22-Elec-B7 Power Systems Engineering · May 2017
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. National Exams, May 2017 — 16-Elec-B7 Power Systems Engineering. Open-book, 3 hours, seven problems of equal value (25 points each); any five constitute a complete paper, and only the first five in the answer book are marked. All seven are solved here, because the set is a study resource rather than a sitting.
Reference texts. This exam code follows M. E. El-Hawary, Electrical Power Systems: Design and Analysis (IEEE Press) — the notation is his throughout: the bundle-conductor mean radii and long-line ABCD constants of Problem 1, the round-rotor power-angle relations of Problem 2, the three-winding equivalent circuit of Problem 3, the sequence-network fault reduction of Problem 6 and the equal-area criterion of Problem 7. Corroborating references: J. D. Glover, M. S. Sarma and T. J. Overbye, Power System Analysis and Design, 6th ed. (ch. 4–5 transmission-line parameters, ch. 6 power flow, ch. 7–9 symmetrical components and faults, ch. 11 transient stability); J. J. Grainger and W. D. Stevenson, Power System Analysis; and S. J. Chapman, Electric Machinery Fundamentals, 5th ed., for the synchronous-machine and transformer chapters. Canadian practice references where protection and grounding are discussed: CSA C22.1 Canadian Electrical Code, Part I, CSA C22.3 for overhead systems, and IEEE C37 (protective relaying) and IEEE 142 Green Book (grounding).
Check: four judgement calls carried through the solutions, recorded here rather than hedged inside the answers.
(i) Problem 1 states neither a frequency nor a line length. Parts (a)–(c) need neither. Part (d) needs both, so 60 Hz is used (Canadian national exam) and the ABCD constants are given as closed-form functions of length, evaluated at a representative 400 km with a sensitivity table at 200 km and 600 km. The characteristic impedance and the surge-impedance loading do not depend on either quantity.
(ii) Problem 1 gives “bundle separation S” for a bundle whose figure shows eight sub-conductors on a circle. S is read as the distance between adjacent sub-conductors, so the bundle radius is $A = S/[2\sin(\pi/N)] = 0.6533\ \text{m}$ — the standard El-Hawary reading. If a marker instead reads S as the bundle diameter, every mean radius scales by the same factor and the method is unchanged.
(iii) Problem 5 says “the voltage at both sources is 1 p.u.” above a figure that draws three generators. All three are taken at 1.0 pu, which is the only reading that closes the network; the three internal e.m.f.s then merge into one node.
(iv) Problem 6: the zero-sequence source reactance is printed as $X_{0S}=j0.04$, possibly followed by a fifth digit. The value $j0.04$ is used. Reading it as $j0.045$ moves the zero-sequence Thévenin reactance from 0.19978 to 0.20051 pu and the fault current by 0.1 % — below the resolution of any answer here.
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.
(a) Consequences of short-circuit faults. A short circuit collapses the impedance seen by the sources, so the first consequence is a current of several thousand per cent of rating flowing until a breaker clears it. That current does mechanical and thermal damage: the $i^{2}$ electromagnetic forces on parallel conductors and transformer windings peak in the first half-cycle and can physically deform bus work and coil ends, while the $i^{2}Rt$ heating destroys insulation and, at the fault itself, produces an arc whose energy is the dominant arc-flash hazard to personnel — the reason Canadian practice requires incident-energy studies and labelling under CSA Z462. The second consequence is a voltage collapse across the faulted region: buses electrically near the fault lose most of their voltage, so motors stall or trip, contactors drop out, and sensitive process load is lost over an area far wider than the faulted element. The third is a threat to system stability: with the fault on, generators near it can export almost no power while their turbines continue to deliver mechanical torque, so their rotors accelerate, and if clearing is slow they lose synchronism — exactly the mechanism analysed in Problem 7. Fourth, unbalanced faults inject negative- and zero-sequence currents, which cause double-frequency rotor heating in generators, induce voltages in parallel communication circuits, and raise the earth-potential rise at substation ground grids to values dangerous to anyone standing nearby. Finally, every fault is followed by a switching transient and by the loss of the faulted element, which weakens the network and may cascade if the remaining paths are overloaded.
(b) Transformer protective schemes. Three functionally distinct schemes are universal on power transformers. Differential protection (ANSI device 87T) is the main unit protection: currents are measured at every winding, referred to a common base through matching ratios and phase-shift compensation, and summed. In healthy operation the sum is zero to within the ratio error, so any significant residual means the fault is inside the protected zone and the relay trips instantaneously. It is percentage-biased so that through-fault current-transformer saturation does not cause a false trip, and it is restrained against the second-harmonic content of magnetising inrush and the fifth harmonic of over-excitation, which would otherwise look like internal faults. Overcurrent and earth-fault protection (devices 51, 51N, 50) is the back-up: an inverse-time characteristic on each phase and in the neutral trips for faults the differential cannot see, notably those beyond the transformer terminals, and is graded in time with the downstream feeder relays so that the nearest device operates first. A restricted-earth-fault element gives sensitive detection of winding-to-core faults close to the neutral, where the driving voltage and hence the differential current are small. Mechanical and thermal protection is the third family: the Buchholz relay in the pipe between tank and conservator collects the gas evolved by incipient insulation breakdown and alarms, then trips on a surge of oil produced by a violent internal fault; sudden-pressure and pressure-relief devices act on the same principle; and winding-temperature devices with a thermal image of the hot spot alarm and trip on overload. To these are commonly added over-excitation (volts-per-hertz, device 24) protection, which prevents core saturation when the transformer is energised at high voltage or low frequency, and surge arresters at the bushings to limit lightning and switching overvoltages.
(c)–(d) Given.
| Element | Symbol | Reactance (pu) |
|---|---|---|
| Each generator, subtransient | $X_g$ | $j0.20$ |
| Each step-up transformer | $X_T$ | $j0.10$ |
| Line A (bus 2 to bus 3) | $X_A$ | $j0.20$ |
| Line B (bus 2 to bus 3) | $X_B$ | $j0.20$ |
| Tie, bus 2 to bus 5 | $X_{25}$ | $j0.10$ |
| Internal e.m.f. of every source | $E$ | $1.0\angle0^\circ$ pu |
| Fault | — | bolted three-phase, mid-point of line B |
Find. The fault current at the mid-point of line B, and the voltages that survive at buses 4 and 5 while the fault is on.
[Figure not reproduced: Figure 5 — The five-bus system of Figure (4) redrawn. Three identical generating units feed buses 2, 3 and 5; lines A and B run in parallel between buses 2 and 3, and the bolted three-phase fault sits at the mid-point of line B. See the official exam paper.]
Approach. With every internal e.m.f. at $1.0\angle0^\circ$ the three sources merge into a single node, so the problem reduces to finding the Thévenin reactance from that node to the fault point. Split line B at its mid-point, collapse the two radial source branches on bus 2, then apply one delta–star transform to the (bus 2, bus 3, F) triangle. Bus voltages during the fault follow by back-substitution.
Final Results
| Quantity | Symbol | Result |
|---|---|---|
| Thévenin reactance at the fault | $X_{th}$ | $j0.160625$ pu |
| (c) Fault current | $I_F$ | $6.2257\angle-90^\circ$ pu (622.6 MVA on a 100 MVA base) |
| Voltage at bus 1 | $V_1$ | 0.56420 pu |
| Voltage at bus 2 | $V_2$ | 0.34630 pu |
| Voltage at bus 3 | $V_3$ | 0.27626 pu |
| (d) Voltage at bus 4 | $V_4$ | 0.51751 pu |
| (d) Voltage at bus 5 | $V_5$ | 0.50973 pu |