Aircraft secondary power system

Details Aircraft secondary power system Aircraft secondary power system

H - Electricity

02

J

H02J 4/00 (2006.01) B64D 41/00 (2006.01) H02J 3/02 (2006.01)

Patent

CA 2294403

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.

Système d'alimentation en énergie secondaire conçu pour un aéronef et mettant une application un système de distribution électrique à fréquence variable alimentant en courant une ou plusieurs charges pouvant tolérer des composantes de distorsion. De plus, un système de distribution de courant continu est couplé au système de distribution à fréquence variable et est isolé d'une distribution électrique à fréquence fixe. La distorsion provoquée par le redressement du système de courant continu est isolée du système à fréquence fixe, ce qui améliore la qualité de l'énergie du système à fréquence fixe.

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