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.
SYSTEMS AND METHODS FOR A SHUTDOWN OF AN ELECTRIC AIRCRAFT PORT IN RESPONSE TO A FAULT DETECTION
2023-05-04
Patent
Elektronische Ressource
Englisch
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