An electrical propulsion system for an aircraft includes a central bus and a plurality of branches, each branch having at least one electrical power source, at least one electric propulsion device, and a branch bus, connected to each source and to each propulsion device of the branch. Each branch includes a DC/DC voltage converter connecting the branch bus to the central bus, said DC/DC voltage converter being configured to galvanically isolate said branch bus from the central bus.
SYSTÈME DE PROPULSION ÉLECTRIQUE POUR UN AÉRONEF
ELECTRICAL PROPULSION SYSTEM FOR AN AIRCRAFT
ELEKTRISCHES ANTRIEBSSYSTEM FÜR EIN FLUGZEUG
2024-11-06
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
SYSTÈME ÉLECTRIQUE D’UNE PROPULSION ÉLECTRIQUE D’UN AÉRONEF
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