Hybrid energy storage system control for an aircraft engine

1. A power system of an aircraft, the power system comprising:

a hybrid energy storage system comprising at least two energy storage subsystems each having a different power-energy density;

one or more electric motors operably coupled to the hybrid energy storage system and to an aircraft engine; and

a means for controlling one or more electric power flows of the hybrid energy storage system to/from the one or more electric motors based on a modeled electric power demand associated with an engine load of one or more spools of the aircraft engine, wherein the modeled electric power demand is determined by a model-based control based on current engine load data and a projected engine load over one or more future time steps, the projected engine load being determined by an engine system model.

2. The power system of claim 1 , wherein the means for controlling the one or more electric power flows of the hybrid energy storage system comprises a power management controller operable to detect one or more conditions of the at least two energy storage subsystems and configure the one or more electric power flows between the hybrid energy storage system and the one or more electric motors.

3. The power system of claim 2 , wherein the power management controller is operable to configure at least one of the one or more electric power flows from a first energy storage subsystem of the at least two energy storage subsystems to charge a second energy storage subsystem of the at least two energy storage subsystems.

4. The power system of claim 3 , wherein the first energy storage subsystem comprises a battery system and the second energy storage subsystem comprises a super/ultra-capacitor, and further comprising a bidirectional converter operably coupled to the super/ultra-capacitor and power conditioning electronics operably coupled to the one or more electric motors.

5. The power system of claim 4 , wherein the power management controller is operable to configure at least one of the one or more electric power flows from the super/ultra-capacitor through the bidirectional converter and the power conditioning electronics to power the one or more electric motors.

6. The power system of claim 5 , wherein the bidirectional converter is operably coupled to the battery system, and the power management controller is operable to configure at least one of the one or more electric power flows from the battery system through the bidirectional converter and the power conditioning electronics to power the one or more electric motors and/or engine subsystem loads.

7. The power system of claim 6 , wherein the power management controller is operable to select between powering the one or more electric motors by the super/ultra-capacitor and/or the battery system based on a power level of the modeled electric power demand and the one or more conditions of the super/ultra-capacitor and the battery system, and further wherein the power management controller is operable to control the one or more electric motors in a generator mode and charge the super/ultra-capacitor.

8. The power system of claim 6 , wherein the power management controller is operable to select between powering the one or more electric motors by the super/ultra-capacitor and/or the battery system based on an expected duration of the modeled electric power demand and the one or more conditions of the super/ultra-capacitor and the battery system.

9. The power system of claim 1 , wherein the power management controller is operable to predictively switch to source power from the hybrid energy storage system instead of the aircraft engine when the one or more electric motors are being operated.

10. A method comprising:

determining, by a controller, an engine load of one or more spools of an aircraft engine;

determining, by the controller, a modeled electric power demand based on the engine load, wherein the modeled electric power demand is determined by a model-based control based on current engine load data and a projected engine load over one or more future time steps, the projected engine load being determined by an engine system model; and

configuring one or more electric power flows of a hybrid energy storage system based on the modeled electric power demand, wherein the hybrid energy storage system comprises at least two energy storage subsystems each having a different power-energy density.

11. The method of claim 10 , further comprising:

detecting one or more conditions of the at least two energy storage subsystems; and

configuring the one or more electric power flows between the hybrid energy storage system and one or more electric motors based on the one or more conditions of the at least two energy storage subsystems.

12. The method of claim 11 , further comprising:

configuring at least one of the one or more electric power flows from a first energy storage subsystem of the at least two energy storage subsystems to charge a second energy storage subsystem of the at least two energy storage subsystems.

13. The method of claim 12 , wherein the first energy storage subsystem comprises a battery system and the second energy storage subsystem comprises a super/ultra-capacitor, and further comprising:

configuring at least one of the one or more electric power flows from the super/ultra-capacitor through a bidirectional converter and power conditioning electronics to power the one or more electric motors.

14. The method of claim 13 , further comprising:

configuring at least one of the one or more electric power flows from the battery system through the bidirectional converter and the power conditioning electronics to power the one or more electric motors and/or engine subsystem loads.

15. The method of claim 14 , further comprising:

selecting between powering the one or more electric motors by the super/ultra-capacitor and/or the battery system based on a power level of the modeled electric power demand and the one or more conditions of the super/ultra-capacitor and the battery system; and

controlling the one or more electric motors in a generator mode to charge the super/ultra-capacitor.

16. The method of claim 14 , further comprising:

selecting between powering the one or more electric motors by the super/ultra-capacitor and/or the battery system based on an expected duration of the modeled electric power demand and the one or more conditions of the super/ultra-capacitor and the battery system.

17. The method of claim 10 , further comprising:

predictively switching to source power from the hybrid energy storage system instead of the aircraft engine when the one or more electric motors are being operated.

18. A system for an aircraft, the system comprising:

a gas turbine engine comprising at least one shaft;

a hybrid energy storage system comprising a super/ultra-capacitor and a battery system;

one or more electric motors operably coupled to the hybrid energy storage system and to the at least one shaft; and

a means for controlling one or more electric power flows of the hybrid energy storage system to/from the one or more electric motors based on a modeled electric power demand associated with an engine load of the gas turbine engine, wherein the modeled electric power demand is determined by a model-based control based on current engine load data and a projected engine load over one or more future time steps, the projected engine load being determined by an engine system model.

19. The system of claim 18 , wherein the means for controlling the one or more electric power flows of the hybrid energy storage system comprises a power management controller operable to detect one or more conditions of the super/ultra-capacitor and the battery system and configure the one or more electric power flows from the hybrid energy storage system to the one or more electric motors based on the one or more conditions and the engine load of the at least one shaft.

20. The system of claim 19 , wherein the power management controller is operable to predictively switch to source power from the hybrid energy storage system instead of the gas turbine engine when the one or more electric motors are being operated.