Near zero velocity lubrication system for a turbine engine
A system is provided for a turbine engine. This turbine engine system includes a rotating assembly, a bearing and a lubrication system. The bearing is configured with the rotating assembly. The lubrication system is configured to lubricate the bearing. The lubrication system includes a lubricant pump and a lubricant reservoir. The lubricant pump is mechanically coupled with and driven by the rotating assembly. The lubricant pump is configured with the lubricant reservoir so as to be at least partially submersed in lubricant contained within the lubricant reservoir.
1. A system for a turbine engine, comprising:
a rotating assembly including a fan rotor, a compressor rotor, a turbine rotor and a gear system, the gear system mechanically coupled between the fan rotor and the turbine rotor;
a bearing configured with the gear system;
a lubrication system configured to lubricate the bearing, the lubrication system comprising a lubricant pump and a lubricant reservoir;
a guide vane; and
a tower shaft extending radially through the guide vane, a first end of the tower shaft mechanically coupled with the gear system, and a second end of the tower shaft mechanically coupled with the lubricant pump;
wherein the lubricant pump is configured with the lubricant reservoir so as to be at least partially submersed in lubricant contained within the lubricant reservoir, and wherein a sidewall of the lubricant reservoir forms an outer peripheral boundary of a core gas path within the turbine engine.
2. The system of claim 1 , wherein the bearing comprises a journal bearing.
3. The system of claim 1 , wherein the fan rotor is operable to windmill, and the lubrication system is configured to lubricate the bearing during the windmilling.
4. The system of claim 1 , wherein the lubrication system is configured to lubricate the bearing as the rotating assembly rotates in a first rotational direction and a second rotational direction.
5. The system of claim 1 , wherein the lubrication system is operable to lubricate the bearing where the rotating assembly rotates at less than about five revolutions per minute.
6. The system of claim 1 , wherein the lubrication system further includes a clutch configured to:
mechanically couple the lubricant pump to the tower shaft where the rotating assembly rotates at or below a threshold rotational velocity; and
mechanically decouple the lubricant pump from the tower shaft where the rotating assembly rotates above the threshold rotational velocity.
7. The system of claim 6 , wherein the clutch is a mechanically actuated clutch.
8. The system of claim 6 , wherein the clutch is an electrically actuated clutch.
9. The system of claim 6 , wherein the clutch is configured for mounting with the turbine engine as a line replaceable unit.
10. The system of claim 1 , wherein the lubricant pump is configured for mounting with the turbine engine as a line replaceable unit.
11. The system of claim 1 , wherein the lubrication system further includes a lubricant flow regulator arranged inline between the lubricant pump and the bearing.
12. The system of claim 1 , further comprising:
a combustor; and
a second lubrication system configured to lubricate the bearing during at least a mode of operation where the combustor is operational;
wherein the lubrication system is configured to lubricate the bearing during at least another mode of operation where the combustor is non-operational.
13. The system of claim 1 , wherein the first end of the tower shaft is a gravitational upper end of the tower shaft, and the second end of the tower shaft is a gravitational lower end of the tower shaft.
14. The system of claim 1 , wherein
the gear system comprises a ring gear; and
the first end of the tower shaft is mechanically coupled with the ring gear.
15. The system of claim 1 , further comprising:
a first bevel gear mounted to the tower shaft at the first end of the tower shaft; and
a second bevel gear mounted to the gear system and meshed with the first bevel gear.
16. The system of claim 1 , wherein the second end of the tower shaft is within the lubricant reservoir.
17. A system for a turbine engine, comprising:
a rotating assembly including a fan rotor, a compressor rotor, a turbine rotor and a gear system, the gear system mechanically coupled between the fan rotor and the turbine rotor;
a bearing configured with the gear system;
a lubrication system configured to lubricate the bearing as the rotating assembly rotates at less than about five revolutions per minute, the lubrication system including a lubricant pump and a lubricant reservoir;
a guide vane; and
a tower shaft extending through the guide vane and between a first end and a second end, the first end mechanically coupled with the gear system, and the second end mechanically coupled with the lubricant pump;
wherein the lubricant pump is configured with the lubricant reservoir so as to be at least partially submersed in lubricant contained within the lubricant reservoir.
18. A system for a turbine engine, comprising:
a rotating assembly including a fan rotor, a compressor rotor, a turbine rotor and a gear system, the gear system mechanically coupled between the fan rotor and the turbine rotor;
a bearing rotatably supporting a component of the gear system;
a lubrication system configured to lubricate the bearing, the lubrication system comprising a lubricant pump and a lubricant reservoir;
a guide vane; and
a tower shaft extending through the guide vane and between a first shaft end and a second shaft end, the first shaft end mechanically coupled with the gear system at the first shaft end, and a second shaft end mechanically coupled with the lubricant pump;
wherein the lubricant pump is configured with the lubricant reservoir so as to be at least partially submersed in lubricant contained within the lubricant reservoir.
19. The system of claim 18 , wherein
the gear system comprises a ring gear; and
the first shaft end is mechanically coupled with the ring gear.
20. The system of claim 18 , further comprising:
a first bevel gear mounted to the tower shaft at the first shaft end; and
a second bevel gear mounted to the gear system and meshed with the first bevel gear.