Hybrid electric engine power distribution
Examples described herein provide a computer-implemented method for managing battery usage for a hybrid electric engine of an aircraft. The method includes receiving a flight plan comprising flight plan data for a flight of an aircraft. The method further includes receiving battery data about a battery system of the aircraft. The method further includes determining waypoints for when to apply electric power from the battery system based at least in part on the flight plan data and the battery data. The method further includes controlling, based at least in part on the waypoints, an electric motor while the flight plan is executed. The method further includes updating, while the flight plan is executed, the waypoints based at least in part on data received during the flight.
1. A method for managing battery usage for a hybrid electric engine of an aircraft, the method comprising:
receiving a flight plan comprising flight plan data for a flight of an aircraft;
receiving battery data about a battery system of the aircraft;
determining waypoints for when to apply electric power from the battery system based at least in part on the flight plan data and the battery data;
controlling, based at least in part on the waypoints, an electric motor while the flight plan is executed; and
updating, while the flight plan is executed, the waypoints based at least in part on data received during the flight, wherein determining waypoints further comprises prioritizing the waypoints at least in part on a calculated efficiency ratio between fuel saved and electric power used, calculated as lbs of fuel/kWh of electric power.
2. The method of claim 1 , wherein the prioritizing is further based at least in part on a fuel price.
3. The method of claim 1 , wherein updating the waypoints comprises:
identifying a climb boost opportunity based at least in part on the data received during the flight and the battery data.
4. The method of claim 1 , wherein the flight plan data defines a plurality of flight events, wherein the plurality of flight events comprises a taxi out event, a takeoff event, a climb event, a cruise event, a descent event, and a taxi back event.
5. The method of claim 4 , wherein determining the waypoints comprises assigning a priority to each of the plurality of flight events relative to the other of the plurality of flight events based upon the prioritizing the waypoints step.
6. A controller comprising processing circuitry to:
receive a flight plan comprising flight plan data for a flight of an aircraft;
receive battery data about a battery system of the aircraft;
determine waypoints for when to apply electric power from the battery system based at least in part on the flight plan data and the battery data;
control, based at least in part on the waypoints, an electric motor while the flight plan is executed; and
update, while the flight plan is executed, the waypoints based at least in part on data received during the flight wherein determining waypoints further comprises prioritizing the waypoints at least in part on a calculated efficiency ratio between fuel saved and electric power used, calculated as lbs of fuel/kWh of electric power.
7. The controller of claim 6 , wherein the prioritizing is further based at least in part on a fuel price.
8. The controller of claim 6 , wherein updating the waypoints comprises:
identifying a climb boost opportunity based at least in part on the data received during the flight and the battery data.
9. The controller of claim 6 , wherein the flight plan data defines a plurality of flight events, wherein the plurality of flight events comprises a taxi out event, a takeoff event, a climb event, a cruise event, a descent event, and a taxi back event, and wherein determining the waypoints comprises assigning a priority to each of the plurality of flight events relative to the other of the plurality of flight events based upon the prioritizing the waypoints step.