A 40-Kva 400-Cycle Aircraft Alternator

A-c auxiliary-power systems for aircraft date back to World War I. Recently numerous technical articles have indicated an intense revival of interest in this subject. Heart of any electric system is the generator which supplies electric power to all parts of the system. An alternator, especially designed and built for 208-volt three-phase systems is described in this paper. Light weight and reliability dominate the design, which involved a large number of new and unusual problems.

[1]  W. K. Boice,et al.  Basic considerations in selection of electric systems for large aircraft , 1944, Electrical Engineering.

[2]  C. G. Veinott,et al.  Effect of altitude on electric breakdown and flashover of aircraft insulation , 1944, Electrical Engineering.

[3]  W. M. Davidson,et al.  A-C and D-C short-circuit tests on aircraft cable , 1944, Electrical Engineering.

[4]  D. E. Fritz,et al.  Alternating versus direct current for aircraft-radio power supply , 1944, Electrical Engineering.

[5]  Melville F. Peters,et al.  Optimum voltage for airplanes , 1939, Electrical Engineering.

[6]  Cyril G. Veinott Blast-Tube Cooling for Aircraft Generators , 1944, Transactions of the American Institute of Electrical Engineers.

[7]  J. E. Yarmack Aircraft electric power-supply system , 1943, Electrical Engineering.

[8]  D. W. Exner Parallel operation of airplane alternators , 1943, Electrical Engineering.

[9]  H. E. Keneipp Testing Aircraft Generators , 1944, Transactions of the American Institute of Electrical Engineers.

[10]  J. D. Miner Design Considerations for D-C Aircraft Generators , 1944, Transactions of the American Institute of Electrical Engineers.