A system for a shutdown of an electric aircraft port in response to a fault detection is presented. The system includes a sensor communicatively connected to a charging component, wherein the sensor is configured to detect at least a measured charger datum and generate a sensor datum as a function of the at least a measured charger datum. The system further includes a computing device, wherein the computing device is configured to identify a fault element as a function of the sensor datum, determine a disruption element as a function of the identification of the fault element. and initiate a shutdown protocol of the port as a function of the disruption element.


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    Titel :

    SYSTEMS AND METHODS FOR A SHUTDOWN OF AN ELECTRIC AIRCRAFT PORT IN RESPONSE TO A FAULT DETECTION


    Beteiligte:
    WIEGMAN HERMAN (Autor:in)

    Erscheinungsdatum :

    2023-05-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    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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