Bearing cage deflector

• US 9,194,429 B2
• Filed: 07/16/2014
• Issued: 11/24/2015
• Est. Priority Date: 08/06/2013
• Status: Active Grant

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Ashmore, Daren Richard, Plant, James Alan, Opacic, Steven
• Primary Examiner(s): Charles, Marcus
• Application Number:
  US14/332,639
• Publication Number:
  US 20150043861A1
• Time in Patent Office: 496 Days
• Field of Search: 384/99, 384/462, 384465-466, 384470-474, 384/490, 384/506, 384/523, 384/572, 384/601, 384/607, 384621-623, 384/586
• US Class Current: 1/1
• CPC Class Codes: F16C 19/26 with a single row of rollers
• CPC Class Codes: F16C 2360/23 Gas turbine engines in general F02C
• CPC Class Codes: F16C 33/38 Ball cages
• CPC Class Codes: F16C 33/385 made from metal, e.g. cast or machined window cages
• CPC Class Codes: F16C 33/46 Cages for rollers or needles
• CPC Class Codes: F16C 33/4629 made from metal, e.g. cast or machined window cages
• CPC Class Codes: F16C 33/6681 Details of distribution or circulation inside the bearing, e.g. grooves on the cage or passages in the rolling elements
• CPC Class Codes: F16C 33/7823 of sealing lips
• CPC Class Codes: F16C 33/7893 mounted to a cage or integral therewith

Abstract

A bearing cage for a rolling element bearing assembly, the bearing cage including a cage body having an inner surface defining a bore coaxially aligned with the principal rotational axis of the bearing cage; a plurality of pockets, each pocket being suitable for housing a rolling element of the rolling element bearing assembly, the pockets being arranged sequentially around the cage body with respect to the principal rotational axis of the bearing cage; and a skirt projecting from the cage body in the axial direction; characterized by a flow deflector projecting from the skirt in the radial direction.

Claims

1. An annular bearing arrangement configured for providing free rotation between two coaxially aligned bodies between which the bearing arrangement is coaxially aligned, the bearing arrangement including:

a bearing chamber having a gas inlet and a lubricant inlet and arranged to house a rolling element bearing assembly,

the rolling element bearing assembly including a bearing cage having

a cage body close to or in axial alignment with the gas inlet and having an inner surface defining a bore coaxially aligned with the principal rotational axis of the bearing cage,

a plurality of pockets, each pocket housing a rotatable rolling element of the rolling element bearing assembly, the pockets being arranged sequentially around the cage body with respect to the principal rotational axis of the bearing cage, and

a skirt projecting from the cage body in the axial direction and past the lubricant inlet,

wherein;

the bearing cage includes a flow deflector projecting from the skirt in the radial direction at an axial position which is between the lubricant inlet and the gas inlet and which is arranged to intercept gas flow entering by the gas inlet so as to deflect the gas flow away from the cage body.

2. The bearing arrangement according to claim 1, wherein the flow deflector is arranged to block the direct line of sight between the source and the cage body.

3. The bearing arrangement according to claim 1, wherein the source of gas flow is a seal provided to seal the bearing chamber.

4. The bearing arrangement according to claim 3, wherein the seal is configured to permit gas to flow into the bearing chamber when the gas pressure on the external side of the seal exceeds the gas pressure inside the bearing chamber by a predetermined amount.

5. The bearing arrangement according to claim 1, further including an additional skirt projecting from the cage body in an opposite axial direction to the skirt, a respective flow deflector projecting from each skirt in the radial direction.

6. The bearing arrangement according to claim 5, wherein the each flow deflector projects radially outwardly from the principal rotational axis of the bearing cage.

7. The bearing arrangement according to claim 1, wherein the flow deflector includes an outwardly facing deflector face, the deflector face being shaped, along its extent of projection in the radial direction, to extend in the axial direction towards the cage body.

8. The bearing arrangement according to claim 7, wherein the deflector face, along its extent of projection in the radial direction, is formed to include one or more compound angles.

9. The bearing arrangement according to claim 7, wherein the deflector face is curved along at least a portion of its extent of projection in the radial direction.

10. The bearing arrangement according to claim 7, wherein the deflector face is curved along at least a portion of its extent of projection in the radial direction, such that the closest region of the deflector face to the cage body is formed in an intermediate region along the extent of projection in the radial direction of the deflector face.

11. The bearing arrangement according to claim 1, wherein the skirt extends circumferentially entirely around the principal rotational axis of the bearing cage.

12. The bearing arrangement according to claim 1, wherein the flow deflector extends circumferentially entirely around a respective skirt.

13. The bearing arrangement according to claim 1, wherein the bearing chamber includes a chamber exit, and the flow deflector is arranged to deflect the gas flow towards the chamber exit.

14. The bearing arrangement according to claim 13, wherein the chamber exit is located radially outwards of the flow deflector with respect to the principal axis of rotation of the bearing cage.