Claims
- 1. A drill bit for subterranean drilling, comprising:
a bit body including a longitudinal centerline, a leading end having a face for contacting a formation having a compressive strength during drilling, and a trailing end having a structure associated therewith for connecting the bit body to a drill string, the face of the leading end including a bearing surface sized and configured to transfer a range of weight-on-bit from the body of the bit through the bearing surface to the formation, wherein the range of weight-on-bit comprises any weight-on-bit which results in the bearing surface contacting the formation at a stress of less than substantially the compressive strength of the formation; wherein the bearing surface area is configured and located so that the bearing surface area in contact with the formation remains substantially constant within the range of weight-on-bit; and at least one superabrasive cutter for engaging the formation during drilling secured to a selected portion of the face of the leading end of the bit body.
- 2. The drill bit of claim 1, wherein the at least one superabrasive cutter comprises a plurality of superabrasive cutters and the face of the leading end comprises a plurality of blade structures protruding from the bit body, at least some of the plurality of blade structures carrying at least one of the plurality of superabrasive cutters and the blade structures exhibiting in total a combined bearing surface area of sufficient size to maintain substantially the stress on the formation not exceeding the compressive strength thereof.
- 3. The drill bit of claim 2, wherein the at least some of the plurality of blade structures each extend from a respective point generally proximate the longitudinal centerline of the bit body generally radially outward toward a gage of the bit body and longitudinally toward the trailing end of the bit body.
- 4. The drill bit of claim 2, wherein a maximum weight-on-bit of the range of weight-on-bit equals the combined bearing surface area multiplied by the compressive strength of the formation.
- 5. The drill bit of claim 3, wherein the at least some of the plurality of blade structures each carry several of the plurality of superabrasive cutters and exhibit at least one bearing surface, and wherein each of the plurality of blade structures generally encompasses each of the several of the plurality of superabrasive cutters carried thereon with a limited portion of each of the several superabrasive cutters exposed by a preselected extent perpendicular from the respective at least one bearing surface proximate each of the several superabrasive cutters so as to control a respective depth-of-cut for each of the several superabrasive cutters.
- 6. The drill bit of claim 2, wherein the bit body comprises at least one of steel and a metal matrix.
- 7. The drill bit of claim 5, wherein at least a portion of the at least one bearing surface of at least one of the plurality of blade structures includes a wear-resistant exterior.
- 8. The drill bit of claim 5, wherein the bit body comprises steel and the at least one bearing surface of at least one of the plurality of blade structures includes an exterior hard facing.
- 9. The drill bit of claim 8, wherein the exterior hard facing comprises tungsten carbide particles.
- 10. The drill bit of claim 2, wherein at least one bearing surface of at least one of the plurality of blade structures comprises a wear-resistant exterior.
- 11. The drill bit of claim 5, wherein the at least one bearing surface is built up with a hard facing on at least a portion thereof substantially surrounding at least one of the plurality of superabrasive cutters so as to effectively limit an amount of exposure of the at least one of the superabrasive cutters.
- 12. The drill bit of claim 7, wherein the wear-resistant exterior comprises at least one of the group consisting of carbide, tungsten carbide, synthetic diamond, natural diamond, polycrystalline diamond, thermally stable polycrystalline diamond, cubic boron nitride, and hard facing material.
- 13. The drill bit of claim 5, wherein the face of the leading end of the bit body comprises cone, nose, flank, shoulder, and gage regions.
- 14. The drill bit of claim 13, wherein the portion of the bearing surface area positioned in the cone region exhibits a greater amount of bearing surface area than the portion of bearing surface area positioned in the nose region.
- 15. The drill bit of claim 14, wherein the portion of the bearing surface area positioned in the nose region exhibits a greater amount of bearing surface area than the portion of bearing surface area positioned in the flank region.
- 16. The drill bit of claim 15, wherein the portion of the bearing surface area positioned in the flank region and exhibits a greater amount of bearing surface area than the portion of the bearing surface area positioned in the shoulder region.
- 17. The drill bit of claim 13, wherein portion of the bearing surface area positioned in the cone region exhibits a greater amount of bearing surface area than the portion of the bearing surface area positioned in the shoulder region.
- 18. The drill bit of claim 2, wherein at least one superabrasive cutter of the plurality comprises a chamfered region extending at least partially about a circumferential periphery thereof.
- 19. The drill bit of claim 2, wherein at least one superabrasive cutter of the plurality includes an effective backrake angle not exceeding approximately 20° with respect to an intended direction of drill bit rotation perpendicular to the formation to be engaged by the at least one superabrasive cutter of the plurality.
- 20. The drill bit of claim 19, further comprising a superabrasive cutter of the plurality positioned and secured to the bit body in a gage region of the drill bit and having an effective backrake angle substantially exceeding approximately 20°.
- 21. The drill bit of claim 19, wherein the at least one superabrasive cutter further includes a superabrasive backrake angle of approximately 30° or greater.
- 22. The drill bit of claim 5, wherein at least one wear knot structure is disposed upon the at least one bearing surface proximate at least one superabrasive cutter of the plurality, the at least one wear knot structure exhibiting a radially outermost wear knot surface that is generally inset a preselected distance from a rotational profile exhibited by an outermost portion of an exposed portion of at least one rotationally associated superabrasive cutter upon the drill bit being rotated.
- 23. The drill bit of claim 22, wherein the at least one wear knot structure comprises a plurality of wear knot structures and the preselected distance that the radially outermost wear knot surface of each of the plurality of wear knot structures is inset from the rotational profile exhibited by the outermost portion of the exposed portion of the at least one rotationally associated superabrasive cutter ranges from approximately 0.05 of an inch to approximately 0.2 of an inch.
- 24. The drill bit of claim 1, wherein the at least one superabrasive cutter comprises a chamfered peripheral edge portion of a preselected width and chamfer angle.
- 25. The drill bit claim 1, comprising at least another bearing surface configured to transfer another weight-on-bit from the body of the bit through the another bearing surface to the formation at a weight-on-bit above which results in the another bearing surface contacting the formation at a stress of less than substantially the compressive strength of the formation.
- 26. A method of drilling a subterranean formation without generating an excessive amount of torque-on-bit, comprising:
engaging the formation, the formation having a compressive strength, with at least one cutter of a drill bit within a selected depth-of-cut range; applying a weight-on-bit within a range of weight-on-bit in excess of that required for the at least one cutter to penetrate the formation and above which results in a bearing surface contacting the formation so as to cause the bearing surface to contact the formation, wherein the area of the bearing surface contacting the formation remains substantially constant over the range of excess weight-on-bit; and transferring the excess weight-on-bit from the body of the bit through a bearing surface to the formation at a stress less than substantially the compressive strength of the formation.
- 27. The method of claim 26, wherein transferring the excess weight-on-bit from the body of the bit through a bearing surface to the formation comprises transferring the excess weight-on-bit to at least one formation-facing bearing surface on the drill bit generally surrounding at least a portion of the at least one cutter.
- 28. The method of claim 27, wherein transferring the excess weight-on-bit from the body of the bit through a bearing surface to the formation comprises transferring the excess weight-on-bit from the body of the bit through a bearing surface to the formation without precipitating substantial plastic deformation thereof.
- 29. The method of claim 27, wherein transferring the excess weight-on-bit to at least one formation-facing bearing surface on the drill bit generally surrounding at least a portion of the at least one cutter comprises transferring the excess weight-on-bit to at least one wear knot rotationally following at least one of the superabrasive cutters.
- 30. The method of claim 29, wherein transferring the excess weight-on-bit to at least one wear knot rotationally following at least one of the superabrasive cutters comprises transferring the excess weight-on-bit to a plurality of wear knots on the formation-facing bearing surfaces.
- 31. The method of claim 30, wherein transferring the excess weight-on-bit to the plurality of wear knots on the formation-facing bearing surfaces comprises transferring the excess weight-on-bit to a plurality of wear knots on formation-facing bearing surfaces respectively located on the plurality of blade structures.
- 32. The method of claim 27, wherein transferring the excess weight-on-bit to at least one formation-facing bearing surface on the drill bit generally surrounding at least a portion of the at least one cutter comprises transferring the excess weight-on-bit to a hard facing material affixed to a selected portion of the respective at least one formation-facing bearing surface proximate at least one of the superabrasive cutters.
- 33. The method of claim 32, wherein transferring the excess weight-on-bit to a hard facing material comprises transferring the excess weight-on-bit to a hard facing material affixed to a steel-bodied bit.
- 34. The method of claim 33, wherein transferring the excess weight-on-bit to a hard facing material affixed to a steel-bodied bit comprises transferring the excess weight-on-bit to a hard facing material affixed to a steel-bodied bit within at least a cone region of the steel-bodied bit.
- 35. The method of claim 26, further comprising:
applying an additional weight-on-bit in excess of the excess weight-on-bit required for the bearing surface to contact the formation and above which results in the bearing surface and another bearing surface contacting the formation; and transferring the additional excess weight-on-bit from the body of the bit through the another bearing surface to the formation at a stress less than substantially the compressive strength of the formation.
- 36. A method of designing a drill bit for drilling subterranean formations, the drill bit under design including a plurality of superabrasive cutters disposed about the formation-engaging leading end of the drill bit, the method comprising:
selecting a maximum depth-of-cut for the at least some of the plurality of superabrasive cutters; selecting a cutter profile arrangement to which the at least some of the plurality of superabrasive cutters are to be radially and longitudinally positioned on the leading end of the drill bit; and configuring within the design of the drill bit a sufficient total amount of formation-facing bearing surface area to axially support the drill bit at a stress less than substantially the compressive strength of the formation should the drill bit be subjected to a weight-on-bit exceeding a weight-on-bit which would cause the bearing surface area to contact the formation, wherein the bearing surface area is sized and configured to remain substantially constant over a range of excess weight-on-bit.
- 37. The method of claim 36, further comprising including within the drill bit under design a plurality of kerf regions of a preselected width positioned laterally intermediate of selected rotationally adjacently positioned superabrasive cutters.
- 38. The method of claim 36, wherein selecting a cutter profile arrangement comprises selecting at least one cutter of the plurality to be respectively located in at least one of a cone region, a nose region, a flank region, and a shoulder region of the drill bit.
- 39. The method of claim 38, further comprising selecting a quantity of wear knots to be respectively positioned on the drill bit so at to rotationally follow at least some of the plurality of superabrasive cutters.
- 40. The method of claim 36, wherein configuring within the design of the drill bit a sufficient total amount of formation-facing bearing surface area comprises selecting an amount of hard facing to be disposed on at least a portion of the at least one respective formation-facing bearing surface at least partially surrounding the at least some of the plurality of superabrasive cutters.
- 41. The method of claim 36, further comprising:
including within the design of the drill bit another formation-facing bearing surface area to axially support the drill bit at a stress less than substantially the compressive strength of the formation should the drill bit be subjected to an additional excess weight-on-bit exceeding the excess weight-on-bit; and configuring the another formation-facing bearing surface area to correspond to the additional excess weight-on-bit transferred from the body of the bit through the another bearing surface to the formation at a weight-on-bit above which results in the another bearing surface contacting the formation at a stress of less than substantially the compressive strength of the formation.
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] Related Applications: This application is a continuation of U.S. patent application Ser. No. 09/738,687, filed Dec. 15, 2000, pending, which is a continuation-in-part of now issued U.S. Pat. No. 6,298,930 B1 entitled Drill Bits with Controlled Cutter Loading and Depth of Cut filed Aug. 26, 1999.
Continuations (1)
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Number |
Date |
Country |
Parent |
09738687 |
Dec 2000 |
US |
Child |
10266534 |
Oct 2002 |
US |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
09383228 |
Aug 1999 |
US |
Child |
09738687 |
Dec 2000 |
US |