the Rotor: Quantities in 3-Phase Induction Motors | Electrical Machines

SECTION 01

\[\%~\mbox{slip}~(s)=\dfrac{N_{s}-N_{r}}{N_{s}}\times100\]

Slip is ratio and have no units
\(N_s>N_r\)
\(N_{s}=N_{r}\Rightarrow\)relative speed = 0 \(\Rightarrow\) No rotor emf/current \(\Rightarrow\) No Torque
At standstill/blocked rotor \(N_r=0 \Rightarrow\) \(s=1\)
At synchronous speed \(N_s = N_r \Rightarrow\) \(s=0\)

SECTION 02

When the rotor is stationary, the frequency of rotor current is the same as the supply frequency
When rotor starts revolving, then the frequency depends upon the relative speed or on slip speed
\[\begin{aligned} N_{s}-N & =\dfrac{120f_r}{P}~\mbox{and}~N_{s}=\dfrac{120f}{P}\\ \Longrightarrow\dfrac{f_r}{f} & =\dfrac{N_{s}-N}{N_{s}}=s\\ \Rightarrow f_r & =sf \end{aligned}\]
. Then Let any slip-speed, the frequency of the rotor current be
Thus rotor currents have a frequency \(f_r=sf\) and when flowing through the individual phases of rotor winding, give rise to rotor magnetic fields

However, the rotor itself is running at speedw

\[=\dfrac{120f_{r}}{P}=\dfrac{120sf}{P}=sN_{s}\]
These individual rotor magnetic fields produce a combined rotating magnetic field, whose speed relative to rotor is
However, the rotor itself is running at speed \(N\) w.r.t space
\[= sN_s+N=sN_s+N_s(1-s)=N_s\]
Hence, the speed of rotor field in space = speed of rotor magnetic field relative to rotor + speed of rotor relative to space

Key Concepts

No matter what the vale of \(s\), rotor currents and 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 field rotate synchronously, which means that they are stationary w.r.t each other
These two synchronously rotating magnetic fields, in fact, superimpose on each other and give rise to the actually existing rotating field

Relation between Torque and Rotor Power factor

\[\begin{aligned} T & \propto\phi I_{2}\cos\phi_{2}\\ \Rightarrow T & =K\phi I_{2}\cos\phi_{2} \end{aligned}\]
\[\begin{aligned} I_{2} & =\mbox{rotor current at standstill}\\ \phi_{2} & =\mbox{angle between rotor e.m.f and rotor current}\\ K & =\mbox{a constant} \end{aligned}\]
We know,
Denoting rotor e.m.f at standstill by \(E_2\), we have \(E_2 \propto \phi\)
Therefore, \(T \propto E_{2}I_{2}\cos\phi_{2} \quad \Rightarrow T =K_{1}E_{2}I_{2}\cos\phi_{2}\)
Hence, \(\phi_{2}\uparrow\Rightarrow\cos\phi_{2}\downarrow\Rightarrow T\downarrow~\mbox{and vice-versa}\)