SYSTEM FOR OVERVOLTAGE PROTECTION IN AN ELECTRIC AIRCRAFT AND A METHOD FOR ITS USE

A system for overvoltage protection in an electric aircraft, and a method for its use. The system includes an energy storage element, an overvoltage protection device, a ground conductor, at least a current conductor, at least a sensor, and a controller. The overvoltage protection device is configured to control transmission of electrical power through the connector. The at least a sensor is configured to detect an output voltage of the connector. The controller is communicatively connected to the at least a sensor. The controller is configured to determine an overvoltage output, and activate the over based on detection of the overvoltage output.