A power distribution circuit for an electrically powered aircraft includes a plurality of batteries and a plurality of electric propulsion systems. A plurality of isolated power distribution circuits each couple a battery of the plurality of batteries to two or more electric propulsion systems. The plurality of electric propulsion systems are positioned on the aircraft to apply balanced forces to the aircraft such that in the event of a failure, the aircraft remains stable and only experiences a loss in altitude or speed.


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    Titel :

    ELECTRICALLY POWERED PROPULSION SYSTEMS FOR AIRCRAFT


    Weitere Titelangaben:

    ELEKTRISCH ANGETRIEBENE ANTRIEBSSYSTEME FÜR FLUGZEUGE
    SYSTÈMES DE PROPULSION À ALIMENTATION ÉLECTRIQUE POUR AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    13.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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