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.


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    Title :

    ARCHITECTURE ÉLECTRIQUE D'AÉRONEF, AÉRONEF COMPRENANT L'ARCHITECTURE ET PROCÉDÉ DE FONCTIONNEMENT DE L'ARCHITECTURE


    Additional title:

    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


    Contributors:

    Publication date :

    2020-12-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    ARCHITECTURE ELECTRIQUE D'AERONEF, AERONEF COMPRENANT L'ARCHITECTURE ET PROCEDE DE FONCTIONNEMENT DE L'ARCHITECTURE

    LACAUX FREDERIC / GUGUEN STEPHANE / MAALOUF AMIRA | European Patent Office | 2021

    Free access

    ARCHITECTURE ELECTRIQUE DE PILOTAGE DE CONVERTISSEURS ET AERONEF COMPRENANT L'ARCHITECTURE

    LACAUX FREDERIC / GUGUEN STEPHANE / DEVAUTOUR JOEL | European Patent Office | 2022

    Free access