System and method for communicating a pre-charging package stream of an electric aircraft

1. A system for communicating at least a pre-charging datum for an electric vehicle, the system comprising:

an electric aircraft, wherein the electric aircraft comprises:

a sensor, wherein the sensor is configured to:

detect a connection with a charging connector;

at least a battery pack, wherein the at least a battery pack comprises a plurality of battery cells;

an aircraft recharging component, the aircraft recharging component comprising an aircraft side recharging component, wherein the aircraft side recharging component is configured to form a charge connection with the charging connector;

a controller, wherein the controller is configured to:

generate a battery parameter set as a function of the connection with the charging connector, wherein generating the battery parameter set further comprises:

selecting a training set as a function of the battery parameter set, wherein the battery parameter set is correlated to an element of charging data;

training a pre-charge machine learning model using the training set; and

generating using the pre-charge machine learning model, a pre-charge function based on the battery parameter set; and

transmit the battery parameter set to the charging connector.

2. The system of claim 1 , wherein the electric aircraft further comprises an electric aircraft port.

3. The system of claim 2 , wherein the electric aircraft port is configured to mate with the charging connector.

4. The system of claim 2 , wherein the electric aircraft port is configured to receive a current from the charging connector as a function of the connection with the charging connector.

5. The system of claim 2 , wherein the current is a direct current.

6. The system of claim 2 , wherein the electric aircraft port is further configured to support bidirectional charging.

7. The system of claim 1 , wherein the aircraft recharging component comprises an aircraft side recharging component coupled to the sensor.

8. The system of claim 1 , wherein the electric aircraft further comprises a database.

9. The system of claim 1 , wherein the battery parameter set comprises:

at least a charge requirement;

at least a charging parameter; and

at least a cooling parameter.

10. The system of claim 1 , wherein the pre-charge function comprises a determination on whether the charging connector has a capability to provide recharge to the electric aircraft.

11. A method for communicating at least a pre-charging datum for an electric vehicle, the method comprising:

detecting, by a sensor, a connection with a charging connector;

forming, by an aircraft recharging component, a charge connection with a charge station;

generating, by a controller, a battery parameter set, wherein generating the battery parameter set further comprises:

selecting a training set as a function of the battery parameter set, wherein the battery parameter set is correlated to an element of charging data;

training a pre-charge machine learning model using the training set; and

generating using the pre-charge machine learning model, a pre-charge function based on the battery parameter set and transmitting the battery parameter set to the charging connector.

12. The method of claim 11 , wherein the electric aircraft further comprises an electric aircraft port.

13. The method of claim 12 , wherein the electric aircraft port is configured to mate with the charging connector.

14. The method of claim 12 , wherein the electric aircraft port is configured to receive a current from the charging connector as a function of the connection with the charging connector.

15. The method of claim 14 , wherein the current is a direct current.

16. The method of claim 12 , wherein the electric aircraft port is further configured to support bidirectional charging.

17. The method of claim 11 , wherein the aircraft recharging component comprises an aircraft side recharging component coupled to the sensor.

18. The method of claim 11 , wherein the electric aircraft further comprises a database.

19. The method of claim 11 , wherein the battery parameter set comprises:

at least a charge requirement;

at least a charging parameter; and

at least a cooling parameter.

20. The method of claim 11 , wherein the pre-charge function comprises a determination on whether the charging connector has a capability to provide recharge to the electric aircraft.