This invention relates in general to rolling cone earth-boring bits, and in particular to an insert ring that is mounted between the bearing pin and the seal for resisting wear and corrosion.
A typical roller cone earth-boring bit has a bit body with three bit legs. A bearing pin extends from each bit leg, and a cone rotatably mounts on the bearing pin. The bearing surfaces between the cavity of the cone and the bearing pin are filled with a lubricant. A seal is located between the cone and the bearing pin to seal lubricant within and keep drilling fluid from entry.
Many designs for seals have been proposed and used. One type comprises an elastomeric ring that is located in a groove in the cone near the mouth of the cavity. The ring normally rotates with the cone and seals against the stationary bearing pin. The ring and seal groove are designed to provide a selected contact pressure of the inner diameter of the ring with the bearing pin. A high downward force is imposed on the drill bit during operation, resulting in a higher contact pressure on the lower side of the bearing pin than on the upper side. Also, during operation, there may be slight cone movement relative to the axis of the bearing pin. This movement results in varying contact pressure on both the bearing and seal. Varying contact pressure can cause excessive heat and wear in certain areas of the seal, shortening the life. Also, cuttings from the earth formation are able to contact portions of the seal and tend to cause it to wear.
U.S. Pat. Nos. 5,005,989, 5,570,750, and 4,934,467 disclose installing a rigid insert ring on the bearing pin for engagement by the inner diameter of the seal ring. The insert ring is of harder material than the bearing pin for reducing wear on the seal ring. In the FIG. 7 embodiment of the '989 patent, the insert ring is located on and fixed relative to the bearing pin by a vulcanized layer.
The earth boring bit of this invention has a rigid insert ring mounted on the bearing pin. The insert ring has an inner diameter greater than an outer diameter of the bearing pin, defining a clearance between the insert ring and the bearing pin to allow the insert ring to float relative to an axis of the bearing pin. An inner seal is in sealing engagement with the bearing pin and the inner diameter of the insert ring. A cone is rotatably mounted on the bearing pin, the cone having a cavity containing an outer seal groove. An outer seal is located in the outer seal groove and in dynamic sealing engagement with an outer diameter of the insert ring. An anti-rotation member mounted to a portion of the bit body is in engagement with a portion of the insert ring to prevent rotation of the insert ring.
Preferably, the insert ring is of uniform thickness around its circumference. In the preferred embodiment, the anti-rotation member is a pin that has an axis normal to the portion of the seal ring that it engages. Also, in the preferred embodiment, the insert ring has a radially extending flange that abuts the bit leg. The flange on the insert ring may be partially recessed within an annular groove formed on the bit leg. Preferably the inner seal is located in a groove formed in the bearing pin.
Referring to
An annular groove 17 is formed around the junction of bit leg 13 and bearing pin 15. Recess 17 is formed in a portion of bit leg 13 referred to as a last machined surface 19. Last machined surface 19 is a generally flat surface located in a plane perpendicular to the bearing pin axis 23. Last machined surface 19 extends radially outward from annular recess 17. A portion of last machined surface 19 on the lower side of bit leg 13 is referred to as the shirttail 21. Recess 17 has a radial width that is about the same as the radial width of last machined surface 19 at shirttail 21.
A rigid insert ring 25 is installed on bearing pin 15 at the junction with bit leg 13. Insert ring 25 is preferably an L-shaped member in cross-section, having a cylindrical portion 27 that extends around bearing pin 15 and a flange portion 29 that extends radially outward from cylindrical portion 27. Flange portion 29 locates within recess 17 and has a mating contour. In this embodiment, flange portion 29 has a thickness that is about twice the depth of recess 17, so that it protrudes a short distance forward from last machined surface 19. Flange portion 29 in this embodiment is thicker than cylindrical portion 27. Cylindrical portion 27 may taper on its forward end. The thickness of cylindrical portion 27 is preferably uniform around the circumference of ring 25.
The inner diameter of cylindrical portion 27 is slightly greater than the outer diameter of bearing pin 15 by a few thousandths of an inch in the preferred embodiment. Slight, non-rotational movement or floating of insert ring 25 relative to the axis of bearing pin 15 is allowed to occur by the clearance provided between the inner diameter of cylindrical portion 27 and the outer diameter of bearing pin 15. An inner seal 31, which is an elastomeric O-ring in this embodiment, is located in a groove formed in bearing pin 15 and seals against the inner diameter of cylindrical portion 27 of insert ring 25. Inner seal 31 preferably has a uniform cross-sectional thickness around its circumference.
An anti-rotation member prevents insert ring 25 from rotating relative to bearing pin 15. In this embodiment, a recess or slot 33, shown in
Referring again to
A variety of different bearing arrangements may be utilized between cone 37 and bearing pin 15. In the example shown, a rearward set of cylindrical roller bearings 43 is carried within a groove in cavity 41 for engaging bearing pin 15. This embodiment also discloses an intermediate set of roller bearings 45 engaging a smaller diameter portion of bearing pin 15 and a set of nose roller bearings 47 engaging an even smaller diameter portion of bearing pin 15. A thrust washer 49 is located on a thrust shoulder of bearing pin 15 for engaging a mating surface within cone cavity 41. Cone 37 is retained on bearing pin 15 by a plurality of balls 51 that engage mating recesses in cone cavity 41 and on bearing pin 15.
Cone cavity 41 is filled with a lubricant that is supplied from a lubricant reservoir and pressure compensator (not shown) through passages (not shown) to the spaces between cone 37 and bearing pin 15. A variety of seals may be employed to seal the lubricant within cone cavity 41 and prevent encroachment of drilling bit fluid from the exterior. In this embodiment, the seal comprises an elastomeric seal 53 located within a seal groove 55 formed near the entrance or mouth of cone cavity 41. Referring to
Referring still to
Annular rib 59 extends over a portion of insert ring flange 29 and has a flat face separated from last machined surface 19 by a small clearance. The width of this clearance is less than the thickness of flange 29, thereby restricting the entry of borehole cuttings. Outer seal groove 55 is spaced slightly forward toward the bit axis of rotation from inner backface portion 57. The portion of cone 37 between inner backface portion 57 and groove 55 is a thin flange 62 that separates outer seal 53 from insert ring flange 29. Outer seal 53 thus does not contact insert ring flange 29.
Anti-rotation pin 35 has a flat face that is separate from cone annular rib 59 by a small clearance. In this embodiment, the face of anti-rotation pin 35 is substantially flush with the portion of last machined surface 19 located radially outward from annular groove 17, which receives insert ring flange 29. The hole for receiving anti-rotation pin 35 is partly in groove 17 and partly in last machined surface 19 just outward from groove 17. As a result, a portion of anti-rotation pin 35 protrudes from the base of groove 17.
One or more diverter pins 63 may be mounted in holes in bit leg 13 and protrude forward, each having an axis parallel to bearing pin axis 23 (
In operation, as bit 11 rotates, each cone 37 rotates about bearing pin axis 23. Drilling fluid is pumped down a drill string, which flows out nozzles and back up around the exterior of bit 11 along with cuttings. Seal 53 normally rotates in unison with cone 37 and slidingly engages the outer surface of insert ring cylindrical portion 27. Cone 37 will wobble or move slightly relative to the axis of bearing pin 15 because of the weight imposed on bit 11. Insert ring 25 will tend to move with cone 37, thus will float relative to the axis of bearing pin 15. This floating movement tends to maintain a desired contact pressure of outer seal 53 with floating insert ring 25.
Diverter pins 63, if used, may reduce the amount of cuttings and debris that otherwise would enter the spaces between last machined surface 19 and backface portions 57 and 61. Some cuttings and debris, nevertheless, will come into contact with insert ring 25. Insert ring 25 is preferably formed of a metal that is more resistant to abrasion and corrosion than the material of bit leg 13, bearing pin 15 and cone 37, to inhibit the wear that would normally occur at the intersection between last machined surface 19 and bearing pin 15.
The invention has significant advantages. The insert ring reduces differences in contact pressure applied to the seal. The insert ring also provides protection for the seal against contact with cuttings and debris.
While the invention has been shown in only one of its forms, it should be apparent to those skilled in the art that it is not so limited, but is susceptible to various changes without departing from the scope of the invention.
This application claims the benefit of U.S. provisional application Ser. No. 60/756,901, filed Jan. 6, 2006.
Number | Name | Date | Kind |
---|---|---|---|
4666001 | Burr | May 1987 | A |
4762189 | Tatum | Aug 1988 | A |
4825964 | Rives | May 1989 | A |
4934467 | Langford, Jr. | Jun 1990 | A |
5005989 | Karlsson | Apr 1991 | A |
5295549 | Dolezal et al. | Mar 1994 | A |
5570750 | Williams | Nov 1996 | A |
5875861 | Daly et al. | Mar 1999 | A |
6305483 | Portwood | Oct 2001 | B1 |
6427790 | Burr | Aug 2002 | B1 |
6513607 | Peterson et al. | Feb 2003 | B2 |
Number | Date | Country | |
---|---|---|---|
20070158114 A1 | Jul 2007 | US |
Number | Date | Country | |
---|---|---|---|
60756901 | Jan 2006 | US |