A method of electrically powering an electrical load in an aircraft, the method including electrically powering the electrical load with a main source that generates electricity; measuring an instantaneous parameter characterizing the main source; determining a level of use of the main source from the measured instantaneous parameter; adjusting the voltage of the main source as a function of the level of use; measuring an output voltage from the main source; comparing the measured voltage or the level of use with a predetermined threshold value; and whenever the measured voltage is less than the predetermined threshold value, electrically powering the electrical load from an auxiliary source that stores electricity so as to supply additional electric power to the electrical load.


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    Title :

    PROCÉDÉ ET SYSTÈME D'ALIMENTATION D'UNE CHARGE ÉLECTRIQUE DANS UN AÉRONEF


    Additional title:

    POWER SUPPLY METHOD AND POWER SUPPLY SYSTEM FOR AN ELECTRICAL LOAD WITHIN AN AIRCRAFT
    STROMVERSORGUNGSVERFAHREN UND STROMVERSORGUNGSSYSTEM FÜR EINE ELEKTRISCHE LAST IN EINEM LUFTFAHRZEUG


    Contributors:

    Publication date :

    2023-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F03D Windkraftmaschinen , WIND MOTORS / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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