Retainer

Abstract

A retainer (30) for maintaining a relative angular spacing of a plurality of rolling elements includes a body (34) having an annular portion (38) and a plurality of engaging portions (42). Each of the engaging portions is configured to engage at least one of the plurality of rolling elements. The body is made of a sintered powdered metal infiltrated with bronze.

Claims

1. A retainer for maintaining a relative angular spacing of a plurality of rolling elements, the retainer comprising: a body including an annular portion and a plurality of engaging portions, each of the engaging portions configured to engage at least one of the plurality of rolling elements, wherein the body is made of a sintered powdered metal infiltrated with bronze such that the infiltrated retainer has a porosity less than or equal to 30%.

2. The retainer of claim 1, wherein the engaging portions are finished by machining.

3. The retainer of claim 1, wherein the engaging portions are finished by mass finishing.

4. The retainer of claim 1, wherein the body is made of stainless steel infiltrated with bronze.

5. The retainer of claim 4, wherein the body is made of 316 or 420 stainless steel infiltrated with bronze.

6. The retainer of claim 1, wherein the body is made of mild steel or low carbon steel infiltrated with bronze, the mild steel having a carbon content between about 0.3% and about 0.6% and the low carbon steel having a carbon content of about 0.3% or less.

7. The retainer of claim 1, wherein the body is made of iron infiltrated with bronze.

8. The retainer of claim 1, wherein at least one of the engaging portions includes a dimple for retaining lubricant between the at least one engaging member and one of the rolling elements.

9. The retainer of claim 1, wherein the annular portion includes at least one hollow section.

10. The retainer of claim 1, wherein at least one of the engaging portions includes a recessed portion for reducing a contact area between the at least one engaging portion and one of the rolling elements.

11. The retainer of claim 1, wherein the annular portion includes at least one recess for reducing the weight of the annular portion.

12. A bearing assembly comprising: an inner raceway; an outer raceway; a plurality of rolling elements disposed between the inner raceway and the outer raceway; and a retainer for maintaining a relative angular spacing of the rolling elements, wherein the retainer is made of a sintered powdered metal infiltrated with bronze such that the infiltrated retainer has a porosity less than or equal to 30%.

13. A method of manufacturing a retainer for maintaining a relative angular spacing of a plurality of rolling elements, the method comprising: forming a body of the retainer from powdered metal using an additive manufacturing process; and infiltrating the body of the retainer with bronze such that the infiltrated retainer has a porosity less than or equal to 30%.

14. The method of claim 13, wherein infiltrating the body of the retainer with bronze increases the density and reduces the porosity of the body.

15. The method of claim 13, wherein infiltrating the body of the retainer with bronze improves tribological characteristics of the retainer.

16. The method of claim 13, wherein forming the body includes sequentially forming a plurality of layers of powdered metal and binding the plurality of layers with an adhesive.

17. The method of claim 13, wherein the additive manufacturing process is a 3D printing process.

18. The method of claim 13, wherein forming the body of the retainer includes forming an annular portion and a plurality of engaging portions, each of the engaging portions configured to engage at least one of the rolling elements.

19. The method of claim 18, further comprising finishing the engaging portions using a machining process.

20. The method of claim 18, further comprising finishing the engaging portions using a mass finishing process.

21. The method of claim 18, wherein forming the body includes forming a dimple in at least one of the engaging portions for retaining lubricant between the at least one engaging portion and one of the rolling elements.

22. The method of claim 18, wherein the annular portion includes at least one hollow section.

23. The method of claim 18, wherein at least one of the engaging portions includes a recessed portion for reducing a contact area between the at least one engaging portion and one of the rolling elements.

24. The method of claim 18, wherein the annular portion includes at least one recess for reducing the weight of the annular portion.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a cutaway view of a typical ball bearing including a retainer that can be manufactured by a method in accordance with the invention.

(2) FIG. 2 is a perspective view of a typical tapered roller bearing including a retainer that can be manufactured by a method in accordance with the invention.

(3) FIG. 3 is a cutaway view of a typical cylindrical roller bearing including a retainer that can be manufactured by a method in accordance with the invention.

(4) FIG. 4 is a cutaway view of a typical spherical roller bearing including a retainer that can be manufactured by a method in accordance with the invention.

(5) FIG. 5 is an exploded view of a typical constant velocity joint including a retainer that can be manufactured by a method in accordance with the invention.

(6) FIG. 6 is a perspective view of a retainer in accordance with an embodiment of the invention.

(7) FIG. 7 is a perspective view of a retainer in accordance with another embodiment of the invention.

(8) FIG. 8 is a perspective view of a portion of a retainer in accordance with another embodiment of the invention.

(9) FIG. 9 is a perspective view of a portion of a retainer in accordance with another embodiment of the invention.

(10) Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting.

DETAILED DESCRIPTION

(11) FIGS. 1-5 illustrate a variety of exemplary antifriction hearings 10, each of which includes an inner raceway 14, an outer raceway 18 (not shown in FIG. 2), a plurality of rolling elements 22 arranged and positioned between the raceways 14, 18, and a retainer 26. The retainer 26 maintains separation of the rolling elements 22 and guides the rolling elements 22 for uniform rotation with respect to the inner and outer raceways 14, 18.

(12) FIG. 6 illustrates a retainer or cage 30 according to an embodiment of the invention. The retainer 30 of FIG. 6 may be assembled, for example, as pail of a double-row spherical roller bearing. The retainer 30 includes a body 34 having an annular portion 38 and a plurality of engaging portions 42 extending axially from the annular portion 38. Adjacent engaging portions 42 define pockets 46 that can receive a complement of rolling elements (not shown).

(13) FIG. 7 illustrates a retainer 30a according to another embodiment of the invention. The retainer 30a is similar to the retainer 30 of FIG. 6, and like components are given like reference numerals with the letter a. The retainer 30a of FIG. 7 may be assembled, for example, as part of a spherical or cylindrical roller bearing. The retainer 30a includes a body 34a having two, axially-spaced rings 50, 54 interconnected by a plurality of engaging portions 42a. Adjacent engaging portions 42a define pockets 46a that can receive a complement of rolling elements (not shown).

(14) A method of manufacturing any of the retainers 26, 30, 30a illustrated in FIGS. 1-7, as well as other retainers not illustrated or described herein, in accordance with the invention is described below.

(15) The body 34, 34a of the retainer 30, 30a is formed from powdered metal by an additive manufacturing process, and more specifically by a three-dimensional (3D) printing process. Unlike subtractive manufacturing processes (e.g., machining) that remove material in order to form a finished part, additive manufacturing processes progressively add material to form a finished part.

(16) To produce the retainer 30, 30a, a slicing algorithm first divides a 3D computer or CAD model of the retainer 30, 30a into numerous thin slices or layers along a central axis of the retainer 30, 30a. layer data from the slicing, algorithm is then sent to and interpreted by a 3D printing apparatus (not shown) which, as described in further detail below, can sequentially construct the retainer 30, 30a layer by layer to produce a complete part.

(17) The 3D printing apparatus can include a powder bed, a spreader, and a printing head. It should be understood that the 3D printing apparatus can be configured in any manner and can include any number and variety of other components and features. Each layer of the retainer 30, 30a begins with a thin distribution of powdered metal spread over a surface of the powder bed by the spreader. In some embodiments the powdered metal can be iron. In other embodiments, the powdered metal can be mild or low carbon steels. Mild steels have a carbon content between about 0.3% and about 0.6%, while low carbon steels have a carbon content of about 0.3% or less. In still other embodiments, the powdered metal can be mild steel having a carbon content of about 0.15% or less. In yet other embodiments, the powdered metal can be stainless steel, such as 316 stainless steel or 420 stainless steel. Alternatively, the powdered metal can be any other metal or metal alloy.

(18) The printing head then selectively joins particles of the powdered metal that make up a particular layer of the retainer 30, 30a. In some embodiments, the printing head dispenses a binder material or adhesive to join the powder particles. In other embodiments, the printing head includes a laser that melts or sinters targeted areas to join the powder particles. Once the powdered metal particles are joined to form a cohesive layer, the powder bed is lowered and the spreader applies the next powder layer on top of the partially-constructed retainer 30, 30a. This layer-by-layer process repeats until the retainer 30, 30a is completely formed within a surrounding area of unbound metal powder.

(19) Next, for embodiments where the powder particles are joined by binder or adhesive, the retainer 30, 30a can be heated to an elevated temperature for a predetermined time period in order to cure the binder or adhesive and strengthen the retainer 30, 30a. Once the retainer 30, 30a has cured, the surrounding unbound powder is removed from the retainer 30, 30a using vibration, vacuum, high velocity air, or any other suitable method. Alternatively, the surrounding unbound powder can be removed before the curing process.

(20) The retainer 30, 30a is then heated in a sintering process for additional strengthening. During sintering, the retainer 30, 30a is heated in a furnace and held at a temperature less than a melting temperature of the powdered metal for a predetermined time period (e.g., 12-36 hours). The sintering process can burn off any binder or adhesive, and accelerates molecular diffusion to bond the powdered metal together. In other embodiments, such as those where the powder particles are joined by laser sintering, the curing and/or sintering processes can be omitted.

(21) The sintered retainer 30, 30a is generally a porous structure having, a density between about 50% and about 70% of a theoretical density of the powdered metal material (i.e., the density of the metal in wrought form). Depending on the desired application, the retainer 30, 30a can be used as a finished part in this state, or may undergo additional machining, treatment, or polishing. In other embodiments, the porous retainer 30, 30a can be infiltrated with another material, such as a lower inciting temperature metal, to increase the density of the retainer 30, 30a and provide it with desirable properties. More specifically, it has been found that infiltration of the porous retainer 30, 30a with bronze or copper increases the density and strength, reduces porosity, and provides superior tribological characteristics (i.e., reduces wear and/or friction experienced by the retainer and/or rolling elements during operation).

(22) The infiltration process can constitute a separate heating process or can be performed concurrently or sequentially with the sintering process. A predetermined quantity of infiltrant (e.g., bronze powder) is deposited over the retainer 30, 30a, then heated to a temperature above the melting point of the infiltrant. Gravity, capillary action, and/or pressure draws the melted infiltrant into the porous retainer 30, 30a until the infiltrated retainer 30, 30a has a porosity less than or equal to about 30%. In some embodiments the infiltrated retainer 30, 30a has a porosity less than or equal to about 20%. In other embodiments the infiltrated retainer 30, 30a has a porosity less than or equal to about 10%. In still other embodiments, the infiltrated retainer 30, 30a has a porosity less than or equal to about 5%.

(23) The infiltrated retainer 30, 30a possesses both the strength benefits of the base metal (e.g., mild steel, stainless steel, etc.) and the tribological benefits of the infiltrant, thereby eliminating the compromise required when selecting conventional retainer materials. For example, a retainer manufactured from mild steel powder infiltrated with bronze in accordance with the method described above has superior strength compared to a conventional brass or bronze retainer and superior tribological characteristics compared to a conventional steel retainer.

(24) The use of additive manufacturing processes such as 3D printing has many advantages in the manufacturing of retainers. For example, the process requires no tooling, thus small and medium production volumes can be made cost effectively. For high production volumes, a conventional powder metal compaction and sintering process can be used to create a porous powder metal retainer, which can then be infiltrated in the manner described above.

(25) FIG. 8 illustrates a retainer 30b according to another embodiment of the invention. The retainer 30b is similar to the retainer 30 of FIG. 6, and like components are given like reference numerals with the letter b. The retainer 30b includes an annular portion 38b and a plurality of engaging portions 42b that define pockets 46b for receiving a plurality of rolling elements (not shown). Each of the engaging portions 42b includes dimples 58 that can retain lubricant, reduce an overall weight of the retainer 30b, and reduce a contact area between the engaging portions 42b and the rolling elements.

(26) FIG. 9 illustrates a retainer 30c according to another embodiment of the invention. The retainer 30c is similar to the retainer 30 of FIG. 6, and like components are given like reference numerals with the letter c. The retainer 30c includes an annular portion 38c and a plurality of engaging portions 42c that define pockets 46c for receiving a plurality of rolling elements (not shown). Each of the engaging portions 42c includes a recessed area or channel 62 that can retain lubricant, reduce an overall weight of the retainer 30c, and reduce a contact area between the engaging portions 42c and the rolling elements. In addition, the annular portion 38c is substantially hollow to reduce an overall weight of the retainer 30c.

(27) The retainers 30b, 30c of FIGS. 8 and 9 incorporate features and geometries that are easily producible with the 3D printing process described above, but otherwise cost prohibitive or not possible with traditional manufacturing methods.

(28) In some embodiments, any of the retainers 30, 30a, 30b, 30c described herein may undergo one or more finishing processes to improve the surface finish, dimensional accuracy, corrosion resistance, wear resistance, hardness, or appearance of the engaging portions 42, 42a, 42b, 42c. Such finishing processes may be particularly advantageous in high performance and high precision bearing applications. The engaging portions 42, 42a, 42b, 42c can be finished by machining, mass finishing (e.g., tumble: or vibratory finishing), superfinishing, polishing, or any other finishing process.

(29) Various features of the invention are set forth in the following claims.