Modified aircraft idle for reduced thermal cycling

1. An engine assembly comprising:

a multi-spool combustion turbine engine including a high spool and at least one lower spool;

a plurality of offtakes powered by the combustion turbine engine, at least one of the plurality of offtakes configured to selectively take power from the at least one lower spool; and

a controller configured to operate the combustion turbine engine through a range between a first low-idle mode, a second high-idle mode, and a maximum takeoff power rating mode, wherein the controller is configured to select between the low-idle mode or the high-idle mode on taxi-in based at least in part on an expected turnaround time of the engine between a taxi-in and a following taxi-out;

wherein the controller operates the engine in the low-idle mode by directing at least a first portion of power from the at least one lower spool to the plurality of offtakes, and wherein the controller operates the engine in the high idle mode by increasing a speed of the high spool relative to a speed of the high spool in the low-idle mode, thereby increasing a compressor outlet (T 3 ) temperature in the high idle mode relative to a T 3 temperature in the low-idle mode.

2. The engine assembly of claim 1 , wherein the plurality of offtakes comprises one or more of a starter/generator, a boost motor, and an electric propulsion unit.

3. The engine assembly of claim 1 , wherein the engine assembly is a hybrid engine assembly further comprising an electric propulsion unit and means for storing energy to power the electric propulsion unit.

4. The engine assembly of claim 3 , wherein the electric propulsion unit is operable in series or parallel with the combustion turbine engine.

5. The engine assembly of claim 3 , wherein the high-idle mode includes operating the plurality of offtakes from the lower spool to charge batteries at a first charging rate to retain the increased idle speed and increased T 3 relative to the idle speed and T 3 of the low-idle mode.

6. The engine assembly of claim 5 , wherein the low-idle mode includes operating the plurality of offtakes from the lower spool to charge batteries at a second charging rate lower than the first charging rate.

7. The engine assembly of claim 5 , wherein the controller is configured to operate the high-idle mode on taxi-in and the low-idle mode on either taxi-in or taxi-out.

8. The engine assembly of claim 7 , wherein the controller is operative to accept an input corresponding to the expected turnaround time of the engine.

9. The engine assembly of claim 1 , wherein the high-idle mode includes directing at least a second portion of power from the lower spool to the high spool.

10. The engine assembly of claim 9 , further comprising a generator connected to the lower spool and a corresponding motor connected to the high spool, wherein the controller is configured to operate the generator and the motor to selectively transfer a portion of power from the at least one lower spool to the high spool.

11. A method of operating an aircraft, the method comprising:

selectively operating an engine assembly including a multi-spool combustion turbine engine and a plurality of offtakes, the engine assembly operable through a range between a first low-idle mode, a second high idle mode, and a maximum takeoff power rating mode; and

powering the plurality of offtakes by connection to at least one lower spool of the combustion turbine engine, at least one of the plurality of offtakes configured to selectively take power from the at least one lower spool;

wherein the combustion turbine engine operates in the low-idle mode by directing at least a first portion of power from the at least one lower spool to the plurality of offtakes, and wherein the combustion turbine engine operates in the high idle mode by increasing a speed of a high spool relative to a speed of the high spool in the low-idle mode, thereby increasing a compressor outlet (T 3 ) temperature in the high idle mode relative to a T 3 temperature in the low-idle mode; and

wherein the high idle mode is operable on taxi-in and the low-idle mode is operable on taxi-in or taxi-out based on an expected turnaround time.

12. The method of claim 11 , wherein the plurality of offtakes comprises one or more of a starter/generator, a boost motor, and an electric propulsion unit.

13. The method of claim 11 , wherein the aircraft is a hybrid aircraft further comprising an electric propulsion unit and means for storing energy to power the electric propulsion unit.

14. The method of claim 13 , wherein the electric propulsion unit is operable in series or parallel with the combustion turbine engine.

15. The method of claim 11 , wherein the high-idle mode includes operating the plurality of offtakes from the lower spool to charge batteries at a first charging rate to retain the increased idle speed and increased T 3 relative to the idle speed and T 3 of the low-idle mode.

16. The method of claim 15 , further comprising:

accepting an input corresponding to the expected turnaround time between a taxi-in and a following taxi-out; and

from at least the input, determining whether the taxi-in operation should begin with the low-idle mode or the high-idle mode.

17. The method of claim 11 , wherein at least a second portion of power is directed from the at least one lower spool to the high spool.