NivaarExam PrepOfficial exam papers ↗

22-Elec-B7 Power Systems Engineering · December 2015

Question 7 of 7: Equal-Area Criterion and the Critical Clearing Angle

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

Notes on this paper

Paper format. National Exams, December 2015 — 07-Elec-B7 Power Systems Engineering. Open-book, 3 hours. Seven problems are printed; any five constitute a complete paper and all questions are of equal value (25 points each). All seven are solved in full below, because the set is a study resource rather than a timed sitting.

Reference texts. The syllabus for this code follows M. E. El-Hawary, Electrical Power Systems: Design and Analysis (IEEE Press) — the notation used throughout this paper (the cantilever transformer model, the ABCD two-port, the two-reaction salient-pole construction) is his. Corroborating references: J. D. Glover, M. S. Sarma and T. J. Overbye, Power System Analysis and Design, 6th ed.; J. Grainger and W. Stevenson, Power System Analysis; and, for the machine chapters, S. J. Chapman, Electric Machinery Fundamentals, 5th ed. Canadian practice references where grounding and protection are discussed: CSA C22.1 Canadian Electrical Code, Part I and CSA C22.3 No. 1 for overhead systems.

Check: two points read off the printed figures. (i) Figure (1) of Problem 4 prints the line admittance as y = −j10 pu, i.e. a series reactance of j0.10 pu. The negative sign is the physically correct one for an inductive line and is used here. (ii) In Figure (3-a) of Problem 6, transformer T2 carries its delta on the generator side and T1 carries its delta on the motor side; both line-side windings are wye with a solidly earthed neutral. That reading governs the zero-sequence network built in Problem 6(a).

Problem 7: Equal-Area Criterion and the Critical Clearing Angle (25 points)

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.

Given.

QuantityValue
Machine internal voltageE = 1.2 pu
Infinite-bus voltageV = 1.0 pu at 0°
Machine transient reactancej0.20 pu
Sending and receiving transformersj0.05 pu each
Each of the two parallel linesX = 0.40 pu
Fault position on line 1α = 0.20 from the sending bus
Mechanical (load) powerPm = 1.0 pu

Find. The initial rotor angle, the power-angle curves during and after the fault, and the critical clearing angle beyond which the machine cannot be saved by opening the faulted line.

EE = 1.20 puj0.20j0.05sending busline 2: jX = j0.40j alpha X = j0.08j(1-alpha)X = j0.32line 1F three-phase faultj0.05V = 1.0 pualpha = 0.20 of the way along line 1; the fault is cleared by opening line 1
Figure 7.1 — the single machine against an infinite bus. The fault sits one fifth of the way along line 1, so the faulted line contributes j0.08 on the sending side of F and j0.32 on the receiving side.

Approach. Compute the transfer reactance for each of the three network states (pre-fault, during fault, post-fault); the during-fault case needs a delta–star transform because the bolted fault ties an interior point of the network to the reference. Then apply the equal-area criterion, which gives the critical clearing angle in closed form.

  1. Part (a) — pre-fault transfer reactance and initial angle. With both lines healthy the path from the machine internal voltage to the infinite bus is $$X_{\text{pre}}=0.20+0.05+\frac{(0.40)(0.40)}{0.40+0.40}+0.05=0.20+0.05+0.20+0.05=0.50\ \text{pu}$$ so the pre-fault power-angle curve is $$P_{\text{pre}}=\frac{EV}{X_{\text{pre}}}\sin\delta=\frac{(1.2)(1.0)}{0.50}\sin\delta =2.400\sin\delta$$ Setting this equal to the 1.0 pu load gives the initial operating point: $$\sin\delta_0=\frac{1.0}{2.400}=0.41667$$ $$\boxed{\delta_0=24.62^{\circ}=0.4297\ \text{rad}}$$
  2. Part (b) — transform the faulted network. A bolted three-phase fault at F holds that point at reference potential, so F, the machine neutral and the infinite-bus neutral are all the same node. Call the sending bus $P$ and the receiving bus $Q$. Three branches now form a delta between $P$, $Q$ and the reference $N$: $$X_{PQ}=0.40\ (\text{the healthy line}),\quad X_{PN}=\alpha X=0.08,\quad X_{QN}=(1-\alpha)X=0.32$$ whose perimeter is $0.80$. Converting to a star: $$Z_P=\frac{(0.40)(0.08)}{0.80}=0.040,\quad Z_Q=\frac{(0.40)(0.32)}{0.80}=0.160,\quad Z_N=\frac{(0.08)(0.32)}{0.80}=0.032$$
  3. Reduce the resulting T network to a transfer reactance. Adding the generator and transformer reactances to the appropriate star arms, $$X_a=0.25+Z_P=0.290\ \text{pu},\qquad X_b=0.05+Z_Q=0.210\ \text{pu}$$ with $Z_N=0.032$ pu remaining as the shunt arm to the reference. For a T network the transfer reactance between the two source terminals is $$X_{\text{transfer}}=X_a+X_b+\frac{X_aX_b}{Z_N} =0.290+0.210+\frac{(0.290)(0.210)}{0.032}=0.500+1.9031=2.4031\ \text{pu}$$ The shunt arm appears in the denominator, which is why a fault close to the sending bus (a small $Z_N$) is so much more severe than one further out. The during-fault curve is therefore $$\boxed{P_{\text{during}}=\frac{(1.2)(1.0)}{2.4031}\sin\delta=0.4994\sin\delta}$$ Because the peak of this curve, 0.499 pu, is well below the 1.0 pu mechanical power, the machine accelerates throughout the fault and no equilibrium exists while the fault is on — clearing is not optional.
  4. Part (c) — post-fault curve. The fault is cleared by opening the faulted line, so line 1 disappears altogether and only line 2 carries the power: $$X_{\text{post}}=0.20+0.05+0.40+0.05=0.70\ \text{pu}$$ $$\boxed{P_{\text{post}}=\frac{(1.2)(1.0)}{0.70}\sin\delta=1.7143\sin\delta}$$ The system survives on this curve because its peak, 1.714 pu, still exceeds the 1.0 pu mechanical input; had it not, the machine would be lost regardless of how fast the breakers operated.
  5. delta (deg)P (pu)03060901201501800.51.01.52.02.5P(m) = 1.0 pu24.6278.48144.31A1A2pre-fault: P = 2.400 sin deltaduring fault: P = 0.499 sin deltapost-fault: P = 1.714 sin delta
    Figure 7.2 — the three power-angle curves with the accelerating area A1 (during the fault) and the decelerating area A2 (after clearing). The critical clearing angle is the abscissa at which the two areas are equal.
  6. Part (d) — set up the equal-area balance. The largest angle from which the machine can still be recovered on the post-fault curve is the unstable equilibrium point of that curve: $$\delta_{\max}=180^{\circ}-\sin^{-1}\!\left(\frac{P_m}{P_{\text{post,max}}}\right) =180^{\circ}-\sin^{-1}\!\left(\frac{1.0}{1.7143}\right)=180^{\circ}-35.69^{\circ}$$ $$\delta_{\max}=144.31^{\circ}=2.5187\ \text{rad}$$ The accelerating area between $\delta_0$ and the clearing angle $\delta_{cr}$ must equal the decelerating area between $\delta_{cr}$ and $\delta_{\max}$: $$\int_{\delta_0}^{\delta_{cr}}\left(P_m-P_{2}\sin\delta\right)d\delta =\int_{\delta_{cr}}^{\delta_{\max}}\left(P_{3}\sin\delta-P_m\right)d\delta$$ where $P_2=0.4994$ and $P_3=1.7143$.
  7. Solve for the critical clearing angle. Performing both integrations and collecting the terms in $\cos\delta_{cr}$ gives the standard closed form $$\cos\delta_{cr}=\frac{P_m(\delta_{\max}-\delta_0)-P_{2}\cos\delta_0 +P_{3}\cos\delta_{\max}}{P_{3}-P_{2}}$$ with the angles in radians in the first term. Substituting: $$\begin{aligned} P_m(\delta_{\max}-\delta_0) &= 1.0(2.5187-0.4297)=2.0890\\ P_{2}\cos\delta_0 &= (0.4994)(0.90906)=0.45394\\ P_{3}\cos\delta_{\max} &= (1.7143)(-0.81223)=-1.39240 \end{aligned}$$ $$\cos\delta_{cr}=\frac{2.0890-0.45394-1.39240}{1.7143-0.4994} =\frac{0.24265}{1.21494}=0.19972$$ $$\boxed{\delta_{cr}=78.48^{\circ}}$$ Numerically integrating the two areas at this angle returns $A_1=A_2=0.5857$ pu-radians, which closes the equal-area balance and confirms the result. The machine therefore has $78.48^{\circ}-24.62^{\circ}=53.86^{\circ}$ of swing available to it; converting that to a critical clearing time would need the inertia constant, which the question does not supply.

Final Results.

QuantityValue
Pre-fault transfer reactance0.500 pu
Pre-fault power-angle curveP = 2.400 sin δ
Initial power angle δ024.62° (0.4297 rad)
During-fault transfer reactance2.4031 pu
During-fault power-angle curveP = 0.4994 sin δ
Post-fault transfer reactance0.700 pu
Post-fault power-angle curveP = 1.7143 sin δ
Maximum swing angle δmax144.31°
Critical clearing angle δcr78.48°
Equal areas A1 = A20.5857 pu-rad
Back to the paper →