Electrical Machines · Chapter 61

Torque Equation of the Induction Motor

Part 4 · Induction Motors — one equation for starting, running and maximum torque, and a result about rotor resistance that decides how machines are designed.

Prof. Mithun Mondal Engineering Devotion Digital Textbook
i Learning Objectives

By the end of this chapter you should be able to:

  • Derive the starting torque from the rotor quantities of Chapter 60.

  • State and use the constant \(K_1 = 3/2\pi n_s\) to obtain torque in newton metres.

  • Explain why a cage motor gives poor starting torque per ampere.

  • Explain the two competing effects in a slip-ring starter.

  • Derive the condition \(R_2 = X_{20}\) for maximum starting torque.

  • Show that torque varies as the square of the supply voltage.

  • Obtain the torque under running conditions as a function of slip.

  • Derive \(s_{max} = R_2/X_{20}\) and show that \(T_{max}\) is independent of \(R_2\).

Section 61-1

Starting Torque

The torque developed by the motor at the instant of starting is called the starting torque. In some cases it is greater than the normal running torque, and in others somewhat less.

! Notation, Fixed Once and For All

Following Chapter 60, the subscript 20 always means "at standstill":

SymbolMeaning
\(E_{20}\)Rotor EMF per phase at standstill
\(X_{20}\)Rotor reactance per phase at standstill
\(R_2\)Rotor resistance per phase — the same at all slips
\(E_2 = sE_{20}\), \(X_2 = sX_{20}\)The running values

Some texts write \(E_2\) and \(X_2\) for the standstill values and \(E_r\), \(X_r\) for the running ones. The physics is identical; only be sure which convention a formula assumes before using it.

At standstill \(s = 1\), so the rotor quantities take their standstill values:

\[Z_{20} = \sqrt{R_2^{2} + X_{20}^{2}}\]
\[I_2 = \frac{E_{20}}{Z_{20}} = \frac{E_{20}}{\sqrt{R_2^{2} + X_{20}^{2}}}, \qquad \cos\phi_2 = \frac{R_2}{Z_{20}} = \frac{R_2}{\sqrt{R_2^{2} + X_{20}^{2}}}\]
🔧
Substituting into \(T = K_1E_{20}I_2\cos\phi_2\)
The starting torque
\[\begin{aligned} T_{st} &= K_1E_{20}\cdot\frac{E_{20}}{\sqrt{R_2^{2}+X_{20}^{2}}}\times\frac{R_2}{\sqrt{R_2^{2}+X_{20}^{2}}}\\[6pt] \Longrightarrow\quad T_{st} &= \frac{K_1E_{20}^{2}R_2}{R_2^{2}+X_{20}^{2}} \end{aligned}\]

If \(E_{20}\) and \(X_{20}\) are both constant, then \(K_2 = K_1E_{20}^{2}\) is constant, and

\[T_{st} = K_2\cdot\frac{R_2}{R_2^{2}+X_{20}^{2}} = K_2\frac{R_2}{Z_{20}^{2}}\]

This second form is the useful one for Section 61-5, because it isolates the dependence on rotor resistance — the one quantity a designer can choose freely.

Section 61-2

The Constant \(K_1\)

So far the torque has been a proportionality. To obtain an actual value in newton metres, the constant must be evaluated. It turns out to be

\[K_1 = \frac{3}{2\pi n_s}\]

where \(n_s\) is the synchronous speed in revolutions per second. The factor 3 is for the three phases, and \(2\pi n_s = \omega_s\) is the synchronous speed in radians per second.

📐
Where It Comes From
Torque is air-gap power divided by synchronous speed

The power crossing the air gap in all three phases is \(P_g = 3E_{20}I_2\cos\phi_2\). Torque is that power divided by the speed at which the field turns:

\[T = \frac{P_g}{\omega_s} = \frac{3E_{20}I_2\cos\phi_2}{2\pi n_s}\]

Note that it is the synchronous speed that appears, not the rotor speed — the torque acts between two fields that both rotate at \(N_s\), as Chapter 60 established. Chapter 63 develops this point into the full power-flow analysis.

The Complete Starting-Torque Equation
\[T_{st} = \frac{3}{2\pi n_s}\cdot\frac{E_{20}^{2}R_2}{R_2^{2}+X_{20}^{2}} \quad\mathrm{N\,m}\]

Take care with units: \(n_s\) must be in rev/s, not rev/min. For a 4-pole 50 Hz machine, \(N_s = 1500\) rev/min but \(n_s = 25\) rev/s.

Video · Starting, Running and Maximum Torque
1 Worked Example 61.1 — Starting Torque in Newton Metres

Problem. The 4-pole, 50 Hz machine of Chapter 60 has \(E_{20} = 120\) V, \(R_2 = 0.25~\Omega\) and \(X_{20} = 1.20~\Omega\) per phase. Find the starting torque.

The constant.

\[n_s = \frac{2f}{P} = \frac{2(50)}{4} = 25~\mathrm{rev/s}\]
\[K_1 = \frac{3}{2\pi(25)} = \frac{3}{157.080} = 0.019099\]

The rotor factor.

\[Z_{20}^{2} = (0.25)^{2} + (1.20)^{2} = 0.0625 + 1.4400 = 1.5025\]
\[\frac{E_{20}^{2}R_2}{Z_{20}^{2}} = \frac{(14400)(0.25)}{1.5025} = \frac{3600}{1.5025} = 2396.01\]

Starting torque.

\[T_{st} = (0.019099)(2396.01) = 45.76~\mathrm{N\,m}\]

Comment. Section 61-9 will show that this machine's maximum torque is 114.59 N m, so the starting torque is only 39.9 % of what the machine is capable of — a poor showing, and typical of a cage motor.

Notice how much of the denominator is reactance: 1.44 out of 1.5025, or 95.8 %. The starting torque of a cage machine is limited almost entirely by rotor reactance, not by resistance, and that observation is the key to Sections 61-3 and 61-5.

Section 61-3

Starting Torque of a Cage Motor

  • The resistance of a squirrel-cage rotor is fixed and small compared with its reactance, which is very large at start — because at standstill the frequency of the rotor currents equals the supply frequency.

  • Hence the starting current \(I_2\), though very large in magnitude, lags by a very large angle behind \(E_{20}\), with the result that the starting torque per ampere is very poor.

  • It is roughly 1.5 times the full-load torque, although the starting current is 5 to 7 times the full-load current.

  • Such motors are therefore not very useful where the motor has to start against heavy loads.

The arithmetic of Chapter 60 makes the point precisely. At standstill the rotor power factor of the reference machine is 0.204, so roughly four fifths of that enormous starting current produces no torque at all — it merely heats the rotor and loads the supply. The cage motor's problem is not a shortage of current; it is that the current is in the wrong phase.
Section 61-4

Starting Torque of a Slip-Ring Motor

  • The starting torque of such a motor is increased by improving its power factor, by adding external resistance in the rotor circuit from a star-connected rheostat.

  • The rheostat resistance is progressively cut out as the motor gathers speed.

Two Effects Pulling Opposite Ways
Which one wins depends on how much resistance

Adding external resistance increases the rotor impedance and so reduces the rotor current. But it also improves the rotor power factor. Since \(T \propto I_2\cos\phi_2\), the two effects compete:

  • At first, the effect of improved power factor predominates over the current-decreasing effect of impedance. Hence the starting torque is increased.

  • After a certain point, the effect of increased impedance predominates over the improved power factor, and so the torque starts decreasing.

There is therefore a definite optimum resistance, located in Section 61-5.

Starting torque against rotor resistance R₂ = X₂₀ → Tₛₜ = 114.6 N·m cage: R₂ = 0.25 → 45.8 N·m 01.02.03.04.0 rotor resistance R₂ (Ω/phase)
Starting torque is greatest when the rotor resistance equals the standstill reactance.
Section 61-5

Maximum Starting Torque

Differentiate the starting torque with respect to the rotor resistance and set the result to zero.

\[\begin{aligned} T_{st} &= \frac{K_2R_2}{R_2^{2}+X_{20}^{2}}\\[8pt] \therefore\ \frac{dT_{st}}{dR_2} &= K_2\left[\frac{1}{R_2^{2}+X_{20}^{2}} - \frac{R_2\left(2R_2\right)}{\left(R_2^{2}+X_{20}^{2}\right)^{2}}\right] = 0\\[8pt] &\Longrightarrow\quad R_2^{2}+X_{20}^{2} = 2R_2^{2}\\[8pt] &\Longrightarrow\quad \boxed{R_2 = X_{20}} \end{aligned}\]

Thus \(T_{st}\) is maximum when \(R_2 = X_{20}\). Substituting back:

\[T_{st,max} = \frac{K_1E_{20}^{2}X_{20}}{X_{20}^{2}+X_{20}^{2}} = \frac{K_1E_{20}^{2}}{2X_{20}}\]
The condition has a neat interpretation. When \(R_2 = X_{20}\) the rotor impedance triangle is a right isosceles triangle, so \(\phi_2 = 45^{\circ}\) and \(\cos\phi_2 = 1/\sqrt2\)exactly the condition Chapter 60 found for the greatest value of \(I_2\cos\phi_2\). The two derivations, one by inspection of a table and one by calculus, agree.
2 Worked Example 61.2 — Sizing the Starting Rheostat

Problem. For the machine of Example 61.1, find the external rotor resistance per phase that gives maximum starting torque, and the torque obtained.

Condition.

\[R_2 + R_{ext} = X_{20} = 1.20~\Omega\]
\[R_{ext} = 1.20 - 0.25 = 0.95~\Omega\ \text{per phase}\]

Torque obtained.

\[T_{st,max} = \frac{K_1E_{20}^{2}}{2X_{20}} = \frac{(0.019099)(14400)}{(2)(1.20)} = \frac{275.02}{2.40} = 114.59~\mathrm{N\,m}\]

Improvement.

\[\frac{114.59}{45.76} = 2.504\]

Comment. The starting torque has been two and a half times improved, and Chapter 60 showed that the rotor current at the same time fell from 97.9 A to 70.7 A. More torque from less current is not a paradox — it is the power factor rising from 0.204 to 0.707.

Note that the rheostat must be rated for the full rotor current and for a substantial dissipation, and that it is cut out progressively as the machine accelerates. Leaving it in circuit at full load would waste a great deal of power for no benefit, since at 4 % slip the reactance is negligible and the extra resistance would simply reduce the speed.

Section 61-6

Effect of Supply Voltage

The rotor EMF is induced by the flux, which is set by the applied voltage, so \(E_{20} \propto V\). Hence

\[T_{st} = \frac{K_1E_{20}^{2}R_2}{R_2^{2}+X_{20}^{2}} = \frac{K_1V^{2}R_2}{R_2^{2}+X_{20}^{2}} = \frac{K_3V^{2}R_2}{Z_{20}^{2}}\]
\[\Longrightarrow\quad \boxed{T_{st} \propto V^{2}}\]
Torque Is Very Sensitive to Supply Voltage

A change of 5 % in \(V\) will produce a change of approximately 10 % in the rotor torque.

This is why induction motors stall on voltage dips, and why the starting of a large motor — which itself depresses the supply voltage through the feeder impedance — can be a self-defeating exercise: the very current drawn to start the machine reduces the voltage that produces its torque.

3 Worked Example 61.3 — A Voltage Dip

Problem. The machine of Example 61.1 has a starting torque of 45.76 N m at rated voltage. Find the starting torque at 105 %, 95 % and 90 % of rated voltage.

Table 61.1 — Starting torque against supply voltage.
\(V/V_{rated}\)\(\left(V/V_{rated}\right)^{2}\)Change in \(T\)\(T_{st}\) (N m)
1.051.1025+10.25 %50.45
1.001.000045.76
0.950.9025−9.75 %41.30
0.900.8100−19.00 %37.07

Working, the 90 % row.

\[T_{st} = (45.76)(0.90)^{2} = (45.76)(0.81) = 37.07~\mathrm{N\,m}\]

Comment. The rule of thumb is confirmed: a 5 % voltage change gives about a 10 % torque change, being +10.25 % upward and −9.75 % downward.

The asymmetry is worth noticing. Because the relation is quadratic, a voltage drop costs slightly less torque than an equal rise gains — but the difference is small, and the practical lesson is simply that torque follows voltage steeply in both directions.

A 10 % dip removes nearly a fifth of the torque. If the load torque exceeds what remains, the machine decelerates, the slip rises, the current rises further, the voltage falls further still, and the motor stalls. This runaway is the reason large motors are started on reduced voltage in a controlled way rather than allowed to dip the supply uncontrolled.

Section 61-7

Rotor Quantities Under Running Conditions

  • At standstill, \(s = 1\) and \(f_r = f\).

  • \(E_{20}\) at standstill is maximum, because the relative speed between the rotor and the revolving stator flux is maximum.

  • In fact, an induction motor is equivalent to a three-phase transformer with a short-circuited rotating secondary.

  • Under running conditions the relative speed decreases, and since the rotor EMF is proportional to relative speed, it decreases too.

  • Because the frequency of the rotor quantities also decreases, the rotor reactance decreases with it.

📉
The Three Relations
Hence, under running conditions
\[\begin{aligned} f_r &= sf\\[4pt] E_2 &= sE_{20}\\[4pt] X_2 &= sX_{20} \end{aligned}\]

The reactance falls for a different reason from the EMF. The EMF falls because the rotor is cut more slowly; the reactance falls because \(X = 2\pi f_rL_2\) and the frequency itself has dropped. The rotor resistance, being independent of frequency, does not fall at all.

That asymmetry between \(R_2\) and \(X_2\) is the whole source of the machine's characteristic. Had both scaled with slip, the rotor power factor would be constant and the torque would be a plain straight line.

Section 61-8

Torque Under Running Conditions

The derivation is the same as for starting torque, but with the running values substituted.

\[\begin{aligned} T_r &\propto \Phi\,I_2\cos\phi_2\\[6pt] \Longrightarrow\quad T_r &\propto E_{20}\cdot\frac{E_2}{Z_2}\cdot\frac{R_2}{Z_2} \qquad\left(\because E_{20}\propto\Phi\right)\\[6pt] \Longrightarrow\quad T_r &\propto \left(E_{20}\right)\left(\frac{sE_{20}}{\sqrt{R_2^{2}+\left(sX_{20}\right)^{2}}}\right)\left(\frac{R_2}{\sqrt{R_2^{2}+\left(sX_{20}\right)^{2}}}\right)\\[6pt] \Longrightarrow\quad T_r &\propto \frac{sE_{20}^{2}R_2}{R_2^{2}+\left(sX_{20}\right)^{2}} \end{aligned}\]
The Torque Equation
\[T_r = \frac{3}{2\pi n_s}\left[\frac{sE_{20}^{2}R_2}{R_2^{2}+\left(sX_{20}\right)^{2}}\right] \quad\mathrm{N\,m}\]

Substituting \(s = 1\) recovers the starting torque of Section 61-1 — as it must, since standstill is simply the case \(s = 1\). The starting torque is not a separate formula but a particular value of this one.

Small slip: \(sX_{20} \ll R_2\)
\[T_r \approx \frac{K_1sE_{20}^{2}}{R_2}\]

Torque is proportional to slip — the near-linear working region promised in Chapter 58.

Large slip: \(sX_{20} \gg R_2\)
\[T_r \approx \frac{K_1E_{20}^{2}R_2}{sX_{20}^{2}}\]

Torque falls inversely with slip. Between the two regimes lies a maximum.

4 Worked Example 61.4 — Full-Load Torque and a Power Check

Problem. For the machine of Example 61.1, find the torque at 4 % slip. Then verify the answer by computing the air-gap power, the rotor copper loss and the mechanical output independently.

Torque.

\[sX_{20} = (0.04)(1.20) = 0.0480~\Omega\]
\[R_2^{2}+\left(sX_{20}\right)^{2} = 0.0625 + 0.002304 = 0.064804\]
\[sE_{20}^{2}R_2 = (0.04)(14400)(0.25) = 144.00\]
\[T_r = (0.019099)\left(\frac{144.00}{0.064804}\right) = (0.019099)(2222.09) = 42.44~\mathrm{N\,m}\]

Check, by power. The air-gap power is torque times synchronous angular speed:

\[\omega_s = 2\pi(25) = 157.08~\mathrm{rad/s}, \qquad P_g = (42.44)(157.08) = 6666.3~\mathrm{W}\]

Rotor copper loss, from the rotor current of Chapter 60:

\[I_2 = 18.856~\mathrm{A}, \qquad 3I_2^{2}R_2 = (3)(18.856)^{2}(0.25) = 266.65~\mathrm{W}\]

Compare with \(sP_g\).

\[sP_g = (0.04)(6666.3) = 266.65~\mathrm{W} \quad\checkmark\]

Mechanical power.

\[\omega = 2\pi(24) = 150.80~\mathrm{rad/s}, \qquad P_m = (42.44)(150.80) = 6399.6~\mathrm{W}\]
\[266.65 + 6399.6 = 6666.3 = P_g \quad\checkmark\]

Comment. The two routes agree exactly, which is a strong check on the constant \(K_1\). The rotor copper loss came out as exactly \(sP_g\) without that relation having been assumed anywhere — it fell out of the arithmetic.

That is no accident, and Chapter 63 makes it a general theorem: the air-gap power always divides in the ratio \(s : (1-s)\) between rotor copper loss and mechanical output. Here 4 % is lost and 96 % converted, which is why an induction motor is efficient only at low slip.

Compare this 42.44 N m with the starting torque of 45.76 N m from Example 61.1. The machine develops slightly more torque at standstill than at full load — but it does so while drawing 97.9 A instead of 18.9 A in the rotor.

Section 61-9

Maximum Torque Under Running Conditions

The torque under running conditions is

\[T_r = K_1\cdot\frac{sE_{20}^{2}R_2}{R_2^{2}+\left(sX_{20}\right)^{2}}\]

To make the calculation simple, take \(Y = 1/T_r\). Maximising \(T_r\) is the same as minimising \(Y\), and \(Y\) is much easier to differentiate because the slip appears in the numerator rather than buried in a quotient.

📐
The Derivation
Completing the calculation
\[Y = \frac{1}{T_r} = \frac{R_2^{2}+s^{2}X_{20}^{2}}{K_1sE_{20}^{2}R_2} = \frac{1}{K_1E_{20}^{2}R_2}\left[\frac{R_2^{2}}{s} + sX_{20}^{2}\right]\]

Differentiating with respect to \(s\) and setting to zero:

\[\frac{dY}{ds} = \frac{1}{K_1E_{20}^{2}R_2}\left[-\frac{R_2^{2}}{s^{2}} + X_{20}^{2}\right] = 0\]
\[\Longrightarrow\quad \frac{R_2^{2}}{s^{2}} = X_{20}^{2} \quad\Longrightarrow\quad \boxed{s_{max} = \frac{R_2}{X_{20}}}\]

Equivalently \(sX_{20} = R_2\): the rotor reactance at that slip equals the rotor resistance — the same condition found in Chapter 60 by inspecting the table, and the same as the starting-torque condition of Section 61-5 with \(s = 1\).

The Value of the Maximum

Substituting \(s_{max} = R_2/X_{20}\) back into the torque equation:

\[T_{max} = K_1\cdot\frac{\left(R_2/X_{20}\right)E_{20}^{2}R_2}{R_2^{2}+R_2^{2}} = K_1\cdot\frac{E_{20}^{2}R_2^{2}/X_{20}}{2R_2^{2}}\]
\[\boxed{T_{max} = \frac{K_1E_{20}^{2}}{2X_{20}} = \frac{3E_{20}^{2}}{4\pi n_sX_{20}}}\]

The rotor resistance has vanished completely. \(R_2\) appeared in both numerator and denominator and cancelled.

This is the most consequential result in Part 4. Rotor resistance determines where the maximum torque occurs but not how large it is. A slip-ring machine can move its peak torque anywhere from full-load slip to standstill by adding resistance — and the peak is the same height wherever it lands. That is precisely why the arrangement is worth its cost: nothing is given away in exchange for the improved starting.
The torque equation plotted: R₂ = 0.25 Ω Tₘₐₓ = 114.6 at s = 0.208 Tₛₜ = 45.8 full load 42.4 at s = 0.04 00.250.500.751.0 slip s — running ←————→ standstill
Torque against slip for the reference machine, with the three key points marked.
5 Worked Example 61.5 — The Peak Does Not Move Up or Down

Problem. For the machine of Example 61.1, find \(s_{max}\) and \(T_{max}\). Then repeat with the external resistance of Example 61.2 fitted, and compare.

As built, with \(R_2 = 0.25~\Omega\):

\[s_{max} = \frac{0.25}{1.20} = 0.20833\]
\[T_{max} = \frac{(0.019099)(14400)}{(2)(1.20)} = 114.59~\mathrm{N\,m}\]

With the rheostat, so that \(R_2 = 1.20~\Omega\):

\[s_{max} = \frac{1.20}{1.20} = 1.000\]
\[T_{max} = \frac{(0.019099)(14400)}{(2)(1.20)} = 114.59~\mathrm{N\,m}\]
Table 61.2 — Same peak, different position.
\(R_2\)\(s_{max}\)\(T_{max}\)\(T_{st}\)\(T_{st}/T_{max}\)
0.25 Ω0.2083114.59 N m45.76 N m39.9 %
1.20 Ω1.000114.59 N m114.59 N m100 %

Ratio to full-load torque.

\[\frac{T_{max}}{T_{fl}} = \frac{114.59}{42.44} = 2.700\]

Comment. The two peaks are identical to five figures, because \(T_{max}\) contains no \(R_2\) at all. All the added resistance has done is slide the peak from \(s = 0.208\) to \(s = 1\).

The whole of the machine's maximum torque is now available at the instant of starting, which is exactly what a crane, hoist or crusher requires. Once running, the resistance is cut out and the peak slides back down to 0.208, where it does no harm.

The ratio \(T_{max}/T_{fl} = 2.70\) is the pull-out or breakdown factor: the machine will carry 2.7 times its rated torque momentarily before stalling. Standard machines are designed for a factor between about 2 and 3, and a value much below 2 would leave too little margin for load surges.

Section 61-10

Summary and Key Formulas

  • Starting torque follows from \(T = K_1E_{20}I_2\cos\phi_2\) with the standstill values: \(T_{st} = K_1E_{20}^{2}R_2/(R_2^{2}+X_{20}^{2})\).

  • \(K_1 = 3/2\pi n_s\), with \(n_s\) in rev/s. It arises because torque is air-gap power divided by synchronous angular speed.

  • A cage motor has small \(R_2\) and large \(X_{20}\) at start, so the current is huge but badly lagging: about 1.5 × full-load torque for 5 to 7 × full-load current.

  • A slip-ring motor adds rotor resistance. At first the improved power factor beats the reduced current and torque rises; past the optimum the impedance wins and torque falls.

  • Maximum starting torque when \(R_2 = X_{20}\), giving \(\phi_2 = 45^{\circ}\).

  • \(T \propto V^{2}\): a 5 % voltage change gives about a 10 % torque change.

  • Under running conditions \(f_r = sf\), \(E_2 = sE_{20}\), \(X_2 = sX_{20}\) — but \(R_2\) is unchanged.

  • The torque equation: \(T_r = K_1sE_{20}^{2}R_2/[R_2^{2}+(sX_{20})^{2}]\). Putting \(s = 1\) recovers \(T_{st}\).

  • Maximum torque at \(s_{max} = R_2/X_{20}\), found by minimising \(Y = 1/T_r\).

  • \(T_{max} = K_1E_{20}^{2}/2X_{20}\)independent of \(R_2\). Rotor resistance moves the peak without changing its height.

Table 61.3 — Formulas of this chapter.
QuantityFormulaNotes
The constant\(K_1 = \dfrac{3}{2\pi n_s}\)\(n_s\) in rev/s
Starting torque\(T_{st} = \dfrac{K_1E_{20}^{2}R_2}{R_2^{2}+X_{20}^{2}}\)\(=K_2R_2/Z_{20}^{2}\)
Running torque\(T_r = \dfrac{K_1sE_{20}^{2}R_2}{R_2^{2}+\left(sX_{20}\right)^{2}}\)\(s=1\) gives \(T_{st}\)
Small-slip form\(T_r \approx \dfrac{K_1sE_{20}^{2}}{R_2}\)\(T\propto s\)
Large-slip form\(T_r \approx \dfrac{K_1E_{20}^{2}R_2}{sX_{20}^{2}}\)\(T\propto 1/s\)
Max starting torque\(R_2 = X_{20}\)\(\phi_2 = 45^{\circ}\)
Slip for max torque\(s_{max} = \dfrac{R_2}{X_{20}}\)from \(dY/ds = 0\)
Maximum torque\(T_{max} = \dfrac{K_1E_{20}^{2}}{2X_{20}}\)no \(R_2\)
Voltage sensitivity\(T \propto V^{2}\)5 % → 10 %
Air-gap power\(P_g = T\omega_s\)synchronous speed
Section 61-11

Common Mistakes

  • Using \(N_s\) in rev/min in \(K_1 = 3/2\pi n_s\). It must be rev/s, or the torque comes out 60 times too small.

  • Dividing air-gap power by the rotor speed. Torque is \(P_g/\omega_s\), using the synchronous speed.

  • Thinking maximum torque rises when rotor resistance is added. Only its position moves; \(T_{max}\) is unchanged.

  • Believing more rotor resistance always means more starting torque. Beyond \(R_2 = X_{20}\) it falls again.

  • Leaving the starting rheostat in circuit while running. It wastes power and drops the speed.

  • Taking torque as proportional to \(V\). It goes as \(V^{2}\).

  • Confusing \(X_{20}\) with \(X_2\). The running reactance is \(sX_{20}\), smaller by a factor of 25 at 4 % slip.

  • Treating \(R_2\) as slip-dependent. It is not, and the whole characteristic depends on that.

  • Applying \(T \propto s\) at large slip. It holds only while \(sX_{20} \ll R_2\).

  • Assuming large starting current means large starting torque. At standstill the rotor power factor is about 0.2.

Section 61-12

Chapter Review

Practice Problems

Convert \(N_s\) to rev/s before using \(K_1\). For maximum-torque questions, \(s_{max} = R_2/X_{20}\) and \(T_{max} = K_1E_{20}^{2}/2X_{20}\) are all that is needed.

  1. P61.1 A 6-pole, 50 Hz motor has \(E_{20} = 100\) V, \(R_2 = 0.30~\Omega\) and \(X_{20} = 1.00~\Omega\) per phase. Find \(K_1\) and the starting torque.

    Show answer
    \[n_s = \frac{2(50)}{6} = 16.667~\mathrm{rev/s}, \qquad K_1 = \frac{3}{2\pi(16.667)} = 0.028648\]
    \[T_{st} = (0.028648)\frac{(10000)(0.30)}{0.09+1.00} = (0.028648)\left(\frac{3000}{1.09}\right) = 78.85~\mathrm{N\,m}\]
  2. P61.2 For P61.1, find \(s_{max}\) and \(T_{max}\), and the ratio \(T_{st}/T_{max}\).

    Show answer
    \[s_{max} = \frac{0.30}{1.00} = 0.300\]
    \[T_{max} = \frac{(0.028648)(10000)}{(2)(1.00)} = 143.24~\mathrm{N\,m}\]
    \[\frac{T_{st}}{T_{max}} = \frac{78.85}{143.24} = 0.5505 = 55.05\,\%\]
  3. P61.3 For P61.1, find the external rotor resistance for maximum starting torque, and confirm the torque then obtained.

    Show answer
    \[R_{ext} = X_{20} - R_2 = 1.00 - 0.30 = 0.70~\Omega\ \text{per phase}\]
    \[T_{st} = (0.028648)\frac{(10000)(1.00)}{1.00+1.00} = (0.028648)(5000) = 143.24~\mathrm{N\,m}\]
    Exactly \(T_{max}\) from P61.2, as it must be.
  4. P61.4 For P61.1, find the torque at 4 % slip and the ratio \(T_{max}/T_{fl}\).

    Show answer
    \[sX_{20} = 0.0400, \qquad R_2^{2}+\left(sX_{20}\right)^{2} = 0.09 + 0.0016 = 0.0916\]
    \[T_r = (0.028648)\frac{(0.04)(10000)(0.30)}{0.0916} = (0.028648)\left(\frac{120}{0.0916}\right) = 37.53~\mathrm{N\,m}\]
    \[\frac{T_{max}}{T_{fl}} = \frac{143.24}{37.53} = 3.816\]
  5. P61.5 A motor develops 60 N m of starting torque at rated voltage. Find the starting torque at 80 % voltage.

    Show answer
    \[T = (60)(0.80)^{2} = (60)(0.64) = 38.4~\mathrm{N\,m}\]
    A 20 % voltage loss costs 36 % of the torque.
  6. P61.6 A 4-pole, 50 Hz motor has \(R_2 = 0.20~\Omega\) and \(X_{20} = 1.00~\Omega\). What external resistance places maximum torque at a slip of 0.50?

    Show answer
    \[s_{max} = \frac{R_2 + R_{ext}}{X_{20}} = 0.50 \quad\Longrightarrow\quad R_2 + R_{ext} = (0.50)(1.00) = 0.50~\Omega\]
    \[R_{ext} = 0.50 - 0.20 = 0.30~\Omega\ \text{per phase}\]
  7. P61.7 Derive the torque equation under running conditions and show that \(s = 1\) recovers the starting torque.

    Show answer
    Torque depends on the flux, the rotor current, and the phase angle between rotor EMF and rotor current:
    \[T_r \propto \Phi I_2\cos\phi_2\]
    Since \(E_{20} \propto \Phi\), and using the running values \(E_2 = sE_{20}\) and \(X_2 = sX_{20}\) from Chapter 60:
    \[T_r \propto \left(E_{20}\right)\left(\frac{sE_{20}}{\sqrt{R_2^{2}+\left(sX_{20}\right)^{2}}}\right)\left(\frac{R_2}{\sqrt{R_2^{2}+\left(sX_{20}\right)^{2}}}\right) = \frac{sE_{20}^{2}R_2}{R_2^{2}+\left(sX_{20}\right)^{2}}\]
    With the constant evaluated,
    \[T_r = \frac{3}{2\pi n_s}\left[\frac{sE_{20}^{2}R_2}{R_2^{2}+\left(sX_{20}\right)^{2}}\right]\]

    Setting \(s = 1\):

    \[T_r = \frac{3}{2\pi n_s}\cdot\frac{E_{20}^{2}R_2}{R_2^{2}+X_{20}^{2}} = T_{st}\]

    The starting torque is not a separate formula but simply this one at \(s = 1\), which is what standstill means. One equation covers the whole range from standstill to synchronous speed.

  8. P61.8 Derive \(s_{max}\) and \(T_{max}\), and state the significance of the result.

    Show answer
    Maximising \(T_r\) is the same as minimising \(Y = 1/T_r\), which is easier because the slip separates:
    \[Y = \frac{R_2^{2}+s^{2}X_{20}^{2}}{K_1sE_{20}^{2}R_2} = \frac{1}{K_1E_{20}^{2}R_2}\left[\frac{R_2^{2}}{s}+sX_{20}^{2}\right]\]
    \[\frac{dY}{ds} = \frac{1}{K_1E_{20}^{2}R_2}\left[-\frac{R_2^{2}}{s^{2}}+X_{20}^{2}\right] = 0 \quad\Longrightarrow\quad s_{max} = \frac{R_2}{X_{20}}\]
    Substituting back, with \(s_{max}X_{20} = R_2\) so the denominator is \(2R_2^{2}\):
    \[T_{max} = K_1\frac{\left(R_2/X_{20}\right)E_{20}^{2}R_2}{2R_2^{2}} = \frac{K_1E_{20}^{2}}{2X_{20}}\]

    Significance. \(R_2\) has cancelled entirely. Rotor resistance fixes where the peak occurs but not how high it is.

    A slip-ring machine can therefore slide its peak torque anywhere between full-load slip and standstill by adding resistance, losing nothing in peak value. That is the whole justification for the arrangement — and it also means a cage machine's \(T_{max}\) is fixed once \(E_{20}\) and \(X_{20}\) are settled, no matter what the bars are made of.

  9. P61.9 Why does a cage motor give only about 1.5 times full-load torque while drawing 6 times full-load current?

    Show answer
    Because torque depends on \(I_2\cos\phi_2\), and at standstill the rotor power factor is very poor.

    Why the power factor is poor. At \(s = 1\) the rotor frequency equals the supply frequency, so the rotor reactance takes its full value \(X_{20}\). A cage rotor's resistance is deliberately small, so \(X_{20} \gg R_2\) and

    \[\cos\phi_2 = \frac{R_2}{\sqrt{R_2^{2}+X_{20}^{2}}} \approx 0.2\]

    In the reference machine the reactance contributes 1.44 of the 1.5025 in \(Z_{20}^{2}\)95.8 % of it.

    Roughly four fifths of that huge starting current is therefore in quadrature and produces no torque at all; it merely heats the rotor and burdens the supply.

    The remedies all attack the same thing — raising the effective \(R_2\) at start: external resistance in a slip-ring machine, or a deep-bar or double-cage rotor whose skin effect raises the bar resistance at the high standstill frequency and lowers it again as the frequency falls to \(sf\).

  10. P61.10 Explain why torque varies as \(V^{2}\), and what follows for starting large machines.

    Show answer
    The applied voltage sets the air-gap flux, and the rotor EMF is induced by that flux, so \(E_{20} \propto V\). The torque expression contains \(E_{20}^{2}\):
    \[T_{st} = \frac{K_1E_{20}^{2}R_2}{R_2^{2}+X_{20}^{2}} = \frac{K_3V^{2}R_2}{Z_{20}^{2}} \quad\Longrightarrow\quad T \propto V^{2}\]
    The square arises because the flux acts twice — once in inducing the rotor EMF and hence the current, and again in producing the force on that current.

    Numerically: a 5 % change gives \((1.05)^{2} = 1.1025\) or about 10 %; a 10 % dip gives \((0.90)^{2} = 0.81\), costing 19 % of the torque.

    Consequence for starting. A large motor draws 5 to 7 times rated current at start, which depresses the supply voltage through the feeder impedance — so the very current drawn to start the machine reduces the voltage that produces its torque.

    If the remaining torque falls below the load torque, the machine cannot accelerate: the slip stays high, the current stays high, the voltage stays depressed, and the motor stalls. Starting methods that reduce current in a controlled way — star-delta, autotransformer, soft starters — are preferable to letting the supply sag uncontrolled.

Multiple-Choice Questions
  1. MCQ 1. In \(K_1 = 3/2\pi n_s\), the speed \(n_s\) is in:
    (a) rev/min   (b) rev/s   (c) rad/s   (d) Hz

    Show answer
    (b) rev/s.
  2. MCQ 2. Maximum starting torque occurs when:
    (a) \(R_2 = X_{20}\)   (b) \(R_2 = 0\)   (c) \(R_2 \gg X_{20}\)   (d) \(s = 0\)

    Show answer
    (a) \(R_2 = X_{20}\), giving \(\phi_2 = 45^{\circ}\).
  3. MCQ 3. The slip at maximum torque is:
    (a) \(X_{20}/R_2\)   (b) \(R_2/X_{20}\)   (c) 1   (d) 0

    Show answer
    (b) \(R_2/X_{20}\).
  4. MCQ 4. Adding rotor resistance changes \(T_{max}\):
    (a) it rises   (b) it falls   (c) it is unchanged   (d) it doubles

    Show answer
    (c) it is unchanged — only \(s_{max}\) moves.
  5. MCQ 5. Torque is proportional to:
    (a) \(V\)   (b) \(V^{2}\)   (c) \(V^{3}\)   (d) \(1/V\)

    Show answer
    (b) \(V^{2}\).
  6. MCQ 6. A 5 % fall in supply voltage reduces torque by about:
    (a) 2.5 %   (b) 5 %   (c) 10 %   (d) 25 %

    Show answer
    (c) 10 % — precisely 9.75 %.
  7. MCQ 7. Putting \(s = 1\) in the running torque equation gives:
    (a) \(T_{max}\)   (b) \(T_{st}\)   (c) zero   (d) \(T_{fl}\)

    Show answer
    (b) \(T_{st}\), since standstill is \(s = 1\).
  8. MCQ 8. At small slip the torque is approximately proportional to:
    (a) \(1/s\)   (b) \(s\)   (c) \(s^{2}\)   (d) constant

    Show answer
    (b) \(s\), while \(sX_{20} \ll R_2\).
  9. MCQ 9. Air-gap power equals torque times:
    (a) rotor speed   (b) synchronous speed   (c) slip speed   (d) supply frequency

    Show answer
    (b) synchronous speed, in rad/s.
  10. MCQ 10. A cage motor's poor starting torque per ampere is caused by:
    (a) low rotor current   (b) high rotor reactance at standstill   (c) low supply voltage   (d) skewing

    Show answer
    (b) high rotor reactance at standstill, giving a rotor power factor near 0.2.
Conceptual Questions
  1. Derive the starting torque from the standstill rotor quantities.

  2. Explain the origin of the constant \(3/2\pi n_s\).

  3. Why is the starting torque per ampere of a cage motor so poor?

  4. Describe the two competing effects when rotor resistance is added.

  5. Derive the condition for maximum starting torque.

  6. Show that torque varies as the square of supply voltage, and give the consequences.

  7. Derive the torque equation under running conditions.

  8. Derive \(s_{max}\) and \(T_{max}\), and explain why the latter is independent of rotor resistance.

Looking Ahead

The equation is complete. Chapter 62 plots it as the torque-slip characteristic and reads the machine's behaviour off the curve: the near-linear working region at low slip, the peak at \(s_{max} = R_2/X_{20}\), and the falling branch beyond it.

The falling branch matters more than it looks. Only the region between zero slip and \(s_{max}\) is stable: past the peak, an increase in load slows the machine, which reduces the torque further, which slows it further still. That is what "pull-out" or "breakdown" means, and why the ratio \(T_{max}/T_{fl} = 2.70\) found in Example 61.5 is a margin against stalling rather than a usable rating.

Chapter 62 also draws the family of curves for different \(R_2\), which makes visible what Section 61-9 proved algebraically: every curve reaches the same height, but each peaks at a different slip. Chapter 63 then turns to the power stages, proving in general the \(s : (1-s)\) division that Example 61.4 verified numerically — and showing why rotor-resistance speed control, for all its convenience, throws away a fraction \(s\) of everything crossing the air gap.