Systems and methods for high voltage battery charging and vertiport operations
Aspects of the present disclosure generally relate to systems and methods for the configuration and control of charging and cooling systems for aircrafts driven by electric propulsion systems and in other types of vehicles. In some embodiments, a method of charging an aircraft is disclosed comprising: receiving a mode of operation indicating whether battery packs of the aircraft are connected in parallel prior to joining a charging bus, receiving charging protocol information, and controlling charging operations of the battery packs based on the mode of operation and the charging protocol information.
1. A method of charging an aircraft, the method comprising:
receiving a mode of operation indicating whether battery packs of the aircraft are connected in parallel prior to joining a charging bus;
receiving charging protocol information; and
controlling charging operations of the battery packs based on the mode of operation and the charging protocol information.
2. The method of claim 1 , wherein the received mode of operation indicates a user selection between a first mode indicating that the battery packs are not connected in parallel prior to joining the charging bus and a second mode indicating that the battery packs are connected in parallel prior to joining the charging bus.
3. The method of claim 1 , wherein controlling charging operations comprises:
connecting at least a portion of the battery packs to the charging bus one at a time, beginning with the lowest voltage battery pack, when the received mode of operations indicates the battery packs are not connected in parallel prior to joining the charging bus.
4. The method of claim 1 , wherein controlling charging operations comprises:
connecting at least a portion of the battery packs on the charging bus in sets of connected battery packs, beginning with a battery pack set with the lowest voltage, when the received mode of operation indicates the battery packs are connected in parallel prior to joining the charging bus.
5. The method of claim 1 , wherein controlling charging operations comprises:
connecting at least one of the battery packs to the charging bus when the at least one battery pack is within a threshold voltage of a battery pack already connected to the charging bus.
6. The method of claim 5 , wherein connecting the at least one battery pack to the charging bus comprises connecting multiple battery packs to the charging bus when each of the multiple battery packs is within the threshold voltage.
7. The method of claim 1 , wherein controlling charging operations comprises:
disconnecting a battery pack from the charging bus in response to determining that the battery pack reached a target state of charge.
8. The method of claim 1 , wherein controlling charging operations comprises:
disconnecting a connected set of battery packs from the charging bus once each battery pack in the connected set reaches a respective target state of charge, when the received mode of operation indicates the battery packs are connected in parallel prior to joining the charging bus.
9. The method of claim 1 , wherein controlling charging operations comprises:
connecting all battery packs that are within a threshold voltage to the charging bus, beginning with the battery pack at the lowest voltage, prior to charging the battery packs;
charging the battery packs connected to the charging bus to within a threshold voltage of at least one battery pack remaining disconnected from charging bus; and
connecting the at least one remaining battery pack to the charging bus.
10. The method of claim 1 , wherein the received mode indicates whether the battery packs are connected to low voltage loads prior to joining the charging bus.
11. The method of claim 10 , wherein controlling the charging operations comprises:
controlling charging of the battery packs in consideration of the charge lost to the low voltage loads when the received mode of operation indicates the battery packs are connected to the low voltage loads.
12. The method of claim 1 , further comprising:
wherein the received mode of operation is from a user input device comprising at least one of: a switch, knob, button, lever, or display.
13. The method of claim 12 , wherein the user input device is located in a pilot cockpit.
14. The method of claim 1 , wherein the charging protocol information includes at least one of: an energy target for a battery pack, C-rate target for a battery pack, or time allotted for charging.
15. The method of claim 1 , wherein the charging protocol information includes different energy targets for at least two of the battery packs.
16. The method of claim 15 , wherein the different energy targets are based on flight information.
17. The method of claim 1 ,
wherein a charging profile for charging the battery packs is developed based on the charging protocol information, the charging profile including a charge rate and time for charging at the charge rate; and
wherein controlling charging operations of the battery packs is based on the charging profile.
18. The method of claim 1 , wherein the charging protocol information includes at least one of: an electrical limit of a charging port, a limit of a battery pack contactor, a battery pack thermal limit, or a limit established based on information received from other aircraft.
19. The method of claim 1 , wherein:
charging protocol information includes at least one battery pack limit; and
controlling the charging operations comprises monitoring a current into each of the battery packs and regulating a commanded charge to ensure the at least one battery pack limit is not exceeded.
20. The method of claim 1 , wherein:
charging protocol information includes at least one battery pack temperature limit; and
controlling the charging operations comprises monitoring a temperature of each battery pack and sending a coolant command to ensure the at least one battery pack temperature limit is not exceeded,
wherein the coolant command controls at least one of: a coolant flow rate, coolant pressure, or coolant temperature.
21. The method of claim 1 , further comprising:
receiving the charging protocol information from a user input device,
wherein the user input device comprises at least one of: a switch, a knob, a button, a lever, or a display.
22. The method of claim 1 , further comprising:
wherein the received mode of operation is from a first user input device mounted to a body of the aircraft or a second user input device in a pilot cockpit.
23. The method of claim 22 , wherein the first user input device is configured to receive the charging protocol information when the second user input device is powered off.
24. The method of claim 1 , wherein controlling charging operations comprises commanding a charge rate from a ground charging station via a wired or wireless connection.
25. The method of claim 1 , wherein controlling charging operations comprises commanding, via a wired or wireless connection, a coolant flow rate or pressure from a ground charging station to regulate a temperature of the battery packs during the charging operations.
26. A charging control system for an aircraft comprising at least one processor configured to execute instructions to cause the system to:
receive a mode of operation indicating whether battery packs of the aircraft are connected in parallel prior to joining a charging bus;
receive charging protocol information; and
control charging operations of the battery packs based on the mode of operation and the charging protocol information.
27. A non-transitory computer-readable medium storing instructions which, when executed by at least one processor, cause the at least one processor to:
receive a mode of operation indicating whether battery packs of an aircraft are connected in parallel prior to joining a charging bus;
receive charging protocol information; and
control charging operations of the battery packs based on the mode of operation and the charging protocol information.