FIELD OF THE INVENTION

The present invention generally relates to the field of electric aircrafts. In particular, the present invention is directed to a system and methods for preconditioning a power source of an electric aircraft.

BACKGROUND

Preflight preparations and maintenance of an aircraft is important. Failure to conduct appropriate preflight preparations can result in critical failure of the aircraft during operation.

SUMMARY OF THE DISCLOSURE

In an aspect, a system for preconditioning a power source in an electric aircraft, the system including: a sensor attached to a power source of an electric aircraft, wherein the sensor is configured to detect a condition datum of an operating component of the power source; and a computing device communicatively connected to the sensor, the flight controller configured to: obtain an optimal performance condition of the power source; identify an operating condition of the operating component of the power source as a function of the condition datum; determine a divergent element as a function of the optimal performance condition and the operating condition of the power source; and initiate a power source modification as a function of the divergent element.

In another aspect, a method for preconditioning a power source in an electric aircraft, the method including: detecting, by a sensor attached to a power source of an electric aircraft, a condition datum of the power source; obtaining, by a computing device communicatively connected to the sensor, an optimal performance condition of the power source; identifying an operating condition of the power source as a function of the condition datum; determining a divergent element as a function of the optimal performance condition and the operating condition of the power source; and initiating a power source modification as a function of the divergent element.

These and other aspects and features of non-limiting embodiments of the present invention will become apparent to those skilled in the art upon review of the following description of specific non-limiting embodiments of the invention in conjunction with the accompanying drawings.

