An electrical architecture for an aircraft having a primary three-phase electrical network powering a transformer-rectifier unit serving to power two secondary DC electrical networks. Each of the two secondary electrical networks includes a contactor electrically connected to a generator-starter. The contactors are linked in pairs to prevent them from being closed simultaneously. The second secondary network powers the generator-starter to start a fuel-burning engine. The first secondary network can be powered by the generator-starter to power electrical components. A secondary voltage of the second secondary electrical network is greater than the voltage of the first secondary electrical network, thus making it possible to optimize the weight of the electrical architecture. The two secondary electrical networks may also be powered from autonomous sources of electricity as a replacement for the primary network to power the generator-starter and the electrical components.
ARCHITECTURE ÉLECTRIQUE A DOUBLÉ RÉSEAU ÉLECTRIQUE SECONDAIRE POUR LE DÉMARRAGE DES MOTEURS D'UN AÉRONEF
AN ELECTRICAL ARCHITECTURE WITH PAIRED SECONDARY ELECTRICAL NETWORKS FOR STARTING ENGINES OF AN AIRCRAFT
ELEKTRISCHE SCHALTUNGSARCHITEKTUR MIT DOPPELTEM SEKUNDÄR-STROMKREIS ZUM ANLASSEN DER MOTOREN EINES LUFTFAHRZEUGS
2019-06-26
Patent
Electronic Resource
French
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