Debris resistant thrust bearing assembly for high speed hydraulic centrifugal turbines and pumps

Patent metadata

Field	Value
Publication number	US-9683574-B2
Application number	US-201414468989-A
Country	US
Kind code	B2
Filing date	Aug 26, 2014
Priority date	Dec 22, 2011
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

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.

First claim

What is claimed is:

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;
at least one blade housed within the shroud;
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; and
a stationary element that contacts the disk on a face opposite the shroud, wherein a fluid is configured to flow between the stationary element and the disk so that when the disk rotates, the disk resists the generation of drag between the face of the disk and the stationary element of the bearing assembly.

2. The bearing assembly of claim 1 , wherein:
the disk is annular; and
the 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 heated prior to placing the disk in the recess; and
the radial force is generated by a thermal expansion differential between the shroud and the disk.

6. 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.

7. The bearing assembly of claim 1 , wherein the shroud comprises stainless steel.

8. The bearing assembly of claim 1 , wherein the disk comprises at least one of a ceramic, graphite, and metallic carbide.

9. The bearing assembly of claim 1 , wherein the stationary element comprises at least one of a ceramic, graphite, and metallic carbide.

10. The bearing assembly of claim 1 , wherein a portion of the recess remains vacant when the disk is seated in the recess.

11. A bearing assembly configured for use in turbines and pumps, the bearing assembly comprising:
a shroud 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, wherein the disk comprises a first face and a second face opposite from the first face, wherein a first portion of the first face of the disk is configured to contact a second portion of an outer face of the shroud, and wherein the recess comprises a cavity disposed between a third portion of the first face of the disk and a fourth portion of the outer face of the shroud; and
a stationary element that contacts the second face of the disk, wherein a fluid is configured to flow between the stationary element and the disk so that when the disk rotates, the disk resists the generation of drag between the face of the disk and the stationary element of the bearing assembly.

12. The bearing assembly of claim 11 , wherein the fourth portion of the outer face of the shroud comprises:
first and second surfaces extending away from the third portion of the first face of the disk; and
an arcuate surface extending between the first and second surfaces.

13. The bearing assembly of claim 11 , wherein the disk and the cavity are annular.

14. The bearing assembly of claim 11 , comprising at least one blade housed within the shroud.

Assignees

• Energy Recovery Inc

Inventors

• Winkler Felix
• Calkins Jeffrey Michael

Classifications

• Y02P70/525

  Cross-Sectional Technologies · mapped topic

• F16C2202/52

  Graphite · CPC title

• F04D29/057 Primary

  hydrostatic; hydrodynamic · CPC title

• Y02E10/226

  Cross-Sectional Technologies · mapped topic

• F03B11/063

  Arrangements for balancing axial thrust · CPC title