Rear bearing sleeve for gas turbine auxiliary power unit
The presently disclosed embodiments utilize a rear bearing sleeve interposed between an inner surface of an exhaust housing of a gas turbine auxiliary power unit and the rear roller bearing supporting a turbine within the exhaust housing. In some embodiments, the rear bearing sleeve includes a lubricant supply channel formed in an outer surface thereof for receipt of a supply of lubricant, and at least one lubricant supply opening between the outer surface and an inner surface thereof, the inner surface of the bearing sleeve forming an outer race of the rear roller bearing. The at least one lubricant supply opening supplies the lubricant to a gap between the rear roller bearing and the rear bearing sleeve for formation of a squeeze film viscous damper therebetween.
1. A gas turbine auxiliary power unit, comprising:
a turbine;
an exhaust housing of the auxiliary power unit;
a bearing disposed between the turbine and the exhaust housing;
a bearing sleeve disposed between the bearing and the exhaust housing, wherein the bearing sleeve serves as an outer race of the bearing and wherein a gap is maintained between an inner surface of the bearing sleeve and the bearing;
a lubricant disposed within the gap; and
wherein the turbine is at least partially supported by the bearing.
2. The gas turbine auxiliary power unit of claim 1 , wherein the bearing comprises a roller bearing.
3. The gas turbine auxiliary power unit of claim 1 , wherein the lubricant forms a squeeze film viscous damper between the bearing and the bearing sleeve.
4. The gas turbine auxiliary power unit of claim 1 , wherein the bearing sleeve comprises a material including one of: a high temperature alloy and hardened steel.
5. The gas turbine auxiliary power unit of claim 1 , wherein the bearing sleeve comprises:
an outer surface; and
at least one opening formed between the inner surface and the outer surface.
6. The gas turbine auxiliary power unit of claim 5 , further comprising:
a channel formed in at least a portion of the outer surface, wherein at least one of the at least one openings communicates with the channel.
7. The gas turbine auxiliary power unit of claim 6 , further comprising:
a lubricant delivery line formed in the exhaust housing, wherein the lubricant delivery line communicates with the channel and is configured to supply lubricant to the channel.
8. The gas turbine auxiliary power unit of claim 7 , wherein:
lubricant may flow from the channel, through the at least one opening and into the gap.
9. The gas turbine auxiliary power unit of claim 8 , wherein the lubricant forms a squeeze film viscous damper between the bearing and the bearing sleeve.
10. A bearing sleeve, comprising:
an annular body including an inner surface and an outer surface, wherein the bearing sleeve is an outer race of a bearing for use with a gas turbine auxiliary power unit;
at least one opening formed between the inner surface and the outer surface; and
a channel formed in at least a portion of the outer surface;
wherein the at least one opening formed between the inner surface and the outer surface is in fluid communication with the channel.
11. The bearing sleeve of claim 10 , wherein the bearing sleeve comprises a material including one of: a high temperature alloy and hardened steel.
12. The bearing sleeve of claim 10 , further comprising:
a lubricant delivery line disposed adjacent the annular body, wherein the lubricant delivery line communicates with the channel and supplies lubricant to the channel.
13. The bearing sleeve of claim 10 , wherein the channel extends completely around the outer surface.
14. The bearing sleeve of claim 10 , wherein the at least one opening comprises a plurality of openings.
15. The bearing sleeve of claim 14 , wherein the plurality of openings are spaced equidistant from one another.