Series bearing support apparatus for a gas turbine engine

• US 8,727,629 B2
• Filed: 11/01/2011
• Issued: 05/20/2014
• Est. Priority Date: 11/01/2011
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Do, Kevin Michael, Seppala, Benjamin Johannes, Kerry, David Garry
• Primary Examiner(s): Charles, Marcus
• Application Number:
  US13/286,792
• Publication Number:
  US 20130108440A1
• Time in Patent Office: 931 Days
• Field of Search: 384/99, 384/494, 384/504, 384/507, 384/548, 384/563, 384/565, 384/597, 384/613, 384618-618, 384/535, 384/609, 384/903, 415/129, 415/229, 415/179, 415/170.1, 417/407
• US Class Current: 384/494
• CPC Class Codes: F01D 25/164 Flexible supports; Vibration damping means associated with the bearing
• CPC Class Codes: F16C 19/54 Systems consisting of a plurality of bearings with rolling friction spindle bearings F16C35/08
• CPC Class Codes: F16C 19/545 Systems comprising at least one rolling bearing for radial load in combination with at least one rolling bearing for axial load
• 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

Abstract

A bearing support apparatus for a gas turbine engine, including: a first annular member; a second annular member disposed within the first annular member; first and second axially spaced-apart rolling-element bearings disposed between the first and second annular members so as to enable relative rotation of the first and second members; a first spring element mounting the first bearing to the first member; and a second spring element mounting the second bearing to the first member through the first spring element, such that the first and second bearings are physically supported in series relative to the first member.

Claims

1. A bearing support apparatus for a gas turbine engine, comprising:

a first annular member;

a second annular member disposed within the first annular member;

first and second axially spaced-apart rolling-element bearings disposed between the first and second annular members so as to enable relative rotation of the first and second members;

a first spring support connecting the first bearing to the first member; and

a second spring support connecting the second bearing to the first member through the first spring support, such that the first and second bearings are physically supported in series relative to the first member.

2. The bearing support apparatus of claim 1 wherein the first bearing is a roller bearing.

3. The bearing support apparatus of claim 1 wherein the second bearing is a ball bearing.

4. The bearing support apparatus of claim 1 wherein the first bearing is laterally offset relative to the second bearing.

5. The bearing support apparatus of claim 1 wherein the second bearing is configured to transmit axial loads between the first and second members.

6. The bearing support apparatus of claim 1 wherein the first spring support comprises annular forward and aft rings interconnected by annular array of axially-extending spring fingers.

7. The bearing support apparatus of claim 1 wherein the second spring support comprises annular forward and aft rings interconnected by annular array of axially-extending spring fingers.

8. The bearing support apparatus of claim 1 wherein the first and second spring supports are arranged in an axially overlapping relationship.

9. The bearing support apparatus of claim 1 wherein the first and second spring elements are integral portions of a single member having annular forward, middle, and aft rings, the forward and middle rings being interconnected by annular array of axially-extending forward spring fingers and the middle and aft rings being interconnected by annular array of axially-extending aft spring fingers.

10. The bearing support apparatus of claim 1 further including a squeeze film damper disposed between the first member and one of the spring supports.

11. The bearing support apparatus of claim 1 wherein the first spring support has a first radial stiffness, and the second spring support has a second radial stiffness which is substantially less than the first radial stiffness.

12. The bearing support apparatus of claim 1 wherein the first and second spring supports are separate members which are mechanically coupled together.

13. The bearing support apparatus of claim 12 wherein the second member is a shaft mounted for rotation in the frame.

14. The bearing support apparatus of claim 1 wherein the first member is a stationary frame.

15. A bearing apparatus for a gas turbine engine, comprising:

a stationary, annular frame;

a first spring support comprising annular forward and aft rings interconnected by an annular array of axially-extending first spring fingers, wherein the forward ring is mounted to the frame;

a second spring support comprising annular forward and aft rings interconnected by an annular array of axially-extending second spring fingers, the aft ring mounted to the aft ring of the first spring support;

a roller bearing carried by the aft ring of the second spring support;

a ball bearing carried by the forward ring of the second spring support; and

a shaft mounted in the roller and ball bearings.

16. The bearing apparatus of claim 15 wherein the ball bearing is configured to transmit axial loads between the frame and the shaft.

17. The bearing apparatus of claim 15 wherein the first and second spring supports are arranged in an axially overlapping relationship.

18. The bearing support apparatus of claim 15 wherein the ball bearing is laterally offset relative to the roller bearing.

19. The bearing apparatus of claim 15 further including a squeeze film damper disposed between the frame and the first spring support.

20. The bearing apparatus of claim 15 wherein the first spring support has a first radial stiffness, and the second spring support has a second radial stiffness which is substantially less than the first radial stiffness.