IP Library › Granted Patent US 10,655,499
Granted Patent B2
US 10,655,499 · App. 15/850,912 · Granted May 19, 2020

Flexible preloaded ball bearing assembly

Inventors: Kevin Duffy (Hartford, CT); Ronnie K. Kovacik (Manchester, CT); Michael Gantt (Granby, CT)
Assignee: UNITED TECHNOLOGIES CORPORATION
F01D25/164F02C7/06F16C19/16F16C19/525F16C19/54F16C25/08F16C25/083F16C27/08F16C35/04F05D2240/54F16C19/546F16C19/55F16C27/066F16C2360/23
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Quick Facts
Patent No.
US 10,655,499
App. No.
15/850,912
Granted
May 19, 2020
Kind
B2
Abstract

A preloaded ball bearing assembly includes a primary bearing assembly disposed between a rotating component and a static structure. The assembly also includes a preload bearing assembly disposed in contact with the rotating component. The assembly further includes a flexible support disposed between the primary bearing assembly and the preload bearing assembly.

Claims (39)

1. A preloaded ball bearing assembly comprising:

a shaft;

a static structure;

a primary bearing assembly disposed between the shaft and the static structure;

a preload bearing assembly disposed in contact with the shaft; and

a flexible support formed with the preload bearing assembly as a unitary element and disposed between the primary bearing assembly and the preload bearing assembly.

2. The preloaded ball bearing assembly of claim 1 , further comprising a flange extending from the static structure and in contact with the primary bearing assembly to axially position the primary bearing assembly.

3. The preloaded ball bearing assembly of claim 2 , wherein the flexible support is in contact with the preload bearing assembly.

4. The preloaded ball bearing assembly of claim 2 , wherein the primary bearing assembly comprises a primary ball bearing, a primary bearing outer ring, and a primary bearing inner ring, the primary bearing inner ring in contact with the shaft, the primary bearing outer ring in contact with the static structure and the flange.

5. The preloaded ball bearing assembly of claim 1 , wherein the preload bearing assembly comprises a preload ball bearing, a preload bearing outer ring, and a preload bearing inner ring, the preload bearing inner ring in contact with the shaft, the preload bearing outer ring in contact with the flexible support.

6. The preloaded ball bearing assembly of claim 5 , wherein the preload bearing outer ring and the static structure define a radial clearance therebetween, the flexible support disposed within the radial clearance.

7. The preloaded ball bearing assembly of claim 1 , wherein the flexible support comprises at least a portion of a wave segment.

8. The preloaded ball bearing assembly of claim 1 , wherein the flexible support comprises a plurality of wave segments forming a sinusoidal wave.

9. The preloaded ball bearing assembly of claim 8 , wherein each of the plurality of wave segments are U-shaped.

10. The preloaded ball bearing assembly of claim 2 , wherein the flexible support comprises at least one spiral ring extending between the preload bearing assembly and the primary bearing assembly.

11. The preloaded ball bearing assembly of claim 1 , wherein the flexible support comprises a solid beam extending between the preload bearing assembly and the primary bearing assembly.

12. A gas turbine engine comprising:

a compressor section;

a combustion section;

a turbine section;

a shaft extending axially along a longitudinal centerline of the gas turbine engine; and

a preloaded ball bearing assembly comprising:

a primary bearing assembly disposed between, and in contact with, the shaft and a static structure;

a flange extending from the static structure to axially position the primary bearing assembly;

a preload bearing assembly disposed in contact with the shaft; and

a flexible support formed with the preload bearing assembly as a unitary element and disposed between, and in contact with, the flange and the preload bearing assembly to axially position the preload bearing assembly.

13. The gas turbine engine of claim 12 , wherein the flexible support is integrally formed with the preload bearing assembly.

14. The gas turbine engine of claim 13 , wherein the primary bearing assembly comprises a primary ball bearing, a primary bearing outer ring, and a primary bearing inner ring, the primary bearing inner ring in contact with the shaft, the primary bearing outer ring in contact with the static structure and the flange.

15. The gas turbine engine of claim 12 , wherein the preload bearing assembly comprises a preload ball bearing, a preload bearing outer ring, and a preload bearing inner ring, the preload bearing inner ring in contact with the shaft, the preload bearing outer ring in contact with the flexible support.

16. The gas turbine engine of claim 15 , wherein the preload bearing outer ring and the static structure define a radial clearance therebetween, the flexible support disposed within the radial clearance.

17. The gas turbine engine of claim 12 , wherein the flexible support comprises at least a portion of a wave segment.

18. The gas turbine engine of claim 13 , wherein the flexible support comprises at least one spiral ring extending between the preload bearing assembly and the primary bearing assembly.

19. The gas turbine engine of claim 12 , wherein the flexible support comprises at least one solid beam extending between the preload bearing assembly and the primary bearing assembly.

20. A preloaded ball bearing assembly comprising:

a shaft;

a static structure;

a primary bearing assembly disposed between the shaft and the static structure;

a preload bearing assembly disposed in contact with the shaft, the preload bearing assembly comprises a preload ball bearing, a preload bearing outer ring, and a preload bearing inner ring, the preload bearing inner ring in contact with the shaft; and

a flexible support disposed between the primary bearing assembly and the preload bearing assembly, wherein the preload bearing outer ring and the static structure define a radial clearance therebetween, a portion of the flexible support having a wave segment disposed within the radial clearance.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2018
From: DUFFY, KEVIN; KOVACIK, RONNIE K.; GANTT, MICHAEL
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 044762/0723 →
Continuity (1)
Related Publication 20190195088A1 · Jun 27, 2019
Cited By (1)
US 12,352,208