The present invention relates to thrust bearings, and more particularly, to a combination rotating thrust plate and thrust shaft flange intended to support a rotating shaft in a screw extruder and to a thrust bearing assembly incorporating the combination rotating thrust plate and thrust shaft flange.
Extruders generally force molten material through an extruder barrel utilizing a turning screw. During operation, flights of the screw engage the molten material, moving it along the length of the barrel. Typically, a restriction to flow such as a die defining the desired shape for the extruder material is mounted onto the end of the barrel. The force created by the screw on the material causes it to flow through the restriction. The movement of the material via the action of the screw, as well as the channeling of the material through the restriction, tends to generate very high reaction forces that are transmitted to the device employed to drive and support the screw.
In general, the extruder screw is mounted to an output thrust shaft that in turn forms part of a gear box. The thrust shaft is typically supported by roller-type bearings with the above-described reaction force being absorbed by a thrust bearing also in communication with the thrust shaft. A thrust bearing typically consists of a series of rolling elements sandwiched between two thrust plates. The thrust plates and rollers transfer the reaction forces generated by the processing of the material through the extruder to the gear reducer housing. Due to the magnitude of the reaction force, known thrust plates are generally not stiff enough to withstand the load imposed thereon and must be replaced frequently.
The present invention relates to a thrust bearing assembly, including a single-piece thrust plate and thrust shaft flange. The single-piece thrust plate and thrust shaft flange includes a generally cylindrical body portion defining a rotating base surface and a lateral surface; and a frustoconical body portion defining a frustoconical surface and a base surface. The single-piece thrust plate and thrust shaft flange also includes a bore extending through the cylindrical body portion and the frustoconical body portion. The bore extends substantially perpendicular to the rotating base surface. The bore has a first bore section and a second bore section. The second bore section is adjacent to the rotating base surface and has a smaller diameter than the first bore section. A lip extends between the first and second bore sections. The first bore section, the second bore section and the lip are configured to receive a thrust shaft and accommodate axial thrust forces transmitted from the thrust shaft.
The thrust bearing assembly includes a bearing assembly in operable communication with the generally cylindrical body portion. The bearing assembly supports rotation of the thrust shaft and includes a plurality of first rolling elements. The bearing assembly includes a bearing cage configured to retain the first rolling elements. The thrust bearing assembly further includes a stationary plate having a passage extending therethrough complementary to the second bore section. The thrust shaft is received by the passage and the stationary plate engages the bearing assembly. A plurality of second rolling elements is disposed between the bearing cage and the thrust shaft. The plurality of second rolling elements supports rotation of the bearing cage around the thrust shaft.
In another aspect of the present invention, the second rolling elements are needle bearings. In addition, the second rolling elements can be retained by another cage.
The novel features of the described embodiments are specifically set forth in the appended claims; however, embodiments relating to the structure and process of making the present invention, may best be understood with reference to the following description and accompanying drawings.
As shown in
As shown most clearly in
The frustoconical portion (24) extends inwardly from the generally cylindrical portion (22). Optimally, the frustoconical surface (28) extends at an angle of about 230 degrees from the lateral surface (23) as illustrated in
During operation, thrust forces generated by the extruder and indicated in
Also encompassed by the present invention is the thrust bearing assembly (40) which supports the rotating thrust shaft (20) as shown in
The stationary plate (32) has a generally cylindrical shape with a stationary bore (44) extending therethrough complimentary to the second bore section (16) of the flange plate combination (10). The stationary plate (32) has a stationary base surface (33). The stationary base surface (33) is adapted to engage the rolling elements (26). The rolling elements (26) are evenly interspersed between the flange plate combination (10) and the stationary plate (32).
A bearing cage (46) for retaining the rolling elements (26) in position to assure free radial movement of the flange plate combination (10) is preferably provided. As shown in
An advantage of the present invention is that the thrust bearing assembly includes fewer parts and is therefore easier to maintain, compared to prior art thrust bearings such as that described above with reference to
A further advantage of the present invention is that the rotating flange plate combination (10) has a greater stiffness, or load bearing capacity, compared to prior art rotating thrust plates and thrust flanges of the same material. The thrust bearing assembly (40) of the present invention also has a greater load bearing capacity.
The bearing cage illustrated in
It is to be understood that the present invention is not limited to the embodiments described above, but encompasses any and all embodiments within the scope of the following claims. Accordingly, it is to be understood that the present invention has been described by way of example, and not by limitation.
This application is a continuation in part of U.S. patent application Ser. No. 10/012,980, filed Nov. 5, 2001, which claims the benefit of U.S. Provisional Application Ser. No. 60/246,394 filed on Nov. 7, 2000, which are incorporated herein by reference in their entirety.
Number | Name | Date | Kind |
---|---|---|---|
628526 | Cliff | Jul 1899 | A |
673220 | Perkins | Apr 1901 | A |
1218312 | Perkins | Mar 1917 | A |
2030104 | Eksergian | Feb 1936 | A |
2118760 | Ernst | May 1938 | A |
2374820 | Kaye | May 1945 | A |
2539683 | Ablett | Jan 1951 | A |
2584652 | Antony | Feb 1952 | A |
2659305 | Giori | Nov 1953 | A |
2726070 | Tudor | Dec 1955 | A |
3023058 | Bowers et al. | Feb 1962 | A |
3375549 | Geyer | Apr 1968 | A |
3414341 | Murphy | Dec 1968 | A |
3712693 | Root et al. | Jan 1973 | A |
3795456 | Schafer | Mar 1974 | A |
3829181 | Gunther et al. | Aug 1974 | A |
3923290 | Tillis | Dec 1975 | A |
3934956 | Pitner | Jan 1976 | A |
4033556 | Anders | Jul 1977 | A |
4042284 | Coster | Aug 1977 | A |
4124256 | de Senneville | Nov 1978 | A |
4304539 | Hagiwara et al. | Dec 1981 | A |
4320928 | Chszaniecki | Mar 1982 | A |
4517858 | Schafer | May 1985 | A |
4718840 | Inaba et al. | Jan 1988 | A |
4859166 | Hamada et al. | Aug 1989 | A |
4971460 | Muntnich et al. | Nov 1990 | A |
5150973 | Masur et al. | Sep 1992 | A |
5261750 | Eckhardt et al. | Nov 1993 | A |
5545024 | Iwata et al. | Aug 1996 | A |
5641227 | Geyer | Jun 1997 | A |
5770906 | Hazelton et al. | Jun 1998 | A |
6485188 | Dougherty | Nov 2002 | B1 |
6543938 | Dittenhofer | Apr 2003 | B2 |
20050216084 | Fleischmann et al. | Sep 2005 | A1 |
20120008894 | Plasse | Jan 2012 | A1 |
Number | Date | Country |
---|---|---|
5066058 | Jun 1975 | JP |
2009180235 | Aug 2009 | JP |
0238956 | May 2002 | WO |
Entry |
---|
International Search Report issued in corresponding PCT Application No. PCT/US2012/046581 dated Jan. 9, 2013. |
Number | Date | Country | |
---|---|---|---|
20120008894 A1 | Jan 2012 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 10012980 | Nov 2001 | US |
Child | 13182574 | US |