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)
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.
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.
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:
$$\sin\delta_0=\frac{1.0}{2.400}=0.41667$$
$$\boxed{\delta_0=24.62^{\circ}=0.4297\ \text{rad}}$$
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:
$$Z_P=\frac{(0.40)(0.08)}{0.80}=0.040,\quad
Z_Q=\frac{(0.40)(0.32)}{0.80}=0.160,\quad
Z_N=\frac{(0.08)(0.32)}{0.80}=0.032$$
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.
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.
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.
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 $P_3=1.7143$.
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.