An architecture for an aircraft comprises two air-conditioning systems, two converters, each intended to supply one of the air-conditioning systems, and at least one first electric machine which starts up a first main engine of the aircraft. The electrical architecture is configured such that the two converters can together supply the first electric machine. A method of operating the architecture is also provided.
ARCHITECTURE ÉLECTRIQUE D'AÉRONEF, AÉRONEF COMPRENANT L'ARCHITECTURE ET PROCÉDÉ DE FONCTIONNEMENT DE L'ARCHITECTURE
ELECTRICAL ARCHITECTURE OF AN AIRCRAFT, AIRCRAFT COMPRISING THE ARCHITECTURE AND OPERATING METHOD OF THE ARCHITECTURE
ELEKTRISCHE ARCHITEKTUR FÜR LUFTFAHRZEUG, DIESE ARCHITEKTUR UMFASSENDES LUFTFAHRZEUG UND FUNKTIONSVERFAHREN DER ARCHITEKTUR
2020-12-09
Patent
Electronic Resource
French
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