Lubrication system for aircraft powerplant and clutch system
A system is provided for an aircraft. This aircraft system includes a powertrain and a first lubrication system. The powertrain includes a powerplant, a bladed rotor and a clutch system operatively coupling the powerplant to the bladed rotor. The powerplant is configured to drive rotation of the bladed rotor through the clutch system when the clutch system is engaged. The first lubrication system is fluidly coupled with and is configured to deliver first lubricant to the powerplant and the clutch system.
1. A system for an aircraft, comprising:
a powertrain including a powerplant, a bladed rotor and a clutch system, the clutch system operatively coupling the powerplant to the bladed rotor, the powerplant configured to drive rotation of the bladed rotor through the clutch system when the clutch system is engaged;
a geartrain operatively coupling the clutch system to the bladed rotor; and
a first lubrication system fluidly coupled with and configured to deliver a first lubricant to the powerplant and the clutch system, the first lubrication system fluidly independent of the geartrain, wherein the first lubricant is directed through the clutch system.
2. The system of claim 1 , wherein
the powerplant further includes a power transmission operatively coupling the powerplant to the clutch system; and
the first lubrication system is fluidly coupled to the power transmission and further configured to deliver the first lubricant to the power transmission.
3. The system of claim 2 , wherein
the power transmission comprises a power geartrain operatively coupling the powerplant to the clutch system; and
the first lubrication system is fluidly coupled to the power geartrain and further configured to deliver the first lubricant to the power geartrain.
4. The system of claim 2 , wherein
the power transmission comprises an accessory geartrain; and
the first lubrication system is fluidly coupled to the accessory geartrain and further configured to deliver the first lubricant to the accessory geartrain.
5. The system of claim 2 , wherein the first lubrication system includes
a heat exchanger including an inlet and an outlet; and
a lubricant circuit extending longitudinally through the power transmission, the powerplant and the clutch system from the outlet to the inlet.
6. The system of claim 2 , wherein the first lubrication system includes a lubricant circuit extending in a downstream direction from the power transmission to the powerplant.
7. The system of claim 2 , wherein the first lubrication system includes a lubricant circuit extending in a downstream direction from the powerplant to the power transmission.
8. The system of claim 2 , wherein the first lubrication system includes a lubricant circuit extending in a downstream direction from the power transmission to the clutch system.
9. The system of claim 1 , wherein the first lubrication system includes a lubricant circuit extending in a downstream direction from the powerplant to the clutch system.
10. The system of claim 1 , wherein the powerplant comprises an internal combustion engine.
11. The system of claim 1 , wherein the powerplant comprises an electric motor.
12. The system of claim 1 , further comprising a second lubrication system fluidly independent of the first lubrication system, the second lubrication system fluidly coupled with and configured to deliver a second lubricant to the geartrain.
13. The system of claim 1 , wherein
the bladed rotor comprises a rotorcraft rotor; and
the aircraft comprises a rotorcraft.
14. The system of claim 13 , wherein the rotorcraft rotor is a main rotorcraft rotor.
15. A system for an aircraft, comprising:
a powertrain including a powerplant, a bladed rotor and a clutch system, the clutch system operatively coupling the powerplant to the bladed rotor, the powerplant configured to drive rotation of the bladed rotor through the clutch system when the clutch system is engaged;
a gear system geartrain operatively coupling the clutch system to the bladed rotor; and
a lubrication system including a heat exchanger and a lubricant circuit, the heat exchanger including an inlet and an outlet, the lubricant circuit extending longitudinally from the outlet, through the powerplant and the clutch system, and to the inlet, and the lubrication system fluidly independent of the gear system geartrain.
16. The system of claim 15 , wherein
the powertrain further includes a power transmission operatively coupling the powerplant to the clutch system; and
the lubricant circuit further extends through the power transmission.
17. The system of claim 16 , wherein the lubricant circuit extends sequentially from the power transmission, through the powerplant, to the clutch system.
18. The system of claim 15 , wherein the lubricant circuit extends in a downstream direction from the outlet, through the powerplant and the clutch system, and to the inlet.