Centering spring and damper assembly
An assembly includes a bearing having an annular shape, a bearing support radially outward from the bearing, a squeeze film damper having a first end adjacent the bearing and a second end adjacent the bearing support with the second end forming a squeeze film damping surface, and a first spring between the bearing and the bearing support with the first spring configured to resist a movement of the bearing to center a shaft radially inward from the bearing.
1. An assembly comprising:
a bearing having an annular shape;
a bearing support radially outward from the bearing;
a squeeze film damper having a first end adjacent the bearing and a second end adjacent the bearing support with the second end forming a squeeze film damping surface;
a first spring axially adjacent a first side of the squeeze film damper between the bearing and the bearing support, the first spring configured to resist a movement of the bearing to center a shaft radially inward from the bearing;
a second spring axially adjacent a second side of the squeeze film damper opposite the first spring between the bearing and the bearing support, the second spring configured to resist a movement of the bearing to center the shaft;
a first retaining ring adjacent a radially outer end of the first spring; and
a second retaining ring adjacent a radially inner end of the first spring,
wherein the first spring and the second spring each have a V-shaped cross section when viewed in a circumferential direction with a bottom of the V adjacent to the squeeze film damper.
2. The assembly of claim 1 , wherein the bearing support includes a damper fluid channel configured to provide a damping fluid to a gap between an inner surface of the bearing support and the squeeze film damping surface on the second end of the squeeze film damper.
3. The assembly of claim 1 , wherein the first spring and the second spring are each configured to compress and expand entirely in a radial direction.
4. The assembly of claim 1 , wherein the first spring and the second spring are annular and extend entirely circumferentially around the bearing.
5. The assembly of claim 1 , wherein the squeeze film damper has a beam between the first end and the second end so that the squeeze film damper has an “I” shape.
6. The assembly of claim 1 , further comprising:
two sealing rings between the bearing support and the second end of the squeeze film damper configured to prevent squeeze film damping fluid from flowing out of a gap between the bearing support and the second end of the squeeze film damper.
7. The assembly of claim 1 , wherein the first end of the squeeze film damper forms an outer race of the bearing.
8. An assembly for centering and damping a shaft, the assembly comprising:
a damper having an annular shape with a radially inner first end and a radially outer second end, the radially outer second end having a damping surface on a radially outer side;
at least one spring axially adjacent to the damper configured to resist a radial movement of the shaft;
a first retaining ring adjacent a radially outer end of the at least one spring; and
a second retaining ring adjacent a radially inner end of the at least one spring,
wherein the first retaining ring and the second retaining ring are configured to prevent axial movement of the at least one spring and the damper is entirely axially adjacent to the at least one spring.
9. The assembly of claim 8 , wherein the at least one spring comprises:
a first spring adjacent a first axial side of the damper; and
a second spring adjacent a second axial side of the damper,
wherein the damper is entirely axially between the first spring and the second spring.
10. The assembly of claim 8 , wherein the at least one spring is configured to compress and expand entirely in a radial direction.
11. The assembly of claim 8 , wherein the at least one spring has a V-shaped cross-section when viewed in a circumferential direction.
12. A gas turbine engine comprising:
a shaft;
a bearing radially surrounding at least a portion of the shaft;
a bearing housing radially outward from the bearing;
a squeeze film damper between the bearing and the bearing housing;
two sealing rings between the bearing housing and the squeeze film damper configured to prevent squeeze film damping fluid from flowing out of a gap between the bearing housing and the squeeze film damper; and
a first spring adjacent the squeeze film damper between the bearing and the bearing housing configured to keep the shaft centered with respect to the bearing housing, the first spring having a V-shaped cross section when viewed in a circumferential direction with a bottom of the V being adjacent to the squeeze film damper.
13. The gas turbine engine of claim 12 , further comprising:
a second spring adjacent a side of the squeeze film damper opposite the first spring, the second spring positioned between the bearing and the bearing housing and configured to keep the shaft centered with respect to the bearing housing with the second spring having a V-shaped cross section when viewed in a circumferential direction with the bottom of the V being adjacent to the squeeze film damper.
14. The gas turbine engine of claim 13 , wherein the first spring and the second spring are each entirely between the bearing and the bearing housing.
15. The gas turbine engine of claim 12 , further comprising:
a first retaining ring adjacent a radially outer end of the first spring; and
a second retaining ring adjacent a radially inner end of the first spring,
wherein the first retaining ring and the second retaining ring are configured to prevent axial movement of the first spring.