Parallel operation of airplane alternators
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The increase in airplane electrical loads has made necessary an increase in the distribution voltage to avoid excessive copper weight. Difficulties in the use of higher d-c voltages are mentioned, and past experience with a 400-cycle three-phase system is outlined. In the light of this experience and of new developments in progress, requirements are outlined for a larger 400-cycle system with multiple generating units operating in parallel.
[1] C. R. Hanna,et al. Recent developments in generator voltage regulation , 1939, Electrical Engineering.
[2] T. B. Holliday. Applications of electric power in aircraft , 1941, Electrical Engineering.