Bearing centering spring and damper
A machine has first and second members. A bearing has an inner race mounted to the second member and an outer race rotatable relative to the inner race about an axis. A ring holds the outer race. A radial spring extends radially between the ring and the first member. First and second damper rings extending radially between the ring and the first member at first and second axial sides of the radial spring. First and second damping chambers are radially between an outer diameter surface portion of the respective damper rings and an inner diameter surface portion of the first member.
1. A machine comprising:
a first member;
a second member;
a bearing having an inner race mounted to the second member and an outer race rotatable relative to the inner race about an axis;
a ring holding the outer race;
a radial spring extending radially between the ring and the first member;
a first damper ring extending radially between the ring and the first member at a first axial side of the radial spring;
a first damping chamber radially between an outer diameter surface portion of the first damper ring and an inner diameter surface portion of the first member;
a second damper ring extending radially between the ring and the first member at a second axial side of the radial spring; and
a second damping chamber radially between an outer diameter surface portion of the second damper ring and an inner diameter surface portion of the first member.
2. The machine of claim 1 wherein the radial spring comprises:
an inner diameter band;
an outer diameter band; and
a compliant portion between the inner diameter band and the outer diameter band.
3. The machine of claim 2 wherein in transverse cross-section, the compliant portion has an open area fraction of at least 75%.
4. The machine of claim 2 wherein the outer diameter band has an outer diameter surface having channels providing fluid communication between the first damping chamber and the second damping chamber.
5. The machine of claim 1 further comprising:
one or more fluid passages through the first member in communication with the first damping chamber and the second damping chamber.
6. The machine of claim 1 further comprising:
a first seal between the first damper ring and the first member; and
a second seal between the second damper ring and the first member.
7. The machine of claim 6 wherein:
the first seal is in an outer diameter groove in the first damper ring; and
the second seal is in an outer diameter groove in the second damper ring.
8. The machine of claim 6 wherein:
the first seal is a metallic ring; and
the second seal is a metallic ring.
9. The machine of claim 6 further comprising:
a third seal between the first damper ring and the radial spring; and
a fourth seal between the second damper ring and the radial spring.
10. The machine of claim 1 wherein the ring holds the first damper ring, the radial spring, and the second damper ring under axial compression.
11. The machine of claim 1 wherein the radial spring comprises a sintered titanium alloy.
12. The machine of claim 1 being a gas turbine engine.
13. A method for using the machine of claim 1 , the method comprising:
driving relative rotation of the first member and second member; and
introducing a liquid to the first damping chamber and the second damping chamber, the chambers accommodating radial vibration and the liquid in the chambers damping the radial vibration.
14. A machine comprising:
a first member;
a second member;
a bearing having an inner race mounted to the second member and an outer race rotatable relative to the inner race about an axis;
between the first member and the bearing outer race:
a radial spring;
a first damper ring at a first axial side of the radial spring, a first damping chamber radially between an outer diameter surface portion of the first damper ring and an inner diameter surface portion of the first member; and
a second damper ring at a second axial side of the radial spring, a second damping chamber radially between an outer diameter surface portion of the second damper ring and an inner diameter surface portion of the first member.
15. The machine of claim 14 wherein the radial spring comprises a sintered titanium alloy.
16. The machine of claim 14 further comprising:
one or more fluid passages through the first member in communication with the first damping chamber and the second damping chamber.