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an investigation of dual stator winding induction machines

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4.4 Mutual Induct<strong>an</strong>ces Calculation<br />

The mutual induct<strong>an</strong>ces are the induct<strong>an</strong>ces between <strong>stator</strong> <strong>winding</strong>s <strong>an</strong>d rotor loops,<br />

which is a very import<strong>an</strong>t <strong>an</strong>d interesting part <strong>of</strong> the induct<strong>an</strong>ce calculation. Mutual<br />

induct<strong>an</strong>ces ch<strong>an</strong>ging by the rotor <strong>an</strong>gle under the const<strong>an</strong>t air gap condition are shown in<br />

the previous chapter. The mutual induct<strong>an</strong>ces shown here are under different rotor<br />

eccentricity conditions. These mutual induct<strong>an</strong>ces are quite different from those when the<br />

machine is under the const<strong>an</strong>t air gap condition as shown in the upcoming figures.<br />

4.4.1 Stator Rotor Mutual Induct<strong>an</strong>ces <strong>of</strong> the ABC Winding Set<br />

From the general <strong>winding</strong> function definition, the equation <strong>of</strong> <strong>stator</strong> rotor mutual<br />

induct<strong>an</strong>ce c<strong>an</strong> be expressed as:<br />

2π<br />

[ ] ⋅ dθ<br />

'<br />

'<br />

[ A + A ( θ −θ<br />

) ] ⋅ n ( θ ) ⋅ n ( θ ) − n ( θ ) − K ( θ )<br />

Lij = µ rl ∫ 0 1<br />

rm i j<br />

j<br />

j rm<br />

0 cos (4.12)<br />

0<br />

2π<br />

' A1<br />

'<br />

where, K ( θ rm ) = ∫ n j ( θ ) cos(<br />

θ −θ<br />

rm )<br />

loop, ( θ )<br />

j<br />

j dθ<br />

, n i ( θ ) is the turn function <strong>of</strong><br />

2π<br />

A<br />

th<br />

i rotor<br />

0<br />

0<br />

n is the turn function <strong>of</strong> <strong>stator</strong> th<br />

inverse <strong>of</strong> the air gap function.<br />

'<br />

j <strong>winding</strong> <strong>an</strong>d A A ( θ −θ<br />

)<br />

175<br />

+ is the<br />

0 1 cos rm<br />

The <strong>stator</strong> rotor mutual induct<strong>an</strong>ce under the static rotor eccentricity, dynamic rotor<br />

eccentricity <strong>an</strong>d mixed rotor eccentricity conditions are shown in Figure 4.22, Figure 4.23<br />

<strong>an</strong>d Figure 4.24 respectively.

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