A method for managing the offtake of power produced by an auxiliary power unit of an aircraft. The method comprises a step of calculating a maximum capacity for offtake of mechanical power that the auxiliary power unit can provide to the aircraft, a step of determining an actual offtake of mechanical power taken off by a first mechanical power offtake system of the auxiliary power unit, a step of comparing the maximum capacity for offtake of mechanical power and the actual offtake of mechanical power, a step of optimizing the offtake of mechanical power which step, based on the comparison of the maximum capacity for offtake of mechanical power and the actual offtake of mechanical power, determines at least one corrective action. A device for managing the offtake of power produced by an auxiliary power unit of an aircraft and an aircraft including such a device are provided.


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    Title :

    PROCÉDÉ DE GESTION DU PRÉLÈVEMENT D'UNE PUISSANCE PRODUITE PAR UN GROUPE AUXILIAIRE DE PUISSANCE D'UN AÉRONEF ET AÉRONEF ÉQUIPÉ DUDIT DISPOSITIF DE GESTION DE PRÉLÈVEMENT DE PUISSANCE


    Additional title:

    METHOD FOR MANAGING THE DRAWING OF POWER GENERATED BY AN AUXILIARY POWER UNIT OF AN AIRCRAFT AND AIRCRAFT PROVIDED WITH SAID DEVICE FOR MANAGING DRAWING OF POWER
    VERFAHREN ZUR STEUERUNG DER AUFNAHME EINER LEISTUNG, DIE DURCH EIN HILFSTRIEBWERK EINES LUFTFAHRZEUGS ERZEUGT WIRD, UND MIT DIESER VORRICHTUNG ZUR STEUERUNG DER LEISTUNGSAUFNAHME AUSGESTATTETES LUFTFAHRZEUG


    Contributors:

    Publication date :

    2023-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES




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