Systems and methods for restricting power to a load to prevent engaging circuit protection device for an aircraft

1. A system for restricting power to a load to prevent engaging a circuit protection device for an electric aircraft, the system comprising:

at least an energy source of an electric aircraft, wherein the at least an energy source is communicatively coupled to a load of a plurality of loads, wherein the load comprises at least a portion of a propulsion system of the electric aircraft;

a plurality of sensors mounted on the electric aircraft, wherein each sensor of the plurality of sensors are designed and configured to:

sense at least an electrical parameter of the at least a portion of the propulsion system of the electric aircraft; and

measure the resistance of the at least an energy source;

an aircraft controller communicatively connected to the at least an energy source, wherein the aircraft controller is designed and configured to:

receive at least an electrical parameter of the at least a portion of the propulsion system of the electric aircraft from the plurality of sensors;

compare the at least an electrical parameter to at least a current allocation threshold, wherein the current allocation threshold is generated as a function of at least a circuit protection threshold of load;

detect that the at least an electrical parameter has reached the current allocation threshold;

generate a current allocation threshold notification as a function of the detection, wherein the current allocation threshold notification indicates that the at least an electrical parameter has reached the current allocation threshold.

2. The system of claim 1 , wherein the plurality of sensors further comprises the plurality of sensors communicatively connected to the aircraft controller.

3. The system of claim 1 , wherein the plurality of sensors further includes:

at least a current sensor; and

at least a voltage sensor.

4. The system of claim 1 , wherein comparing the at least an electrical parameter to the at least a current allocation threshold further comprises:

continuous comparison of the at least an electrical parameter to the at least a current allocation threshold.

5. The system of claim 1 , wherein the aircraft controller is configured to:

calculate a power reduction to the load; and

reduce power from the at least an energy source to each load of the plurality of loads by the power reduction.

6. The system of claim 5 , wherein reducing power from the at least an energy source to each load further includes:

disconnecting the communication between the at least an energy source and the at least an electrical circuit; and

reconnecting the communication between the at least an energy source and the at least an electrical circuit.

7. The system of claim 5 , wherein reducing power from the at least an energy source to each load further includes:

preventing communication between the at least an energy source and the at least an electrical circuit.

8. The system of claim 5 , further comprising a user selection device, wherein the user selection device is configured to:

receive the power reduction to the load;

display the power reduction to the load.

9. The system of claim 8 , wherein the user selection device is further configured to:

audibly announce the power reduction to the load.

10. The system of claim 1 further comprising an overload relay.

11. The system of claim 1 further comprising:

a fuse; and

a circuit breaker.

12. A method of restricting power to a load to prevent engaging a circuit protection device for an electric aircraft, the method comprising:

sensing, by a plurality of sensors, at least an electrical parameter of a load of a plurality of loads;

receiving, by an aircraft controller communicatively connected to at least an energy source, from the plurality of sensors:

at least an electrical parameter of at least a portion of the propulsion system of the electric aircraft; and

the measured resistance of the at least an energy source;

comparing the at least an electrical parameter to at least a current allocation threshold, wherein the current allocation threshold is generated as a function of at least a circuit protection threshold of load;

detecting the at least an electrical parameter has reached the current allocation threshold; and

generating a current allocation threshold notification as a function of the detection, wherein the current allocation threshold notification indicates that the at least an electrical parameter has reached the current allocation threshold.

13. The method of claim 12 , wherein sensing the at least an electrical parameter further comprises sensing, by at least a current sensor, a current level.

14. The method of claim 12 , wherein sensing the at least an electrical parameter further comprises sensing, by at least a voltage sensor, a voltage level.

15. The method of claim 12 , wherein comparing the at least an electrical parameter to the at least a current allocation threshold further comprises:

continuous comparison of the at least an electrical parameter to the at least a current allocation threshold.

16. The method of claim 12 , wherein the aircraft controller is configured to:

Calculate a power reduction to the load; and

reduce power from the at least an energy source to each load of the plurality of loads by the power reduction.

17. The method of claim 12 , further comprising a user selection device, wherein the user selection device is configured to:

receive the power reduction to the load;

display the power reduction to the load.

18. The method of claim 17 , wherein the user selection device is further configured to:

audibly announcing the power reduction to the load.

19. The method of claim 16 , wherein reducing power from the at least an energy source to each load further includes:

disconnecting the communication between the at least an energy source and the at least an electrical circuit; and

reconnecting the communication between the at least an energy source and the at least an electrical circuit.

20. The method of claim 16 , wherein reducing power from the at least an energy source to each load further includes:

preventing communication between the at least an energy source and the at least an electrical circuit.