초록 ▼

A rotating assembly adapted for use in turbines and pumps is provided. The rotating assembly includes a shroud that rotates around a central axis and a disk seated in a recess in the shroud so that the disk rotates with the shroud, the disk being oriented perpendicular to the central axis. The rotat

A rotating assembly adapted for use in turbines and pumps is provided. The rotating assembly includes a shroud that rotates around a central axis and a disk seated in a recess in the shroud so that the disk rotates with the shroud, the disk being oriented perpendicular to the central axis. The rotating assembly also includes a stationary element in which at least one surface of the disk contacts a fluid so that when the fluid flows under pressure, the surface of the disk resists the generation of drag between the surface and the stationary element of the rotating assembly. A shroud is provided that includes a circular recess with a cavity on an outer perimeter extending away from the fixed assembly. A method of manufacturing a rotating assembly is provided.

대표청구항 ▼

1. A bearing assembly configured for use in turbines and pumps, the bearing assembly comprising: a shroud that is configured to rotate around a central axis;a disk seated in a recess in the shroud so that the disk is configured to rotate with the shroud, the disk being oriented perpendicular to the

1. A bearing assembly configured for use in turbines and pumps, the bearing assembly comprising: a shroud that is configured to rotate around a central axis;a disk seated in a recess in the shroud so that the disk is configured to rotate with the shroud, the disk being oriented perpendicular to the central axis, wherein the recess comprises a cavity proximate to an outer face of the recess, and an interior surface of the recess between the cavity and the central axis is substantially planar and perpendicular to the central axis; anda stationary element disposed adjacent to the shroud, wherein at least one surface of the disk is configured to contact a fluid so that when the disk rotates, the at least one surface of the disk resists the generation of drag between the at least one surface and the stationary element of the bearing assembly. 2. The bearing assembly of claim 1, wherein: the disk is annular; andthe disk is replaceable. 3. The bearing assembly of claim 1, wherein the disk is installed and secured in the recess by thermal compression. 4. The bearing assembly of claim 3, wherein the thermal compression is accomplished by heating the shroud to a temperature exceeding 150 degrees Celsius, placing the disk in the recess, and allowing the assembly to cool so that the disk is secured in the recess by a radial force between the shroud and the disk. 5. The bearing assembly of claim 4, wherein the disk is not heated prior to placing the disk in the recess. 6. The bearing assembly of claim 4, wherein: the disk is heated prior to placing the disk in the recess; andthe radial force is generated by a thermal expansion differential between the shroud and the disk. 7. The bearing assembly of claim 6, wherein the thermal compression is reversible by heating the combination of the disk and the shroud. 8. The bearing assembly of claim 3, wherein the thermal compression is accomplished by cooling the disk, placing the disk in the recess, and allowing the assembly to warm to room temperature so that the disk is secured in the recess by a radial force between the shroud and the disk. 9. The bearing assembly of claim 1, wherein the shroud comprises stainless steel. 10. The bearing assembly of claim 1, wherein the disk comprises at least one of a ceramic, graphite, and metallic carbide. 11. The bearing assembly of claim 1, wherein the stationary element comprises at least one of a ceramic, graphite, polyether ether ketone, and metallic carbide. 12. The bearing assembly of claim 1, wherein: the cavity is U-shaped with parallel sides and an arcuate bottom andthe cavity comprises parallel sides defining an angle with respect to the interior surface. 13. The bearing assembly of claim 12, wherein the angle is less than or equal to 90 degrees. 14. The bearing assembly of claim 12, wherein the angle is more than 90 degrees. 15. The bearing assembly of claim 14, wherein the angle is substantially 95 degrees. 16. The bearing assembly of claim 1, wherein: the disk contacts the stationary element on a face opposite the recess; anda lubricant flows between the disk and the stationary element. 17. The bearing assembly of claim 16, wherein the lubricant comprises a portion of the fluid. 18. A rotating assembly for contacting a fixed assembly, the rotating assembly configured to rotate around a central axis, the rotating assembly comprising: a shroud comprising a recess, the recess comprising a cavity proximate to an outer face of the recess, wherein the cavity is configured to extend away from the fixed assembly, and an interior surface of the recess between the cavity and the central axis is substantially planar and perpendicular to the central axis; anda disk seated in the recess and contacting an outer face of the recess, the outer face being substantially parallel to the central axis and configured to compress the disk when the shroud is at a temperature less than 250 degrees Celsius. 19. The rotating assembly of claim 18, wherein the shroud is stainless steel. 20. The rotating assembly of claim 18, wherein the disk comprises at least one of ceramic, graphite, and metallic carbide. 21. The rotating assembly of claim 18, wherein the fixed assembly comprises at least one of ceramic, graphite, polyether ether ketone, and metallic carbide. 22. The rotating assembly of claim 18, wherein the cavity is U-shaped with parallel sides and an arcuate bottom. 23. The rotating assembly of claim 18, wherein the central axis intersects the recess substantially centrally. 24. The rotating assembly of claim 18, wherein the cavity comprises parallel sides defining an angle with respect to the interior surface. 25. The rotating assembly of claim 24, wherein the angle is less than 90 degrees. 26. The rotating assembly of claim 24, wherein the angle is more than 90 degrees. 27. The rotating assembly of claim 24, wherein the disk is configured to be installed and secured in the recess by thermal compression. 28. The rotating assembly of claim 27, wherein the thermal compression is accomplished by heating the shroud to a temperature exceeding 150 degrees Celsius, placing the disk in the recess, and allowing the assembly to cool so that the disk is secured in the recess by a radial force between the shroud and the disk. 29. The rotating assembly of claim 28, wherein the disk is not heated prior to placing the disk in the recess. 30. The rotating assembly of claim 28, wherein: the disk is heated prior to placing the disk in the recess; andthe radial force is generated by a thermal expansion differential between the shroud and the disk. 31. The rotating assembly of claim 30, wherein the thermal compression is reversible by heating the combination of the disk and the shroud. 32. The rotating assembly of claim 27, wherein the thermal compression is accomplished by cooling the disk, placing the disk in the recess, and allowing the assembly to warm to room temperature so that the disk is secured in the recess by a radial force between the shroud and the disk. 33. The rotating assembly of claim 18, wherein the shroud is coupled to at least one blade, the at least one blade configured to contact a fluid and when the fluid flows under pressure the at least one blade is configured to urge the shroud to rotate around the central axis. 34. The rotating assembly of claim 18, wherein: the disk contacts the fixed assembly on a face opposite the recess;a lubricant flows between the disk and the fixed assembly; andthe lubricant comprises a portion of the fluid. 35. A method of manufacturing a rotating assembly configured for use in turbines and pumps, the method comprising: arranging a disk in a recess of a shroud, wherein the recess in the shroud comprises a cavity proximate to an outer face of the recess, and an interior surface of the recess between the cavity and the central axis is substantially planar and perpendicular to the central axis; andsecuring the disk in the shroud with a radial force between the shroud and the disk caused by thermal compression of the disk by the shroud. 36. The manufacturing method of claim 35, comprising, before the arranging operation, heating the shroud to a temperature exceeding 150 degrees Celsius. 37. The manufacturing method of claim 36, wherein the disk is not heated prior to arranging the disk in the recess. 38. The manufacturing method of claim 36, wherein: the disk is heated prior to arranging the disk in the recess; andthe radial force is generated by a thermal expansion differential between the shroud and the disk. 39. The manufacturing method of claim 38, wherein the thermal compression is reversible by heating the combination of the disk and the shroud. 40. The manufacturing method of claim 35, comprising: before the arranging operation, cooling the disk;wherein the thermal compression is accomplished by allowing the assembly to warm to room temperature.