Integral centering spring and bearing support and method of supporting multiple damped bearings

• US 9,702,404 B2
• Filed: 10/28/2015
• Issued: 07/11/2017
• Est. Priority Date: 10/28/2015
• Status: Active Grant

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Smedresman, Adam G., Von Berg, Kaleb
• Primary Examiner(s): Pilkington, James
• Application Number:
  US14/925,150
• Publication Number:
  US 20170122369A1
• Time in Patent Office: 622 Days
• CPC Class Codes: F16C 19/28 with two or more rows of rollers
• CPC Class Codes: F16C 23/08 self-adjusting
• CPC Class Codes: F16C 2360/23 Gas turbine engines in general F02C
• CPC Class Codes: F16C 27/04 Ball or roller bearings, e.g. with resilient rolling bodies
• CPC Class Codes: F16C 27/045 with a fluid film, e.g. squeeze film damping
• CPC Class Codes: F16C 37/007 of rolling bearings

Abstract

An assembly includes a centering spring having an annular flange, an annular body, and a plurality of resilient beams extending from the flange to the body. The annular flange defines a passage that extends at least radially inward with respect to a centerline circumscribed by the flange from a radially outer surface of the flange to a radially inner surface of the flange. The annular body is spaced from the flange along the centerline, a radially outer surface of the body forming a first annular cavity relative to an adjacent surface configured to be a first fluid damper. A deflection of the body relative to the flange is restrained by a restoring force produced by the plurality of resilient beams and the first fluid damper. A method includes providing the aforementioned assembly and passing a damping fluid through the passage of the flange.

Claims

1. An assembly comprising:

a centering spring comprising;

an annular flange defining a passage that extends at least radially inward with respect to a centerline circumscribed by the flange;

an annular body spaced from the flange along the centerline, wherein a radially outer surface of the body is spaced from an adjacent surface to form a first annular cavity operative as a first fluid damper; and

a resilient member extending from the flange to the body, wherein a deflection of the body relative to the flange is restrained by a restoring force of the resilient member and the first fluid damper;

wherein the passage extends from a radially outer surface of the flange to a radially inner surface of the flange.

2. The assembly of claim 1 and further comprising:

a housing at least partially surrounding the flange, the body, and the resilient member, wherein the housing includes the adjacent surface.

3. The assembly of claim 2 and further comprising:

a first bearing that is spaced from the radially inner surface of the flange to form a second annular cavity, wherein the second annular cavity is operative as a second fluid damper, and wherein the passage communicates between the second annular cavity and the radially outer surface of the flange; and

a second bearing that mates with a radially inner surface of the body.

4. The assembly of claim 3, wherein the body defines a plurality of circumferentially-spaced holes extending in a substantially axial direction through the body between the radially outer surface of the body and the second bearing.

5. The assembly of claim 3, wherein the passage includes a groove defined by the flange that extends circumferentially along the radially outer surface of the flange.

6. The assembly of claim 2 and further comprising:

a fastening element; and

an axially-rearward-facing surface of the flange configured to mate with an axially-forward-facing surface of the housing, wherein the fastening element and the axially-forward-facing surface of the housing axially restrain the centering spring relative to the housing.

7. The assembly of claim 6, wherein the fastening element is one of a retaining nut mating with an axially-forward-facing surface of the flange and a plurality of fasteners circumferentially-spaced along and extending through the flange.

8. The assembly of claim 1 and further comprising:

a seal carrier mated to the radially inner surface of the flange, wherein the seal carrier supports one or more sealing elements that interface with one or more seal runners;

a first bearing spaced from a radially inner surface of the seal carrier to form a second annular cavity, the second annular cavity operative as a second fluid damper;

a second bearing that mates with the radially inner surface of the body; and

a housing at least partially surrounding the flange, the body, and the plurality of beam, wherein the housing includes the adjacent surface.

9. The assembly of claim 1, the resilient member comprising:

a plurality of beams extending from the flange to the body, wherein a deflection of the body relative to the flange is restrained by a restoring force of the plurality of beams and the first fluid damper.

10. The assembly of claim 9, wherein each of the plurality of beams have a plurality of cross-sections, the cross-sections varying along a length between the flange and the body.

11. The assembly of claim 10, wherein the cross-sections of each beam are polygonal, circular, or oval-shaped.

12. The assembly of claim 10, wherein a minimum cross-section of each beam is disposed at a midpoint between the flange and the body.

13. An assembly for supporting a bearing assembly within a bearing compartment of a gas turbine engine, the assembly comprising:

a centering spring comprising;

a first bearing housing circumscribing a rotor centerline of the gas turbine engine;

a passage defined by the first bearing housing that extends from a radially outer surface of the first bearing housing to a radially inner surface of the first bearing housing;

a second bearing housing spaced from the first bearing housing along the rotor centerline; and

a plurality of resilient members extending from the first bearing housing to the second bearing housing;

a support structure encircling the centering spring, the support structure defining an axially-facing surface configured to engage the first bearing housing;

a first bearing supported by the first bearing housing;

a first damping cavity defined by opposing surfaces of the first bearing housing and the first bearing, wherein the passage is configured to communicate with the first damping cavity; and

a second damping cavity defined by opposing surfaces of the second bearing housing and the support structure;

wherein a deflection of the second bearing housing relative to the first bearing housing is restrained by a restoring force of the plurality of resilient members and the second damping cavity.

14. The assembly of claim 13, wherein the support structure defines a first supply passage and a second supply passage, the first supply passage extending radially through the support structure to communicate with the passage of the first bearing housing and the second supply passage extending radially through the support structure to communicate with the second damping cavity.

15. The assembly of claim 13 and further comprising:

a first piston seal; and

a second piston seal spaced along an outer race of the first bearing, wherein the first and second piston seals engage grooves within the outer race of the first bearing to seal axial ends of the first damping cavity.

16. The assembly of claim 13, wherein each of the plurality of resilient members have a plurality of cross-sections, the cross-sections varying along a length between the first bearing housing and the second bearing housing.

17. A method of supporting a first bearing and a second bearing, the method comprising:

providing a centering spring, the centering spring comprising;

a first bearing housing mated to and restrained by a support structure for engaging the first bearing;

a second bearing housing spaced from the first bearing housing for engaging the second bearing; and

a plurality of resilient beams extending from the first bearing housing to the second bearing housing; and

passing a fluid through a passage defined by the first bearing housing to a first annular cavity defined between a radially inner surface of the first bearing housing and an outer race of a first bearing, wherein the first annular cavity is operative as a first fluid damper.

18. The method of claim 17 and further comprising:

passing the fluid through the support structure to a second annular cavity defined between the support structure and a radially outer surface of the second bearing housing, wherein the second annular cavity is operative as a second fluid damper.

19. The method of claim 18, wherein providing the centering spring includes configuring the plurality of beams such that a deflection of the second bearing housing relative to the first bearing housing is restrained by a restoring force of the plurality of beams and the second fluid damper.

20. The method of claim 17 and further comprising:

mating the second bearing to a radially inner surface of the second bearing housing.