Aircraft secondary power system

Details Aircraft secondary power system Aircraft secondary power system

1997-06-30

1999-11-02

Enad, Elvin G.

Prime-mover dynamo plants

Electric control

Engine control

290 38R, 290 40A, 290 40B, 290 40F, 290 51, 322 10, 322 29, 322 32, 322 90, F02N 1186

Patent

active

059776455

ABSTRACT:
A secondary power system for an aircraft utilizes a variable frequency electrical distribution system that provides power to one or more loads that can tolerate distortion components. In addition, a DC distribution system is coupled to the variable frequency distribution system and is isolated from a fixed frequency electrical distribution. Distortion caused by rectification for the DC system is isolated from the fixed frequency system, thereby improving the power quality in the fixed frequency system.

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