Part 2 · Chapter 5

Overhead Line Construction and Conductors

Before a line can have an inductance or a capacitance it has to be a physical object — so many kilograms of aluminium, strung at a chosen tension, held clear of earth by an insulator string — and almost every one of those choices is settled by one calculation: how much conductor material a given system needs to deliver a given power at a given loss.

Electric Power Systems Prof. Mithun Mondal Reading time ≈ 46 min
i What you'll learn
  • Why every transmission system must be compared at equal power, equal distance, equal loss and equal maximum voltage to earth before any conclusion about it means anything.
  • How the conductor volume of ten different d.c., single-phase, two-phase and three-phase systems is computed, and why the three-phase three-wire system wins.
  • Why aluminium replaced copper although it is the poorer conductor, and what the steel core of ACSR is for.
  • How stranding is counted, why spiralling raises resistance, and what the geometric mean radius of a stranded conductor is — the quantity Chapter 6 will need on its first page.
  • How temperature and skin effect convert a handbook \(R_{dc}\) into the resistance the line actually shows at 50 Hz.
  • Why the unit nearest the conductor in an insulator string is the most stressed, and how string efficiency quantifies it.
  • How the parabolic sag equation follows from a force balance, and how ice and wind enter it.
Section 5-1

What Has to Be Held Up in the Air

Chapters 1 to 4 treated the transmission line as a symbol. Chapter 3 drew it as a single stroke on the single-line diagram; Chapter 4 gave that stroke a per-unit impedance and connected it to the rest of the network. Nothing so far has said what the stroke is made of. Part 2 of this book computes the four parameters — resistance, inductance, capacitance and conductance — that fill in the impedance, and every one of those calculations begins from a geometry: the radius of the conductor, the spacing between phases, the height above earth. This chapter fixes that geometry, and explains why it is what it is.

An overhead line is a deceptively short list of parts. Bare metal conductors carry the current. Insulator strings hang them from steel cross-arms, and the strings are long enough that the conductor cannot flash over to the earthed tower. One or two earth wires run along the tower tops, above everything, to intercept lightning. Towers stand a few hundred metres apart; between them the conductor hangs in a curve, and the depth of that curve — the sag — is what keeps the mechanical tension within safe limits while still leaving statutory clearance to the ground below.

Each of those parts is sized by a different constraint, and the constraints pull against each other. Raise the tension to reduce the sag and the towers can be shorter, but the conductor fatigues and may snap in winter. Increase the phase spacing and the flashover risk falls but the line inductance rises, as Chapter 6 will show. Choose a fatter conductor and the loss falls, but so does the surface electric field, which is the point of the exercise above 220 kV — Chapter 15 returns to it under the name of corona.

earth wire (shield) suspension string span L sag S clearance
The parts of an overhead line and the three dimensions that constrain them
The costliest item is the one that is bought by the tonne. Towers, insulators and fittings are counted in units; conductor is counted in kilometres of metal, three or six strands abreast, and its cost scales with the volume of material. That is why the design of a transmission system starts — historically and logically — with the question of which arrangement of conductors delivers a given power for the least metal.
Section 5-2

Comparing Systems on Equal Terms

Chapter 2 established the central economic fact of transmission: for a three-phase line the volume of conductor material varies as \(1/(V^2\cos^2\phi)\). That settled the choice of voltage. It did not settle the choice of system. Direct current, single phase, two phase and three phase all deliver power along wires, and each can be arranged with or without an earthed neutral. Ten arrangements are worth comparing, and the comparison is only honest if every one of them is asked to do exactly the same job under exactly the same restriction.

Four conditions are held identical across all ten systems.

Held equalSymbolWhy it must be held equal
Power delivered\(P\) wattsA system that delivers less is not competing for the same job.
Length of transmission\(l\) metresVolume scales as \(l^2\); a shorter line would win trivially.
Total line loss\(W\) wattsLoss can always be traded against metal; fixing it removes the trade.
Maximum voltage to earth\(V_m\) volts (peak)This is what the insulation has to withstand — the real physical limit.

The fourth condition deserves the most care, because it is the one students most often get wrong. In an overhead line the conductors hang in air, far apart, and the dielectric that is closest to breaking down is the air path from a conductor down to the earthed tower or to the ground. The limiting quantity is therefore the maximum potential difference between any conductor and earth. In an underground cable the conductors sit side by side inside a common sheath with a few millimetres of insulation between them, so the chief stress is between conductor and conductor, and the comparison must instead fix the maximum voltage between conductors. The two bases give different answers. Everything in this section is the overhead basis; Chapter 9 takes up cables, where the ranking changes.

With the basis fixed, the calculation for each system is mechanical and always the same four steps: find the load current from the power and the available voltage, write the loss as \(nI^2R\) over the \(n\) conductors, solve for the cross-sectional area that the loss budget permits, and multiply that area by the total conductor length to obtain the volume.

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The four-step recipe
\[ I = \frac{P}{V_{\text{available}}\cos\phi}, \qquad W = n I^2\frac{\rho l}{a} \;\Longrightarrow\; a = \frac{n\,I^2\rho l}{W}, \qquad \text{Vol} = n\,a\,l \]

For d.c. systems \(\cos\phi = 1\) and \(V_{\text{available}}\) is the d.c. voltage the arrangement offers; for a.c. systems it is the r.m.s. value derived from the peak-to-earth limit \(V_m\), which is where the factors of \(\sqrt2\) enter.

One system is chosen as the yardstick. Universal practice takes the simplest of all — the two-wire d.c. system with one conductor earthed — and calls its volume \(K\). Every other result is quoted as a multiple of \(K\), so the comparison reduces to a single column of numbers.

Section 5-3

The D.C. Systems

Two-wire d.c., one conductor earthed. One conductor sits at earth potential and the other at \(V_m\); the working voltage between them is therefore \(V_m\), and that is all the arrangement offers. The load current is \(I_1 = P/V_m\), and with two conductors each of resistance \(\rho l / a_1\),

The reference system
\[ W = 2I_1^2\frac{\rho l}{a_1} = 2\left(\frac{P}{V_m}\right)^{\!2}\frac{\rho l}{a_1} \;\Longrightarrow\; a_1 = \frac{2P^2\rho l}{W V_m^2} \]
\[ \text{Vol}_1 = 2a_1 l = \frac{4P^2\rho l^2}{W V_m^2} \;\equiv\; K \]

Two-wire d.c., mid-point earthed. Now the supply is split about an earthed centre point, so one conductor sits at \(+V_m\) and the other at \(-V_m\). The insulation to earth is stressed exactly as before, but the working voltage between the conductors has doubled to \(2V_m\). This is the single most instructive step in the whole comparison, because doubling the useful voltage at no insulation cost halves the current and — the loss being fixed — quarters the metal.

Mid-point earthing buys a factor of four
\[ I_2 = \frac{P}{2V_m}, \qquad W = 2I_2^2\frac{\rho l}{a_2} = \frac{P^2\rho l}{2a_2V_m^2} \;\Longrightarrow\; a_2 = \frac{P^2\rho l}{2WV_m^2} \]
\[ \text{Vol}_2 = 2a_2l = \frac{P^2\rho l^2}{WV_m^2} = \frac{K}{4} \]

Three-wire d.c. The two outers are held at \(+V_m\) and \(-V_m\) with an earthed neutral wire between them. If the two halves of the load are balanced, the neutral carries no current at all, and the outers behave exactly as in the mid-point-earthed system: \(a_3 = a_2\). The neutral is nevertheless installed, since the load will not stay balanced, and standard practice gives it half the cross-section of an outer. The extra half-conductor is pure overhead in the balanced case:

Paying for an idle neutral
\[ \text{Vol}_3 = 2.5\,a_3 l = 2.5\left(\frac{P^2\rho l}{2WV_m^2}\right)l = \frac{5}{4}\cdot\frac{P^2\rho l^2}{WV_m^2} = \frac{5K}{16} = 0.3125\,K \]
The d.c. systems win on metal and lose on everything else. Both earthed-neutral d.c. arrangements beat every a.c. system in the table that follows, and yet no utility built a d.c. distribution network after about 1900. The reason is not in this calculation at all: d.c. offers no transformer, so the voltage at which power is generated is the voltage at which it must be consumed, and the \(1/V^2\) economy of Chapter 2 can never be exploited. Modern HVDC (Chapter 38) reopens the case only because power electronics finally supplied the missing transformer.
Section 5-4

The A.C. Systems and the Verdict

Every a.c. system carries the same two penalties relative to d.c. The insulation limit \(V_m\) is a peak value, so the useful r.m.s. voltage is smaller by \(\sqrt2\); and the load draws current at power factor \(\cos\phi\), so a given real power needs a current larger by \(1/\cos\phi\). Both penalties enter the volume squared. Every a.c. result below therefore carries the factor \(1/\cos^2\phi\), and the comparison between a.c. systems is a comparison of the numerical coefficients in front of it.

Single-phase, two-wire, one conductor earthed. The r.m.s. voltage available is \(V_m/\sqrt2\), so \(I_4 = \sqrt2 P/(V_m\cos\phi)\) and

The worst case in the table
\[ W = 2I_4^2\frac{\rho l}{a_4} = \frac{4P^2\rho l}{V_m^2\cos^2\phi\;a_4} \;\Longrightarrow\; a_4 = \frac{4P^2\rho l}{W V_m^2\cos^2\phi} \]
\[ \text{Vol}_4 = 2a_4 l = \frac{8P^2\rho l^2}{WV_m^2\cos^2\phi} = \frac{2K}{\cos^2\phi} \]

Single-phase, two-wire, mid-point earthed. As in the d.c. case, earthing the mid-point doubles the working voltage to a peak of \(2V_m\), that is \(\sqrt2\,V_m\) r.m.s., and quarters the volume to \(K/(2\cos^2\phi)\).

Single-phase, three-wire. Add a neutral of half section to the previous arrangement. With a balanced load the neutral carries nothing, the outers are unchanged, and the volume becomes \(2.5\,a_5 l = 5K/(8\cos^2\phi)\) — a 25% penalty over the two-wire mid-point system, in exchange for the ability to supply two voltage levels.

Two-phase, four-wire. Two independent single-phase circuits in quadrature, each carrying \(P/2\), each with its own pair of conductors at \(\pm V_m\). Because each pair sees the full \(\sqrt2 V_m\) r.m.s. while carrying only half the power, the current per conductor falls to \(P/(2\sqrt2 V_m\cos\phi)\):

Two phases, four wires
\[ W = 4I_7^2\frac{\rho l}{a_7} = \frac{P^2\rho l}{2a_7V_m^2\cos^2\phi} \;\Longrightarrow\; a_7 = \frac{P^2\rho l}{2WV_m^2\cos^2\phi} \]
\[ \text{Vol}_7 = 4a_7 l = \frac{2P^2\rho l^2}{WV_m^2\cos^2\phi} = \frac{K}{2\cos^2\phi} \]

Two-phase, three-wire. The one arrangement in the list whose neutral is genuinely busy. Two outers, each at \(V_m/\sqrt2\) r.m.s. to the common return, carry currents \(I_8 = P/(\sqrt2 V_m\cos\phi)\) that are \(90^\circ\) apart; the return therefore carries their phasor sum, of magnitude \(\sqrt2 I_8\). Holding the current density constant makes the neutral \(\sqrt2\) times the section of an outer, so its resistance is \(R_8/\sqrt2\):

A loaded neutral is expensive
\[ W = 2I_8^2R_8 + \left(\sqrt2 I_8\right)^2\frac{R_8}{\sqrt2} = I_8^2R_8\left(2+\sqrt2\right) = \frac{P^2\rho l\,(2+\sqrt2)}{2a_8V_m^2\cos^2\phi} \]
\[ \text{Vol}_8 = 2a_8l + \sqrt2\,a_8l = a_8l\left(2+\sqrt2\right) = \frac{P^2\rho l^2 (2+\sqrt2)^2}{2WV_m^2\cos^2\phi} = \frac{1.457\,K}{\cos^2\phi} \]

since \((2+\sqrt2)^2/2 = (6+4\sqrt2)/2 = 5.828\) and \(5.828/4 = 1.457\). The two-phase three-wire system is the second worst in the table, and for the clearest of reasons: it is the only one asked to carry current in a conductor that produces no useful power.

Three-phase, three-wire. Take the conductors star-connected for the calculation, so each carries a phase voltage of \(V_m/\sqrt2\) r.m.s. and a third of the power. Then \(I_9 = \sqrt2 P/(3V_m\cos\phi)\), and

The system that was built
\[ W = 3I_9^2\frac{\rho l}{a_9} = \frac{2P^2\rho l}{3a_9V_m^2\cos^2\phi} \;\Longrightarrow\; a_9 = \frac{2P^2\rho l}{3WV_m^2\cos^2\phi} \]
\[ \text{Vol}_9 = 3a_9 l = \frac{2P^2\rho l^2}{WV_m^2\cos^2\phi} = \frac{0.5\,K}{\cos^2\phi} \]

Three-phase, four-wire. Add a neutral of half section. Balanced three-phase currents sum to zero — the result Chapter 3 derived from \(1+a+a^2=0\) — so the neutral is idle and the outers are unchanged, giving \(3.5\,a_{10}l = 7K/(12\cos^2\phi)\).

SystemConductorsVolumeValue at \(\cos\phi = 0.8\)
D.C. two-wire, one earthed2\(K\)1.000 \(K\)
D.C. two-wire, mid-point earthed2\(K/4\)0.250 \(K\)
D.C. three-wire2.5\(5K/16\)0.3125 \(K\)
1-phase two-wire, one earthed2\(2K/\cos^2\phi\)3.125 \(K\)
1-phase two-wire, mid-point earthed2\(K/(2\cos^2\phi)\)0.781 \(K\)
1-phase three-wire2.5\(5K/(8\cos^2\phi)\)0.977 \(K\)
2-phase four-wire4\(K/(2\cos^2\phi)\)0.781 \(K\)
2-phase three-wire3.41\(1.457K/\cos^2\phi\)2.277 \(K\)
3-phase three-wire3\(\mathbf{K/(2\cos^2\phi)}\)0.781 \(K\)
3-phase four-wire3.5\(7K/(12\cos^2\phi)\)0.911 \(K\)
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The result of the comparison
Three a.c. systems tie for least conductor material at \(K/(2\cos^2\phi)\): single-phase two-wire with mid-point earthing, two-phase four-wire, and three-phase three-wire. Among equals, three-phase three-wire uses the fewest conductors — three instead of two full-voltage pairs or four wires.

The tie is not a coincidence. All three arrangements manage to present the full \(\pm V_m\) swing across a working circuit while spreading the power over the available conductors, and the volume formula cannot distinguish between ways of doing that. What breaks the tie is the count of conductors, and behind that the rotating magnetic field, the constant instantaneous power and the self-starting motor that only three phases provide — the arguments of Chapter 3.

Read the table as a set of ratios, not a set of numbers. The useful facts are structural: earthing a mid-point divides the volume by four; adding an idle half-neutral multiplies it by 1.25 (three-wire) or 1.167 (four-wire); the ordinary earthed single-phase two-wire system needs four times the metal of a three-phase line delivering the same power. Those ratios survive any change of \(\cos\phi\), \(P\), \(l\) or \(W\), because \(K\) contains all of them.
Section 5-5

Conductor Materials

The comparison of Section 5-4 fixed how many conductors to string and at what voltage; it left \(\rho\) as a symbol. Choosing the metal is a separate optimisation, and the honest criterion is not conductivity but cost per unit of conductance, at the required mechanical strength, at the required weight.

Copper is the best available conductor after silver, takes a high tensile strength when hard-drawn, and resists corrosion. It also has a density of about 8890 kg/m³ and a price per tonne that has never been low. Aluminium conducts only 61% as well volume-for-volume, but weighs less than a third as much. Those two numbers combine into the fact that ended the argument.

Aluminium against copper at equal resistance
\[ R_{Al} = R_{Cu} \;\Longrightarrow\; \frac{\rho_{Al}\,l}{a_{Al}} = \frac{\rho_{Cu}\,l}{a_{Cu}} \;\Longrightarrow\; \frac{a_{Al}}{a_{Cu}} = \frac{\rho_{Al}}{\rho_{Cu}} = \frac{2.83}{1.72} = 1.645 \]
\[ \frac{d_{Al}}{d_{Cu}} = \sqrt{1.645} = 1.283, \qquad \frac{m_{Al}}{m_{Cu}} = 1.645\times\frac{2703}{8890} = 0.500 \]

An aluminium conductor of the same resistance is 28% fatter and weighs half as much. Half the weight means lighter towers, longer spans and cheaper foundations; the greater diameter is, if anything, an advantage, because it lowers the electric field at the conductor surface and postpones corona. The single defect is mechanical: hard-drawn aluminium has roughly half the tensile strength of hard-drawn copper and creeps under sustained load, so a long span of pure aluminium sags unacceptably.

The fix is to separate the two duties. ACSR — aluminium conductor, steel reinforced — puts a core of galvanised steel strands, which carry the mechanical tension, inside layers of aluminium strands, which carry the current. The steel contributes almost nothing electrically, and since it sits at the centre where the current density is lowest in any case, nothing is lost. A designation such as 54/7 means 54 aluminium strands over a 7-strand steel core.

Property (at 20 °C)Hard-drawn copperHard-drawn aluminiumGalvanised steel
Resistivity \(\rho\) (\(\times10^{-8}\) Ω·m)1.722.83≈ 14
Conductivity (% IACS)9761≈ 12
Density (kg/m³)889027037800
Ultimate tensile strength (MPa)380–420160–2001300–1500
Temperature coefficient \(\alpha_{20}\) (/°C)0.003930.004030.0045
Inferred zero-resistance temperature \(T\) (°C)241228

Where the mechanical demand is milder, the steel can be dispensed with. AAAC (all-aluminium alloy conductor) uses an aluminium–magnesium–silicon alloy that is stronger than pure aluminium and slightly less conductive; it has no bimetallic corrosion problem and is favoured in coastal and industrial atmospheres. ACAR reinforces aluminium with alloy strands instead of steel. ACSS uses fully annealed aluminium over a high-strength core so that the steel takes essentially all the load, which permits very high operating temperatures and therefore higher current — a retrofit strategy when a right of way cannot be widened.

The catalogue of ACSR sizes is standardised, and Indian practice names them after animals. The four in the table below account for most of the country's transmission network.

Code nameStranding Al/steelOverall dia. (mm)GMR \(D_s\) (m)\(R_{dc}\) at 20 °C (Ω/km)Typical use
Dog6/4.72 + 7/1.5714.15≈ 0.004730.274533–66 kV lines
Panther30/3.00 + 7/3.0021.00≈ 0.008210.1390132 kV lines
Zebra54/3.18 + 7/3.1828.62≈ 0.011510.0688220 and 400 kV, bundled
Moose54/3.53 + 7/3.5331.77≈ 0.012770.0561400 kV, twin or quad bundle
Where these numbers are going. The \(D_s\) column is not decoration. Chapter 6 will show that the inductance of a line depends on the conductor only through this one number, and Chapter 8 will show that bundling several sub-conductors raises the effective \(D_s\) — which is the whole reason 400 kV lines carry two or four Moose conductors per phase instead of one very large one.
Section 5-6

Stranding, Spiralling and the Geometric Mean Radius

A conductor of 500 mm² drawn as a single solid rod would be 25 mm across and effectively unbendable; it could not be coiled on a drum or dead-ended at a tower. Every practical conductor is therefore stranded: many thin wires laid up helically in concentric layers, each layer wound in the opposite sense to the one beneath so that the whole assembly does not unwind under tension.

Concentric stranding follows a fixed arithmetic. A central strand is surrounded by 6 strands, then 12, then 18, and so on, each successive layer taking 6 more than the last. With \(n\) layers counted including the central strand,

Strand count and overall diameter
\[ N = 1 + 6 + 12 + \cdots = 1 + 6\big(1+2+\cdots+(n-1)\big) = 3n(n-1)+1 \]
\[ n = 1,2,3,4,5 \;\Longrightarrow\; N = 1,\,7,\,19,\,37,\,61; \qquad D_{\text{overall}} = (2n-1)\,d \]

where \(d\) is the diameter of one strand. The overall-diameter rule follows by walking outward: each new layer adds one strand diameter on each side.

7 strands, n = 2 D = 3d 19 strands, n = 3 D = 5d steel core aluminium ACSR 6/1 6 Al over 1 steel
Concentric stranding: 1, 7, 19, 37, 61 strands, and the ACSR idea of a load-bearing core

Stranding has two electrical consequences. The first is minor and easily stated: because every strand except the central one follows a helix, its true length exceeds the length of the conductor by one or two per cent, and the d.c. resistance is higher than \(\rho l/A\) by the same fraction. Manufacturers' tables already include this, which is why the catalogue \(R_{dc}\) never quite matches a hand calculation from the area.

The second is the one that matters for the rest of Part 2. Magnetically, a stranded conductor is not a solid cylinder. It is a bundle of parallel filaments, and the flux linking the bundle depends on the distances between the filaments as well as on their individual radii. Chapter 6 will derive the general result, but the definition can be stated now because it is a geometrical fact about the conductor alone, independent of what the line is doing.

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Definition — geometric mean radius
\[ D_s = \sqrt[N^2]{\prod_{i=1}^{N}\prod_{j=1}^{N} D_{ij}}, \qquad D_{ii} \equiv r' = e^{-1/4}\,r = 0.7788\,r \]

The \(N^2\)-th root of the product of every distance from every strand to every strand, including each strand to itself — for which the self-distance is taken as the fictitious radius \(r' = 0.7788r\) that Chapter 6 derives from the internal flux. For a solid round conductor \(N=1\) and \(D_s\) collapses to \(r'\) itself.

Example 4 evaluates this for the seven-strand conductor and finds \(D_s = 2.177\,r_{\text{strand}}\), which is a little less than the physical outer radius \(3r_{\text{strand}}\) — as it must be, since the definition averages distances that include the small self-distances. For ACSR the steel core is normally excluded from the calculation, on the grounds that it carries negligible current, and manufacturers publish the resulting \(D_s\) directly; the values in the table of Section 5-5 are of that kind.

Section 5-7

Resistance: Temperature and Skin Effect

Of the four line parameters, resistance is the only one that dissipates energy, and it is the one most sensitive to conditions of operation. The starting point is elementary,

D.C. resistance
\[ R_{dc} = \frac{\rho\,l}{A}\quad\Omega, \qquad \rho \text{ in }\Omega\text{·m},\; l \text{ in m},\; A \text{ in m}^2 \]

and two corrections turn it into something usable. The first is temperature. Over the range a conductor actually experiences, resistivity rises very nearly linearly with temperature, so \(R_t = R_0(1+\alpha_0 t)\). Plotting \(R\) against \(t\) gives a straight line that, extrapolated backwards, meets the temperature axis at \(t = -1/\alpha_0\). Calling that intercept \(-T\) turns the correction into a ratio of two lengths along the same straight line, which is far easier to use than the coefficient form:

Temperature correction by similar triangles
\[ \frac{R_2}{R_1} = \frac{T + t_2}{T + t_1}, \qquad T = \frac{1}{\alpha_0} \]
\[ T = 241\;^\circ\text{C (hard-drawn copper)}, \qquad T = 228\;^\circ\text{C (hard-drawn aluminium)} \]

An aluminium conductor at its summer operating temperature of 75 °C therefore has resistance \((228+75)/(228+20) = 1.222\) times the catalogue value — a 22% increase that must not be left out of a loss or voltage-drop calculation.

The second correction is the skin effect. Under alternating current, the flux inside the conductor links the inner filaments more completely than the outer ones, so the inner filaments have a larger internal inductance. Since all filaments are in parallel and share the same terminal voltage, current redistributes toward the surface where the impedance is lower. The effective area is reduced and \(R_{ac} > R_{dc}\). The natural scale of the effect is the skin depth,

Skin depth in aluminium at 50 Hz
\[ \delta = \sqrt{\frac{\rho}{\pi f \mu}} = \sqrt{\frac{2.83\times10^{-8}}{\pi(50)(4\pi\times10^{-7})}} = \sqrt{1.434\times10^{-4}} = 11.97\;\text{mm} \]

A Zebra conductor has an outer radius of 14.3 mm, comparable with \(\delta\), so the effect is real but modest: \(R_{ac}/R_{dc}\) for ACSR at 50 Hz typically lies between 1.02 and 1.05. It rises with frequency, with conductor size and with permeability, which is one more reason not to make a solid steel conductor. The hollow-core and expanded-core constructions used at extra-high voltage exploit the same physics from the other side: metal placed at the centre of a large conductor is doing very little, so it may as well be replaced by a light former.

A related redistribution, the proximity effect, arises when the return conductor is close enough for its field to distort the current density in this one. On overhead lines the phase spacing is metres and the effect is negligible; in the closely packed cores of an underground cable it is not, and Chapter 9 returns to it.

Three resistances, one conductor. The \(R_{dc}\) computed from \(\rho l/A\); the catalogue \(R_{dc}\), higher by the spiralling allowance; and the operating \(R_{ac}\), higher again by the temperature ratio and the skin-effect ratio. A loss calculation that quietly uses the first where it needs the third can be 25% adrift, and the error is always in the optimistic direction.
Section 5-8

Insulators and the String Voltage Distribution

An insulator has to do two things at once: hold the mechanical load of the conductor, and stand off the line-to-earth voltage against both a dry power-frequency stress and the far higher transient of a lightning or switching surge. It must do the second in rain, in fog and under a coating of industrial dust, which is why the shape of every insulator is a sequence of sheds — the underside of each shed stays dry, so the leakage path along the surface is several times the straight-line distance.

Four types cover practice. Pin insulators are mounted rigidly on a spindle on the cross-arm and are economic up to about 33 kV; above that they become clumsy and expensive. Suspension insulators are discs with metal caps and pins, connected in a flexible string, with the conductor hanging from the bottom; the number of discs is simply increased with voltage, and a damaged disc can be replaced individually. Strain insulators are suspension strings mounted horizontally where the line dead-ends or turns a sharp corner and the string must take the full pull. Shackle insulators are used on low-voltage distribution.

A rough working figure is one standard disc per 11 kV of line voltage, so an 11 kV line uses one, a 66 kV line four or five, a 132 kV line nine or ten, and a 400 kV line twenty-three or so. But a string of \(n\) identical discs does not divide the voltage into \(n\) equal parts, and the reason is a stray capacitance that cannot be designed away.

earthed cross-arm C V₁ C V₂ = (1+k)V₁ C V₃ = (1+3k+k²)V₁ line conductor kC kC I₂ I₃ each shunt branch adds charging current — the lowest unit carries the most
Why the disc nearest the conductor is the most stressed

Each disc has a self-capacitance \(C\) between its cap and its pin. Each metal link between two discs also has a capacitance to the earthed tower, which is nearby; call it \(kC\), with \(k\) typically between 0.1 and 0.2. The self-capacitances form a series chain from the cross-arm to the conductor, but at every intermediate node some of the current is diverted to earth through the shunt capacitance, so the current in the chain is not the same all the way down. It grows toward the conductor, and since each disc has the same \(C\), the voltage across a disc is proportional to the current through it.

Number the discs 1 at the cross-arm and \(n\) at the conductor. Applying Kirchhoff's current law at the node between disc 1 and disc 2, the current entering disc 2 is the current leaving disc 1 plus the shunt current drawn from that node, which is set by the voltage of the node above earth — namely \(V_1\):

Node between units 1 and 2
\[ \omega C V_2 = \omega C V_1 + \omega (kC) V_1 \;\Longrightarrow\; V_2 = (1+k)V_1 \]

At the next node the shunt capacitance sees the whole voltage accumulated so far, \(V_1+V_2\):

Node between units 2 and 3
\[ \omega C V_3 = \omega C V_2 + \omega(kC)(V_1+V_2) \]
\[ V_3 = (1+k)V_1 + k\big[V_1 + (1+k)V_1\big] = \left(1+3k+k^2\right)V_1 \]

The pattern continues; every step adds a larger increment, so \(V_1 < V_2 < V_3 < \cdots < V_n\) always. The unit nearest the line conductor takes the largest share, is the first to flash over, and is the one that fails in service. The quality of the distribution is measured by

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String efficiency
\[ \eta = \frac{\text{voltage across the whole string}}{n \times \text{voltage across the unit nearest the conductor}} = \frac{V}{n\,V_n} \]

A perfect string would have \(\eta = 100\%\). Real strings run from about 90% for a short string with a long cross-arm down to 50% or less for a long string at extra-high voltage, which is precisely why \(\eta\) falls as \(n\) rises and why simply adding discs gives diminishing returns.

Three remedies follow directly from the derivation, and each attacks a different term. Making the cross-arm longer moves the tower metal away from the string and reduces \(k\) — cheap, but limited by tower economics. Capacitance grading gives the lower discs a larger \(C\), so that the same increasing current produces the same voltage in every unit; it works, but requires several different disc types on one string and is rarely done. Static shielding — a large metal grading ring, bell-mouthed toward the conductor, fitted at the bottom of the string — introduces a capacitance from each link to the line conductor that injects current in the opposite sense to the earth capacitance, cancelling it. The grading ring is standard on every extra-high-voltage string, and it also protects the bottom discs from power-arc damage.

Section 5-9

Supports, Sag and Tension

Supports carry the conductors at a height that guarantees clearance and hold the phases apart at a spacing that guarantees no flashover between them. Wooden and concrete poles serve distribution; steel lattice towers serve transmission, and are classified by the angle of deviation they are designed for — type A for a straight run up to 2°, B up to 15°, C up to 30°, D up to 60°, with special dead-end towers at line terminations and river crossings.

What hangs between two towers is not a straight line. A flexible conductor of uniform weight suspended between two points takes the shape of a catenary, and the vertical distance from the line joining the supports down to the lowest point is the sag. The sag is not an accident to be minimised; it is a design variable, because it fixes the tension, and the tension is what the conductor and the tower have to survive.

Take supports at the same level, a span \(L\), a conductor of weight \(w\) per unit length, and let \(T\) be the horizontal component of tension — constant along the conductor, since no horizontal force acts on it between supports. Put the origin at the lowest point and consider the portion from there out to a general point \((x,y)\). It is in equilibrium under three forces: the horizontal pull \(T\) at the origin, the tension along the curve at \((x,y)\), and the weight \(wx\) of the portion acting at its centroid, a distance \(x/2\) from the origin. Taking moments about \((x,y)\),

Moment balance on a length of conductor
\[ T\,y = (w x)\frac{x}{2} \;\Longrightarrow\; y = \frac{w x^2}{2T} \]

The curve is a parabola — the first term of the catenary, and accurate to better than half a per cent whenever the sag is under about 10% of the span, which covers all normal practice. Setting \(x = L/2\) gives the sag at the support.

🔑
The sag equation
\[ S = \frac{w L^2}{8T}, \qquad T = \frac{\text{ultimate tensile strength}}{\text{factor of safety}} \]

Sag rises as the square of the span and falls as the reciprocal of the tension. Doubling the span for the same tension quadruples the sag, which is why very long crossings need towers of exceptional height rather than exceptional strength.

Real conductors do not hang in still, warm air. Ice builds a concentric sleeve of thickness \(t\) around a conductor of diameter \(d\), whose weight per unit length is \(w_i = \rho_{\text{ice}}\,\pi t (d+t)\) and which acts vertically downward, adding to \(w\). Wind presses on the projected area of the iced conductor, \(w_w = p\,(d+2t)\) per unit length, and acts horizontally. The conductor hangs in the plane of the resultant.

Loading and the two sags
\[ w_t = \sqrt{\left(w + w_i\right)^2 + w_w^2}, \qquad \theta = \tan^{-1}\!\frac{w_w}{w+w_i} \]
\[ S_{\text{slant}} = \frac{w_t L^2}{8T}, \qquad S_{\text{vertical}} = S_{\text{slant}}\cos\theta \]

Only the vertical component reduces ground clearance, so it is the vertical sag that the statutory clearance is measured against, while the slant sag is what determines the tension the tower must resist. When the two supports are at different levels — a hillside, a river bank — the lowest point of the curve is no longer at mid-span. Writing \(x_1\) and \(x_2\) for the horizontal distances from the low point to the lower and higher supports, with \(x_1+x_2 = L\) and a height difference \(h\),

Supports at unequal levels
\[ h = \frac{w}{2T}\left(x_2^2 - x_1^2\right) = \frac{w}{2T}(x_2+x_1)(x_2-x_1) = \frac{wL}{2T}(x_2-x_1) \]
\[ \Longrightarrow\; x_1 = \frac{L}{2} - \frac{T h}{w L}, \qquad x_2 = \frac{L}{2} + \frac{T h}{w L} \]

If \(Th/(wL)\) exceeds \(L/2\), the formula returns a negative \(x_1\), which is the algebra's way of reporting that the lowest point lies outside the span altogether — the conductor rises the whole way from the lower support, and the erection procedure has to be checked for uplift on that tower.

S = wL²/8T L T w·x supports level x₁ x₂ h lowest point supports at unequal levels
The parabolic conductor: moment balance, and the shift of the low point on a slope
Sag is a temperature problem in disguise. A conductor expands when it is hot and when it carries current, and the tension falls as it lengthens; the sag is therefore greatest on the hottest day at full load, and the tension is greatest on the coldest day with an ice load. The clearance is checked at the first condition and the strength at the second, and the sag–tension chart that a designer works from is the pair of curves connecting them. Vibration dampers hung near the clamps handle the third loading case — the low-amplitude aeolian oscillation that a steady light wind sets up, and which fatigues the strands at the point where they are gripped.
Section 5-10

Worked Examples

1 What the comparison costs in kilograms

Problem. 500 kW is to be delivered 1 km away with a line loss of 5% of the transmitted power. Copper of \(\rho = 1.72\times10^{-8}\;\Omega\)·m and density 8890 kg/m³ is used. Find the mass of conductor required (a) by a two-wire d.c. system at 500 V with one conductor earthed, and (b) by a three-phase three-wire a.c. system at 11 kV line voltage and power factor 0.8.

Solution. Loss budget \(W = 0.05\times500\,000 = 25\,000\) W in both cases. For (a) the recipe of Section 5-2 applies directly with \(V_m = 500\) V:

The d.c. line
\[ a_1 = \frac{2P^2\rho l}{WV_m^2} = \frac{2(5\times10^5)^2(1.72\times10^{-8})(1000)}{(2.5\times10^4)(500)^2} = \frac{8.60\times10^{6}}{6.25\times10^{9}} = 1.376\times10^{-3}\;\text{m}^2 \]
\[ \text{Vol} = 2a_1l = 2.752\;\text{m}^3, \qquad m = 2.752\times8890 = 24\,470\;\text{kg} \]

For (b) it is easier to work directly from the line voltage, as in Chapter 2: \(W = P^2\rho l/(a V^2\cos^2\phi)\).

The three-phase line
\[ a = \frac{P^2\rho l}{W V^2\cos^2\phi} = \frac{(5\times10^5)^2(1.72\times10^{-8})(1000)}{(2.5\times10^4)(11\,000)^2(0.64)} = \frac{4.30\times10^{6}}{1.936\times10^{12}} = 2.22\times10^{-6}\;\text{m}^2 \]
\[ \text{Vol} = 3al = 6.66\times10^{-3}\;\text{m}^3, \qquad m = 6.66\times10^{-3}\times8890 = 59.2\;\text{kg} \]

Twenty-four tonnes of copper against fifty-nine kilograms — a ratio of 413. The factor can be assembled from the table of Section 5-4. The three-phase line's peak conductor-to-earth voltage is \(\sqrt2\,(11\,000/\sqrt3) = 8982\) V against 500 V for the d.c. line, and \((8982/500)^2 = 322.6\); the three-phase coefficient of \(0.5\) rather than \(1\) doubles the advantage again; the power factor gives back \(\cos^2\phi = 0.64\). Together \(322.6\times2\times0.64 = 413\). This single arithmetic is the reason no one has ever built a 500 V transmission line.

2 Reading the comparison table as ratios

Problem. A single-phase three-wire system and a three-phase three-wire system deliver the same power over the same distance with the same loss and the same maximum voltage to earth, at a power factor of 0.85. Compare the conductor material required, and state the ratio of the single-phase two-wire earthed system to the three-phase system.

Solution. From the table of Section 5-4, with \(\cos^2\phi = 0.85^2 = 0.7225\):

Two systems at \(\cos\phi = 0.85\)
\[ \text{Vol}_{1\phi,3w} = \frac{5K}{8(0.7225)} = \frac{0.625K}{0.7225} = 0.8651\,K \]
\[ \text{Vol}_{3\phi,3w} = \frac{K}{2(0.7225)} = \frac{0.5K}{0.7225} = 0.6920\,K \]

The single-phase three-wire system needs \(0.8651/0.6920 = 1.25\) times as much metal — exactly 25% more, and the power factor has cancelled out of the ratio because it appears identically in both. The extra 25% is precisely the half-section neutral: \(2.5\) conductor-equivalents against \(2\) for the mid-point-earthed pair the three-phase system ties with.

For the second part, the ordinary single-phase two-wire system with one conductor earthed requires \(2K/\cos^2\phi\), so

The cost of not earthing the mid-point
\[ \frac{\text{Vol}_{1\phi,2w}}{\text{Vol}_{3\phi,3w}} = \frac{2K/\cos^2\phi}{0.5K/\cos^2\phi} = 4 \]

Four times the conductor for the same delivered power — a factor that is again independent of \(P\), \(l\), \(W\) and \(\cos\phi\), and which is simply the square of the doubled voltage the mid-point earth would have provided, times the two-thirds sharing of the three-phase arrangement.

3 Replacing copper with aluminium

Problem. A 132 kV line is designed with a hard-drawn copper conductor of 120 mm² cross-section. It is to be replaced by ACSR of equal d.c. resistance, of which 78% of the cross-section is aluminium and 22% is steel. Find the aluminium area required, the total conductor area, the change in overall diameter, and the change in mass per kilometre. Neglect the conductance of the steel.

Solution. Equal resistance means equal \(\rho/A\), so the aluminium area must be scaled by the resistivity ratio:

Sizing the aluminium
\[ A_{Al} = A_{Cu}\frac{\rho_{Al}}{\rho_{Cu}} = 120\times\frac{2.83}{1.72} = 120\times1.6453 = 197.4\;\text{mm}^2 \]
\[ A_{\text{total}} = \frac{197.4}{0.78} = 253.1\;\text{mm}^2, \qquad A_{\text{steel}} = 55.7\;\text{mm}^2 \]

Diameters follow from the areas, ignoring the small interstices between strands:

Diameter and mass
\[ \frac{d_{ACSR}}{d_{Cu}} = \sqrt{\frac{253.1}{120}} = \sqrt{2.109} = 1.452 \]
\[ m_{Cu} = 120\times10^{-6}\times1000\times8890 = 1066.8\;\text{kg/km} \]
\[ m_{ACSR} = \big(197.4\times2703 + 55.7\times7800\big)\times10^{-6}\times1000 = 533.5 + 434.5 = 968.0\;\text{kg/km} \]

The ACSR conductor is 45% larger in diameter but 9% lighter, and it carries more than twice the breaking load — \(197.4(180) + 55.7(1350) = 110.7\) kN of ultimate strength against \(120(400) = 48\) kN for the copper, almost all of it contributed by the steel. The diameter increase is not a penalty at 132 kV and becomes a positive benefit at 400 kV, where the surface voltage gradient must be held below the corona threshold of Chapter 15. Note also how much of the mass is now steel: the core weighs almost as much as the aluminium, which is why very high steel fractions are used only where the mechanical demand — long river crossings, heavy ice zones — really requires them.

4 The geometric mean radius of a seven-strand conductor

Problem. A seven-strand conductor is made of identical solid round strands of radius \(r\). Find its geometric mean radius, and compare it with the GMR of a solid conductor having the same overall diameter.

Solution. Six strands sit on a circle of radius \(2r\) about a central strand. The definition of Section 5-6 requires the \(49\)th root of the product of all \(7\times7\) distances, so the distances must be counted carefully.

DistanceValueHow many
Strand to itself\(r' = 0.7788r\)7
Centre to outer, and outer to centre\(2r\)12
Outer to adjacent outer (hexagon side)\(2r\)12
Outer to next-but-one outer\(2\sqrt3\,r\)12
Outer to diametrically opposite outer\(4r\)6

The counts total \(7+12+12+12+6 = 49\), as they must. The hexagon side equals the circumradius, which is why the first two rows share the value \(2r\).

Taking the 49th root
\[ D_s = \Big[(0.7788r)^7\,(2r)^{24}\,(2\sqrt3\,r)^{12}\,(4r)^{6}\Big]^{1/49} \]
\[ \ln\frac{D_s}{r} = \frac{7(-0.24993) + 24(0.69315) + 12(1.24245) + 6(1.38629)}{49} = \frac{38.1132}{49} = 0.77782 \]
\[ D_s = e^{0.77782}\,r = 2.177\,r \]

The overall radius of the conductor is \(3r\), so a solid conductor of the same outside diameter would have \(D_s = 0.7788\times3r = 2.336r\). Stranding therefore lowers the GMR by about 7%, and by the formula \(L = 2\times10^{-7}\ln(D_{eq}/D_s)\) of Chapter 6 this raises the inductance slightly. The same calculation for 19 strands gives \(D_s = 3.582\,r_{\text{strand}}\) against a solid \(0.7788\times5r = 3.894r\) — a deficit of 8%, so the gap does not close as layers are added. It hardly matters: \(D_s\) enters only through a logarithm, and an 8% change in it shifts the inductance of a typical line by well under 2%.

5 Voltage distribution along a three-unit string

Problem. A 33 kV three-phase line uses suspension strings of three identical discs. The capacitance of each link to earth is one-tenth of the self-capacitance of a disc. Find the voltage across each disc and the string efficiency. Repeat for a link-to-earth capacitance of one-fifth, and comment.

Solution. The string stands off the line-to-earth voltage, not the line voltage:

Voltage across the string
\[ V = \frac{33}{\sqrt3} = 19.05\;\text{kV} \]

With \(k = 0.1\), the results of Section 5-8 give \(V_2 = 1.1V_1\) and \(V_3 = (1+0.3+0.01)V_1 = 1.31V_1\), so

Solving for \(V_1\)
\[ V = V_1\left(1 + 1.1 + 1.31\right) = 3.41\,V_1 = 19.05 \;\Longrightarrow\; V_1 = 5.587\;\text{kV} \]
\[ V_2 = 6.146\;\text{kV}, \qquad V_3 = 7.319\;\text{kV} \]
\[ \eta = \frac{19.05}{3\times7.319} = \frac{19.05}{21.957} = 86.8\% \]

With \(k = 0.2\): \(V_2 = 1.2V_1\), \(V_3 = (1+0.6+0.04)V_1 = 1.64V_1\), and the sum is \(3.84V_1\).

A larger earth capacitance
\[ V_1 = \frac{19.05}{3.84} = 4.961\;\text{kV}, \quad V_2 = 5.953\;\text{kV}, \quad V_3 = 8.136\;\text{kV} \]
\[ \eta = \frac{19.05}{3\times8.136} = 78.0\% \]

Doubling \(k\) has pushed nearly 43% of the string voltage onto the bottom disc and cost nearly nine points of efficiency. Since \(k\) is set by how close the earthed tower steel is to the string, this is the quantitative case for a longer cross-arm — and, at higher voltages where \(n\) is large and \(\eta\) falls further, for the grading ring.

6 Sag under ice and wind

Problem. A transmission line conductor of diameter 19.5 mm weighs 0.85 kg/m and has an ultimate strength of 8000 kg. It is strung with a factor of safety of 2 over a span of 200 m. Find the sag in still air, and the vertical sag when the conductor carries a 10 mm radial coat of ice (ice density 910 kg/m³) and a wind pressure of 40 kg/m² acts on the projected area.

Solution. The working tension is \(T = 8000/2 = 4000\) kg. In still air the sag equation applies with \(w = 0.85\) kg/m:

Still-air sag
\[ S = \frac{wL^2}{8T} = \frac{0.85\times200^2}{8\times4000} = \frac{34\,000}{32\,000} = 1.063\;\text{m} \]

Now the loading. The ice sleeve is an annulus of inner diameter \(d = 0.0195\) m and thickness \(t = 0.010\) m, so its cross-sectional area is \(\pi t(d+t)\):

Ice and wind loads per metre
\[ w_i = 910\,\pi\,(0.010)(0.0195+0.010) = 910\times\pi\times2.95\times10^{-4} = 0.843\;\text{kg/m} \]
\[ w_w = 40\,(d+2t) = 40\,(0.0195+0.020) = 40\times0.0395 = 1.580\;\text{kg/m} \]

The ice adds to the weight; the wind acts at right angles to it.

Resultant load and the two sags
\[ w+w_i = 0.85+0.843 = 1.693\;\text{kg/m}, \qquad w_t = \sqrt{1.693^2 + 1.580^2} = \sqrt{5.363} = 2.316\;\text{kg/m} \]
\[ \theta = \tan^{-1}\frac{1.580}{1.693} = 43.03^\circ, \qquad S_{\text{slant}} = \frac{2.316\times200^2}{8\times4000} = 2.895\;\text{m} \]
\[ S_{\text{vertical}} = S_{\text{slant}}\cos\theta = 2.895\times0.7311 = 2.116\;\text{m} \]

The vertical sag has doubled, from 1.06 m to 2.12 m, and it is that figure the ground-clearance check must use. The slant sag is larger still, and the conductor swings 43° out of the vertical plane, which is what sets the horizontal phase spacing and the width of the right of way. Observe also that the vertical sag could have been obtained directly as \((w+w_i)L^2/(8T) = 1.693\times40\,000/32\,000 = 2.116\) m: the wind changes the plane of the curve but not the vertical component of the load, so it affects the tension and the swing, not the clearance. Both routes agree, which is the check worth doing.

Review

Chapter Summary

Equal terms

Systems are compared at equal \(P\), \(l\), \(W\) and maximum voltage to earth — the last because air to the tower is what breaks down.

The reference \(K\)

\(K = 4P^2\rho l^2/(WV_m^2)\), the volume of the two-wire d.c. line with one conductor earthed.

Mid-point earthing

Doubles the working voltage at no insulation cost, so it divides the conductor volume by four.

The winner

Three-phase three-wire ties at \(K/(2\cos^2\phi)\) and wins on conductor count — three wires, not four.

Aluminium

1.645 times the area, 1.28 times the diameter, half the weight of copper at equal resistance; steel core supplies the strength.

Stranding

\(N = 3n(n-1)+1\), \(D = (2n-1)d\); the seven-strand GMR is \(2.177r\).

Resistance

\(R_2/R_1 = (T+t_2)/(T+t_1)\) with \(T = 228\) °C for aluminium; skin effect adds a further 2–5% at 50 Hz.

String efficiency

\(\eta = V/(nV_n)\); the bottom disc is worst because shunt capacitance to earth adds charging current at every link.

Sag

\(S = wL^2/(8T)\) from a moment balance; ice adds vertically, wind horizontally, and only the vertical component eats clearance.

Practice

Practice Problems

Unless stated otherwise, compare systems at equal power, distance, loss and maximum voltage to earth, and take \(\rho_{Cu} = 1.72\times10^{-8}\;\Omega\)·m, \(\rho_{Al} = 2.83\times10^{-8}\;\Omega\)·m.

  1. Starting from the four-step recipe of Section 5-2, derive the conductor volume of the two-phase four-wire system and confirm that it equals \(K/(2\cos^2\phi)\). State clearly at each step which voltage you are using and why.
  2. A three-phase four-wire system and a three-phase three-wire system supply the same balanced load. Show that the four-wire system requires \(7/6\) times the conductor material, and explain why the ratio does not depend on the power factor.
  3. Repeat the ten-system comparison on the underground basis, in which the maximum voltage between conductors — not between conductor and earth — is held equal. Show that the two-wire d.c. system with one conductor earthed and the mid-point-earthed system now require the same volume, and explain in one sentence why the advantage of mid-point earthing disappears.
  4. A hard-drawn copper conductor of 150 mm² is replaced by an all-aluminium conductor of the same d.c. resistance. Find the aluminium area, the ratio of diameters, the ratio of masses, and the percentage change in the breaking load if the tensile strengths are 400 MPa and 180 MPa respectively.
  5. A 19-strand conductor is made of strands of radius \(r\). The 361 inter-strand distances fall into nine classes: \(r'\) (19 of them), \(2r\) (84), \(2\sqrt3 r\) (60), \(4r\) (54), \(2\sqrt7 r\) (72), \(6r\) (24), \(4\sqrt3 r\) (18), \(2\sqrt{13}\,r\) (24) and \(8r\) (6). Confirm that the counts total 361 and show that the geometric mean radius is \(3.582\,r\).
  6. An ACSR conductor has a d.c. resistance of 0.139 Ω/km at 20 °C. Find its resistance at an operating temperature of 80 °C, and then the a.c. resistance if the skin-effect ratio is 1.04. By what percentage would the \(I^2R\) loss of a 200 km line be underestimated if the catalogue value at 20 °C were used?
  7. A string of four suspension discs has a link-to-earth capacitance equal to \(0.15\) of the disc self-capacitance. Derive \(V_4\) in terms of \(V_1\), find the voltage across each disc for a line-to-earth voltage of 76 kV, and compute the string efficiency. Compare with the three-disc result of Example 5 and explain the trend.
  8. A conductor weighing 1.2 kg/m is strung between two supports 250 m apart whose levels differ by 8 m, at a working tension of 3000 kg. Locate the lowest point of the curve, find the sag measured from each support, and determine whether the conductor rises the whole way from the lower support.
Tip: in every comparison problem, write down the four equal quantities before touching a formula, then ask what voltage the arrangement actually presents to the load. Nearly every wrong answer in this topic comes from using \(V_m\) where \(2V_m\) is available, or from forgetting that \(V_m\) is a peak and the a.c. systems get only \(V_m/\sqrt2\). The algebra afterwards is the same four lines every time.