THRUST BEARING CAGE WITH PILOTING FLANGE

Abstract

A thrust bearing cage includes a piloting feature to radially locate a thrust bearing with respect to one of the shafts. Specifically, the bearing cage includes an axial extension at an outer diameter that extends beyond the rollers and around an outer diameter of end of the shaft. This feature permits elimination of a washer.

Claims

1. A bearing comprising: a cage; and a plurality of rollers retained by the cage; wherein the cage includes a piloting lip extending axially beyond the rollers.

2. The bearing of claim wherein the piloting lip defines at least one hole to permit flow of lubricant.

3. The bearing of claim wherein the piloting lip extends around a full circumference of the cage.

4. The bearing of claim wherein the piloting lip is located at an outer diameter of the cage.

5. The bearing of claim wherein the piloting lip is located at an inner diameter of the cage.

6. The bearing of claim wherein the rollers are cylindrical.

7. An assembly, comprising: a first shaft having a first axial end; a second shaft having a second axial end; a cage including a piloting lip extending axially beyond the first axial end; and a plurality of rollers retained by the cage and bearing against the first axial end and the second axial end.

8. The assembly of claim 7, wherein the piloting lip defines at least one hole to permit flow of lubricant.

9. The assembly of claim 7, wherein the piloting lip is located at an outer diameter of the cage and extends beyond an outer diameter of the first end.

10. The assembly of claim 7, wherein the rollers are cylindrical.

11. The assembly of claim 7, wherein the rollers bear directly against the first end.

12. The assembly of claim 11, wherein the rollers bear directly against the second end.

13. A raceless axial bearing configured to be positioned between axial ends of first and second shafts, comprising: a cage including a plurality of pockets and an axially extending lip; a plurality of rollers retained in the pockets; and wherein the piloting lip extends axially beyond the rollers such that the bearing is self-piloting on a shaft end of one of the shafts and the rollers are adapted to directly contact the axial ends of the first and second shafts.

14. The bearing of claim 13, wherein the piloting lip defines at least one hole to permit flow of lubricant.

15. The bearing of claim 13, wherein the piloting lip extends around a full circumference of the cage.

16. The bearing of claim 13, wherein the piloting lip is located at an outer diameter of the cage.

17. The bearing of claim 13, wherein the piloting lip is located at an inner diameter of the cage.

18. The bearing of claim 13, wherein the rollers are cylindrical.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0007] FIG. 1 is a pictorial view of a prior art axial roller bearing.

[0008] FIG. 2 is a cross-sectional view of a washerless prior art axial roller bearing.

[0009] FIG. 3 is a cross-sectional view of the bearing of FIG. 2 in an installed condition.

[0010] FIG. 4 is a cross-sectional view of a prior art roller bearing having a washer.

[0011] FIG. 5 is a cross-sectional view of the bearing of FIG. 5 in an installed condition.

[0012] FIG. 6 is a pictorial view of a washerless axial roller bearing.

[0013] FIG. 7 is a cross-sectional view of the bearing of FIG. 6.

[0014] FIG. 8 is a cross-sectional view of the bearing of FIG. 6 in an installed condition.

DETAILED DESCRIPTION

[0015] Embodiments of the present disclosure are described herein. It should be appreciated that like drawing numbers appearing in different drawing views identify identical, or functionally similar, structural elements. Also, it is to be understood that the disclosed embodiments are merely examples and other embodiments can take various and alternative forms. The figures are not necessarily to scale; some features could be exaggerated or minimized to show details of particular components. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a representative basis for teaching one skilled in the art to variously employ the embodiments. As those of ordinary skill in the art will understand, various features illustrated and described with reference to any one of the figures can be combined with features illustrated in one or more other figures to produce embodiments that are not explicitly illustrated or described. The combinations of features illustrated provide representative embodiments for typical applications. Various combinations and modifications of the features consistent with the teachings of this disclosure, however, could be desired for particular applications or implementations.

[0016] The terminology used herein is for the purpose of describing particular aspects only, and is not intended to limit the scope of the present disclosure. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood to one of ordinary skill in the art to which this disclosure belongs. Although any methods, devices or materials similar or equivalent to those described herein can be used in the practice or testing of the disclosure, the following example methods, devices, and materials are now described.

[0017] FIGS. 6 and 7 illustrate an improved thrust bearing cage 10′ and rollers 12. FIG. 6 is a pictorial view, whereas FIG. 7 is a cross sectional view. Cage 10′ includes an axial extension 26. In the embodiment illustrated, the axial extension is at an outer edge. A number of holes 28 may be included in the axial extension.

[0018] FIG. 8 illustrates how the cage and rollers of FIGS. 6 and 7 may be utilized between two coaxial shafts 14 and 16′. Although hollow shafts are illustrated, one or both shafts may be solid. The rollers 12 axially separate end faces of shafts 14 and 16′ and transmit axial forces between the shafts. The end faces may include hardened races for the rollers. In this application, radial positioning of the cage 10′ is accomplished by the axial extension 26 and an outer surface of one of the two shafts. The optional holes 28 provide a path for lubricating fluid to exit the bearing. In an alternative embodiment, the axial extension may be at an inner edge of the cage and may interface with an inner surface of a hollow shaft.

[0019] Unlike the bearing of FIGS. 1-3, neither shaft needs a piloting feature. The shafts may be identical to one another, reducing the number of distinct parts in an assembly. The assembly of FIGS. 6-8 has fewer parts that the assembly of FIGS. 4-5, reducing cost. Furthermore, it is more robust in the presence of impact thrust loads.

[0020] While exemplary embodiments are described above, it is not intended that these embodiments describe all possible forms encompassed by the claims. The words used in the specification are words of description rather than limitation, and it is understood that various changes can be made without departing from the spirit and scope of the disclosure. As previously described, the features of various embodiments can be combined to form further embodiments of the disclosure that may not be explicitly described or illustrated. While various embodiments could have been described as providing advantages or being preferred over other embodiments or prior art implementations with respect to one or more desired characteristics, those of ordinary skill in the art recognize that one or more features or characteristics can be compromised to achieve desired overall system attributes, which depend on the specific application and implementation. As such, to the extent any embodiments are described as less desirable than other embodiments or prior art implementations with respect to one or more characteristics, these embodiments are not outside the scope of the disclosure and can be desirable for particular applications.