Systems and methods for providing mechanical power to an aircraft accessory with a turbine engine
An example system for providing mechanical power to an aircraft accessory with a turbine engine, where the turbine engine includes a low-speed spool and a high-speed spool, includes an accessory gearbox disposed between the low-speed spool and the high-speed spool and a clutch disposed within or external to the accessory gearbox. The accessory gearbox is configured to drive the aircraft accessory, and the clutch is configured to enable either the high-speed spool or the low-speed spool to provide mechanical power to the aircraft accessory via the accessory gearbox.
1. A system for providing mechanical power to an aircraft accessory with a turbine engine, wherein the turbine engine includes a low-speed spool and a high-speed spool, the system comprising:
an accessory gearbox disposed between the low-speed spool and the high-speed spool, the accessory gearbox configured to drive the aircraft accessory; and
a clutch disposed within the accessory gearbox, the clutch configured to enable either the high-speed spool or the low-speed spool to provide mechanical power to the aircraft accessory via the accessory gearbox,
wherein the accessory gearbox further includes a first gear train and a second gear train, wherein the first gear train is coupled to a first shaft of the clutch and the first gear train is driven by a high-speed spool drive shaft, and wherein the second gear train is coupled to a second shaft of the clutch and the second gear train is driven by a low-speed spool drive shaft.
2. The system of claim 1 , wherein the clutch is a friction clutch.
3. The system of claim 1 , wherein the first shaft of the clutch and the second shaft of the clutch are concentric.
4. The system of claim 1 , wherein the first shaft of the clutch and the second shaft of the clutch are positioned side by side.
5. The system of claim 1 , wherein the first shaft of the clutch is also coupled to a plurality of engine accessories.
6. The system of claim 5 , wherein the plurality of engine accessories always receive mechanical power from the high-speed spool.
7. The system of claim 1 , wherein the clutch enables the low-speed spool to provide mechanical power to the aircraft accessory based on a rotational speed of the second shaft of the clutch being higher than a rotational speed of the first shaft of the clutch.
8. The system of claim 1 , wherein based on a rotational speed of the first shaft of the clutch being higher than a rotational speed of the second shaft of the clutch, the clutch locks to the high-speed spool drive shaft to enable the high-speed spool to provide mechanical power to the aircraft accessory.
9. The system of claim 1 , wherein the clutch is a first clutch, and the system further comprises:
a second clutch coupled between the low-speed spool drive shaft and the second gear train of the accessory gearbox.
10. The system of claim 9 , wherein based on the second clutch being open, the first clutch locks to the high-speed spool drive shaft to enable the high-speed spool to provide mechanical power to the aircraft accessory.
11. The system of claim 9 , wherein based on the high-speed spool providing mechanical power to the aircraft accessory, the second clutch is opened.
12. The system of claim 9 , wherein based on the second clutch being closed, the first clutch overruns the high-speed spool drive shaft to enable the low-speed spool to provide mechanical power to the aircraft accessory.
13. The system of claim 9 , wherein based on failure of the second clutch, the first clutch locks to the high-speed spool drive shaft to enable the high-speed spool to provide mechanical power to the aircraft accessory.
14. The system of claim 1 , further comprising an electrical motor power source coupled to the clutch, wherein the electrical motor power source provides mechanical power to the aircraft accessory via the accessory gearbox.
15. A system for providing mechanical power to an aircraft accessory with a turbine engine, wherein the turbine engine includes a low-speed spool and a high-speed spool, the system comprising:
an accessory gearbox disposed between the low-speed spool and the high-speed spool, the accessory gearbox configured to drive the aircraft accessory; and
a clutch disposed external to the accessory gearbox, the clutch configured to enable either the high-speed spool or the low-speed spool to provide mechanical power to the aircraft accessory via the accessory gearbox,
wherein the accessory gearbox further includes a first gear train and a second gear train, wherein the first gear train is coupled to a first shaft of the clutch and the first gear train is driven by a high-speed spool drive shaft, and wherein the second gear train is coupled to a second shaft of the clutch and the second gear train is driven by a low-speed spool drive shaft.
16. The system of claim 15 , wherein the clutch is a first clutch and the system further comprises:
a second clutch coupled between the low-speed spool drive shaft and the second gear train of the accessory gearbox.
17. The system of claim 15 , wherein the first shaft of the clutch and the second shaft of the clutch are concentric.
18. A method for providing mechanical power to an aircraft accessory with a turbine engine, wherein the turbine engine includes a low-speed spool and a high-speed spool and an accessory gearbox disposed between the low-speed spool and the high-speed spool that is configured to drive the aircraft accessory, the method comprising:
enabling, via a clutch of the accessory gearbox, either the high-speed spool or the low-speed spool to provide mechanical power to the aircraft accessory via the accessory gearbox,
wherein the accessory gearbox further includes a first gear train and a second gear train, wherein the first gear train is coupled to a first shaft of the clutch and the first gear train is driven by a high-speed spool drive shaft, and wherein the second gear train is coupled to a second shaft of the clutch and the second gear train is driven by a low-speed spool drive shaft.
19. The method of claim 18 , further comprising:
locking the clutch to the high-speed spool drive shaft to enable the high-speed spool to provide mechanical power to the aircraft accessory via the accessory gearbox based on a relative rotational speed of the second gear train of the accessory gearbox, that is coupled between the low-speed spool drive shaft and the clutch, being lower than occurring from the high-speed spool drive shaft.
20. The method of claim 18 , further comprising:
causing the clutch to overrun the high-speed spool drive shaft to enable the low-speed spool to provide mechanical power to the aircraft accessory via the accessory gearbox based on a speed of the second gear train of the accessory gearbox, that is coupled between the low-speed spool drive shaft and the clutch, being higher than occurring from the high-speed spool drive shaft.