The present disclosure is directed to a gas-lubricated bearing assembly for a gas turbine engine and method of damping same. The bearing assembly includes a bearing pad for supporting a rotary component and a bearing housing attached to or formed integrally with the bearing pad. The bearing housing
The present disclosure is directed to a gas-lubricated bearing assembly for a gas turbine engine and method of damping same. The bearing assembly includes a bearing pad for supporting a rotary component and a bearing housing attached to or formed integrally with the bearing pad. The bearing housing includes a first fluid damper cavity, a second fluid damper cavity in restrictive flow communication with the first fluid damper cavity via a restrictive channel configured as a clearance gap, and a damper fluid configured within the first and second fluid damper cavities. More specifically, the damper fluid of the present disclosure is configured to withstand the high temperature environment of the engine. Thus, the bearing housing is configured to transfer the damper fluid from the first fluid damper cavity to the second fluid damper cavity via the restrictive channel in response to a force acting on the bearing pad.
대표청구항▼
1. A bearing assembly for a gas turbine engine, the bearing assembly comprising: a bearing pad for supporting a rotary component; anda bearing housing attached to or formed integrally with the bearing pad, the bearing housing comprising:a first fluid damper cavity positioned adjacent to the bearing
1. A bearing assembly for a gas turbine engine, the bearing assembly comprising: a bearing pad for supporting a rotary component; anda bearing housing attached to or formed integrally with the bearing pad, the bearing housing comprising:a first fluid damper cavity positioned adjacent to the bearing pad;a second fluid damper cavity spaced from the first fluid damper cavity and in restrictive flow communication with the first fluid damper cavity via a restrictive channel configured as a clearance gap; anda damper fluid configured within the first and second fluid damper cavities, the bearing housing configured to transfer the damper fluid from the first fluid damper cavity to the second fluid damper cavity via the restrictive channel in response to a force acting on the bearing pad;wherein each of the first and second fluid damper cavities comprises a fill hole to allow the first and second fluid damper cavities to be filled, respectively. 2. The bearing assembly of claim 1, wherein the first and second fluid damper cavities and the restrictive channel are sealed together and together define a fixed volume. 3. The bearing assembly of claim 1, wherein the damper fluid comprises a fluid comprising a viscosity that decreases with temperature by less than 10% for every 100 degrees Fahrenheit. 4. The bearing assembly of claim 3, wherein the damper fluid comprises a liquid metal. 5. The bearing assembly of claim 4, wherein the liquid metal comprises a gallium-based liquid metal. 6. The bearing assembly of claim 5, wherein the gallium-based liquid metal comprises a gallium indium alloy. 7. The bearing assembly of claim 1, wherein a coefficient of thermal expansion of the damper fluid is approximately equal to a coefficient of thermal expansion of the bearing housing plus or minus about 20%. 8. The bearing assembly of claim 7, further comprising an accumulation component configured to absorb excess damper fluid caused by a mismatch in the coefficient of thermal expansion of the damper fluid and the coefficient of thermal expansion of the bearing housing. 9. The bearing assembly of claim 8, wherein the accumulation component is mounted to the bearing housing. 10. The bearing assembly of claim 1, wherein the bearing assembly defines a radial direction, the first fluid damper cavity being spaced from the second fluid damper cavity along the radial direction. 11. The bearing assembly of claim 1, wherein the bearing housing comprises a first wall comprising a semi-rigid portion and a rigid portion, wherein the semi-rigid portion of the first wall at least partially defines the first fluid damper cavity, and wherein the rigid portion of the first wall at least partially defines the second fluid damper cavity. 12. The bearing assembly of claim 11, wherein the bearing housing further comprises a second wall comprising a semi-rigid portion, wherein the semi-rigid portion of the second wall at least partially defines the second fluid damper cavity. 13. The bearing assembly of claim 1, wherein the bearing housing comprises a semi-rigid column extending towards the bearing pad for providing the bearing pad with an airflow and fully supporting the bearing pad. 14. A method for providing damping to a gas-lubricated bearing assembly of a gas turbine engine, the bearing assembly having a bearing pad for supporting a rotary component and a bearing housing attached to or formed integrally with the bearing pad, the method comprising: filling a first fluid damper cavity of the bearing housing positioned adjacent to the bearing pad with a damper fluid;filling a second fluid damper cavity of the bearing housing spaced from the first fluid damper cavity with the damper fluid, the second fluid damper cavity in restrictive flow communication with the first fluid damper cavity via a restrictive channel; andallowing the damper fluid to flow between the first and second fluid damper cavities via the restrictive channel in response to a force acting on the bearing pad, the flow of damper fluid providing damping to the gas-lubricated bearing assembly;wherein each of the first and second fluid damper cavities comprises a fill hole to allow the first and second fluid damper cavities to be filled, respectively. 15. The method of claim 14, further comprising controlling the damping of the gas-lubricated bearing assembly as a function of at least one of volumetric displacement of the damper fluid per unit linear displacement of the bearing pad, a size of the restrictive channel, and a viscosity of the damper fluid. 16. The method of claim 14, wherein filling the first fluid damper cavity of the bearing housing and filling the second fluid damper cavity of the bearing housing further comprises: filling the first damper cavity with the damper fluid; andallowing the damper fluid to flow from the filled first fluid damper cavity to the second fluid damper cavity via the restrictive channel. 17. The method of claim 16, further comprising: providing a damper fluid filling system having inlet tubing, outlet tubing, one or more valves, a vacuum pump, and a damper fluid reservoir for filling the first and second damper cavities;arranging the inlet tubing with the fill hole of the first damper cavity;arranging the outlet tubing with the fill hole of the second damper cavity;filling the first damper cavity with the damper fluid via the inlet tubing;allowing the damper fluid to flow from the filled first fluid damper cavity to the second fluid damper cavity via the restrictive channel; andonce the first and second cavities are filled, removing the inlet and outlet tubing and capping the fill holes of the first and second fluid damper cavities. 18. The method of claim 17, further comprising, before filling the first fluid damper cavity, evacuating, via the vacuum pump, air from within the first and second fluid damper cavities so as drop a pressure within the first and second fluid damper cavities. 19. The method of claim 18, further comprising: providing at least one valve in the inlet tubing and at least one valve in the outlet tubing;arranging the inlet tubing and the inlet tubing valve with the damper fluid reservoir;arranging the outlet tubing and the outlet tubing valve with the vacuum pump;closing the inlet tubing valve and opening the outlet tubing valve during evacuating; andopening the inlet tubing valve and the outlet tubing valve during filling.
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