Gas turbine engine and method for operating same

1. A method for operating a gas turbine engine, the method comprising:

providing a first gas turbine engine spool comprising a first compressor, a first turbine, and a first shaft, the first shaft interconnecting the first compressor and the first turbine;

directing pressurized air from the first compressor to an auxiliary turbine during a first loading condition of the first turbine and controlling a flow rate of the pressurized air directed to the auxiliary turbine;

generating electrical energy, during the first loading condition, with an auxiliary generator in rotational communication with the auxiliary turbine;

storing the electrical energy in an energy storage device during the first loading condition; and

applying the electrical energy stored in the energy storage device to an electrical load at a second loading condition of the first turbine, the second loading condition greater than the first loading condition.

2. The method of claim 1 , wherein the auxiliary turbine is in rotational communication with first shaft.

3. The method of claim 2 , wherein the auxiliary turbine and the auxiliary generator have a motor-generator configuration and wherein applying the electrical energy stored in the energy storage device to the electrical load further comprises applying the electrical energy to the auxiliary generator causing the auxiliary turbine to apply a rotational force to the first shaft.

4. The method of claim 3 , wherein applying the electrical energy to the auxiliary generator causing the auxiliary turbine to apply the rotational force to the first shaft further comprises mechanically disconnecting the first turbine from the first shaft.

5. The method of claim 1 , wherein controlling the flow rate of the pressurized air directed to the auxiliary turbine further comprises establishing a first flow rate of the pressurized air at the first loading condition and a second flow rate of the pressurized air, different than the first flow rate of the pressurized air, at the second loading condition.

6. The method of claim 5 , wherein the first flow rate is greater than the second flow rate.

7. The method of claim 1 , wherein generating the electrical energy further comprises applying a first rotational force to the auxiliary generator with the auxiliary turbine, the method further comprising applying a second rotational force to the first shaft with the auxiliary turbine while applying the first rotational force to the auxiliary generator with the auxiliary turbine.

8. The method of claim 7 , further comprising controlling a ratio of the first rotational force to the second rotational force based on a fuel flow of the gas turbine engine.

9. The method of claim 1 , further comprising providing a second gas turbine engine spool comprising a second compressor, a second turbine, and a second shaft, the second shaft interconnecting the second compressor and the second turbine.

10. The method of claim 9 , wherein the first gas turbine engine spool is a high-pressure spool and the second gas turbine engine spool is a low-pressure spool.

11. The method of claim 9 , wherein the first gas turbine engine spool is a high-pressure spool and the second gas turbine engine spool is a low-pressure spool.

12. The method of claim 1 , further comprising controlling a flow rate of the pressurized air directed to the auxiliary turbine.

13. The method of claim 12 , wherein controlling the flow rate of the pressurized air further comprises establishing a first flow rate of the pressurized air at the first loading condition and a second flow rate of the pressurized air, different than the first flow rate of the pressurized air, at the second loading condition.

14. The method of claim 13 , wherein the first flow rate is greater than the second flow rate.

15. The method of claim 1 , further comprising providing a second gas turbine engine spool comprising a second compressor, a second turbine, and a second shaft, the second shaft interconnecting the second compressor and the second turbine.

16. A method for operating a gas turbine engine, the method comprising:

providing a first gas turbine engine spool comprising a first compressor, a first turbine, and a first shaft, the first shaft interconnecting the first compressor and the first turbine;

directing pressurized air from a pressurized air source to an auxiliary turbine during a first loading condition of the first turbine;

generating electrical energy with an auxiliary generator in rotational communication with the auxiliary turbine, during the first loading condition, by applying a first rotational force to the auxiliary generator with the auxiliary turbine, the auxiliary turbine and the auxiliary generator having a motor-generator configuration;

storing the electrical energy in an energy storage device during the first loading condition; and

applying the electrical energy stored in the energy storage device to the auxiliary generator, at a second loading condition of the first turbine, causing the auxiliary turbine to apply a rotational force to the first shaft, the second loading condition greater than the first loading condition.

17. The method of claim 16 , wherein the auxiliary turbine is in rotational communication with first shaft and the auxiliary generator via a gearbox system.

18. The method of claim 17 , further comprising applying a second rotational force to the first shaft with the auxiliary turbine while applying the first rotational force to the auxiliary generator with the auxiliary turbine.

19. The method of claim 18 , further comprising controlling a ratio of the first rotational force to the second rotational force.

20. The method of claim 16 , further comprising applying the electrical energy stored in the energy storage device to one or more electrical loads at the second loading condition.