The invention relates to a drive system (1) for an aircraft (100). The drive system (1) has a first energy store (10) for supplying electrical energy and a second energy store (20) for supplying electrical energy. In addition, the drive system (1) has at least one electric drive (30) for supplying drive power for the aircraft. An energy distribution unit (40) of the drive system (1) is designed to transmit the supplied electrical energy of the first energy store (10) and the supplied electrical energy of the second energy store (20) to the at least one electric drive (30). The energy distribution unit (40) is also designed to charge the second energy store (20) using a first portion of the energy supplied by the first energy store (10) and at the same time to transmit a second portion of the energy supplied by the first energy store (10) to the at least one electric drive (30), in order therefore to supply the drive power for the aircraft (100). In addition, an aircraft (100) having a drive system (1) and a method for supplying drive power for an aircraft (100) are disclosed.


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    Titel :

    DRIVE SYSTEM FOR AN AIRCRAFT AND METHOD FOR SUPPLYING DRIVE POWER FOR AN AIRCRAFT


    Weitere Titelangaben:

    ANTRIEBSSYSTEM FÜR EIN FLUGZEUG UND VERFAHREN ZUR BEREITSTELLUNG VON ANTRIEBSLEISTUNG FÜR EIN FLUGZEUG
    SYSTÈME DE COMMANDE POUR AÉRONEF ET PROCÉDÉ DE FOURNITURE DE PUISSANCE D'ENTRAÎNEMENT POUR UN AÉRONEF


    Beteiligte:
    HUNKEL PETER (Autor:in)

    Erscheinungsdatum :

    2020-10-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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