By the end of this chapter you should be able to:
Define slip and give its values at standstill and at synchronous speed.
Derive the frequency of the rotor current, \(f_r = sf\).
Derive the rotor EMF, \(E_2 = sE_{20}\).
Derive the rotor reactance, \(X_2 = sX_{20}\), and explain why it matters most.
Compute rotor impedance, current and power factor at any slip.
Find the speed of the rotor field relative to the rotor and to space.
Prove that the two fields are stationary relative to each other at every slip.
Relate torque to rotor power factor.
Slip
Slip is a ratio and has no units.
In motoring, \(N_s \gt N_r\) always.
If \(N_s = N_r\) then the relative speed is zero \(\Rightarrow\) no rotor EMF or current \(\Rightarrow\) no torque.
At standstill or blocked rotor, \(N_r = 0\) so \(s = 1\).
At synchronous speed, \(N_s = N_r\) so \(s = 0\).
The last is the slip speed — the relative speed between the rotating field and the rotor, and the quantity that actually does the inducing.
Typical full-load slips are 2 to 6 %, smaller in large machines. The whole useful operating range of an induction motor therefore lies in the first few percent of the slip axis, with the remaining 95 % of it reserved for starting and abnormal conditions.
Problem. A 4-pole, 50 Hz induction motor has \(N_s = 1500\) rev/min. Tabulate the slip, slip speed and rotor frequency at rotor speeds of 0, 750, 1200, 1440 and 1500 rev/min.
| \(N\) (rev/min) | Slip speed | \(s\) | \(f_r = sf\) | Condition |
|---|---|---|---|---|
| 0 | 1500 | 1.0000 | 50.00 Hz | Standstill |
| 750 | 750 | 0.5000 | 25.00 Hz | Accelerating |
| 1200 | 300 | 0.2000 | 10.00 Hz | Near maximum torque |
| 1440 | 60 | 0.0400 | 2.00 Hz | Full load |
| 1500 | 0 | 0.0000 | 0 Hz | Synchronous — no torque |
Working, the full-load row.
Comment. The whole useful range is the last row but one. A machine that spends its life at 4 % slip passes through the other 96 % of the axis only during the second or two it takes to start.
Frequency of the Rotor Current
When the rotor is stationary, the frequency of the rotor current is the same as the supply frequency.
When the rotor starts revolving, the frequency depends upon the relative speed, or on the slip speed.
Let the frequency of the rotor current at any slip speed be \(f_r\). Then the slip speed must correspond to that frequency in the same way that the synchronous speed corresponds to the supply frequency:
Rotor EMF
The rotor is a winding cut by a flux, so its EMF obeys the same equation as any other — the transformer EMF equation of Chapter 41:
The flux \(\Phi\) and the turns \(N_2\) are fixed by the machine. The only quantity that varies with speed is the frequency, and that varies as \(sf\). Hence
where \(E_{20}\) is the standstill rotor EMF per phase — the value at \(s = 1\) — and \(E_2\) the value at any slip.
Some texts write \(E_2\) for the standstill value and others for the running value. Throughout this book the subscript 20 means "at standstill": \(E_{20}\) and \(X_{20}\) are the values at \(s = 1\), and \(E_2 = sE_{20}\), \(X_2 = sX_{20}\) are the running values.
The rotor resistance carries no such subscript because \(R_2\) does not vary with slip — resistance is independent of frequency. That asymmetry between \(R_2\) and \(X_2\) is the source of everything in Chapters 61 and 62.
Rotor Reactance — the Crucial One
The rotor winding has leakage inductance \(L_2\), fixed by its geometry. Its reactance, however, depends on the frequency at which it is worked:
where \(X_{20} = 2\pi fL_2\) is the standstill reactance.
Both the rotor EMF and the rotor reactance are proportional to slip, but the rotor resistance is not. The rotor impedance therefore changes its character with speed — dominated by reactance at standstill, almost purely resistive in normal running.
Reactance is at its maximum. The rotor current lags badly, the power factor is poor, and the machine draws a heavy current while developing only moderate torque.
Reactance nearly vanishes. The rotor is almost purely resistive, the power factor approaches unity, and the current is nearly in phase with the EMF.
This single dependence explains the shape of every characteristic in Part 4: the low starting torque despite huge starting current, the existence of a maximum torque at an intermediate slip, and the almost-linear torque-slip relation near full load.
Impedance, Current and Power Factor
With the three quantities established, the rotor circuit per phase follows at once.
Problem. A 4-pole, 50 Hz motor has a standstill rotor EMF of 120 V per phase, rotor resistance 0.25 Ω and standstill rotor reactance 1.20 Ω per phase. Tabulate \(E_2\), \(X_2\), \(Z_2\), \(I_2\) and \(\cos\phi_2\) at slips of 1.0, 0.5, 0.2083, 0.10 and 0.04.
| \(s\) | \(E_2\) (V) | \(X_2\) (Ω) | \(Z_2\) (Ω) | \(I_2\) (A) | \(\cos\phi_2\) | \(\phi_2\) |
|---|---|---|---|---|---|---|
| 1.0000 | 120.00 | 1.2000 | 1.22577 | 97.898 | 0.20395 | 78.23° |
| 0.5000 | 60.00 | 0.6000 | 0.65000 | 92.308 | 0.38462 | 67.38° |
| 0.2083 | 25.00 | 0.2500 | 0.35355 | 70.711 | 0.70711 | 45.00° |
| 0.1000 | 12.00 | 0.1200 | 0.27731 | 43.273 | 0.90152 | 25.64° |
| 0.0400 | 4.80 | 0.0480 | 0.25457 | 18.856 | 0.98206 | 10.87° |
Working, the full-load row at \(s = 0.04\).
Comment. Two things happen together as the slip rises, and both are consequences of \(X_2 = sX_{20}\).
First, the current rises but far less than proportionally. From \(s = 0.04\) to \(s = 1\) the EMF grows 25-fold but the current only 5.19-fold, because the impedance grows too. That 5.19 is the familiar starting-current ratio of a cage motor.
Second, the power factor collapses, from 0.982 to 0.204. At standstill the rotor current lags its EMF by 78°, so most of it produces no torque at all — which is why a cage motor draws six times its rated current at start yet develops only about twice its rated torque.
The middle row is worth marking. At \(s = 0.2083\) the reactance \(sX_{20} = 0.25~\Omega\) exactly equals the resistance, so \(\phi_2 = 45^{\circ}\) and \(\cos\phi_2 = 1/\sqrt2\). Section 60-8 shows that this is precisely where the torque is greatest.
Speed of the Rotor Field
Rotor currents have a frequency \(f_r = sf\), and when flowing through the individual phases of the rotor winding they give rise to rotor magnetic fields. Those individual fields combine, exactly as in Chapter 59, into a single rotating field.
The combined rotor field rotates, relative to the rotor, at the speed corresponding to its own frequency:
The rotor field runs ahead of the rotor at exactly the slip speed — which is intuitive, since the rotor currents are themselves produced by that same relative motion.
A cage rotor deserves a note here. It has no defined phase windings, yet the same result holds: the induced bar currents arrange themselves into whatever pole pattern the stator field demands, and their combined field rotates at \(sN_s\) relative to the rotor just as a wound rotor's would.
Why the Two Fields Are Stationary
The rotor field travels at \(sN_s\) relative to the rotor, but the rotor itself is running at speed \(N\) with respect to space. Adding the two gives the speed of the rotor field in space.
No matter what the value of \(s\), the rotor currents and the stator current each produce a sinusoidally distributed magnetic field of constant magnitude and constant space speed \(N_s\).
In other words, both rotor and stator fields rotate synchronously, which means that they are stationary with respect to each other.
These two synchronously rotating magnetic fields superimpose on each other and give rise to the actually existing rotating field in the air gap.
The slip has cancelled completely. Whether the machine is at standstill, at half speed or at full load, the two fields keep station with one another — and that is what makes a steady, non-pulsating torque possible. Two fields at a fixed relative angle produce a constant torque; two fields in relative motion would produce a torque that alternated and averaged to nothing.
Problem. For the 4-pole, 50 Hz machine with \(N_s = 1500\) rev/min, tabulate the rotor speed, the rotor-field speed relative to the rotor, and their sum, at slips of 1.0, 0.5, 0.04 and 0.
| \(s\) | \(N = (1-s)N_s\) | \(sN_s\) | Sum | \(f_r\) |
|---|---|---|---|---|
| 1.00 | 0 | 1500 | 1500 | 50 Hz |
| 0.50 | 750 | 750 | 1500 | 25 Hz |
| 0.04 | 1440 | 60 | 1500 | 2 Hz |
| 0.00 | 1500 | 0 | 1500 | 0 Hz |
Working at \(s = 0.04\), from the rotor frequency.
Comment. The two contributions trade off perfectly. At standstill the rotor supplies none of the speed and the field supplies all 1500; at synchronous speed the rotor supplies all of it and the field none. Every intermediate case splits the 1500 between them.
This is the mechanism by which the machine keeps its torque steady while its speed changes. The rotor may run at any speed it likes; its field will always be found travelling at \(N_s\).
Torque and Rotor Power Factor
Torque depends on the flux, on the rotor current, and on the phase angle between them — only the component of rotor current in phase with the EMF produces torque.
| Symbol | Meaning |
|---|---|
| \(I_2\) | Rotor current |
| \(\phi_2\) | Angle between rotor EMF and rotor current |
| \(K\) | A constant |
Since the standstill rotor EMF is proportional to the flux, \(E_{20} \propto \Phi\), the constant can absorb the proportionality:
Rotor current that lags its EMF badly contributes little torque however large it is — which is exactly the situation at standstill, where \(\phi_2\) approaches 78° in Example 60.2.
Substituting the expressions of Section 60-5 turns this into a formula in slip alone, which is the business of Chapter 61:
Problem. For the machine of Example 60.2, tabulate \(I_2\), \(\cos\phi_2\) and the product \(E_{20}I_2\cos\phi_2\) across the slip range, and identify where the torque is greatest.
| \(s\) | \(I_2\) (A) | \(\cos\phi_2\) | \(E_{20}I_2\cos\phi_2\) |
|---|---|---|---|
| 1.0000 | 97.898 | 0.20395 | 2396.0 |
| 0.5000 | 92.308 | 0.38462 | 4260.4 |
| 0.3000 | 82.137 | 0.57040 | 5622.1 |
| 0.2083 | 70.711 | 0.70711 | 6000.0 |
| 0.1500 | 58.430 | 0.81153 | 5690.2 |
| 0.1000 | 43.273 | 0.90152 | 4681.4 |
| 0.0400 | 18.856 | 0.98206 | 2222.1 |
The maximum. The product peaks where the reactance equals the resistance:
Comment. The current alone is a poor guide. It is largest at standstill (97.9 A) where the torque is nearly at its smallest, and smallest at full load (18.9 A) where the machine is doing its useful work. Only the product matters.
The maximum occurs at a clean and memorable condition: the rotor reactance equals the rotor resistance, so the rotor power factor is exactly \(1/\sqrt2\) and \(\phi_2 = 45^{\circ}\). Above that slip the falling power factor dominates; below it, the falling current does.
Comparing the extremes: starting torque is 39.9 % of maximum and full-load torque 37.0 %, so this machine has a pull-out torque 2.70 times its full-load value. Chapter 62 develops all of this properly.
Problem. External resistance is added to the rotor of the machine of Example 60.2, raising \(R_2\) from 0.25 Ω to 1.20 Ω per phase. Find the new slip for maximum torque and the new rotor power factor at standstill, and comment.
New slip for maximum torque.
Rotor power factor at standstill, now that \(R_2 = X_{20}\):
Standstill current.
Comment. Adding rotor resistance has moved the maximum-torque point all the way to \(s = 1\) — the machine now develops its greatest torque at the instant of starting, which is precisely what a crane or hoist requires.
Note what has happened to the current. It has fallen from 97.9 A to 70.7 A, yet the torque has risen from 39.9 % to 100 % of maximum. More torque from less current — because the power factor improved from 0.204 to 0.707, and it is the product that counts.
This is the whole justification for the slip-ring machine of Chapter 57. The resistance is cut out once the motor is running, because at full-load slip the extra resistance would be dissipating a great deal of power to no purpose. Chapter 62 will show the striking companion result: the value of the maximum torque is unchanged by all this — only its position moves.
Summary and Key Formulas
Slip \(s = (N_s - N)/N_s\) is dimensionless. At standstill \(s = 1\); at synchronous speed \(s = 0\) and there is no torque.
Rotor frequency \(f_r = sf\), obtained by applying \(N = 120f/P\) to the slip speed and to the synchronous speed and dividing. The pole number cancels.
Rotor EMF \(E_2 = sE_{20}\), since flux and turns are fixed and only frequency varies.
Rotor reactance \(X_2 = sX_{20}\) — the crucial relation, because \(R_2\) does not vary with slip.
Hence \(Z_2 = \sqrt{R_2^{2} + (sX_{20})^{2}}\), \(I_2 = sE_{20}/Z_2\) and \(\cos\phi_2 = R_2/Z_2\).
As slip rises the current rises much less than proportionally (5.19× for a 25× EMF change in Example 60.2) while the power factor collapses from 0.982 to 0.204.
The rotor field travels at \(sN_s\) relative to the rotor, hence at \(sN_s + N = N_s\) in space.
Both fields therefore rotate at \(N_s\) and are stationary with respect to each other, whatever the slip — which is what permits a steady torque.
\(T \propto \Phi I_2\cos\phi_2 = K_1E_{20}I_2\cos\phi_2\): a poor rotor power factor wastes current.
The product is greatest when \(sX_{20} = R_2\), where \(\cos\phi_2 = 1/\sqrt2\) and \(\phi_2 = 45^{\circ}\).
| Quantity | Formula | Notes |
|---|---|---|
| Slip | \(s = \dfrac{N_s - N}{N_s}\) | dimensionless |
| Slip speed | \(N_s - N = sN_s\) | the relative motion |
| Rotor frequency | \(f_r = sf\) | pole number cancels |
| Rotor EMF | \(E_2 = sE_{20}\) | only \(f\) varies in \(4.44k_wf\Phi N\) |
| Rotor reactance | \(X_2 = sX_{20}\) | but \(R_2\) is constant |
| Rotor impedance | \(Z_2 = \sqrt{R_2^{2} + \left(sX_{20}\right)^{2}}\) | — |
| Rotor current | \(I_2 = \dfrac{sE_{20}}{\sqrt{R_2^{2} + \left(sX_{20}\right)^{2}}}\) | flattens at large \(s\) |
| Rotor power factor | \(\cos\phi_2 = \dfrac{R_2}{Z_2}\) | 0.204 at standstill |
| Rotor field, rel. to rotor | \(sN_s\) | \(=120f_r/P\) |
| Rotor field, in space | \(sN_s + N = N_s\) | for every \(s\) |
| Torque | \(T = K_1E_{20}I_2\cos\phi_2\) | — |
| In terms of slip | \(T \propto \dfrac{sE_{20}^{2}R_2}{R_2^{2} + \left(sX_{20}\right)^{2}}\) | Chapter 61 |
| Slip for maximum torque | \(s_{max} = \dfrac{R_2}{X_{20}}\) | \(\phi_2 = 45^{\circ}\) there |
Common Mistakes
Taking rotor reactance as constant. It is \(sX_{20}\), and the whole character of the machine follows from that.
Making rotor resistance depend on slip. It does not — resistance is independent of frequency.
Using \(E_2\) for the standstill value. Here \(E_{20}\) is at standstill and \(E_2 = sE_{20}\) is the running value.
Expecting rotor current to rise in proportion to slip. The impedance rises too, so it flattens off.
Judging torque by rotor current alone. The current is largest at standstill, where the torque is nearly least.
Using \(E_2\) rather than \(E_{20}\) in the torque product. It is the flux — hence the standstill EMF — that appears there.
Thinking the rotor field travels at \(N\). It travels at \(sN_s\) relative to the rotor and at \(N_s\) in space.
Supposing the two fields move relative to each other. They never do, at any slip.
Believing a cage rotor cannot produce a rotating field because it has no phase windings. The bar currents arrange themselves accordingly.
Forgetting to cut out the external rotor resistance once a slip-ring motor is running.
Chapter Review
Find the slip first; then \(f_r\), \(E_2\) and \(X_2\) all follow by multiplying by \(s\). Only \(R_2\) stays put.
P60.1 A 6-pole, 50 Hz motor runs at 940 rev/min. Find the slip, slip speed and rotor frequency.
Show answer
\[N_s = \frac{120(50)}{6} = 1000~\mathrm{rev/min}\]\[N_s - N = 60~\mathrm{rev/min}, \qquad s = \frac{60}{1000} = 0.0600\]\[f_r = (0.06)(50) = 3.00~\mathrm{Hz}\]P60.2 A motor has \(E_{20} = 100\) V, \(R_2 = 0.30~\Omega\) and \(X_{20} = 1.00~\Omega\) per phase. Find \(E_2\), \(X_2\), \(Z_2\), \(I_2\) and \(\cos\phi_2\) at 5 % slip.
Show answer
\[E_2 = (0.05)(100) = 5.00~\mathrm{V}, \qquad X_2 = (0.05)(1.00) = 0.0500~\Omega\]\[Z_2 = \sqrt{0.09 + 0.0025} = \sqrt{0.0925} = 0.30414~\Omega\]\[I_2 = \frac{5.00}{0.30414} = 16.440~\mathrm{A}, \qquad \cos\phi_2 = \frac{0.30}{0.30414} = 0.98639\]P60.3 For P60.2, repeat at standstill and find the ratio of standstill to 5 % slip current.
Show answer
\[Z_2 = \sqrt{0.09 + 1.00} = \sqrt{1.09} = 1.04403~\Omega\]\[I_2 = \frac{100}{1.04403} = 95.783~\mathrm{A}, \qquad \cos\phi_2 = \frac{0.30}{1.04403} = 0.28735\]The EMF rose 20-fold but the current only 5.83-fold.\[\frac{95.783}{16.440} = 5.826\]P60.4 For P60.2, find the slip at which the torque is maximum and the rotor power factor there.
Show answer
There \(X_2 = 0.30 = R_2\), so\[s_{max} = \frac{R_2}{X_{20}} = \frac{0.30}{1.00} = 0.300\]\[Z_2 = \sqrt{2}\,(0.30) = 0.42426~\Omega, \qquad \cos\phi_2 = \frac{1}{\sqrt2} = 0.70711, \qquad \phi_2 = 45^{\circ}\]P60.5 An 8-pole, 50 Hz motor runs at 720 rev/min. Find the speed of the rotor field relative to the rotor and relative to space.
Show answer
\[N_s = \frac{120(50)}{8} = 750, \qquad s = \frac{750-720}{750} = 0.0400\]\[\text{relative to rotor} = sN_s = (0.04)(750) = 30~\mathrm{rev/min}\]\[\text{in space} = 30 + 720 = 750 = N_s \quad\checkmark\]P60.6 A slip-ring motor has \(R_2 = 0.20~\Omega\) and \(X_{20} = 0.80~\Omega\). What external resistance per phase gives maximum torque at starting?
Show answer
Maximum torque at start requires \(s_{max} = 1\), that is \(R_2 + R_{ext} = X_{20}\):\[R_{ext} = 0.80 - 0.20 = 0.60~\Omega\ \text{per phase}\]P60.7 Derive \(f_r = sf\), \(E_2 = sE_{20}\) and \(X_2 = sX_{20}\), and explain why the third is the most consequential.
Show answer
Frequency. Applying \(N = 120f/P\) to the slip speed and to the synchronous speed:so \(f_r = sf\). The pole number cancels.\[N_s - N = \frac{120f_r}{P}, \qquad N_s = \frac{120f}{P} \quad\Longrightarrow\quad \frac{f_r}{f} = \frac{N_s-N}{N_s} = s\]EMF. From \(E = 4.44k_wf\Phi N_2\), the flux and turns are fixed by the machine and only the frequency varies, so \(E_2/E_{20} = f_r/f = s\) and \(E_2 = sE_{20}\).
Reactance. The leakage inductance \(L_2\) is fixed by geometry, but reactance depends on frequency:
\[X_2 = 2\pi f_rL_2 = 2\pi\left(sf\right)L_2 = s\left(2\pi fL_2\right) = sX_{20}\]Why the third matters most. The rotor resistance is independent of frequency and so does not vary with slip. The rotor impedance therefore changes its character as the machine speeds up — dominated by reactance at standstill, almost purely resistive at low slip.
That single asymmetry between \(R_2\) and \(X_2\) produces the poor starting power factor, the existence of a maximum torque at an intermediate slip, and the near-linear torque-slip relation near full load. Had both varied alike, the machine would have no characteristic shape at all.
P60.8 Prove that the stator and rotor fields are stationary relative to each other at every slip, and explain why it matters.
Show answer
The rotor currents have frequency \(f_r = sf\), so the field they jointly produce rotates relative to the rotor atThe rotor itself runs at \(N\) with respect to space, so the rotor field's speed in space is\[\frac{120f_r}{P} = \frac{120\,sf}{P} = s\,\frac{120f}{P} = sN_s\]\[sN_s + N = sN_s + N_s\left(1-s\right) = N_s\]The slip cancels completely. Both fields therefore rotate at \(N_s\) and are stationary with respect to one another, whatever the rotor is doing.
Why it matters. Two fields at a fixed relative angle produce a steady torque. Two fields in relative motion would produce a torque that alternated in sign and averaged to nothing, and the machine could deliver no useful output at all.
It also means the two fields can be superimposed to give the single resultant air-gap field that actually exists — which is what makes the equivalent circuit of Chapter 64 possible.
P60.9 Why does a cage motor draw about six times rated current at start yet develop only about twice rated torque?
Show answer
Because torque depends on \(I_2\cos\phi_2\), not on \(I_2\) alone, and the two move in opposite directions as slip rises.The current. At standstill the rotor EMF is at its maximum \(E_{20}\), so the current is large — but the impedance is also at its maximum, since \(X_2 = sX_{20} = X_{20}\). In Example 60.2 the EMF rose 25-fold from full load to standstill while the current rose only 5.19-fold.
The power factor. With the reactance at its largest, the rotor current lags its EMF by nearly 78°, so \(\cos\phi_2\) falls from 0.982 to 0.204 — most of that large current is doing nothing useful.
\[\frac{I_2\cos\phi_2\ \text{at }s=1}{I_2\cos\phi_2\ \text{at }s=0.04} = \frac{(97.898)(0.20395)}{(18.856)(0.98206)} = \frac{19.966}{18.518} = 1.078\]So a five-fold rise in current buys only about 8 % more torque-producing current in this machine.
The remedy is to raise \(R_2\) at starting — external resistance in a slip-ring machine, or a deep-bar or double-cage rotor — which improves \(\cos\phi_2\) and shifts maximum torque towards standstill.
P60.10 Explain the effect of adding rotor resistance, using the rotor power factor.
Show answer
Adding resistance raises \(R_2\) without altering \(X_{20}\), so the slip for maximum torquemoves towards standstill. Choosing \(R_2 = X_{20}\) puts it exactly at \(s = 1\).\[s_{max} = \frac{R_2}{X_{20}}\]What happens to the current and power factor. In Example 60.5 raising \(R_2\) from 0.25 to 1.20 Ω changed the standstill values from
\[I_2 = 97.9~\mathrm{A},\ \cos\phi_2 = 0.204 \quad\longrightarrow\quad I_2 = 70.7~\mathrm{A},\ \cos\phi_2 = 0.707\]The current fell while the torque rose to its maximum — more torque from less current, because the power factor improved by a factor of 3.5.
Why it is removed afterwards. At full-load slip the extra resistance would dissipate a great deal of power for no benefit, so the rings are short-circuited once the machine is up to speed. Chapter 62 adds the striking companion result: the value of maximum torque is entirely unaffected by rotor resistance — only its position moves.
MCQ 1. At standstill the slip is:
(a) 0 (b) 0.5 (c) 1 (d) infiniteShow answer
(c) 1, since \(N = 0\).MCQ 2. The rotor frequency is:
(a) \(f\) (b) \(sf\) (c) \(f/s\) (d) \((1-s)f\)Show answer
(b) \(sf\).MCQ 3. The rotor reactance at slip \(s\) is:
(a) \(X_{20}\) (b) \(sX_{20}\) (c) \(X_{20}/s\) (d) \(s^{2}X_{20}\)Show answer
(b) \(sX_{20}\), since reactance follows frequency.MCQ 4. The rotor resistance at slip \(s\) is:
(a) \(sR_2\) (b) \(R_2/s\) (c) \(R_2\), unchanged (d) zeroShow answer
(c) \(R_2\), unchanged — resistance is independent of frequency.MCQ 5. As slip rises from 0.04 to 1, the rotor power factor:
(a) rises (b) falls (c) is unchanged (d) becomes leadingShow answer
(b) falls — from 0.982 to 0.204 in Example 60.2.MCQ 6. The rotor field rotates, relative to the rotor, at:
(a) \(N_s\) (b) \(N\) (c) \(sN_s\) (d) zeroShow answer
(c) \(sN_s\), the slip speed.MCQ 7. The rotor field rotates, in space, at:
(a) \(sN_s\) (b) \(N\) (c) \(N_s\) (d) \((1-s)N_s\)Show answer
(c) \(N_s\), for every value of slip.MCQ 8. Stator and rotor fields are:
(a) stationary relative to each other (b) in relative motion at \(sN_s\) (c) counter-rotating (d) unrelatedShow answer
(a) stationary relative to each other, which is what allows a steady torque.MCQ 9. Torque is proportional to:
(a) \(I_2\) (b) \(I_2\cos\phi_2\) (c) \(I_2^{2}\) (d) \(\cos\phi_2\)Show answer
(b) \(I_2\cos\phi_2\), times the flux.MCQ 10. The torque is maximum when:
(a) \(sX_{20} = R_2\) (b) \(s = 1\) always (c) \(s = 0\) (d) \(\cos\phi_2 = 1\)Show answer
(a) \(sX_{20} = R_2\), where \(\phi_2 = 45^{\circ}\).
Define slip and give its values at standstill and at synchronous speed.
Derive the frequency of the rotor current.
Derive the rotor EMF and the rotor reactance, and explain why only one of \(R_2\) and \(X_2\) varies.
Obtain the rotor impedance, current and power factor as functions of slip.
Explain why the rotor current rises much less than proportionally with slip.
Find the speed of the rotor field relative to the rotor and to space.
Prove that the two fields are stationary relative to each other, and say why it matters.
Relate torque to rotor power factor and locate the maximum.
Looking Ahead
Every quantity the torque equation needs is now in hand. Chapter 61 substitutes them into \(T = K_1E_{20}I_2\cos\phi_2\) and obtains the torque equation in slip alone:
It also settles the constant \(k\), which turns out to be \(3/2\pi n_s\) when torque is measured in newton metres — so that the equation can be used numerically and not merely proportionally.
Chapter 62 then draws the torque-slip characteristic and establishes the two results this chapter has been pointing towards. Maximum torque occurs at \(s_{max} = R_2/X_{20}\), where the rotor reactance equals its resistance and \(\phi_2 = 45^{\circ}\). And the value of that maximum, \(T_{max} = kE_{20}^{2}/2X_{20}\), contains no \(R_2\) at all — so rotor resistance moves the peak without changing its height, which is exactly the property that makes a slip-ring machine worth its cost.
Chapter 63 accounts for the power flow and shows that the air-gap power divides in the ratio \(s : (1-s)\) between rotor copper loss and mechanical output — so that a machine running at 50 % slip wastes half of everything crossing the gap, which is why rotor-resistance speed control is so inefficient. Chapter 64 then assembles the equivalent circuit, and the whole of Part 3's transformer theory returns with the rotor resistance divided by the slip.