Rotary machine with gas bearings
US-2017298772-A1 · Oct 19, 2017 · US
US10704600B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10704600-B2 |
| Application number | US-201815924804-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 19, 2018 |
| Priority date | Apr 18, 2016 |
| Publication date | Jul 7, 2020 |
| Grant date | Jul 7, 2020 |
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A bearing includes a bearing pad for supporting a rotary component and a housing attached to or formed integrally with the bearing pad. The housing includes a flexible column extending towards the bearing pad for providing the bearing pad with an airflow. The column supports the bearing pad from a location inward of an outer periphery of the bearing pad along an axial direction of the bearing. With such a configuration, a resistance of the bearing pad along a radial direction of the bearing is less at the outer periphery than a resistance of the bearing pad along the radial direction proximate the column.
Opening claim text (preview).
What is claimed is: 1. A bearing defining an axial direction and a radial direction, the bearing comprising: a bearing pad for supporting a rotary component and defining an outer periphery, a housing attached to or formed integrally with the bearing pad, the housing comprising a column extending towards the bearing pad for providing the bearing pad with an airflow, the column supporting the bearing pad from a location inward of the outer periphery of the bearing pad along the axial direction; wherein the column fully supports the bearing pad. 2. The bearing of claim 1 , wherein the bearing pad comprises a sintered porous metal selected from the group consisting of cobalt-alloy, nickel-alloy, and iron-alloy. 3. The bearing of claim 1 , wherein the bearing pad comprises a sintered porous carbon graphite. 4. The bearing of claim 1 , wherein the bearing is adapted to support the rotary component of a turbomachine. 5. The bearing of claim 4 , wherein the turbomachine is selected from the group consisting of a steam turbine, a centrifugal compressor, and a turbocharger. 6. The bearing of claim 5 , wherein the column supports the bearing pad such that a resistance of the bearing pad along the radial direction at the outer periphery is less than a resistance of the bearing pad along the radial direction proximate the column. 7. The bearing of claim 1 , wherein the bearing pad defines a center along the axial direction, and wherein the column is located approximately at the center of the bearing pad along the axial direction. 8. The bearing of claim 7 , wherein the bearing pad comprises an inner surface, wherein the inner surface defines one or more openings in airflow communication with the column. 9. The bearing of claim 1 , wherein the bearing defines a circumferential direction, wherein the bearing pad defines a center along the circumferential direction, and wherein the column is located approximately at the center of the bearing pad along the circumferential direction. 10. The bearing of claim 9 , wherein the bearing pad comprises an inner surface, wherein the inner surface defines one or more openings in airflow communication with the column. 11. The bearing of claim 1 , wherein the column is a single column fully supporting the bearing pad. 12. The bearing of claim 1 , wherein the column is a flexible column fully supporting the bearing pad. 13. A bearing defining an axial direction and a radial direction, the bearing comprising: a bearing pad for supporting a rotary component and defining an outer periphery, a housing attached to or formed integrally with the bearing pad, the housing comprising a column extending towards the bearing pad for providing the bearing pad with an airflow, the column supporting the bearing pad from a location inward of the outer periphery of the bearing pad along the axial direction, wherein the column fully supports the bearing pad, and wherein the bearing pad comprises plurality of gas distribution holes. 14. The bearing of claim 13 , wherein the plurality of gas distribution holes are disposed across the bearing pad. 15. The bearing of claim 14 , wherein the plurality of gas distribution holes are adapted to provide an evenly distributed pressure field to support and/or lubricate the rotary component. 16. The bearing of claim 13 , wherein the plurality of gas distribution holes have a diameter of between about 50 micrometers and about 2540 micrometers. 17. The bearing of claim 16 , wherein the column supports the bearing pad such that a resistance of the bearing pad along the radial direction at the outer periphery is less than a resistance of the bearing pad along the radial direction proximate the column. 18. The bearing of claim 13 , wherein the plurality of gas distribution holes have a diameter of between about 127 micrometers and about 508 micrometers. 19. The bearing of claim 13 , wherein the column is a single column fully supporting the bearing pad. 20. The bearing of claim 13 , wherein the column is a flexible column fully supporting the bearing pad.
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