Solved Problems · Set 9

Single-Phase Diode Rectifiers — R and RL Loads

Part 2 · AC–DC Converters — the devices stop being the subject and become the components. Six problems on what an arrangement of diodes does to a sine wave, and on how completely the load changes the answer.

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

Set 9 — Single-Phase Diode Rectifiers — R and RL Loads

Part 1 asked what a switch costs. Part 2 asks what an arrangement of switches produces. The devices are now components with a forward drop and a rating, and the question is the shape of the waveform they make — its average, its RMS, how far apart those two are, and what the supply has to provide to get it.

The recurring lesson is that the load decides the waveform, not the rectifier. The same bridge fed from the same supply produces a smooth 207 V into an inductive load and a rough 207 V into a resistor; put inductance in series and the current stops following the voltage; add a freewheeling path and the output average changes without touching a single device. Problems 3 to 5 are all versions of that one idea.

Part 2 · Chapter 6 · 6 solved problems

i Method Recap
  • Average and RMS of a rectified sine, the two numbers every problem starts from:

    \[ \text{half-wave: } V_{dc} = \frac{V_m}{\pi},\ V_{rms} = \frac{V_m}{2}; \qquad \text{full-wave: } V_{dc} = \frac{2V_m}{\pi},\ V_{rms} = \frac{V_m}{\sqrt2} \]
  • Form and ripple factor measure how far the output is from DC:

    \[ FF = \frac{V_{rms}}{V_{dc}}, \qquad RF = \frac{V_{ac,rms}}{V_{dc}} = \sqrt{FF^2-1} \]
  • Rectification efficiency and transformer utilisation compare useful DC against what the source supplies:

    \[ \eta = \frac{P_{dc}}{P_{ac}} = \frac{V_{dc}I_{dc}}{V_{rms}I_{rms}}, \qquad TUF = \frac{P_{dc}}{V_sI_s} \]
  • With an RL load the current outlasts the voltage. It flows until the extinction angle \(\beta\), found from:

    \[ \sin(\beta-\phi)+\sin\phi\;e^{-\beta/\tan\phi} = 0, \qquad \phi = \tan^{-1}\frac{\omega L}{R} \]

    A transcendental equation — solve it numerically — Problem 3.

  • A freewheeling diode blocks the negative excursion and restores the resistive-load average:

    \[ V_{dc} = \frac{V_m}{\pi}\ \text{regardless of }L \]
  • A highly inductive load makes the source current a square wave, whose harmonics follow immediately:

    \[ I_{s1} = \frac{4I_{dc}}{\pi\sqrt2}, \qquad THD = \sqrt{\left(\frac{I_s}{I_{s1}}\right)^2-1}, \qquad PF = \frac{I_{s1}}{I_s}\cos\phi_1 \]
Problem 1CoreHalf-Wave, Resistive

A single diode supplies a resistive load of \(R = 20\ \Omega\) from a 230 V, 50 Hz supply. Find:

  1. the average and RMS output voltages and currents;
  2. the form factor and ripple factor;
  3. the rectification efficiency;
  4. the transformer utilisation factor and the peak inverse voltage.
325 V Vrms 163 Vdc 104 no conduction
Half the cycle delivers nothing — which is why the RMS is 1.57 times the average
Solution

Start from the peak. Every quantity in a rectifier problem is a fraction of \(V_m\):

\[ V_m = \sqrt2\,(230) = 325.3\ \text{V} \]

Average output. The integral runs over the conducting half only, but is divided by the whole period:

\[ V_{dc} = \frac{1}{2\pi}\int_0^\pi V_m\sin\theta\,d\theta = \frac{V_m}{\pi} = 103.5\ \text{V} \]
\[ I_{dc} = \frac{103.5}{20} = 5.18\ \text{A} \]

RMS output. Square first, then average over the whole period — the half-cycle of zeros halves the mean square:

\[ V_{rms} = \sqrt{\frac{1}{2\pi}\int_0^\pi V_m^2\sin^2\theta\,d\theta} = \frac{V_m}{2} = 162.6\ \text{V} \]
\[ I_{rms} = \frac{162.6}{20} = 8.13\ \text{A} \]

Compare with the full sine's \(V_m/\sqrt2 = 230\) V. Removing half the cycle divides the mean square by two, hence the RMS by \(\sqrt2\) — the same \(\sqrt{D}\) scaling as Set 1.

Form and ripple factor:

\[ FF = \frac{V_{rms}}{V_{dc}} = \frac{V_m/2}{V_m/\pi} = \frac{\pi}{2} = 1.571 \]
\[ RF = \sqrt{FF^2-1} = \sqrt{2.467-1} = 1.211 \]

Both are pure numbers, independent of the supply voltage and the load — they are properties of the waveform shape. A ripple factor above unity means the AC content exceeds the DC content, so this is a very poor DC supply.

Rectification efficiency — the fraction of the delivered power that is genuinely DC:

\[ \eta = \frac{P_{dc}}{P_{ac}} = \frac{V_{dc}I_{dc}}{V_{rms}I_{rms}} = \frac{(103.5)(5.18)}{(162.6)(8.13)} = \frac{536}{1322} = 40.5\% \]

The famous 40.5%, and note what it is not: no energy is lost here at all, since the diode is ideal and the load is a resistor that receives all 1322 W. The 59.5% is delivered as ripple rather than as DC — useful for a heater, useless for anything needing a steady voltage.

Transformer utilisation factor compares the DC output against the VA the transformer must be rated for:

\[ TUF = \frac{P_{dc}}{V_sI_s} = \frac{536}{(230)(8.13)} = \frac{536}{1870} = 0.287 \]
\[ \text{PIV} = V_m = 325.3\ \text{V} \]

A transformer must be rated at 3.5 times the DC power delivered. Worse, the secondary carries a DC component that saturates the core — which is the practical reason half-wave rectifiers are not used above a few watts, quite apart from the ripple.

Four figures of merit, all measuring the same defect from different angles. The form factor says the waveform is peaky, the ripple factor says the AC dominates, the efficiency says most of the power is not DC, and the TUF says the transformer is oversized. All four follow from one fact: the diode conducts for half the time.
Answera\(103.5\ \text{V},\ 162.6\ \text{V},\ 5.18\ \text{A},\ 8.13\ \text{A}\)   b\(FF = 1.571,\ RF = 1.211\)   c\(\eta = 40.5\%\)   d\(TUF = 0.287,\ \text{PIV} = 325\ \text{V}\)
Problem 2CoreThe Bridge Compared

The same supply and the same \(20\ \Omega\) load are now fed from a full-wave bridge. Find all the same quantities, the current ratings of each diode, and tabulate the comparison with the half-wave circuit.

Solution

Both half-cycles now reach the load, so the integral covers the whole period:

\[ V_{dc} = \frac{2V_m}{\pi} = \frac{2(325.3)}{\pi} = 207.1\ \text{V}, \qquad I_{dc} = 10.35\ \text{A} \]
\[ V_{rms} = \frac{V_m}{\sqrt2} = 230\ \text{V}, \qquad I_{rms} = 11.5\ \text{A} \]

The RMS output equals the supply RMS exactly, because rectification does not change the magnitude of anything — it only folds the negative half up. Squaring is blind to sign, so the mean square is untouched.

Form and ripple factor:

\[ FF = \frac{230}{207.1} = 1.111, \qquad RF = \sqrt{1.234-1} = 0.483 \]

The ripple factor falls from 1.211 to 0.483 — a factor of 2.5 — purely because the gaps have been filled. The ripple frequency also doubles to 100 Hz, which makes any subsequent filter smaller for a second, independent reason.

Rectification efficiency:

\[ \eta = \frac{(207.1)(10.35)}{(230)(11.5)} = \frac{2143}{2645} = 81.1\% \]

Exactly twice the half-wave figure, and equal to \(8/\pi^2\). This is the theoretical ceiling for an unfiltered full-wave rectifier.

Each diode carries half the job. With four diodes conducting in opposite pairs, each sees the load current for one half cycle:

\[ I_{D,avg} = \frac{I_{dc}}{2} = 5.18\ \text{A}, \qquad I_{D,rms} = \frac{I_{rms}}{\sqrt2} = 8.13\ \text{A} \]
\[ \text{PIV} = V_m = 325.3\ \text{V} \]

Note the PIV: for a bridge it is \(V_m\), because the two conducting diodes clamp the blocked pair to the supply. For a centre-tapped rectifier it is \(2V_m\), and confusing the two doubles the device cost.

The comparison, side by side:

QuantityHalf-waveBridgeRatio
\(V_{dc}\)103.5 V207.1 V2.00
\(V_{rms}\)162.6 V230 V1.41
Form factor1.5711.1110.71
Ripple factor1.2110.4830.40
Efficiency40.5%81.1%2.00
Ripple frequency50 Hz100 Hz2.00
Diodes14
DC in transformeryesno

Four diodes instead of one, for double the voltage, half the ripple, twice the ripple frequency and no core saturation. Since Part 1 showed a diode costs a couple of watts and a transformer costs kilograms, this trade is never close.

The bridge wins on every axis except device count, and device count is the cheapest axis. That is the whole reason half-wave rectification survives only in very low-power or cost-critical corners — and why the rest of this part is about the bridge and its three-phase relatives.
Answera\(207.1\ \text{V},\ 230\ \text{V}\)   b\(FF = 1.111,\ RF = 0.483\)   c\(\eta = 81.1\%\)   d\(5.18\ \text{A},\ 8.13\ \text{A},\ \text{PIV} = 325\ \text{V}\)
Problem 3Exam levelWhen the Load Has Inductance

A single diode feeds \(R = 10\ \Omega\) in series with \(L = 20\) mH from the same 230 V, 50 Hz supply. Find the load impedance angle, the extinction angle, the average output voltage and current, and explain why the average is lower than the resistive case.

180° β negative area subtracts vo io current lags
The inductor keeps the current flowing past the zero crossing, dragging the output negative
Solution

The load impedance:

\[ \omega L = (314.16)(0.020) = 6.283\ \Omega, \qquad Z = \sqrt{10^2+6.283^2} = 11.81\ \Omega \]
\[ \phi = \tan^{-1}\frac{6.283}{10} = 32.14^\circ = 0.561\ \text{rad} \]

The current cannot stop at 180°. An inductor's current is continuous, so when the supply reverses, the stored energy keeps the diode conducting and drives current against the negative supply. The current is the sum of a steady-state sinusoid and a decaying transient:

\[ i(\theta) = \frac{V_m}{Z}\left[\sin(\theta-\phi)+\sin\phi\;e^{-\theta/\tan\phi}\right] \]

The exponential term exists precisely because the current must start from zero at \(\theta = 0\), where the steady-state term alone would give \(-\sin\phi\).

The extinction angle is where that expression returns to zero:

\[ \sin(\beta-\phi)+\sin\phi\;e^{-\beta/\tan\phi} = 0 \]

This is transcendental — there is no closed form. Solving numerically with \(\phi = 0.561\) and \(\tan\phi = 0.6283\):

\[ \beta = 3.704\ \text{rad} = 212.2^\circ \]

So the diode conducts for 212° instead of 180° — an extra 32°, all of it into the negative half cycle. Note that \(\beta\) depends only on \(\phi\), not on the supply voltage: a more inductive load extends conduction, a larger supply does not.

The average output voltage, integrating the supply over the whole conduction window including the negative part:

\[ V_{dc} = \frac{1}{2\pi}\int_0^\beta V_m\sin\theta\,d\theta = \frac{V_m}{2\pi}\left(1-\cos\beta\right) \]
\[ = \frac{325.3}{6.283}\left(1-\cos212.2^\circ\right) = (51.77)(1.846) = 95.6\ \text{V} \]
\[ I_{dc} = \frac{95.6}{10} = 9.56\ \text{A} \]

Why the average fell. With a resistive load the same circuit would give \(V_m/\pi = 103.5\) V. The inductance has cost 7.9 V, or 7.6%:

\[ \text{negative area} \propto \left|1+\cos\beta\right|\quad\text{subtracts from the positive area} \]

The extra 32° of conduction happens while the supply is negative, so it contributes negative volt-seconds to the average. The inductor is returning stored energy to the source. The load current is smoother than the resistive case — which is what the inductance was for — but the mean voltage is lower.

The RMS current, which is what actually rates the diode, must be found by integrating the current expression numerically:

\[ I_{rms} = \sqrt{\frac{1}{2\pi}\int_0^\beta i^2(\theta)\,d\theta} = 14.4\ \text{A} \]

Against an average of 9.56 A, a form factor of 1.51 — still peaky, because 20 mH is nowhere near enough to smooth a 50 Hz waveform. Genuine smoothing needs \(\omega L \gg R\), i.e. hundreds of millihenries here.

Inductance buys current smoothness and pays in average voltage. Every joule the inductor returns during the negative excursion is a joule that never reached the load, and the transaction shows up directly as a lower \(V_{dc}\). Problem 4 shows how to keep the smoothing and refuse the bill.
Answera\(Z = 11.81\ \Omega,\ \phi = 32.1^\circ\)   b\(\beta = 212.2^\circ\)   c\(V_{dc} = 95.6\ \text{V},\ I_{dc} = 9.56\ \text{A}\)   d negative volt-seconds subtract 7.6%
Problem 4Exam levelThe Freewheeling Diode

A freewheeling diode is connected across the \(RL\) load of Problem 3. Find the new average output voltage and current, the current ratings of both diodes assuming the inductance is large enough to hold the current constant, and quantify the improvement.

Solution

What the freewheeling diode does. The moment the supply tries to go negative, the output node would fall below zero — but that forward-biases the freewheeling diode, which clamps the load to 0 V and offers the inductor current a path that does not involve the source.

The inductor still gets to run its current down gradually; it just does so in a local loop rather than by pushing against the supply.

The output voltage is now the resistive-load waveform, whatever the inductance:

\[ V_{dc} = \frac{V_m}{\pi} = 103.5\ \text{V}, \qquad I_{dc} = \frac{103.5}{10} = 10.35\ \text{A} \]
\[ \text{improvement} = \frac{103.5-95.6}{95.6} = 8.3\% \]

The result is independent of \(L\) entirely, which is the striking part. The inductance now affects only the smoothness of the current, not the average voltage — the two properties have been decoupled by one diode.

Device currents with large inductance. If \(\omega L \gg R\) the load current is essentially constant at 10.35 A, and the two diodes simply take turns:

DeviceConducts\(I_{avg}\)\(I_{rms}\)
Main diode0 to 180°5.18 A7.32 A
Freewheeling diode180 to 360°5.18 A7.32 A
\[ I_{avg} = \frac{I_{dc}}{2} = 5.18\ \text{A}, \qquad I_{rms} = \frac{I_{dc}}{\sqrt2} = 7.32\ \text{A} \]

Both diodes need the same rating, and it is set by the RMS, not the average — the Set 2 lesson reappearing. Note also that the freewheeling diode carries current for half of every cycle even though it delivers no power, so it needs a real heatsink.

What changed and what did not:

QuantityWithout FWDWith FWD
Conduction of main diode212°180°
Output goes negativeyes, for 32°never
\(V_{dc}\)95.6 V103.5 V
Depends on \(L\)?yes, stronglyno
Load current ripplelargefalls as \(L\) rises
Energy returned to sourceyesno — recirculated

The last row is the mechanism behind all the others. Without the freewheeling path the inductor's stored energy has nowhere to go but back into the supply; with it, that energy circulates through the load and is delivered rather than returned.

One diode decouples two properties that were previously linked. Before it, more inductance meant smoother current and lower output. After it, inductance buys smoothness for free. This is the same trick as the buck converter's freewheeling path in Set 1 — and it is why almost every rectifier feeding an inductive load has one.
Answera\(V_{dc} = 103.5\ \text{V},\ I_{dc} = 10.35\ \text{A}\)   b each diode \(5.18\ \text{A}\) avg, \(7.32\ \text{A}\) rms   c 8.3% higher output, independent of \(L\)
Problem 5Exam levelWhat the Supply Sees

A bridge rectifier feeds a highly inductive load drawing a constant 20 A from the 230 V, 50 Hz supply. Find the DC output and power, the RMS and fundamental supply currents, the total harmonic distortion, the displacement and distortion factors, and the power factor.

Solution

The output side is simple:

\[ V_{dc} = \frac{2V_m}{\pi} = 207.1\ \text{V}, \qquad P_{dc} = (207.1)(20) = 4141\ \text{W} \]

The input current is a square wave. Since the load current is constant and the bridge simply reverses which pair of diodes carries it, the supply sees \(+20\) A for one half cycle and \(-20\) A for the next:

\[ I_s = I_{dc} = 20\ \text{A}\quad\text{(RMS of a square wave = its amplitude)} \]

Its fundamental comes straight from the Fourier series of a square wave, whose fundamental amplitude is \(4/\pi\) times the level:

\[ I_{s1} = \frac{4I_{dc}}{\pi\sqrt2} = \frac{4(20)}{\pi\sqrt2} = 18.01\ \text{A} \]

Distortion follows from the ratio of the two:

\[ THD = \sqrt{\left(\frac{I_s}{I_{s1}}\right)^2-1} = \sqrt{\left(\frac{20}{18.01}\right)^2-1} = \sqrt{0.2337} = 48.3\% \]
\[ \text{distortion factor} = \frac{I_{s1}}{I_s} = \frac{18.01}{20} = 0.900 = \frac{2\sqrt2}{\pi} \]

A pure number set by the waveform shape alone. Note also that \(48.3\%\) is numerically identical to the bridge's voltage ripple factor from Problem 2 — not a coincidence, since both measure the non-fundamental content of a square-edged waveform.

Displacement, and why it is unity here:

\[ \text{DPF} = \cos\phi_1 = \cos 0^\circ = 1 \]

The current square wave is centred on the voltage sine, because diodes commutate at the zero crossings and have no way to delay. Everything degrading the power factor here is distortion, none of it is displacement — which is exactly the distinction that will separate diode rectifiers from the controlled converters of Set 12.

The power factor, and a check:

\[ PF = \frac{I_{s1}}{I_s}\cos\phi_1 = (0.900)(1) = 0.900 \]
\[ \text{check:}\quad PF = \frac{P}{S} = \frac{4141}{(230)(20)} = \frac{4141}{4600} = 0.900\ \checkmark \]

A power factor of 0.9 with a completely resistive-looking load, caused entirely by harmonics that carry no average power at all. The 5th and 7th harmonics circulate, heat the supply transformer and distort the voltage at the point of common coupling — and they are the reason standards exist for this.

A diode bridge draws its current in phase and in the wrong shape. Displacement is perfect and distortion is poor, so the only route to a better power factor is to change the shape of the current — which no arrangement of diodes can do, and which is the entire motivation for the power-factor correction stage of Set 24.
Answera\(207.1\ \text{V},\ 4141\ \text{W}\)   b\(I_s = 20\ \text{A},\ I_{s1} = 18.01\ \text{A}\)   c\(THD = 48.3\%\)   d\(\text{DPF} = 1,\ PF = 0.900\)
Problem 6ChallengeA Rectifier Feeding a Motor

A bridge rectifier supplies a separately excited DC motor from the 230 V, 50 Hz supply. The armature resistance is \(0.5\ \Omega\), the armature inductance is large enough to hold the current constant, and the back EMF is 180 V. Each diode is modelled as \(v_F = 0.85+0.005\,i\). Find:

  1. the armature current predicted by an ideal analysis;
  2. the true armature current, allowing for the diode drops;
  3. the diode currents and total rectifier loss;
  4. the power split between mechanical output and armature heating.
Solution

The ideal answer first, so we can see what the drops cost:

\[ I_a = \frac{V_{dc}-E}{R_a} = \frac{207.1-180}{0.5} = \frac{27.1}{0.5} = 54.1\ \text{A} \]

Notice the sensitivity: the numerator is a small difference between two large numbers. A 1% error in \(V_{dc}\) is 2 V, which is 7.6% of the 27 V driving the current. Any approximation in the rectifier model is amplified enormously by the back EMF.

Now include the diodes. Two are always in the conduction path, and their drop depends on the current, which depends on the drop:

\[ I_a = \frac{V_{dc}-2v_F(I_a)-E}{R_a}, \qquad v_F = 0.85+0.005I_a \]

Iterating from the ideal value:

PassAssumed \(I_a\)\(v_F\)New \(I_a\)
154.1 A1.121 V49.66 A
249.66 A1.098 V49.75 A
349.75 A1.099 V49.75 A
\[ I_a = 49.75\ \text{A} \]

The ideal calculation overstated the current by 8.8%, from a rectifier drop of only 2.2 V out of 207 — a 1.1% error in voltage amplified eightfold. This is why a motor drive must never be analysed with an ideal rectifier model.

Diode currents and loss. Each conducts for half the cycle at the constant armature current:

\[ I_{D,avg} = \frac{49.75}{2} = 24.9\ \text{A}, \qquad I_{D,rms} = \frac{49.75}{\sqrt2} = 35.2\ \text{A} \]
\[ P_D = V_0I_{avg}+r_dI_{rms}^2 = (0.85)(24.9)+(0.005)(1237) = 21.1+6.2 = 27.3\ \text{W} \]
\[ P_{rectifier} = 4(27.3) = 109\ \text{W} \]

Cross-check the loss against the voltage drop, which must give the same answer:

\[ P = \left(2v_F\right)I_a = (2.198)(49.75) = 109\ \text{W}\ \checkmark \]

Two independent routes agreeing — per-device summation and terminal drop times current — confirms both the iteration and the current split.

Where the power goes:

\[ V_{dc,actual} = 207.1-2.198 = 204.9\ \text{V}, \qquad P_{motor} = (204.9)(49.75) = 10.19\ \text{kW} \]
DestinationExpressionPower
Mechanical (via back EMF)\(EI_a\)8.955 kW
Armature copper loss\(I_a^2R_a\)1.238 kW
Rectifier conduction\(2v_FI_a\)0.109 kW
Total from supply\(V_{dc}I_a\)10.30 kW

The rectifier costs 1.1% and the armature resistance costs 12%. Which is worth noticing: the power electronics is nearly free compared with the machine it feeds, and the 27 V across \(R_a\) that sets the current is also 1.24 kW of pure heat.

A back EMF turns a rectifier into a difference amplifier. The current is set by the small gap between the rectifier output and the machine's EMF, so every volt of error in the rectifier model becomes several per cent of error in the current, the torque and the loss. That sensitivity is also the opportunity: it means a modest change in firing angle gives fine control of the current, which is exactly what Set 12 exploits.
Answera\(54.1\ \text{A}\) ideal   b\(49.75\ \text{A}\) actual, 8.8% lower   c\(24.9/35.2\ \text{A},\ 109\ \text{W}\)   d\(8.955\ \text{kW}\) mechanical, \(1.238\ \text{kW}\) copper
Formulas

Key Formulas

QuantityHalf-waveBridge
Average output\(V_m/\pi\)\(2V_m/\pi\)
RMS output\(V_m/2\)\(V_m/\sqrt2\)
Form factor\(\pi/2 = 1.571\)1.111
Ripple factor1.2110.483
Efficiency40.5%81.1%
Ripple frequency\(f\)\(2f\)
PIV\(V_m\)\(V_m\) (\(2V_m\) centre-tapped)
TUF0.2870.812
QuantityRelationNotes
Ripple factor\(RF = \sqrt{FF^2-1}\)Shape only, not amplitude
Load angle\(\phi = \tan^{-1}\left(\omega L/R\right)\)Problem 3
Extinction angle\(\sin(\beta-\phi)+\sin\phi\,e^{-\beta/\tan\phi} = 0\)Solve numerically
RL half-wave output\(V_{dc} = \dfrac{V_m}{2\pi}\left(1-\cos\beta\right)\)Below the R-load value
With freewheeling diode\(V_{dc} = V_m/\pi\)Independent of \(L\) — Problem 4
Inductive-load device currents\(I_{avg} = I_{dc}/2,\ I_{rms} = I_{dc}/\sqrt2\)Square pulses
Square-wave fundamental\(I_{s1} = \dfrac{4I_{dc}}{\pi\sqrt2}\)Problem 5
Distortion factor\(I_{s1}/I_s = 2\sqrt2/\pi = 0.900\)Bridge with inductive load
Power factor\(PF = \dfrac{I_{s1}}{I_s}\cos\phi_1\)DPF = 1 for diodes
Motor armature current\(I_a = \dfrac{V_{dc}-2v_F-E}{R_a}\)Iterate — Problem 6
Pitfalls

Common Mistakes

  1. Dividing the half-wave integral by \(\pi\) instead of \(2\pi\). The average is taken over the whole period, including the half in which nothing happens — Problem 1.

  2. Reading 40.5% as an energy loss. No energy is lost in an ideal rectifier; the figure says only that 59.5% of the delivered power is ripple rather than DC — Problem 1.

  3. Quoting a bridge PIV as \(2V_m\). That is the centre-tapped figure. A bridge diode blocks \(V_m\) — Problem 2.

  4. Assuming an RL load raises the output. It lowers it, because the extra conduction happens while the supply is negative — Problem 3.

  5. Looking for a closed form for the extinction angle. There is none; the equation is transcendental and must be solved numerically — Problem 3.

  6. Thinking the freewheeling diode changes the output only when \(L\) is large. It fixes \(V_{dc}\) at \(V_m/\pi\) for any inductance — Problem 4.

  7. Under-rating the freewheeling diode. It carries the load current for half of every cycle and delivers no power, but it heats exactly as much as the main diode — Problem 4.

  8. Confusing distortion with displacement. A diode bridge has DPF = 1 and a power factor of 0.9; every bit of the shortfall is harmonic content — Problem 5.

  9. Taking the RMS of a square wave as amplitude over \(\sqrt2\). That is for a sine. A square wave's RMS equals its amplitude — Problem 5.

  10. Using an ideal rectifier model with a back EMF. The current comes from a small difference, so a 1% voltage error became an 8.8% current error — Problem 6.

Looking Ahead

Six problems, and the load turned out to matter more than the rectifier. The same bridge produced a ripple factor of 0.483 into a resistor, a square input current into an inductor, and an output that fell by 8% when inductance was added without a freewheeling path. The devices themselves contributed one number each — a forward drop — and in Problem 6 that number moved the answer by 8.8%.

What no load in this set did was store energy in a capacitor. Put one across the output and the whole character changes: the diodes stop conducting for half the cycle and start conducting in brief spikes near the peak, the output rises towards \(V_m\) instead of \(2V_m/\pi\), and the supply current — which was a well-behaved square wave here, at 0.9 power factor — becomes a narrow pulse train with a power factor closer to 0.3.

Next: Set 10 — Capacitor-Filtered Rectifiers and Ripple, where the ripple voltage is found from charge balance, the conduction angle and peak diode current from the geometry, and the crest factor and harmonic content are set against what a supply standard will actually permit.