = 48.0\ \text{kW} \]
\[ \text{check: } P_{dc} = (500)(100) = 50.0\ \text{kW}, \quad I_a^2R_a = 2.0\ \text{kW}, \quad 50.0-2.0 = 48.0\ \checkmark \]

Now brake regeneratively at the same speed. Here is the obstacle: the thyristors force \(I_a > 0\), and the machine is still turning the same way, so \(E\) is still \(+480\) V. With both positive, power must flow into the machine, whatever the firing angle.

A single converter cannot reverse the current and cannot reverse the machine's EMF. It can reverse only its own output voltage — which by itself is not enough.

Reverse the field. Reversing \(K\phi\) reverses \(E\) without changing the speed or the direction of rotation:

\[ E = -480\ \text{V}, \qquad V_{dc} = E+I_aR_a = -480+20 = -460\ \text{V} \]
\[ \cos\alpha = \frac{-460}{560.4} = -0.821 \;\Longrightarrow\; \alpha = 145.2^\circ \]
\[ P_{returned} = (460)(100) = 46.0\ \text{kW} \]

The machine generates 48 kW, the armature resistance takes 2 kW, and 46 kW reaches the supply. The braking torque is \(-450\) N·m — full rated torque, in the opposite sense.

The catch with field reversal. The field winding is highly inductive, so its time constant is long:

\[ \tau_f = \frac{L_f}{R_f} \sim 0.5\text{–}2\ \text{s} \]

Compared with an armature time constant of tens of milliseconds. A field-reversal drive therefore takes a second or more to change from motoring to braking, which is fine for a rolling mill and useless for a servo. Worse, the flux passes through zero during the reversal, so torque is momentarily lost entirely.

The four quadrants, and what reaches them:

QuadrantSpeedTorqueSingle converterDual converter
I — forward motoring++yesyes
II — forward braking+field reversal onlyyes, instantly
III — reverse motoringfield reversal onlyyes
IV — reverse braking+noyes

A single converter with field reversal covers three quadrants slowly. Genuine four-quadrant operation at armature speed needs two converters in anti-parallel — one for each current direction — which is the dual converter of Set 16.

A thyristor converter can reverse voltage but never current, and a machine needs both. Field reversal supplies the missing sign at the cost of a second of delay; armature reversal by contactor is worse; a second anti-parallel converter supplies it in milliseconds and is what every fast reversing drive uses.
Answera\(\alpha = 26.9^\circ,\ 1019\ \text{rpm},\ 450\ \text{N}\!\cdot\!\text{m},\ 48\ \text{kW}\)   b\(\alpha = 145.2^\circ,\ 46\ \text{kW}\) returned   c cannot reverse current — needs a dual converter
Problem 6ChallengeA 167 kW Converter

A 415 V six-pulse full converter is to deliver 300 A over a firing range of 0 to 90°. Each thyristor is modelled as \(v_T = 1.2+0.002\,i\), the loop stray inductance is 2 µH, and the device \(di/dt\) rating is 200 A/µs. Find the output and efficiency at \(\alpha = 0\), the device losses and ratings, the \(di/dt\) requirement, and the thermal budget.

Solution

Output at full conduction. Two thyristors are always in the path:

\[ v_T = 1.2+(0.002)(300) = 1.8\ \text{V}, \qquad \Delta V = 2(1.8) = 3.6\ \text{V} \]
\[ V_{dc} = 560.4-3.6 = 556.8\ \text{V}, \qquad P_o = (556.8)(300) = 167.1\ \text{kW} \]

Device currents and losses:

\[ I_{T,avg} = \frac{300}{3} = 100\ \text{A}, \qquad I_{T,rms} = \frac{300}{\sqrt3} = 173.2\ \text{A} \]
\[ P_T = V_{T0}I_{avg}+r_TI_{rms}^2 = (1.2)(100)+(0.002)(30{,}000) = 120+60 = 180\ \text{W} \]
\[ P_{total} = 6(180) = 1080\ \text{W}, \qquad \text{check: } (3.6)(300) = 1080\ \text{W}\ \checkmark \]
\[ \eta = \frac{167{,}100}{167{,}100+1080} = 99.36\% \]

The \(di/dt\) constraint, and why the firing range matters. At turn-on the instantaneous commutating voltage appears across the loop inductance, and it is largest at the largest firing angle:

\[ v_{max} = V_{m(line)} = 586.9\ \text{V}\ \text{at }\alpha = 90^\circ \]
\[ \frac{di}{dt} = \frac{586.9}{2\times10^{-6}} = 293\ \text{A}/\mu\text{s} \;>\; 200\ \text{A}/\mu\text{s} \]
\[ L_{min} = \frac{586.9}{200\times10^{6}} = 2.93\ \mu\text{H} \]

So a small series reactor is needed — about 1 µH added to the existing 2. Note that this constraint is set by the largest firing angle the converter will ever use, not by the operating point: at \(\alpha = 0\) the commutating voltage at turn-on is zero and there is no \(di/dt\) problem at all.

The thermal budget, closing back to Set 8:

\[ R_{th(j-a)} \le \frac{T_{j,max}-T_a}{P_T} = \frac{125-40}{180} = 0.472\ \text{K/W} \]

With a typical \(R_{th(j-c)} = 0.10\) and interface 0.05, the heatsink must reach 0.32 K/W per device — or, for all six on one baseplate carrying 1080 W, roughly 0.06 K/W overall. That is forced air or water at this rating.

The complete specification:

ConstraintRequiredSet by
Blocking voltage587 V peak → 1200 V classline peak, 2× margin
Average current100 Aload / 3
RMS current173.2 Athe binding current limit
Dissipation180 W per deviceboth loss terms
Heatsink0.32 K/W per deviceSet 8 thermal chain
\(di/dt\)2.93 µH totallargest \(\alpha\), not the operating point
\(dv/dt\)RC snubber per deviceSet 4
Fault \(I^2t\)fuse below device ratingSet 4

Six of the eight rows come straight from Part 1. The converter analysis of Part 2 supplies the currents and the voltages; everything that decides whether the devices survive was established before any waveform was drawn.

A converter is specified at its worst operating point on each axis separately, and they are different points. The currents are worst at full load, the blocking voltage at any load, the \(di/dt\) at the largest firing angle, and the commutation margin at the largest inverting angle. Checking everything at one convenient operating point is how converters pass their design review and fail in service.
Answera\(556.8\ \text{V},\ 167.1\ \text{kW},\ \eta = 99.36\%\)   b\(180\ \text{W}\) each, \(1080\ \text{W}\) total   c\(L \ge 2.93\ \mu\text{H}\)   d\(R_{th} \le 0.472\ \text{K/W}\)
Formulas

Key Formulas

QuantityRelationNotes
6-pulse output\(V_{dc} = \dfrac{3V_{m(line)}}{\pi}\cos\alpha\)Continuous conduction
3-pulse output\(V_{dc} = \dfrac{3\sqrt3}{2\pi}V_{m(ph)}\cos\alpha\)Exactly half
Thyristor currents\(I_{dc}/3,\ I_{dc}/\sqrt3\)Independent of \(\alpha\)
Line currents\(I_{dc}\sqrt{2/3},\ \dfrac{\sqrt6}{\pi}I_{dc}\)Same as the diode bridge
Power factor\(PF = \dfrac{3}{\pi}\cos\alpha\)DF is always 0.955
RMS output\(V_{m(line)}\sqrt{\dfrac12+\dfrac{3\sqrt3}{4\pi}\cos2\alpha}\)Note \(\cos2\alpha\) — Problem 4
Ripple factor\(\sqrt{\left(V_{rms}/V_{dc}\right)^2-1}\)4.2% → 53.5% over 0–60°
Ripple frequency\(6f = 300\ \text{Hz}\)Independent of \(\alpha\)
Inverter voltage\(V_{dc} = -P/I_{dc}\)Current stays positive
Extinction angle\(\gamma = 180^\circ-\alpha-\mu\)Must exceed \(\omega t_q\) plus margin
Turn-off angle\(\omega t_q\)2.70° for 150 µs at 50 Hz
Machine equation\(V_{dc} = E+I_aR_a,\ E = K\phi\,\omega\)Holds in all quadrants
Bridge drop\(\Delta V = 2v_T\)Two devices in series
Turn-on \(di/dt\)\(V_{m(line)}\sin\alpha/L\), worst at \(\alpha = 90^\circ\)Problem 6
Pitfalls

Common Mistakes

  1. Using the phase peak in the six-pulse cosine law. It works on line voltages; \(3V_{m(line)}/\pi\) or equivalently \(3\sqrt3\,V_{m(ph)}/\pi\) — Problem 1.

  2. Expecting the device currents to fall as \(\alpha\) rises. Each thyristor conducts 120° at every firing angle — Problem 1.

  3. Assuming a slower drive loads the supply less. The line current is 40.8 A at every operating point in Problem 1's table, including the one delivering zero power.

  4. Forgetting the transformer DC of the three-pulse circuit. Each phase carries \(I_{dc}/3\) one way only — Problem 2.

  5. Believing inversion is limited by the thyristor. \(\omega t_q\) was 2.7° against a 15° design limit; the margin is for overlap and supply disturbance — Problem 3.

  6. Assuming the extinction-angle limit costs a lot of voltage. Restricting \(\alpha\) to 165° still gives 96.6% of full output, because the cosine is flat near 180° — Problem 3.

  7. Using \(\cos\alpha\) in the RMS output formula. The RMS depends on \(\cos2\alpha\) and falls far more slowly than the average — Problem 4.

  8. Sizing the smoothing reactor at \(\alpha = 0\). The ripple is six times worse at 60°, which is where the drive spends its low-speed life — Problem 4.

  9. Expecting a single converter to brake a motor. It can reverse its voltage but not its current, so it needs field reversal or a second converter — Problem 5.

  10. Checking \(di/dt\) at the operating point. It is worst at the largest firing angle the converter can command, not the one it usually uses — Problem 6.

Looking Ahead

Six problems on the converter that actually gets built. The cosine law held on the six-pulse bridge with the device currents unchanged from the diode case; the ripple factor turned out to depend on \(\cos2\alpha\) and worsened twelvefold across the working range; inversion reached 96.6% of full voltage before the extinction angle became the binding constraint; and a four-quadrant requirement proved to need a second converter, because thyristor current has only one sign.

Every one of those results assumed the supply is an ideal voltage source — that current can transfer from one phase to the next instantaneously. It cannot. Real supplies have inductance, commutation takes a finite angle during which two phases are short-circuited together, and the consequences are threefold: the output voltage falls in proportion to load current, the displacement factor worsens beyond \(\cos\alpha\), and the supply voltage itself is notched at the point of common coupling.

Next: Set 15 — Source Inductance and Overlap Angle, where the overlap angle is computed for both single- and three-phase converters, the equivalent commutation resistance that drops voltage without dissipating power is derived, the supply notches are checked against a standard, and the inversion limit of Set 14 is recomputed with the overlap included.