Question 2 of 7: Line Transposition and the Salient-Pole Machine
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2013 —
07-Elec-B7 Power Systems Engineering. Open-book, three hours, non-communicating
calculator permitted. Seven problems of equal value (20 points each); any five
constitute a complete paper and only the first five appearing in the answer book
are marked. All seven are solved here, because the set is a study
resource.
Reference texts.
M. E. El-Hawary, Electrical Power Systems: Design and Analysis,
rev. ed., IEEE Press/Wiley — the source of this paper's notation
(ABCD two-port, the “cantilever” transformer equivalent, and the
equal-area treatment of transient stability).
J. D. Glover, T. J. Overbye and M. S. Sarma, Power System Analysis and
Design, 6th ed., Cengage — transmission-line parameters (Ch. 4–5),
power flow (Ch. 6), symmetrical faults (Ch. 7), symmetrical components and
unsymmetrical faults (Ch. 8–9), transient stability (Ch. 11).
J. J. Grainger and W. D. Stevenson, Power System Analysis,
McGraw-Hill — sequence networks and fault calculations.
S. J. Chapman, Electric Machinery Fundamentals, 5th ed.,
McGraw-Hill — transformers (Ch. 2) and synchronous machines (Ch. 4–5).
Canadian practice: CSA C22.3 No. 1 Overhead Systems (conductor
temperature, sag and clearance), CAN/CSA-C88 and CSA C50 (power transformers and
insulating oil), and CSA C22.3 No. 1 Annex on fault-current duty.
Problem 2: Line Transposition and the Salient-Pole Machine (20 points)
Part (a) — transposition. An overhead three-phase circuit
is almost never built with its three phase conductors symmetrically placed with
respect to one another and to ground: a flat horizontal configuration, a vertical
configuration on a single pole, or a triangular configuration on a delta tower all
put the three conductors at different mutual spacings. Because the inductance and
capacitance of a phase depend on the logarithm of its distance to the other
phases, unequal spacing makes the three phase impedances and admittances unequal.
The circuit is then unbalanced even when the loads are balanced: it
produces negative- and zero-sequence voltages, which cause double-frequency rotor
heating in connected machines, spurious operation of ground relays, and telephone
interference from residual currents.
Transposition is the practice of rotating the physical
positions of the three phase conductors at intervals along the route so that each
phase occupies each of the three available positions for one third of the total
length. Over a complete transposition cycle the average distance from any one
phase to the other two is the same for all three phases, and the line becomes
electrically balanced: the series impedance matrix becomes fully symmetric, the
mutual couplings are equalised, and the sequence impedances decouple. That is what
licenses the single-phase, per-phase-equivalent analysis used everywhere else in
this paper, including the geometric-mean-distance formula
$D_m = \sqrt[3]{D_{ab}D_{bc}D_{ca}}$.
Mechanically it is done at a transposition structure. The three
conductors are dead-ended on a heavier tower, and jumpers carry each phase across
to the next position in a fixed rotation (a → b → c → a) —
either on a purpose-built transposition tower with staggered arms, or in a
substation, or, on a very long line, at the two one-third points of the route so
that the cycle completes over the whole line. On modern lines full transposition
is often omitted on short circuits, where the residual unbalance is tolerable, and
is instead achieved statistically over a network by transposing only long or
critical lines; where a double-circuit line is involved the two circuits are also
phased so as to cancel one another's unbalance.
Given (parts b and c).
Quantity
Value
Meaning
$X_d$
$1.15\ \text{pu}$
direct-axis synchronous reactance
$X_q$
$0.95\ \text{pu}$
quadrature-axis synchronous reactance
$r_a$
$\approx 0$
armature resistance, neglected
$A$
$0.98\angle 0.2^\circ$
line constant
$B$
$0.2\angle 85^\circ$
line constant
$V_L,\ I_L$
$1.0\angle 0^\circ$ pu, $1.0\angle 0^\circ$ pu
load voltage and current, unity power factor
Find. The apparent power the machine delivers at its own
terminals, then the excitation (internal) voltage $E_f$ and the torque angle
$\delta$ measured from the terminal voltage.
Approach. The load is at the receiving end of the
line, so the machine sits at the sending end: push the load voltage and
current back through the ABCD model to get the machine terminal quantities, form
$S = V_t I_a^{*}$, then apply the two-reaction (Blondel) construction for a
salient-pole machine.
Recover the fourth line constant. Only $A$ and $B$ are
printed, but reciprocity supplies $C$ exactly as in Problem 1:
$$C=\frac{A^{2}-1}{B}=\frac{0.0402\angle170.40^\circ}{0.2000\angle85.00^\circ}
=0.2009\angle85.40^\circ$$
Again the result is essentially $+j0.2009$, a pure shunt susceptance.
Machine terminal voltage. The load is the receiving end, so
$$V_t=A V_L+B I_L
=0.9800\angle0.20^\circ\times 1.0+0.2000\angle85.00^\circ\times 1.0
=1.0178\angle11.49^\circ\ \text{pu}.$$
The 11.5° advance is the transmission angle across the line.
Apparent power output of the machine. With both terminal
phasors known,
$$S=V_t I_a^{*}
=\left(1.0178\angle11.49^\circ\right)\left(1.0167\angle11.56^\circ\right)^{*}$$
$$\boxed{S=1.0348\angle-0.07^\circ\ \text{pu}
= 1.0348\;-\;j0.0013\ \text{pu}}$$
so $|S| = 1.0348$ pu, $P = 1.0348$ pu
and $Q = -0.0013$ pu. The machine therefore delivers about
1.035 pu of real power and essentially no net reactive power: the
line's charging susceptance $C$ happens to supply almost exactly the reactive
absorption of its own series reactance $B$ at this loading, so the machine runs at
unity power factor even though it is 11.5° ahead of the load.
Part (c) — set up the two-reaction construction. A
salient-pole rotor presents different reluctance along the pole axis ($d$) and
between poles ($q$), so a single synchronous reactance will not do. With $r_a$
neglected, the torque angle is obtained from the phasor
$E_q = V_t + jX_q I_a$, whose direction defines the $q$-axis:
$$\tan\delta=\frac{I_a X_q\cos\varphi}{V_t+I_a X_q\sin\varphi}$$
where $\varphi$ is the angle by which $I_a$ lags $V_t$. Here
$\varphi = -0.0724^\circ$ (a whisker leading), and
$I_a X_q = 0.9659$ pu, so
$$\tan\delta=\frac{0.9659}
{1.0178-0.0012}
=0.9501
\;\Longrightarrow\;\boxed{\delta=43.54^\circ}$$
Resolve the armature current onto the two axes. The current
lies at $(\delta+\varphi)$ from the $q$-axis, so
$$I_d=I_a\sin(\delta+\varphi)=1.0167
\sin(43.46^\circ)=0.6994\ \text{pu},
\qquad I_q=I_a\cos(\delta+\varphi)=0.7380\ \text{pu}.$$
Only $I_d$ magnetises along the pole axis, and only it is multiplied by $X_d$.
Excitation voltage. Projecting the phasor equation onto the
$q$-axis with $r_a=0$,
$$E_f=V_t\cos\delta+I_d X_d
=1.0178\cos(43.54^\circ)
+0.6994\times 1.15$$
$$\boxed{E_f=1.5422\ \text{pu}}$$
An excitation of 1.54 pu against a terminal voltage of 1.02 pu is a
normal over-excited condition for a machine holding a 43.5° torque angle.
Independent check on the whole construction. The salient-pole
power expression must reproduce the real power already found from
$V_t I_a^{*}$:
$$P=\frac{E_f V_t}{X_d}\sin\delta
+\frac{V_t^{2}}{2}\left(\frac{1}{X_q}-\frac{1}{X_d}\right)\sin 2\delta
=0.9401
+0.0947
=1.0348\ \text{pu},$$
which matches step 4 to four figures. The second term is the reluctance power,
about 8 % of the total here — the part a round-rotor model would have
missed.
Figure 2.1 — two-reaction (Blondel) phasor diagram. Adding jIaXq to Vt locates the q-axis and therefore the torque angle; Ef then lies along the same axis, longer by Id(Xd − Xq).