In former papers 1,2,3 the authors have analyzed the behavior of homopolar inductor alternators, considering all non-linearities and load conditions. As a logical sequence, a means to find the main dimensions of a new design for a specific aerospace power system is presented. The limitations imposed by the high-speed operation are pointed out. Dimensional analysis is used as a method for optimizing alternators for minimum armature leakage for frequency-changing power system. The relation of slot width to slot depth of the armature is optimized for minimum excitation.
Design Considerations and Optimization of Homopolar Inductor Alternators of Aerospace Power Systems
IEEE Transactions on Aerospace and Electronic Systems ; AES-2 , 4 ; 106-115
1966-07-01
1384375 byte
Article (Journal)
Electronic Resource
English