System for generating, converting, distributing and...

Details System for generating, converting, distributing and... System for generating, converting, distributing and...

H - Electricity

02

J

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

Patent

CA 2667270

The invention relates to a system for generating, converting, distributing and electrically starting on board an aircraft of the ~bleedless~ type, that is to say with an electrical power architecture and no pneumatic network, characterized in that the electrical distribution channels for high power loads specific to aircraft of the ~bleedless~ type and the electrical distribution channels for conventional loads including technical loads, such as the avionics, the lighting and the fuel pumps and payloads are separate and are powered by separate generators (SG-B, SG-Y; SG-G1, SG-G2) driven by the jet engines (Eng1, Eng2) of the aircraft.

L'invention concerne un système de génération, conversion, distribution et démarrage électrique à bord d'un aéronef de type "bleedless" c'est-à-dire à architecture électrique de puissance sans réseau pneumatique, caractérisé en ce que les canaux de distribution électrique pour charges de fortes puissance spécifiques aux aéronefs de type "bleedless" et les canaux de distribution électrique pour charges conventionnelles comprenant les charges techniques, telles que l'avionique, l'éclairage et les pompes carburants et les charges commerciales sont séparés et sont alimentés par des générateurs distincts (SG-B, SG-Y; SG-G1, SG-G2) entraînés par les réacteurs (Eng1, Eng2) de l'aéronef.

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