The present invention relates to bearing cages, and more particularly to bearing cages with improved PV (Pressure×Velocity) capabilities.
Bearings are commonly used whenever two contacting parts rotate with respect to one another, such as in automatic transmissions and planetary gear sets. During part assembly, handling individual rolling elements is cumbersome and time consuming. To combat these issues, rolling elements are installed into bearing cages to produce a lightweight, easy to manipulate assembly able to simplify rolling element installation and maintain equal rolling element spacing during part assembly and operation.
Once installed, normal operation of a planetary gear set causes a bearing assembly to rotate simultaneously with respect to the planetary gear axis and the carrier gear axis. Due to the mass of the bearing cage, the rotation results in large amounts of centripetal acceleration, and consequently, movement of the bearing cage radially outwardly to contact the inner surface of the bore in which it was received. As carrier speeds increase, the pressure of the outer surfaces of the cage contacting the inner surface of the respective bore similarly increases. Ultimately, the pressure forces, in addition to the added velocity, increase the PV (Pressure×Velocity) experienced by the bearing cage and may limit the bearing assembly's operating envelope.
The present invention relates generally to a bearing assembly for use in a transmission including at least one planetary gear set. The bearing assembly includes a bearing cage with increased outer surface area to produce a lower PV during normal operating conditions. Specific geometry, such as contact area, contact area placement, and the number of contact locations, is manipulated to more effectively decrease the PV experienced by the bearing cage. The bearing cage further includes the ability to have each rolling element loaded from the outside of the cage.
In one embodiment, the bearing cage may comprise a first end portion defining a first radially exterior contact surface defined at a radially-outermost diameter of the bearing cage and having a first axial contact length, a second end portion spaced a distance from the first end portion and defining a second radially exterior contact surface defined at the radially-outermost diameter of the bearing cage and having a second axial contact length, and a plurality of spanning members extending between the first and second end portions. Each spanning member defines a spanning member axial contact length Cspan defined at a radially-outermost diameter of the bearing cage by at least one contact pad on the spanning member. The sum total of the first axial contact length, the second axial contact length, and the spanning member axial contact length Cspan defines a total contact length Ctotal where the ratio of the total contact length Ctotal to the overall axial length L1 is at least 0.380.
In another embodiment, the bearing cage comprises a first end portion, a second end portion spaced a distance from the first end portion to define an overall axial length L1, and a plurality of spanning members extending between the first and second end portions. Each of the plurality of spanning members defines a pair of distal contact pads and at least one intermediate contact pad, and each contact pad is positioned at a radially-outermost diameter of the bearing cage.
In yet another embodiment, the bearing cage comprises a first end portion, a second end portion spaced a distance from the first end portion, and a plurality of spanning members extending between the first and second end portions to define a spanning member axial length L2. Each spanning member defines a spanning member axial contact length Cspan defined at a radially-outermost diameter of the bearing cage by at least one contact pad on the spanning member and the ratio of the spanning member axial contact length Cspan to the spanning member axial length L2 is at least 0.370.
a is a section view showing a portion of
a and 7b are section views of two prior art bearing cages.
c is a perspective view of another prior art bearing cage.
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. The use of “including,” “comprising,” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Unless specified or limited otherwise, the terms “mounted,” “connected,” “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
With reference to
The bearing cage 22 is substantially cylindrical and includes a first end portion 38 that is substantially annular and coaxial with the central axis 18, a second end portion 42 spaced a distance from the first end portion 38 and coaxial the central axis 18, and a plurality of spanning portions or members 46 extending axially between the first and second end portions 38, 42. During normal operation, the bearing cage 22 simultaneously rotates about both the central axis 18 and a carrier axis 19 generally located at the center of the planetary gear set 14. At normal transmission speeds, the bearing cage 22 is subject to centripetal acceleration able to potentially deform the cage 22. More specifically, the centripetal acceleration may result in the radially-outermost regions of the cage 22 expanding radially outwardly until contacting the inner surface 31 of the central bore 30. Any additional increase in the overall rotational speed of the planetary gear set 14 results in an increased force where the radially outer surfaces of the cage 22 contact the inner surface 31 of the central bore 30. Therefore, the PV experienced by a bearing cage 22 increases relative to the carrier speed.
With continued reference to
Each of the plurality of spanning members 46 extends axially between the first and second end portions 38, 42, while varying in diameter between the outer diameter 50 and at least one secondary diameter 66 to define one or more contact pads 70a, b, c and one or more intermediate spans 74. Each contact pad 70a, b, c may be defined as any segment of the spanning member 46 in position to potentially contact the central bore 30 during standard operation of the needle bearing cage assembly 10 (i.e., at the outer diameter 50). Each contact pad 70a, b, c is generally shaped and sized to maximize the contact area with the inner surface 31 of the central bore 30 for a given amount of axial length. More specifically, the contact pads 70a, b, c may be greater in width than the adjacent intermediate spans 74. In some specific embodiments, the bearing cage 22 has at least 20% of the maximum possible outer surface area in position to contact the inner surface 31 of the central bore 30. The maximum outer surface area is defined as the outer surface area (SAmax=πDL) of a solid cylindrical piece having an identical outer diameter D (i.e., outer diameter 50) and identical overall axial length L (i.e., axial length L1) of the specified bearing cage 22 (see
With continued reference to
In the illustrated construction of
Each contact pad 70a, b, c of the bearing cage 22 may include one or more retention members 78 (see
In some specific embodiments, each retention member 78 is positioned to deflect upon introduction of the rolling element 24. More specifically, each retention member 78 may be positioned on one of the one or more intermediate contact pads 70b, spaced away from the end portions 38, 42, to promote deflection. Positioning the retention members 78 so that they may deflect upon introduction of a rolling element 24 allows the rolling elements 24 to be held with a tighter tolerance, thereby reducing the amount of deflection each rolling element 24 may exhibit with respect to the bearing cage 22 once the roller is retained. Reduced roller element deflection is desired in high volume installation applications which typically utilize automated machinery. In alternate external loading techniques, stationary retention members require larger tolerances with respect to the rolling elements, and as a result, permit larger rolling element deflection often resulting in the elements interfering with the central bore 30 and inhibiting the installation process. In the present invention, the retention members 78 facilitate automated assembly by minimizing rolling element deflection.
As depicted in
With continued reference to
In particular constructions, the spanning members 46 define a sufficient size and/or quantity of contact pads 70a, b, c such that no individual intermediate span 74 extends longer than about 15-29% of the overall spanning length L2 (shown in
With reference to
In addition to determining the spanning member contact ratio (Cspan/L2), an overall contact ratio may be calculated for the bearing cage 22. With reference to
In the illustrated embodiment, the bearing cage 22 is generally formed from a wrap and weld technique well known in the art. However, in alternate embodiments, any construction technique known to one skilled in the art may be utilized to create the above described bearing cage 22. Moreover, the above described bearing cage 22 may be adapted to receive any number of rolling element types and/or variations such as balls, tapered rollers, and the like, and can be used in a variety of bearing applications.
With reference to
Various features of the invention are set forth in the following claims.
This application claims priority to U.S. Provisional Application No. 61/186,997, filed Jun. 15, 2009, the entire disclosure of which is incorporated by reference herein.
Number | Name | Date | Kind |
---|---|---|---|
1951042 | Walter | Mar 1934 | A |
3114960 | Einaudi | Dec 1963 | A |
3240542 | Jahn | Mar 1966 | A |
5232290 | Buschle et al. | Aug 1993 | A |
5391005 | Alling | Feb 1995 | A |
6561945 | Shattuck et al. | May 2003 | B2 |
6892455 | Feest | May 2005 | B1 |
20060252596 | Abarquez et al. | Nov 2006 | A1 |
Number | Date | Country |
---|---|---|
1725627 | Jul 1956 | DE |
1198623 | Aug 1965 | DE |
1963209 | Jun 1967 | DE |
4214987 | Nov 1992 | DE |
10223432 | Dec 2003 | DE |
69627937 | May 2004 | DE |
102007057045 | May 2009 | DE |
2098738 | Sep 2009 | EP |
919983 | Feb 1963 | GB |
7259865 | Oct 1995 | JP |
10115322 | May 1998 | JP |
11082696 | Mar 1999 | JP |
2003106336 | Apr 2003 | JP |
2004011689 | Jan 2004 | JP |
2004353809 | Dec 2004 | JP |
2005214390 | Aug 2005 | JP |
2006170369 | Jun 2006 | JP |
2008075791 | Apr 2008 | JP |
2008232280 | Oct 2008 | JP |
2008261476 | Oct 2008 | JP |
Entry |
---|
“Trends Regarding Needle Roller Bearings for Automatic Transmission Planetary Gears,” by K. Chihara and T. Satou, Koyo Engineering Journal English Edition No. 168E, pp. 39-42 (2005). |
Office Action dated Jun. 15, 2012 for co-pending German Patent Application No. 10 2010 023 746.9-12. |
Number | Date | Country | |
---|---|---|---|
20100322549 A1 | Dec 2010 | US |
Number | Date | Country | |
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61186997 | Jun 2009 | US |