22-Elec-B7 Power Systems Engineering · December 2017
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. National Exams, December 2017 — 16-Elec-B7 Power Systems Engineering, 3 hours, open book, any non-communicating calculator permitted. The paper prints seven problems; the rubric states that any five questions constitute a complete paper and that all questions are of equal value, so only the first five in the answer book are marked. All seven are worked here, because this set is a study resource rather than a sitting. Sub-part point values are reproduced from the paper.
Reference texts. This exam code follows M. E. El-Hawary, Electrical Power Systems: Design and Analysis (IEEE Press) — the notation used below is his: the long-line ABCD constants of Problem 1, the round-rotor power-angle relations of Problem 2, the cantilever transformer equivalent of Problem 3, the power-flow injection equations of Problem 4, the network-reduction fault analysis of Problems 5 and 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. 5 transmission lines, ch. 6 power flow, ch. 7–9 symmetrical components and unsymmetrical faults, ch. 11 transient stability); J. J. Grainger and W. D. Stevenson, Power System Analysis; and S. J. Chapman, Electric Machinery Fundamentals, 5th ed. (ch. 2 transformers, ch. 4–5 synchronous machines). Canadian practice references for the protection and grounding discussion: CSA C22.1 Canadian Electrical Code, Part I and the relevant IEEE C37 and C57 series.
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) — consequences of short-circuit faults. A short circuit replaces a load impedance of the order of one per unit with something close to zero, so the current rises to whatever the network's Thevenin reactance permits — commonly ten to twenty times rated, and on a strong transmission bus far more. The consequences divide into four groups.
Thermal. Conductor heating goes as $I^{2}t$, so a fault current twenty times rated deposits four hundred times the normal heat. Cable insulation, joints, current transformers and busbar supports can be destroyed in a fraction of a second, which is why fault-clearing times are specified in cycles rather than seconds and why a through-fault duration curve is part of every transformer specification.
Mechanical. Electromagnetic force between parallel conductors goes as $I^{2}$ as well. Transformer windings, switchgear busbars and cable cleats all face peak forces during the first asymmetric half-cycle, and repeated through-faults progressively loosen transformer windings until an eventual turn-to-turn failure occurs.
System-wide electrical. The faulted bus is dragged towards zero volts, and the depression propagates through the network in proportion to the electrical distance from the fault. Motors stall or drop out, contactors release, power electronic converters trip on undervoltage, and the reactive absorption of the recovering motors after clearing can cause a second, slower voltage dip. Unbalanced faults additionally inject negative-sequence current, which produces double-frequency rotor heating in generators, and zero-sequence current, which raises earth-potential rise and can interfere with communications circuits.
Stability. Because a fault suppresses the transfer power while the prime movers keep delivering mechanical power, every generator that can still see the network accelerates. If the fault is not cleared before the critical clearing time, synchronism is lost — which is precisely the calculation carried out in Problem 7 of this paper. Protection speed is therefore a stability requirement, not merely an equipment-protection one.
Part (b) — transformer protective schemes. Four functionally distinct schemes, in the order in which they would be applied to a transmission-class unit:
1. Percentage differential protection (ANSI 87T). Currents are measured at every winding, referred to a common base through the CT ratios and the vector group, and summed. In healthy operation and for any external fault the sum is nominally zero; an internal fault destroys that balance and the relay operates. Because CT saturation, tap-changer travel and magnetising inrush all produce spurious differential current, the characteristic is percentage-biased (the operating threshold rises with through current) and is restrained by second-harmonic detection for inrush and fifth-harmonic detection for overexcitation. It is the primary, unit protection: fast, and inherently selective because it looks only inside its own CT boundary.
2. Buchholz / gas-and-oil relay and sudden-pressure relay. Mounted in the pipe between tank and conservator of an oil-filled unit, the Buchholz relay collects gas liberated by incipient faults. Slow gas accumulation from partial discharge or a hot joint operates an alarm float; a surge of oil driven by a violent internal arc operates a trip vane. The sudden-pressure relay serves the same purpose by rate-of-rise of tank pressure. These are the only schemes that detect faults producing negligible terminal current, such as a single shorted turn, and they are purely mechanical, hence independent of the CT and VT circuits.
3. Restricted earth fault (ANSI 64REF) and neutral overcurrent (ANSI 51N/51G). A residual connection of the three phase CTs of a star winding is balanced against a CT in the neutral earthing connection. Any current that enters the winding zone and does not leave it must have gone to earth inside the zone, so the scheme is a high-impedance differential dedicated to earth faults and is far more sensitive than phase differential to a fault near the star point, where the driving voltage is only a small fraction of phase voltage.
4. Backup overcurrent and thermal protection (ANSI 50/51, 49). Time- and instantaneous-overcurrent elements graded with the downstream feeders give backup if the unit protection or its supply fails, and clear uncleared through-faults. Winding-temperature and top-oil devices (ANSI 49) protect against sustained overload rather than against faults, tripping or initiating cooling on a thermal replica of the winding hot spot. In Canadian practice the overall scheme, its CT requirements and its coordination are governed by the relevant IEEE C37 series, with the installation itself falling under CSA C22.1.
Given. The six-bus system of Figure (3), all reactances in per unit on a common base, every source at 1.0 pu, with a bolted three-phase fault at the mid-point of Line B.
| Element | Reactance | Element | Reactance |
|---|---|---|---|
| Generator at bus 1 | 0.2 | Transformer bus 1–bus 2 | 0.1 |
| Line A (bus 2–bus 3) | 0.2 | Line B (bus 2–bus 3) | 0.2 |
| Transformer bus 3–bus 4 | 0.3 | Generator at bus 4 | 0.2 |
| Transformer bus 2–bus 5 | 0.1 | Transformer at bus 5 / its generator | 0.1 / 0.2 |
| Transformer bus 3–bus 6 | 0.2 | Transformer at bus 6 / its generator | 0.3 / 0.2 |
Find. The fault current at the mid-point of Line B, and the voltage at bus 2 while the fault is on.
[Figure not reproduced: Figure 5.1 — The single-line diagram of Figure (3), redrawn. The fault F sits at the mid-point of Line B, so Line A remains a healthy path between buses 2 and 3 and the network cannot be reduced by series–parallel steps alone. See the official exam paper.]
Approach. Collapse the four generator branches onto buses 2 and 3, which leaves a delta between buses 2, 3 and the fault point sitting on two shunt arms; one delta–star transform then reduces the whole network to a single Thevenin reactance, and back-substitution through the star recovers the bus voltages.
| Quantity | Symbol | Value (pu) |
|---|---|---|
| Source branch reduced onto bus 2 | $z_{N2}$ | 0.171429 |
| Source branch reduced onto bus 3 | $z_{N3}$ | 0.291667 |
| Star arms of the 2–3–F delta | $Z_{s2},Z_{s3},Z_{sF}$ | 0.0500, 0.0500, 0.0250 |
| Thevenin reactance at the fault | $X_{\text{th}}$ | 0.159355 |
| Fault current (part c) | $|I_F|$ | 6.2753 |
| Current contributed via bus 2 | $I_a$ | 3.80763 |
| Current contributed via bus 3 | $I_b$ | 2.46766 |
| Voltage at bus 2 during fault (part d) | $|V_2|$ | 0.34726 |
| Voltage at bus 3 during fault | $|V_3|$ | 0.28027 |