An accurate knowledge of the magnetic field distribution is of great importance in finding the best designs for electrical machinery. It is the purpose of this paper to present a new numerical method for the determination of three-dimensional flux distribution in the end zone of a highspeed aerospace homopolar alternator, and for the calculation of end leakage reactance. The new analysis is applied to an experimental 95 kVA, 115/200 V, 3400 Hz, 40 800 r/min, three-phase, wye-connected, homopolar alternator.


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    Title :

    End Leakage of Aerospace Homopolar Alternators


    Contributors:


    Publication date :

    1970-09-01


    Size :

    2237598 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English