Part 3 · Chapter 10

Short Transmission Lines

When a line is short enough that its shunt capacitance draws a negligible current, the whole of its behaviour collapses into one series impedance and one phasor equation — and from that single equation come voltage regulation, efficiency, the power angle and the limit on how much power the line can carry.

Electric Power Systems Prof. Mithun Mondal Reading time ≈ 44 min
i What you'll learn
  • What is actually being neglected when a line is called short, and how to check the neglect with a number rather than a rule of thumb.
  • How the single equation \(\mathbf{V}_s=\mathbf{V}_r+\mathbf{I}\mathbf{Z}\) generates the whole phasor diagram, and why the approximate drop \(IR\cos\phi+IX\sin\phi\) is accurate to a fraction of a per cent.
  • Why the short line's ABCD constants are \(A=D=1\), \(B=Z\), \(C=0\), and what \(AD-BC=1\) is telling you.
  • Why regulation is worst at a lagging power factor, zero at one particular leading power factor, and negative beyond it.
  • Why efficiency and regulation both improve as \(\cos\phi\) rises, and how much a capacitor bank is worth.
  • Where the power angle \(\delta\) comes from, why \(P\approx V_sV_r\sin\delta/X\), and why a short line never reaches that limit.
  • Which of these results survive into Chapters 11 and 12 and which are artefacts of dropping \(C\).
Section 10-1

From Parameters to Performance

Part 2 is finished. Chapter 5 gave the resistance per kilometre and the corrections that make it larger than the handbook's d.c. figure; Chapter 6 gave the inductance \(L=2\times10^{-7}\ln(D_{eq}/D_s)\); Chapter 7 gave the capacitance \(C_n=2\pi\varepsilon/\ln(D_{eq}/r)\); Chapter 8 showed how bundling alters both; Chapter 9 did the same job for a cable. The outcome in every case was three numbers per kilometre — \(r\), \(x=\omega L\) and \(b=\omega C\) — and nothing was done with them.

Part 3 does something with them. The question it asks is the one an operator asks: with a known load drawing a known current at a known power factor at the far end of the line, what voltage must be applied at the near end, how much power is lost on the way, and how far can the load be increased before something gives? Those three questions are line performance, and the quantities that answer them have standard names — the sending-end voltage and current, the voltage regulation, the transmission efficiency, and the power angle.

Every calculation in Part 3 is made per phase. Chapter 3 established the licence: a balanced three-phase network is solved as one single-phase circuit carrying the phase voltage \(V_L/\sqrt3\), the line current \(I_L\) and one third of the three-phase power, with the neutral as the reference. Every \(V\) in this chapter is therefore a phase voltage unless it is explicitly marked \(V_{LL}\), and every impedance is the impedance of one conductor. When a numerical answer is wanted in three-phase terms it is converted back at the end, never in the middle.

The line itself is a distributed object: the resistance and inductance are spread along it, and so is the capacitance to earth, so strictly the voltage and current vary continuously with distance and satisfy a pair of differential equations. Chapter 12 solves them. For most lines that machinery is unnecessary, and lines are classified by how much of it can be dispensed with:

ClassLengthModelChapter
ShortUp to about 80 kmSeries \(R\) and \(L\) lumped; \(C\) ignored entirely10
MediumAbout 80 to 250 kmSeries \(R\) and \(L\); \(C\) lumped at one or two points (nominal T, nominal \(\pi\))11
LongOver about 250 kmParameters distributed; hyperbolic solution of the wave equation12

The lengths in that table are conventional, not physical. What actually decides the class is how large the shunt admittance is compared with the load — a quantity that depends on the voltage and the loading as much as on the kilometres, as the next section shows and as Chapter 9's cables demonstrate emphatically.

Section 10-2

When Capacitance Can Be Dropped

The short-line model makes exactly one approximation: the shunt admittance \(Y=j\omega C\) is set to zero. That is a strong statement, and it deserves to be tested rather than asserted.

Take a 50 km, 33 kV overhead line with the typical parameters of Chapters 6 and 7: \(C_n = 0.0095\ \mu\text{F/km}\), so the whole line has \(C = 0.475\ \mu\)F. Its charging current, drawn whether or not there is any load, is

Charging current of a 50 km, 33 kV line
\[ I_c = \omega C V_{ph} = 314.16\times0.475\times10^{-6}\times\frac{33\,000}{\sqrt3} = 1.49\times10^{-4}\times19\,053 = 2.84\ \text{A} \]

A 10 MVA load on the same line draws \(10\times10^{6}/(\sqrt3\times33\,000) = 175\) A. The charging current is 1.6% of it — and worse for the approximation than that figure suggests it is, because the charging current is in quadrature with the load current, so it changes the magnitude of the total by only about \(0.5\times(0.016)^2\), which is one part in eight thousand. Neglecting \(C\) on such a line is not an approximation so much as a rounding.

The second test is independent of the load. Chapter 12 will show that the exact \(A\) constant of a line is \(\cosh(\gamma l)\), which for a lossless line is \(\cos(\beta l)\) with \(\beta=\omega\sqrt{LC}\). For the line above, \(\sqrt{LC} = \sqrt{1.3\times10^{-3}\times9.5\times10^{-9}} = 3.51\times10^{-6}\) s/km and \(\beta = 1.10\times10^{-3}\) rad/km. Even at 80 km, \(\beta l = 0.088\) rad, or \(5.1^\circ\), and \(\cos(\beta l) = 0.9961\). The short-line model takes \(A=1\); the error is four parts in a thousand.

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The short-line criterion
A line may be treated as short when its charging current is a small fraction of its full-load current, equivalently when the electrical length \(\beta l = \omega\sqrt{LC}\,l\) is small compared with one radian. At 50 Hz on an overhead line this holds to about 80 km.

Neither form of the criterion mentions the voltage, but the voltage enters through the loading: a line carrying its rated current is easier to treat as short than the same line lightly loaded, because the charging current is fixed while the load current is not. A line on open circuit is never short — its entire current is charging current, which is the Ferranti effect of Chapter 14.

Cables break the rule at a tenth of the length. Chapter 9 found \(C\approx0.28\ \mu\text{F/km}\) for a 33 kV cable — thirty times the overhead value. A 20 km cable therefore has \(C=5.6\ \mu\)F and a charging current of \(314.16\times5.6\times10^{-6}\times19\,053 = 33.5\) A, which is over a tenth of a typical 300 A rating. "Short line" is a statement about \(\omega C l\), not about kilometres, and for cables the medium-line model of Chapter 11 is needed almost from the start.
Section 10-3

The Equivalent Circuit

With the shunt branch gone, nothing remains but a series resistance and a series inductance between the two ends. Because there is no path off the line, the current that enters at the sending end is the same current that leaves at the receiving end — the single most useful consequence of the approximation, and the one that makes every calculation in this chapter elementary.

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The short-line equations
\[ \mathbf{I}_s = \mathbf{I}_r = \mathbf{I}, \qquad \mathbf{V}_s = \mathbf{V}_r + \mathbf{I}\,\mathbf{Z}, \qquad \mathbf{Z} = R + jX = (r + jx)\,l \]

\(R\) and \(X\) are the total resistance and reactance of one conductor over the whole length, obtained by multiplying Chapter 5's \(r\) and Chapter 6's \(x=\omega L\) by the number of kilometres. The impedance angle \(\theta=\tan^{-1}(X/R)\) is typically \(65^\circ\) to \(80^\circ\) on an overhead line — the reactance dominates — and much lower on a cable, where the conductors are close together and \(x\) is small.

LOAD R jX I_s I_r V_s V_r neutral (reference) I_s = I_r and V_s = V_r + I Z
The whole of the short-line model: one series impedance, one current

The equation \(\mathbf{V}_s=\mathbf{V}_r+\mathbf{I}\mathbf{Z}\) is a statement about complex numbers, and the only difficulty students meet with it is forgetting that fact. The arithmetic is fixed by choosing \(\mathbf{V}_r\) as the reference phasor, so that \(\mathbf{V}_r = V_r\angle0^\circ = V_r+j0\), and writing the current with the sign its power factor demands:

The current, in the three cases
\[ \text{lagging p.f.:}\;\; \mathbf{I}=I\angle-\phi_r = I\cos\phi_r - jI\sin\phi_r \]
\[ \text{unity p.f.:}\;\; \mathbf{I}=I\angle0^\circ, \qquad \text{leading p.f.:}\;\; \mathbf{I}=I\angle+\phi_r = I\cos\phi_r + jI\sin\phi_r \]

Multiplying out for the lagging case, which is the usual one, separates the sending-end voltage into its two rectangular components:

Sending-end voltage, resolved
\[ \mathbf{V}_s = (V_r+j0) + (R+jX)\big(I\cos\phi_r - jI\sin\phi_r\big) \]
\[ = \underbrace{\big(V_r + IR\cos\phi_r + IX\sin\phi_r\big)}_{\text{in phase with } \mathbf{V}_r} \;+\; j\underbrace{\big(IX\cos\phi_r - IR\sin\phi_r\big)}_{\text{in quadrature with } \mathbf{V}_r} \]

Both components have a clear meaning. The in-phase part is what raises the magnitude of the sending-end voltage above the receiving-end value; the quadrature part is what turns \(\mathbf{V}_s\) through the angle \(\delta\) which Section 10-8 identifies as the power angle. Notice already that at a lagging power factor both terms of the in-phase part are positive and both add to \(V_r\), while at a leading power factor \(\sin\phi_r\) changes sign and the reactance term subtracts. That single sign is responsible for most of what the rest of the chapter has to say.

Section 10-4

The Phasor Diagram and the Approximate Drop

The algebra of Section 10-3 is complete, but it hides the geometry, and the geometry is what makes the results memorable. Draw \(\mathbf{V}_r\) horizontally from an origin \(O\) to a point \(F\). The current lags it by \(\phi_r\), so draw \(\mathbf{I}\) from \(O\) at that angle below the horizontal. From \(F\) add \(\mathbf{I}R\), which is parallel to the current because a resistance produces a drop in phase with the current it carries; call its tip \(B\). From \(B\) add \(\mathbf{I}X\), which leads the current by \(90^\circ\); call its tip \(D\). Then \(OD\) is \(\mathbf{V}_s\).

φ_r δ V_r IR IX V_s I O F B D G OD² = OG² + GD² , OG = OF + FG
The short-line phasor diagram: V_s is the closing side of O–F–B–D

Drop a perpendicular from \(D\) onto the horizontal, meeting it at \(G\). The triangle \(OGD\) is right-angled, so

Reading the sending-end voltage off the diagram
\[ OD^{2} = OG^{2}+GD^{2} = \big(OF+FG\big)^{2}+GD^{2} \]
\[ V_s = \sqrt{\big(V_r\cos\phi_r + IR\big)^{2} + \big(V_r\sin\phi_r + IX\big)^{2}} \]

The second line is the same statement made with the current, rather than the voltage, taken as the reference direction — the form in which it is usually quoted, and the form in which the two right-hand terms are recognisably "the component of everything along the current" and "the component of everything across it". Either version expands to the same thing as the rectangular resolution of Section 10-3, and the power factor at the sending end follows from the same triangle:

Sending-end power factor and power angle
\[ \cos\phi_s = \frac{OG}{OD} = \frac{V_r\cos\phi_r+IR}{V_s}, \qquad \tan\delta = \frac{IX\cos\phi_r - IR\sin\phi_r}{V_r + IR\cos\phi_r + IX\sin\phi_r} \]

Exact as these expressions are, they are more machinery than the problem needs. On any real line \(FG\) and \(GD\) are small compared with \(OF\) — the drop is a few per cent of the voltage — and \(D\) lies very nearly on the horizontal. Then \(OD \approx OG\), and the sending-end magnitude is obtained by simply adding the in-phase part of the drop to \(V_r\):

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The approximate voltage drop
\[ V_s - V_r \;\approx\; IR\cos\phi_r \pm IX\sin\phi_r \qquad (+\text{ for lagging},\; -\text{ for leading}) \]

The neglected term is \(GD^2/(2\,OG)\). With \(GD\) equal to 2% of \(OG\) the error is one part in five thousand; with \(GD\) equal to 10% it is one part in two hundred. The approximation is therefore excellent precisely when it matters — on a line whose regulation is acceptable — and degrades only on a line that is already too heavily loaded to be operated.

Why \(X\) matters more than \(R\). On a 66 kV line \(X\) is three or four times \(R\), and at \(\cos\phi=0.8\) the term \(IX\sin\phi_r\) is comparable with or larger than \(IR\cos\phi_r\). The voltage drop on a transmission line is therefore mostly caused by reactive current flowing through reactance, not by real current flowing through resistance. That single observation is the reason voltage is controlled by managing reactive power (Chapter 34) rather than by managing load.
Section 10-5

ABCD Constants

A transmission line, seen from its two ends, is a four-terminal network: two terminals at the sending end, two at the receiving end. It is linear, it is passive, and it contains no independent sources. For any network of that kind the sending-end quantities must be linear combinations of the receiving-end quantities, and the four coefficients of the combination are the generalised circuit constants, universally written \(A\), \(B\), \(C\) and \(D\):

The general two-port relations
\[ \mathbf{V}_s = A\mathbf{V}_r + B\mathbf{I}_r, \qquad \mathbf{I}_s = C\mathbf{V}_r + D\mathbf{I}_r, \qquad \begin{bmatrix}\mathbf{V}_s\\ \mathbf{I}_s\end{bmatrix} = \begin{bmatrix}A & B\\ C & D\end{bmatrix}\begin{bmatrix}\mathbf{V}_r\\ \mathbf{I}_r\end{bmatrix} \]

The short line's constants are read straight off Section 10-3. Comparing \(\mathbf{V}_s=\mathbf{V}_r+\mathbf{Z}\mathbf{I}_r\) with the first relation gives \(A=1\) and \(B=\mathbf{Z}\); comparing \(\mathbf{I}_s=\mathbf{I}_r\) with the second gives \(C=0\) and \(D=1\).

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ABCD constants of a short line
\[ \begin{bmatrix}\mathbf{V}_s\\ \mathbf{I}_s\end{bmatrix} = \begin{bmatrix}1 & \mathbf{Z}\\ 0 & 1\end{bmatrix}\begin{bmatrix}\mathbf{V}_r\\ \mathbf{I}_r\end{bmatrix}, \qquad A=D=1\ \text{(dimensionless)},\quad B=\mathbf{Z}\ (\Omega),\quad C=0\ (\text{S}) \]

Two checks apply to every set of ABCD constants in this book. \(AD-BC=1\) always, because the line is a reciprocal network; here \(1\times1-\mathbf{Z}\times0=1\). And \(A=D\) whenever the network is symmetrical — looks the same from both ends — which a uniform line is.

Three things make the ABCD form worth adopting even for a network as simple as this one. First, it is the form in which Chapters 11 and 12 will state their results, so the short line becomes the special case \(A=1,\ C=0\) of a single framework rather than a separate piece of theory. Second, the constants are exactly what is needed to invert the problem: given the sending-end conditions, the receiving-end quantities follow by inverting the matrix, and because the determinant is unity the inverse is written down at sight:

Working backwards from the sending end
\[ \begin{bmatrix}\mathbf{V}_r\\ \mathbf{I}_r\end{bmatrix} = \begin{bmatrix}D & -B\\ -C & A\end{bmatrix}\begin{bmatrix}\mathbf{V}_s\\ \mathbf{I}_s\end{bmatrix} \qquad\Longrightarrow\qquad \mathbf{V}_r = \mathbf{V}_s - \mathbf{Z}\mathbf{I}_s, \quad \mathbf{I}_r=\mathbf{I}_s \]

Third, networks in cascade multiply. A transformer of series impedance \(\mathbf{Z}_T\) feeding a line of impedance \(\mathbf{Z}_L\) is the product of two matrices, and because both are of the same form the product is trivial — but the same rule handles a line feeding a transformer feeding another line, and it is how a whole transmission path is reduced to four numbers. Chapter 4's per-unit system makes that cascade painless by removing the turns ratios from the matrices altogether.

Cascade of a transformer and a short line
\[ \begin{bmatrix}1 & \mathbf{Z}_T\\ 0 & 1\end{bmatrix}\begin{bmatrix}1 & \mathbf{Z}_L\\ 0 & 1\end{bmatrix} = \begin{bmatrix}1 & \mathbf{Z}_T+\mathbf{Z}_L\\ 0 & 1\end{bmatrix} \]
Section 10-6

Voltage Regulation

Consumers' equipment is designed for a nominal voltage and tolerates a few per cent of departure from it. The load on a line, however, varies through the day by a factor of two or more (Chapter 30), and every change in load changes the drop along the line. The measure of that sensitivity is the voltage regulation: the rise in receiving-end voltage, expressed as a percentage of the full-load value, when the full load at a specified power factor is thrown off while the sending-end voltage is held constant.

The definition is easy to apply to a short line because throwing off the load makes \(I=0\), and with no current there is no drop: the no-load receiving-end voltage is simply \(V_s\).

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Voltage regulation
\[ \%\,\text{Regulation} = \frac{\big|V_{r,\text{no load}}\big| - \big|V_{r,\text{full load}}\big|}{\big|V_{r,\text{full load}}\big|}\times100 = \frac{|V_s|-|V_r|}{|V_r|}\times100 \]

The second form holds only because \(A=1\) for a short line. In general the no-load receiving voltage is \(V_s/A\), and Chapters 11 and 12 must use \(\big(|V_s|/|A| - |V_r|\big)/|V_r|\). It is a comparison of magnitudes throughout; the angle between the two voltages plays no part.

Substituting the approximate drop of Section 10-4 gives the working formula and, with it, the whole story of how regulation depends on the load:

Regulation in terms of the load
\[ \%\,\text{Reg} \approx \frac{I\big(R\cos\phi_r \pm X\sin\phi_r\big)}{V_r}\times100 \]

At a lagging power factor both terms are positive and regulation is large. As the power factor improves the reactive term shrinks. At unity it vanishes and only \(IR\cos\phi_r\) remains. At a leading power factor the reactive term reverses and begins to cancel the resistive one — and at one particular leading power factor it cancels it exactly. Setting the approximate drop to zero gives that condition immediately as \(\tan\phi_r = R/X\); the exact condition follows from demanding \(|V_s|=|V_r|\) in the full expression:

Exact condition for zero regulation
\[ V_r^{2} = \big(V_r\cos\phi_r+IR\big)^{2}+\big(IX-V_r\sin\phi_r\big)^{2} \quad\text{(leading p.f.)} \]
\[ 0 = 2V_rI\big(R\cos\phi_r - X\sin\phi_r\big) + I^{2}|\mathbf{Z}|^{2} \]
\[ R\cos\phi_r - X\sin\phi_r = |\mathbf{Z}|\cos(\phi_r+\theta) \;\Longrightarrow\; \cos(\phi_r+\theta) = -\frac{I|\mathbf{Z}|}{2V_r}, \qquad \theta=\tan^{-1}\frac{X}{R} \]
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The two extremes of regulation
Regulation is zero at the leading power factor \(\phi_r = \cos^{-1}\!\big(-I|\mathbf{Z}|/2V_r\big)-\theta\), and greatest at the lagging power factor for which \(\tan\phi_r = X/R\), that is when the load angle equals the line's impedance angle \(\theta\).

The maximum follows by differentiating \(R\cos\phi_r+X\sin\phi_r\) with respect to \(\phi_r\): the derivative \(-R\sin\phi_r+X\cos\phi_r\) vanishes at \(\tan\phi_r=X/R\). At that power factor the entire drop lies along \(\mathbf{V}_r\), the quadrature component \(IX\cos\phi_r-IR\sin\phi_r\) is zero, and \(\mathbf{V}_s\) is exactly in phase with \(\mathbf{V}_r\) — a line delivering power with no angle across it at all.

% Reg 12 6 0 −6 0.6lead 0.87lead unity 0.8lag 0.45lag zero regulation max: tanφ = X/R negative regulation
Regulation against power factor for a fixed current — negative at strongly leading loads

Beyond the zero-regulation point the regulation is negative: the receiving-end voltage is higher than the sending-end voltage under load, and throwing the load off makes it fall. A leading load draws current that flows backwards through the reactance in the phasor sense and produces a rise instead of a drop. It is the same mechanism as the Ferranti effect of Chapter 14, where the leading current is drawn not by a capacitive load but by the line's own capacitance — which is why a short line, having no capacitance in its model, cannot show the Ferranti effect at all.

Section 10-7

Transmission Efficiency

The second performance figure is the fraction of the power fed in at one end that emerges at the other. Since the short-line model has no shunt branch, there is no leakage and no charging current, and the only loss is the \(I^2R\) of the three conductors:

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Transmission efficiency
\[ \eta = \frac{\text{power delivered at the receiving end}}{\text{power delivered at the receiving end}+\text{losses}} = \frac{P_r}{P_r+3I^{2}R} \]

Equivalently \(\eta = P_r/P_s\) with \(P_s=\sqrt3\,V_{s(LL)}I\cos\phi_s\) computed from the sending-end quantities. The two routes must agree, and checking that they do is the standard arithmetic check on a line calculation — the discrepancy exposes an error in \(\cos\phi_s\) or in \(V_s\) immediately.

Substituting \(I = P_r/(\sqrt3\,V_{r(LL)}\cos\phi_r)\) turns the loss into a statement about the quantities the designer controls:

The loss, in terms of what is chosen
\[ 3I^{2}R = 3R\left(\frac{P_r}{\sqrt3\,V_{r(LL)}\cos\phi_r}\right)^{2} = \frac{P_r^{2}R}{V_{r(LL)}^{2}\cos^{2}\phi_r}, \qquad \eta = \frac{1}{1+\dfrac{P_rR}{V_{r(LL)}^{2}\cos^{2}\phi_r}} \]

Chapter 2 arrived at the proportionality \(1/(V^2\cos^2\phi)\) by an argument about conductor volume; here it reappears as a statement about loss at fixed conductor size. The two are the same fact seen from opposite sides: for a given loss, raising the voltage lets the conductor shrink; for a given conductor, raising the voltage cuts the loss. Both scale as the inverse square, and both are equally sensitive to the power factor.

One structural point separates a line from the transformer of an earlier course. A transformer has iron loss that is present whether or not it is loaded, so its efficiency rises to a maximum where copper loss equals iron loss and falls again. The short line has no no-load loss whatever, so its efficiency simply falls as the load rises — it is highest when the line is doing nothing. Quoting a line's efficiency therefore means nothing unless the load at which it was computed is quoted too, and the convention is to state it at full load.

Regulation and efficiency pull the same way. Both improve when \(\cos\phi_r\) rises, both worsen as \(I\) rises, and both are proportional to line length through \(R\) and \(X\). A single remedy — reducing the reactive current the line has to carry — improves both at once, which is why power-factor correction is the first thing tried on a line that is failing either test. Chapter 13 develops regulation and efficiency for the general two-port, where \(A\neq1\) and the two figures no longer track each other so simply.
Section 10-8

Power Transfer and the Power Angle

So far the load has been given and the line asked to carry it. Turn the question round: with both ends held at fixed voltages — as they are in a real network, where generators and tap-changers regulate the busbars — how much power flows, and what determines it?

Let \(\mathbf{V}_s = V_s\angle\delta\), \(\mathbf{V}_r=V_r\angle0^\circ\) and \(\mathbf{Z}=|Z|\angle\theta\). The current is fixed by the two voltages, and the complex power delivered at the receiving end follows from its definition:

Complex power at the receiving end
\[ \mathbf{I} = \frac{\mathbf{V}_s-\mathbf{V}_r}{\mathbf{Z}} = \frac{V_s\angle\delta - V_r\angle0^\circ}{|Z|\angle\theta} \]
\[ \mathbf{S}_r = \mathbf{V}_r\mathbf{I}^{*} = \frac{V_sV_r}{|Z|}\angle(\theta-\delta) \;-\; \frac{V_r^{2}}{|Z|}\angle\theta \]

Separating real and imaginary parts gives the two quantities that the receiving-end busbar actually sees:

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Received power and reactive power, per phase
\[ P_r = \frac{V_sV_r}{|Z|}\cos(\theta-\delta) - \frac{V_r^{2}}{|Z|}\cos\theta, \qquad Q_r = \frac{V_sV_r}{|Z|}\sin(\theta-\delta) - \frac{V_r^{2}}{|Z|}\sin\theta \]

The angle \(\delta\) by which \(\mathbf{V}_s\) leads \(\mathbf{V}_r\) is the power angle or load angle. It is the only variable on the right-hand side that changes with loading once the two voltage magnitudes are fixed, so on a line between two regulated busbars, power flow is controlled by angle and by nothing else.

The maximum receivable power is found by inspection: \(P_r\) is largest when \(\cos(\theta-\delta)=1\), that is when \(\delta=\theta\).

The steady-state limit
\[ P_{r,\max} = \frac{V_sV_r}{|Z|} - \frac{V_r^{2}}{|Z|}\cos\theta \qquad\text{at}\qquad \delta = \theta \]

For an overhead line the resistance is small enough that setting \(R=0\) costs little accuracy, and then \(|Z|=X\) and \(\theta=90^\circ\). The two expressions collapse into the pair that the rest of this book uses constantly:

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The lossless form
\[ P = \frac{V_sV_r}{X}\sin\delta \quad\text{per phase}, \qquad P_{3\phi} = \frac{V_{s(LL)}V_{r(LL)}}{X}\sin\delta, \qquad Q_r = \frac{V_sV_r\cos\delta - V_r^{2}}{X} \]

Real power depends on the angle between the two voltages; reactive power depends on the difference in their magnitudes. That separation is the foundation of the load-flow formulation of Chapter 18, of the decoupling that makes the fast-decoupled method of Chapter 20 work, and of the swing equation of Chapter 27.

The theoretical maximum at \(\delta=\theta\) is never reached on a short line, and the reason is worth stating plainly. Example 5 evaluates \(P_{r,\max}\) for a 20 km, 132 kV line and finds it to be over 700 MW, while the thermal rating of the same conductors is perhaps 100 MW. The line melts long before it becomes unstable. A short line is therefore thermally limited. As length grows, \(|Z|\) grows with it and \(P_{r,\max}\) falls in inverse proportion, until on a long line the stability limit falls below the thermal one and the line becomes stability limited — the transition that Chapters 14 and 28 examine, and the reason series capacitors are installed on long lines to reduce the effective \(X\).

Section 10-9

Compensation, and Where the Model Stops

Sections 10-6 and 10-7 both reduce to the same complaint: the line is carrying more current than the real power requires, because the load draws reactive power as well. The reactive component contributes nothing to \(P_r\) but is fully charged for in \(I^2R\) and, through \(IX\sin\phi_r\), dominates the voltage drop.

The remedy is to supply the reactive power locally. A capacitor bank connected at the receiving-end busbar generates \(Q_c\) on the spot, so the line carries only the difference. Requiring the load's real power \(P\) to be delivered at an improved power factor \(\cos\phi_2\) instead of \(\cos\phi_1\) fixes the rating:

Capacitor rating for power-factor correction
\[ Q_c = P\big(\tan\phi_1 - \tan\phi_2\big) \]

The effect on the line is immediate and quadratic in the current: raising the power factor from 0.8 to 0.95 cuts the current by a factor \(0.8/0.95=0.842\) and the loss by \(0.842^2=0.709\), a 29% reduction, while the drop falls by rather more because the \(X\sin\phi_r\) term shrinks faster than the current does. Example 6 works both figures through.

Two other forms of compensation appear later in the book and are mentioned here so that their place in the argument is clear. A series capacitor inserted in the line subtracts from \(X\), which reduces the drop and raises \(P_{r,\max}\) directly — the natural remedy for a line that is long rather than heavily loaded (Chapter 38). A shunt reactor does the opposite of a capacitor bank and is used on lightly loaded lines whose own capacitance is producing too much reactive power, which is a problem the short-line model cannot even express (Chapter 14).

That last point is the honest summary of this chapter's limits. Everything derived here follows from setting \(Y=0\), so every phenomenon that lives in the shunt branch is invisible: no charging current, no Ferranti rise on open circuit, no surge impedance, no reactive generation by the line itself, no travelling waves. All of them return in Chapters 11 to 14. What survives unchanged is the framework — per-phase working, the phasor equation, the ABCD matrix, the definitions of regulation and efficiency, and the power-angle relation — and that framework is why the short line is studied first even though few interesting lines are short.

QuantityShort line (Ch. 10)What changes in Chapters 11–12
\(A=D\)\(1\)\(1+\tfrac12 YZ\), then \(\cosh\gamma l\)
\(B\)\(Z\)\(Z(1+\tfrac14 YZ)\), then \(Z_c\sinh\gamma l\)
\(C\)\(0\)\(Y(1+\tfrac14 YZ)\), then \(\sinh(\gamma l)/Z_c\)
\(I_s\) versus \(I_r\)EqualDiffer by the charging current
No-load \(V_r\)\(V_s\)\(V_s/A > V_s\) — the Ferranti effect
Regulation\(\big(|V_s|-|V_r|\big)/|V_r|\)\(\big(|V_s|/|A|-|V_r|\big)/|V_r|\)
Limiting constraintConductor temperatureStability, then voltage collapse
Section 10-10

Worked Examples

1 A complete short-line calculation

Problem. A three-phase, 50 Hz short line delivers 5 MW at 11 kV and 0.8 power factor lagging. Each conductor has a resistance of \(1.0\ \Omega\) and a reactance of \(2.0\ \Omega\). Find the sending-end voltage, the power angle, the sending-end power factor, the voltage regulation and the transmission efficiency.

Solution. Work per phase with \(\mathbf{V}_r\) as reference. The line current and the receiving phase voltage are

Current and reference voltage
\[ I = \frac{P}{\sqrt3\,V_{LL}\cos\phi_r} = \frac{5\times10^{6}}{\sqrt3\times11\,000\times0.8} = 328.0\ \text{A}, \qquad V_r = \frac{11\,000}{\sqrt3} = 6350.9\ \text{V} \]

With \(\cos\phi_r=0.8\) and \(\sin\phi_r=0.6\), the two components of the drop are

In-phase and quadrature components
\[ IR\cos\phi_r + IX\sin\phi_r = 328.0\,(1\times0.8+2\times0.6) = 328.0\times2.0 = 656.1\ \text{V} \]
\[ IX\cos\phi_r - IR\sin\phi_r = 328.0\,(2\times0.8-1\times0.6) = 328.0\times1.0 = 328.0\ \text{V} \]
\[ V_s = \sqrt{(6350.9+656.1)^{2}+328.0^{2}} = \sqrt{7007.0^{2}+328.0^{2}} = 7014.7\ \text{V} \]

so \(V_{s(LL)} = \sqrt3\times7014.7 = 12\,150\) V, and

Angle, power factor, regulation, efficiency
\[ \delta = \tan^{-1}\frac{328.0}{7007.0} = 2.68^\circ, \qquad \phi_s = \delta+\phi_r = 2.68^\circ+36.87^\circ = 39.55^\circ, \quad \cos\phi_s = 0.771 \]
\[ \%\text{Reg} = \frac{7014.7-6350.9}{6350.9}\times100 = 10.45\% \]
\[ \text{Loss} = 3I^{2}R = 3\times328.0^{2}\times1 = 322.8\ \text{kW}, \qquad \eta = \frac{5000}{5000+322.8} = 93.94\% \]

Two checks. The approximate drop \(656.1\) V gives \(10.33\%\) against the exact \(10.45\%\) — an error of one part in ninety, from neglecting a quadrature component that is 4.7% of the in-phase one. And the sending-end power computed independently, \(\sqrt3\times12\,150\times328.0\times0.771 = 5323\) kW, agrees with \(5000+323\) kW.

2 The same load at three power factors

Problem. For the line of Example 1, find the regulation when the same 5 MW is delivered at unity power factor and at 0.8 leading. Then find the power factor, at the full-load current of Example 1, for which the regulation would be exactly zero.

Solution. At unity power factor the same power needs less current: \(I=5\times10^{6}/(\sqrt3\times11\,000) = 262.4\) A. The drop has no reactive contribution in phase with \(\mathbf{V}_r\):

Unity power factor
\[ V_s = \sqrt{(6350.9+262.4)^{2}+(2\times262.4)^{2}} = \sqrt{6613.3^{2}+524.9^{2}} = 6634.1\ \text{V}, \quad \%\text{Reg} = 4.46\% \]

At 0.8 leading the current is 328.0 A again, but \(\sin\phi_r\) changes sign and the reactance term now subtracts from the in-phase component while adding to the quadrature one:

0.8 power factor leading
\[ IR\cos\phi_r - IX\sin\phi_r = 328.0(0.8-1.2) = -131.2\ \text{V}, \qquad IX\cos\phi_r+IR\sin\phi_r = 721.7\ \text{V} \]
\[ V_s = \sqrt{(6350.9-131.2)^{2}+721.7^{2}} = 6261.4\ \text{V}, \qquad \%\text{Reg} = -1.41\% \]

The receiving end is now at a higher voltage than the sending end. Somewhere between unity and 0.8 leading the regulation passes through zero, and Section 10-6 locates it exactly. With \(|\mathbf{Z}| = \sqrt{1+4} = 2.236\ \Omega\) and \(\theta=\tan^{-1}2 = 63.43^\circ\),

Zero-regulation power factor
\[ \cos(\phi_r+\theta) = -\frac{I|\mathbf{Z}|}{2V_r} = -\frac{328.0\times2.236}{2\times6350.9} = -0.0578 \;\Longrightarrow\; \phi_r+\theta = 93.31^\circ \]
\[ \phi_r = 93.31^\circ-63.43^\circ = 29.88^\circ \text{ leading}, \qquad \cos\phi_r = 0.867\ \text{leading} \]

Verify: with \(\mathbf{I}=328.0\angle29.88^\circ = 284.4+j163.2\), the drop is \((284.4+j163.2)(1+j2) = -42.0+j732.0\), so \(\mathbf{V}_s = 6308.9+j732.0\) and \(|V_s| = 6351.2\) V — equal to \(V_r\) to within rounding.

3 Working backwards from a fixed sending-end voltage

Problem. A three-phase short line of impedance \(6+j8\ \Omega\) per phase is supplied at a constant 33 kV. It delivers 5 MW at 0.8 power factor lagging. Find the receiving-end voltage and the regulation.

Solution. This is the harder direction, because the current depends on the unknown voltage. Let \(V\) be the receiving phase voltage; then \(I = 5\times10^{6}/(3V\times0.8) = 2.0833\times10^{6}/V\). The two components of the drop are \(I(R\cos\phi_r+X\sin\phi_r) = 9.6I\) and \(I(X\cos\phi_r-R\sin\phi_r) = 2.8I\), so with \(V_s = 33\,000/\sqrt3 = 19\,053\) V,

A quadratic in \(V^2\)
\[ 19\,053^{2} = \big(V+9.6I\big)^{2}+\big(2.8I\big)^{2} = V^{2} + 2(9.6)(2.0833\times10^{6}) + \frac{(9.6^{2}+2.8^{2})(2.0833\times10^{6})^{2}}{V^{2}} \]
\[ V^{4} - \big(3.6300\times10^{8}-4\times10^{7}\big)V^{2} + 4.3403\times10^{14} = 0 \]
\[ V^{2} = \frac{3.2300\times10^{8}\pm\sqrt{1.0433\times10^{17}-1.7361\times10^{15}}}{2} = \frac{3.2300\times10^{8}\pm3.2030\times10^{8}}{2} \]

The upper root gives \(V^{2} = 3.2165\times10^{8}\), so \(V = 17\,935\) V and \(V_{r(LL)} = 31.06\) kV. Then

Regulation
\[ \%\text{Reg} = \frac{19\,053-17\,935}{17\,935}\times100 = 6.23\%, \qquad I = \frac{2.0833\times10^{6}}{17\,935} = 116.2\ \text{A} \]

The lower root, \(V=1162\) V, is not an arithmetic artefact. It is a genuine solution of the circuit equations: the same 5 MW can be delivered at a very low voltage and a very high current — 1793 A, dissipating 57.9 MW in the line to deliver 5 MW. No system operates there, but the existence of a second solution is the algebraic signature of voltage collapse, and the point at which the two roots merge is the loadability limit that Chapter 34 studies. A short line at ordinary loading sits far from it, which is why the upper root is taken without comment.

4 Choosing the conductor from a regulation target

Problem. A 15 km, three-phase line is to deliver 8 MW at 33 kV and 0.85 power factor lagging with a voltage regulation not exceeding 5%. The reactance is \(0.35\ \Omega\)/km and the conductor material has \(\rho = 2.86\times10^{-8}\ \Omega\)m. Find the minimum conductor cross-section, and the efficiency with the next standard size of 150 mm².

Solution. The current and the permitted drop come first:

Current and drop budget
\[ I = \frac{8\times10^{6}}{\sqrt3\times33\,000\times0.85} = 164.7\ \text{A}, \qquad \Delta V_{\text{allowed}} = 0.05\times\frac{33\,000}{\sqrt3} = 952.6\ \text{V} \]

With \(X = 0.35\times15 = 5.25\ \Omega\) and \(\sin\phi_r = 0.5268\), the reactive part of the drop is already fixed and the resistance gets whatever is left:

Solving for \(R\), then for the area
\[ R\cos\phi_r + X\sin\phi_r \le \frac{952.6}{164.7} = 5.785\ \Omega \;\Longrightarrow\; 0.85R \le 5.785-5.25\times0.5268 = 3.020 \]
\[ R \le 3.553\ \Omega, \qquad a = \frac{\rho l}{R} = \frac{2.86\times10^{-8}\times15\,000}{3.553} = 1.208\times10^{-4}\ \text{m}^{2} = 120.8\ \text{mm}^{2} \]

Taking 150 mm² gives \(R = 4.29\times10^{-4}/1.5\times10^{-4} = 2.86\ \Omega\). Checking the regulation exactly rather than approximately:

Verification and efficiency
\[ V_s = \sqrt{(19\,053+855.7)^{2}+486.7^{2}} = 19\,914\ \text{V}, \qquad \%\text{Reg} = \frac{861.6}{19\,053}\times100 = 4.52\% \;\checkmark \]
\[ \text{Loss} = 3\times164.7^{2}\times2.86 = 232.6\ \text{kW}, \qquad \eta = \frac{8000}{8232.6} = 97.17\% \]

Notice that the reactance consumed 2.77 V of drop per ampere against the resistance's 2.43 V even though the conductor was chosen as small as the target allowed — and that no choice of conductor could have met a 3% target, since \(X\sin\phi_r\) alone accounts for 2.8% of the voltage. When the reactive term exhausts the budget, the answer is not more copper but a higher power factor or a shorter electrical distance.

5 The power angle, and why a short line never reaches its limit

Problem. A 20 km, 132 kV three-phase line has \(\mathbf{Z} = 5+j15\ \Omega\) per phase. Both ends are held at 132 kV. Find the maximum power the receiving end can take, the power angle when 50 MW is transferred, and the reactive power that must be supplied at the receiving end to keep its voltage at 132 kV.

Solution. \(|\mathbf{Z}| = \sqrt{25+225} = 15.81\ \Omega\) and \(\theta = \tan^{-1}(15/5) = 71.57^\circ\), so \(\cos\theta = 0.3162\) and \(\sin\theta = 0.9487\). Per phase, \(V_s = V_r = 76\,210\) V and \(V_r^{2}/|Z| = 3.673\times10^{8}\).

Maximum transfer, at \(\delta=\theta\)
\[ P_{r,\max} = \frac{V_sV_r}{|Z|}\big(1-\cos\theta\big) = 3.673\times10^{8}\times0.6838 = 2.512\times10^{8}\ \text{W per phase} \]
\[ P_{r,\max(3\phi)} = 3\times251.2 = 753\ \text{MW at } \delta = 71.6^\circ \]

At 50 MW total, that is \(16.67\) MW per phase:

Power angle and reactive requirement
\[ \cos(\theta-\delta) = \frac{16.67\times10^{6}}{3.673\times10^{8}}+0.3162 = 0.3616 \;\Longrightarrow\; \theta-\delta = 68.80^\circ, \quad \delta = 2.76^\circ \]
\[ Q_r = 3.673\times10^{8}\big(\sin68.80^\circ-\sin71.57^\circ\big) = 3.673\times10^{8}(-0.01636) = -6.01\ \text{MVAr per phase} \]

The negative sign says the receiving end must supply 18.0 MVAr, not absorb it: holding both ends at the same magnitude forces zero regulation, and Example 2 showed that zero regulation demands a leading load. In practice that 18 MVAr comes from a capacitor bank.

Set the 753 MW beside the thermal rating. Conductors carrying 500 A at 132 kV give \(\sqrt3\times132\times0.5 = 114\) MVA. The line's steady-state stability limit is six and a half times its thermal limit, and no operating decision will ever be made on the basis of \(\delta\). Repeat the calculation for a 300 km line, where \(|Z|\) is fifteen times larger, and \(P_{r,\max}\) falls to about 50 MW — below the thermal rating, and now the binding constraint.

6 What a capacitor bank is worth

Problem. The 5 MW, 0.8 lagging load of Example 1 is corrected to 0.95 lagging by a capacitor bank at the receiving-end busbar. Find the rating of the bank and the new regulation, loss and efficiency.

Solution. With \(\tan(\cos^{-1}0.8) = 0.750\) and \(\tan(\cos^{-1}0.95) = 0.329\),

Capacitor rating
\[ Q_c = P\big(\tan\phi_1-\tan\phi_2\big) = 5\,(0.750-0.329) = 2.11\ \text{MVAr} \]

The line now carries only \(I = 5\times10^{6}/(\sqrt3\times11\,000\times0.95) = 276.2\) A, with \(\sin\phi_r = 0.3123\):

The new performance
\[ V_s = \sqrt{(6350.9+434.9)^{2}+438.6^{2}} = 6800.0\ \text{V}, \qquad \%\text{Reg} = \frac{449.1}{6350.9}\times100 = 7.07\% \]
\[ \text{Loss} = 3\times276.2^{2}\times1 = 228.9\ \text{kW}, \qquad \eta = \frac{5000}{5228.9} = 95.62\% \]

Regulation has fallen from 10.45% to 7.07%, loss from 322.8 kW to 228.9 kW — a saving of 94 kW, which over 6000 hours a year is 560 MWh — and efficiency has risen from 93.94% to 95.62%. All of it is bought with a 2.11 MVAr capacitor that has no moving parts and dissipates almost nothing. This is the cheapest improvement available anywhere in a power system, and the reason tariffs penalise a poor power factor (Chapter 30).

Review

Chapter Summary

The model

\(Y=0\), so \(\mathbf{I}_s=\mathbf{I}_r\) and \(\mathbf{V}_s=\mathbf{V}_r+\mathbf{I}\mathbf{Z}\) — valid while \(\omega Cl\) is small, not merely while \(l\) is.

Exact drop

\(V_s=\sqrt{(V_r\cos\phi_r+IR)^2+(V_r\sin\phi_r+IX)^2}\), from the right triangle \(OGD\).

Approximate drop

\(IR\cos\phi_r\pm IX\sin\phi_r\) — good to a fraction of a per cent on any line worth operating.

ABCD

\(A=D=1\), \(B=\mathbf{Z}\), \(C=0\); \(AD-BC=1\) and \(A=D\) check reciprocity and symmetry.

Regulation

\((|V_s|-|V_r|)/|V_r|\); maximum at \(\tan\phi_r=X/R\) lagging, zero at one leading power factor, negative beyond.

Efficiency

\(P_r/(P_r+3I^2R)\), with loss \(\propto 1/(V^2\cos^2\phi)\) — Chapter 2's law seen again.

Power angle

\(P=V_sV_r\sin\delta/X\): real power rides on angle, reactive power on voltage difference.

The binding limit

A short line is thermally limited; its stability limit is several times its rating.

Practice

Practice Problems

Work per phase with the receiving-end voltage as reference, and state at the end whether the exact or the approximate drop was used. Difficulty rises down the list.

  1. A three-phase line of impedance \(3+j5\ \Omega\) per phase delivers 2 MW at 11 kV, 0.85 lagging. Find the sending-end line voltage, the regulation and the efficiency.
  2. Repeat Problem 1 with the same load at 0.85 leading, and account for the change in regulation in one sentence.
  3. A 25 km, 33 kV line has \(r=0.2\ \Omega\)/km and \(x=0.4\ \Omega\)/km and carries 200 A at 0.9 lagging. Find the regulation using the approximate drop, then using the exact expression, and state the percentage error of the approximation.
  4. For the line of Problem 3, find the power factor at which the regulation would be greatest, and the power factor at which it would be zero, both at the same 200 A.
  5. A 20 km, three-phase line is to deliver 6 MW at 22 kV and 0.9 lagging with a regulation of not more than 4%. The reactance is \(0.4\ \Omega\)/km and \(\rho=2.86\times10^{-8}\ \Omega\)m. Determine the least conductor cross-section, and check whether a 3% target is achievable at all.
  6. A short line of impedance \(4+j6\ \Omega\) per phase is supplied at a fixed 66 kV and delivers 12 MW at 0.8 lagging. Find the receiving-end voltage by solving the quadratic in \(V^2\), and quote both roots with a comment on the second.
  7. A line with \(\mathbf{Z}=4+j12\ \Omega\) per phase connects two busbars each held at 110 kV. Find the maximum receivable power and the power angle at which it occurs, then the power angle and the reactive requirement at the receiving end when 40 MW is transferred.
  8. A 4 MW load at 0.75 lagging is supplied over a line of impedance \(2+j4\ \Omega\) per phase at 11 kV. Find the capacitor rating that raises the power factor to 0.98, and tabulate the current, regulation, loss and efficiency before and after.
Tip: before starting any line problem, write down \(V_r\) per phase, \(I\) with its sign convention, and \(R\), \(X\) for the whole length — three lines that take ten seconds and prevent the two errors that account for most lost marks: using the line voltage where the phase voltage belongs, and using the per-kilometre impedance where the total belongs. Then check the answer for plausibility: regulation above about 15% or efficiency below about 90% means either a very long line, a very poor power factor, or an arithmetic slip, and it is nearly always the slip.