Electric supply for an aircraft gas turbine engine equipment

Details Electric supply for an aircraft gas turbine engine equipment Electric supply for an aircraft gas turbine engine equipment

H - Electricity

02

J

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

Patent

CA 2597941

The invention concerns an electric supply for an aircraft gas turbine engine equipment comprising a first bus (24) for distributing a direct or alternating voltage to first electrical equipment items of the engine, a second bus (30) for distributing a higher direct or alternating voltage to the other equipment items of the engine, the first bus and the second bus being connected to a third bus itself connected to an electric power source such as an electric distribution network of the aircraft or an electric generator dedicated to the engine and driven thereby.

Un circuit d'alimentation électrique pour un moteur d'avion à turbine à gaz comporte un premier bus (24) de distribution d'une tension continue ou alternative à des premiers équipements électriques du moteur, un deuxième bus (30) de distribution d'une tension continue ou alternative plus élevée aux autres équipements électriques du moteur, le premier bus et le deuxième bus étant reliés à un troisième bus lui-même relié à une source d'énergie électrique telle qu'un réseau de distribution électrique de l'avion ou un générateur électrique dédié au moteur et entraîné par celui- ci.

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