Operating features are considered and analog-computer modeling of static and dynamic characteristics discussed for three-phase aircraft induction motors (IM) with short-circuited rotors; frequency variation in the 400-710 Hz range is taken into account together with the stable supply voltage. The influence of frequency is investigated and the processes analyzed for an IM with fan load (a fuel-pump electric drive, for example).
Investigation of aircraft induction motors with unstable supply frequency
Untersuchung von Flugzeug-Induktionsmotoren mit instabiler Speisefrequenz
Power Engineering, New York ; 19 , 1 ; 42-51
1981
10 Seiten, 10 Quellen
Article (Journal)
English
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