A power management system for an aircraft with a hybrid power source comprises a rechargeable electricity source and an electricity generating source, a detector determining status data of the elements of the aircraft power consumption electrical circuit, and power data relating to the instantaneous electrical power demanded by the aircraft and/or the charging status of the rechargeable electricity sources, an automaton receiving the power data from the detector and determining a control status for the power sources, an adapter determining a backup electrical configuration when the status data indicate a failure, a controller determining an electrical control for the rechargeable electrical source and the electrical generating source based on the instantaneous electrical power demanded, and a switch emitting commands to the switches of the aircraft power consumption electrical circuit to implement a nominal electrical configuration, or, a backup electrical configuration for the adapter in case of receipt thereof.


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    Title :

    SYSTEME DE GESTION D'ENERGIE POUR AERONEF A SOURCE D'ENERGIE HYBRIDE COMPRENANT AU MOINS UNE SOURCE D'ELECTRICITE RECHARGEABLE ET UNE SOURCE DE GENERATION D'ELECTRICITE


    Additional title:

    SYSTEM FOR MANAGING POWER FOR AN AIRCRAFT WITH A HYBRID POWER SOURCE COMPRISING AT LEAST ONE RECHARGEABLE ELECTRICITY SOURCE AND ONE ELECTRICITY GENERATING SOURCE
    SYSTEM ZUR LEISTUNGSVERWALTUNG FÜR EIN FLUGZEUG MIT EINER HYBRIDEN STROMQUELLE MIT MINDESTENS EINER WIEDERAUFLADBAREN STROMQUELLE UND EINER STROMERZEUGUNGSQUELLE


    Contributors:

    Publication date :

    2024-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge