Squeeze film damper, bearing unit, and turbine
US-9890810-B2 · Feb 13, 2018 · US
US11067121B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11067121-B2 |
| Application number | US-201916355986-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 18, 2019 |
| Priority date | Mar 18, 2019 |
| Publication date | Jul 20, 2021 |
| Grant date | Jul 20, 2021 |
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A multi-film oil damper has a housing defining an annular damper cavity between a radially outward wall and radially extending side walls. The annular damper cavity has an oil inlet configured for connection to a source of pressurized oil. A closure ring defines a radially inward boundary of the annular damper cavity. First and second damper rings are nested together coaxially within the annular damper cavity. At least one of the first damper ring and the second damper ring has an axial end radial thickness less than an intermediate-portion radial thickness.
Opening claim text (preview).
What is claimed is: 1. A multi-film oil damper comprising: a housing defining an annular damper cavity between a radially outward wall and radially extending side walls, the annular damper cavity having an oil inlet configured for connection to a source of pressurized oil; a closure ring defining a radially inward boundary of the annular damper cavity; and a first damper ring and a second damper ring nested together coaxially within the annular damper cavity, wherein at least one of the first damper ring and the second damper ring has an end radial thickness less than a radial thickness at a location intermediate opposed axial ends of the ring, wherein a maximum radial thickness (T) of the first damper ring and of the second damper ring is provided at a middle portion of the first damper ring and the second damper ring between the opposed axial ends thereof, and wherein the middle portion of at least one of the first damper ring and the second damper ring is cylindrical, the at least one of the first damper ring and the second damper ring having an axial end surface oriented perpendicular to the cylindrical middle portion, and defining an axial end edge between the cylindrical middle portion and the axial end surface. 2. The multi-film oil damper according to claim 1 wherein a radially inner surface of the first damper ring and a radially outer surface of the second damper ring define a wedge gap therebetween, and wherein the first damper ring and the second damper ring are symmetric about a central radial axis. 3. The multi-film oil damper according to claim 2 wherein the first damper ring and the second damper ring have axial cross sectional profiles that are identical, and wherein the wedge gap is axially symmetrical. 4. The multi-film oil damper according to claim 1 wherein the axial end edge arcuately merges between the cylindrical middle portion and the axial end surface. 5. The multi-film oil damper according to claim 1 wherein the axial end edge has a constant edge radius. 6. The multi-film oil damper according to claim 1 wherein the axial end edge is a chamfered surface joining the cylindrical middle portion and the axial end surface. 7. The multi-film oil damper according to claim 1 wherein at least one of the first damper ring and the second damper ring has one of: a radially inner axially arcuate surface, and a radially outer axially arcuate surface. 8. The multi-film oil damper according to claim 7 wherein the axially arcuate surface is spherical. 9. The multi-film oil damper according to claim 1 wherein at least one of the first damper ring and the second damper ring has one of: a radially inner cylindrical surface; and a radially outer cylindrical surface. 10. A method of distributing oil between coaxial damper rings of a multi-film oil damper, the method comprising: sealing an oil damper cavity with a radially moveable closure ring injecting pressurized oil into the oil damper cavity via an oil inlet; providing a first damper ring and a second damper ring within the oil damper cavity, the first damper ring and the second damper ring being coaxially nested, one of the first damper ring and the second damper ring having a spherical surface, the first damper ring and the second damper ring having axially adjacent end surfaces that are radially spaced-apart so as to define an axially symmetrical wedge gap, wherein a maximum radial thickness (T) of the first damper ring and of the second damper ring is provided at a middle portion of the first damper ring and the second damper ring; and separating the first damper ring and the second damper ring by applying oil pressure on the spaced apart adjacent axial end surfaces. 11. The method according to claim 10 wherein the axially adjacent end surfaces are arcuate.
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