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22-Elec-B8 Power Electronics and Drives · December 2016

Question 2 of 6: SCR Turn-Off Time, and a Half-Wave Controlled Rectifier with an Inductive Load

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Exams, December 2016 — 07-Elec-B8 Power Electronics and Drives. Open-book, 3 hours, six problems (PROBLEM 1–6) of equal value; the rubric marks only the first five answered. Every problem is solved here, because the set is intended as a study resource.

Reference texts. M. H. Rashid, Power Electronics: Circuits, Devices and Applications, 4th ed. (the EGBC-recommended primary reference for this code); N. Mohan, T. Undeland and W. Robbins, Power Electronics: Converters, Applications and Design, 3rd ed.; B. K. Bose, Modern Power Electronics and AC Drives; R. Krishnan, Electric Motor Drives: Modeling, Analysis and Control.

Conventions used throughout. Angles are electrical degrees measured from the positive-going zero crossing of the supply. For a phase-controlled converter feeding an R–L load the load angle is $\varphi=\tan^{-1}(X/R)=\cos^{-1}(\mathrm{pf})$, the delay angle is $\alpha$, the extinction angle is $\beta$ and the conduction angle is $\gamma=\beta-\alpha$.

Question 2: SCR Turn-Off Time, and a Half-Wave Controlled Rectifier with an Inductive Load (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Part (a) — Five factors that lengthen the turn-off interval of an SCR

The turn-off interval of a thyristor — the circuit-commutated turn-off time $t_q$ — is the minimum time for which the device must be held at reverse or zero voltage after its anode current has fallen to zero before forward voltage may safely be re-applied. It is not a fixed catalogue number but a strong function of how the device is being operated, and a converter design that ignores that dependence commutation-fails in service even though the data-sheet number looked adequate.

1. The magnitude of the forward current before commutation. The stored charge in the lightly doped base regions grows with the on-state current, and every one of those excess carriers must recombine or be swept out before the blocking junction can support forward voltage. A device commutated from full rated current has a measurably longer $t_q$ than the same device commutated from a light load, which is why $t_q$ is always quoted with the test current.

2. The rate of fall of anode current at commutation. A steep $-\mathrm{d}i/\mathrm{d}t$ forces a large reverse-recovery current and leaves the remaining charge distributed deep in the base, where the reverse field reaches it poorly. A gentler current slope allows more of the charge to recombine in place and shortens the recovery. Commutating-circuit inductance is therefore a design variable, not an incidental parasitic.

3. The magnitude of the reverse voltage applied during the recovery interval. Reverse bias actively sweeps carriers out of the junction region. A generous reverse voltage shortens turn-off; a circuit that applies only a volt or two of reverse bias — or none at all, merely holding the device at zero — leaves recombination as the only removal mechanism and can double the effective time required.

4. Junction temperature. Carrier lifetime in silicon increases markedly with temperature, so recombination slows and $t_q$ rises — typically by a factor of roughly two between 25 °C and the 125 °C rated junction temperature. Turn-off time must therefore be evaluated at the hottest credible operating point, not at ambient, and adequate heat-sinking is part of the commutation design.

5. The rate of re-applied forward voltage, and the gate condition. Even after the charge has cleared, a forward $\mathrm{d}v/\mathrm{d}t$ above the device rating injects enough displacement current through the junction capacitance to re-trigger conduction, so the practical turn-off interval is whatever time the circuit needs to keep the device inside its $\mathrm{d}v/\mathrm{d}t$ limit as well as clear of charge. A negative gate bias during recovery extracts carriers from the gate region and shortens the interval; a floating or positive gate lengthens it. Device construction sits behind all five factors: lifetime control by gold doping or electron irradiation produces fast inverter-grade thyristors with $t_q$ of 10–50 µs at the price of higher on-state voltage drop, whereas converter-grade devices intended for 50/60 Hz line commutation may need 100–200 µs.

Parts (b) and (c) — Delay angle, load resistance, and mean output current

Given. A single-thyristor (half-wave) controlled rectifier is supplied from 120 V rms and feeds a series R–L load whose power factor is 0.707; two operating points are specified, one by conduction angle and mean current, the other by conduction angle and resistance.

Given data
QuantitySymbolValue
Supply voltage (rms)$V_s$120 V
Supply peak$V_m$169.71 V
Load power factor$\cos\varphi$0.707
Case (b): conduction angle$\gamma_b$147°
Case (b): mean output current$I_{\text{dc}}$25 A
Case (c): conduction angle$\gamma_c$152°
Case (c): load resistance$R$1.1 Ω

Find. The delay angle at each conduction angle, the resistance that makes the mean current 25 A in case (b), and the mean current that results from $R=1.1\ \Omega$ in case (c).

180°α = 75.75°β = 222.75°γ = 147° (α = 75.75°)γ = 152° (α = 71.22°)supplyωtvnegative area: L returnsstored energy
Figure 2.1 — Half-wave controlled rectifier output at the two specified conduction angles. In both cases the load inductance holds the thyristor in conduction past the 180° zero crossing, so part of the output waveform is negative — that is the stored magnetic energy being returned to the supply.

Approach. The extinction condition of Question 1 applies unchanged, because the conduction interval of a half-wave rectifier is governed by the same differential equation; only the averaging interval differs. Solve it for $\alpha$ at each $\gamma$, then integrate the normalised current over one full cycle and use the power factor to convert between $Z$ and $R$.

  1. Load angle from the power factor. $$\varphi=\cos^{-1}(0.707)=45.01^\circ,\qquad \tan\varphi=1.0004 ,$$ so this load is very nearly the classic $X=R$ case; the reactance and the resistance will come out equal to three figures.
  2. Delay angle for $\gamma=147^\circ$. Substituting into $$\sin(\alpha+\gamma-\varphi)=\sin(\alpha-\varphi)e^{-\gamma/\tan\varphi}$$ and solving numerically, $$\boxed{\alpha_b=75.75^\circ},\qquad \beta_b=\alpha_b+\gamma_b=222.75^\circ .$$ The extinction angle exceeds 180° by nearly 43°, confirming that the inductance is doing substantial work.
  3. Average the current over the whole cycle. A half-wave rectifier delivers one pulse per supply period, so $$I_{\text{dc}}=\frac{1}{2\pi}\int_{\alpha}^{\beta}i\,\mathrm{d}(\omega t) =\frac{V_m}{2\pi Z}\int_{\alpha}^{\beta}u\,\mathrm{d}(\omega t),$$ with $u$ the same normalised waveform as before. Numerically $\int u=1.38662$ for this window.
  4. Solve for the resistance. Substituting $Z=R/\cos\varphi$ and rearranging for $R$, $$R=\frac{V_m\cos\varphi}{2\pi I_{\text{dc}}}\int_{\alpha}^{\beta}u\,\mathrm{d}(\omega t) =\frac{169.71\times0.707}{2\pi\times25}\times1.38662,$$ $$\boxed{R=1.059\ \Omega},\qquad Z=1.498\ \Omega,\qquad X_L=1.059\ \Omega .$$
  5. Delay angle for $\gamma=152^\circ$. Re-solving the extinction condition with the new conduction angle, $$\boxed{\alpha_c=71.22^\circ},\qquad \beta_c=223.22^\circ .$$ Firing 4.5° earlier buys 5° of extra conduction, and the extinction angle barely moves: once the load is strongly inductive, $\beta$ is far more stable than $\alpha$.
  6. Mean current at the new operating point. The window integral becomes $\int u=1.48593$, and with the stated $R=1.1\ \Omega$, $$I_{\text{dc}}=\frac{V_m\cos\varphi}{2\pi R}\int_{\alpha}^{\beta}u\,\mathrm{d}(\omega t) =\frac{169.71\times0.707}{2\pi\times1.1}\times1.48593,$$ $$\boxed{I_{\text{dc}}=25.80\ \text{A}} .$$
  7. Check both answers against the mean output voltage. The inductor can support no average voltage, so the mean load voltage must equal $I_{\text{dc}}R$ exactly. Evaluating the rectifier expression directly, $$V_{\text{dc}}=\frac{V_m}{2\pi}\left(\cos\alpha-\cos\beta\right):\qquad 26.479\ \text{V}=25\times1.0591,\quad 28.375\ \text{V}=25.795\times1.1 .$$ Both close to six figures, which validates the delay angles, the integrals and the impedance split simultaneously.

The one structural difference from Question 1 deserves emphasis, because it is the commonest way to lose the whole of this problem. There the divisor was $2\pi$ per device in a full-wave arrangement that used two devices; here the divisor is $2\pi$ for the output, because a half-wave circuit produces only one pulse per period. Averaging over $\pi$, as one would for a full-wave bridge, would halve the required resistance in part (b) and double the current in part (c).

Final results — Question 2
QuantitySymbolResult
Load angle$\varphi$45.01°
(b) Delay angle at $\gamma=147^\circ$$\alpha_b$75.75°
(b) Extinction angle$\beta_b$222.75°
(b) Load resistance for 25 A$R$1.059 Ω
(b) Load impedance / reactance$Z$ / $X_L$1.498 Ω / 1.059 Ω
(c) Delay angle at $\gamma=152^\circ$$\alpha_c$71.22°
(c) Mean output current with $R=1.1\ \Omega$$I_{\text{dc}}$25.80 A
(c) Mean output voltage (check)$V_{\text{dc}}$28.37 V