An aircraft having a hybrid power source includes horizontal drive thrusters powered by an electric motor and forming a horizontal drive unit, vertical take-off/landing rotors forming with electric motors and a corresponding stored electrical energy source a vertical drive unit comprising an electric power supply bus, power generation sources connected to the electric power supply buses and by an input of a vertical drive unit and to each horizontal drive unit via an output of each vertical drive unit. The electric power supply controller emits a power command to the power generation source according to power requirements of the vertical and/or horizontal drive units. The stored electrical energy sources supply electricity according to the difference between the power requirements of the vertical and/or horizontal drive units. The power generation source recharges the stored electrical energy sources, so that the stored electrical energy sources are passively controlled.


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    Titel :

    AERONEF A SOURCE D'ENERGIE HYBRIDE


    Weitere Titelangaben:

    AIRCRAFT HAVING A HYBRID POWER SOURCE
    FLUGZEUG MIT HYBRIDENERGIEQUELLE


    Beteiligte:
    DINEL CLÉMENT (Autor:in) / FERRAN BENOÎT (Autor:in)

    Erscheinungsdatum :

    19.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64U / 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



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