Compressor
US-2016341249-A1 · Nov 24, 2016 · US
US9822816B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9822816-B2 |
| Application number | US-201515126635-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 19, 2015 |
| Priority date | Mar 19, 2014 |
| Publication date | Nov 21, 2017 |
| Grant date | Nov 21, 2017 |
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Provided is a foil bearing, an air film is formed in a radial bearing gap between a first bearing surface arranged on a top foil and a second bearing surface along with rotation of a shaft, and the shaft is supported with a pressure of the air film. Lubricating powder is interposed between the bearing surfaces. The top foil is partially elastically deformed in a width direction of the radial bearing gap in accordance with the pressure of the air film generated in the radial bearing gap, thereby being alternately shifted between a first state in which a retaining portion capable of retaining the lubricating powder is formed and a second state in which the retaining portion substantially disappears, and shifted from the second state to the first state along with an increase in the pressure of the air film.
Opening claim text (preview).
The invention claimed is: 1. A foil bearing, comprising: a stationary side member; and a rotary side member, any one of the stationary side member and the rotary side member comprising: a top foil formed of a flexible metal thin plate; and an elastic support portion configured to elastically support the top foil, a first bearing surface arranged on the top foil, a second bearing surface of another member opposed to the first bearing surface, an air film formed in a bearing gap between the first bearing surface and the second bearing surface along with rotation of the rotary side member, the rotary side member supported with a pressure of the air film, and powder having lubricity and being interposed between the first bearing surface and the second bearing surface, wherein at least a part of the top foil is elastically deformed in a width direction of the bearing gap in accordance with the pressure of the air film to be shifted alternately between a first state in which a retaining portion capable of retaining the powder is formed and a second state in which the retaining portion substantially disappears, and shifted from the second state to the first state along with an increase in the pressure of the air film. 2. A foil bearing according to claim 1 , wherein the powder is an oxide of abrasion powder generated by abrasion of at least one of a base material of the top foil and a base material of the another member along with slide contact between the first bearing surface and the second bearing surface. 3. A foil bearing according to claim 1 , wherein at least one of the first bearing surface and the second bearing surface includes a protruding portion protruding toward another bearing surface side. 4. A foil bearing according to claim 1 , wherein the powder contains solid lubricant powder different from an abrasion powder of a base material of the top foil and a base material of the another member. 5. A foil bearing according to claim 1 , wherein at least one of the first bearing surface and the second bearing surface is arranged on a lubricating film formed on a base material. 6. A foil bearing according to claim 1 , wherein the bearing gap is a radial bearing gap. 7. A foil bearing according to claim 1 , wherein the bearing gap is a thrust bearing gap. 8. A foil bearing according to claim 1 , wherein the foil bearing is to be used for supporting a rotor of a turbo-machine.
with solids as lubricant, e.g. dry coatings, powder · CPC title
with flexible leaves to create hydrodynamic wedge, e.g. radial foil bearings · CPC title
Gas turbine engines · CPC title
Details of the bearing surface, e.g. means to generate pressure such as lobes or wedges · CPC title
with flexible leaves to create hydrodynamic wedge, e.g. axial foil bearings · CPC title
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