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Stability after tripping one circuit

Short answer

The system remains stable. The rotor swings to approximately 69.9° and settles at the new equilibrium angle of 48.6°.

For the system shown in figure below, the numerical values for different quantities are: E = 1.2 pu, V = 1 pu, Xs = 0.2 pu and reactance of each line is 0.4 pu. Initially the generator is delivering a power of 1.5 pu. If one of the double circuit lines is now tripped out, using equal area criteria determine whether the system would be able to maintain its stability or not. [Figure: generator E∠δ - double circuit line, each circuit X = j0.4 p.u with circuit breakers at both ends - infinite bus V∠0°]

Data: E=1.2E = 1.2 pu, V=1V = 1 pu, Xs=0.2X_s = 0.2 pu, each line 0.40.4 pu, Pm=1.5P_m = 1.5 pu.

Step 1: Power-angle curves

Both lines: XI=0.2+0.42=0.4 pu,Pmax1=1.2×10.4=3.0 puOne line: XII=0.2+0.4=0.6 pu,Pmax2=1.20.6=2.0 pu\begin{aligned} \text{Both lines: } X_I &= 0.2 + \frac{0.4}{2} = 0.4\ \text{pu}, \quad P_{max1} = \frac{1.2\times1}{0.4} = 3.0\ \text{pu} \\ \text{One line: } X_{II} &= 0.2 + 0.4 = 0.6\ \text{pu}, \quad P_{max2} = \frac{1.2}{0.6} = 2.0\ \text{pu} \end{aligned}

Step 2: Angles

δ0=sin⁡−11.53.0=30∘=0.5236 radδ1=sin⁡−11.52.0=48.59∘=0.8481 rad  (new equilibrium)δmax=180∘−48.59∘=131.41∘=2.2935 rad\begin{aligned} \delta_0 &= \sin^{-1}\frac{1.5}{3.0} = 30^\circ = 0.5236\ \text{rad} \\ \delta_1 &= \sin^{-1}\frac{1.5}{2.0} = 48.59^\circ = 0.8481\ \text{rad}\ \ \text{(new equilibrium)} \\ \delta_{max} &= 180^\circ - 48.59^\circ = 131.41^\circ = 2.2935\ \text{rad} \end{aligned}

When the line trips, PeP_e drops to 2.0sin⁡30∘=1.0<Pm2.0\sin30^\circ = 1.0 < P_m, so the rotor accelerates.

Step 3: Equal areas

Accelerating area, from δ0\delta_0 to δ1\delta_1:

A1=Pm(δ1−δ0)−Pmax2(cos⁡δ0−cos⁡δ1)=1.5(0.8481−0.5236)−2.0(0.8660−0.6614)=0.4868−0.4092=0.0775 pu⋅rad\begin{aligned} A_1 &= P_m(\delta_1-\delta_0) - P_{max2}(\cos\delta_0-\cos\delta_1) \\ &= 1.5(0.8481-0.5236) - 2.0(0.8660-0.6614) \\ &= 0.4868 - 0.4092 = 0.0775\ \text{pu·rad} \end{aligned}

Maximum decelerating area, from δ1\delta_1 to δmax\delta_{max}:

A2,max=Pmax2(cos⁡δ1−cos⁡δmax)−Pm(δmax−δ1)=2.0(0.6614+0.6614)−1.5(2.2935−0.8481)=2.6458−2.1681=0.4775 pu⋅rad\begin{aligned} A_{2,max} &= P_{max2}(\cos\delta_1-\cos\delta_{max}) - P_m(\delta_{max}-\delta_1) \\ &= 2.0(0.6614+0.6614) - 1.5(2.2935-0.8481) \\ &= 2.6458 - 2.1681 = 0.4775\ \text{pu·rad} \end{aligned}
 Pe
 3.0 |      ___ before (3 sin d)
 2.0 |    /  _ \__ after (2 sin d)
 1.5 |---/-*-----\----\---- Pm
     |  /A1| A2   \    \
     +-30--48.6--69.9--131.4 delta

Step 4: Result

A2,max=0.4775>A1=0.0775A_{2,max} = 0.4775 > A_1 = 0.0775, so the system is stable and keeps synchronism.

Equating A1=A2A_1 = A_2, that is 1.5(δ2−0.5236)=2.0(0.8660−cos⁡δ2)1.5(\delta_2-0.5236) = 2.0(0.8660-\cos\delta_2), gives a maximum swing of δ2=69.88∘\delta_2 = 69.88^\circ. The rotor then settles at 48.59∘48.59^\circ.

Answer: Stable; the rotor swings to about 69.9° and settles at 48.6°.

✓ Answer checked by Claude Sonnet 5.5

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