Claims
- 1. A bi-center bit adapted to be consecutively used in casing and in formation without the need of removing the bit from the borehole, said bit comprising:
a bit body defining a proximal end adapted for connection to a drill string, a distal end and a pass-through gauge, where the distal end defines a pilot bit and an intermediate reamer section, where each the pilot and reamer section define a cutting face; and a plurality of cutting or wear elements situated on cutting blades disposed about the cutting face of the pilot and reamer sections, where the cutting or wear elements disposed on one or more of the blades which extend to or are proximate to the pass-through gauge define an angle between the line of contact on the cutting or wear element and the material to be drilled of between 5-45°.
- 2. The bi-center bit of claim 1 further including one or more stabilizing elements disposed opposite said reamer section such that the proximal most portion of said stabilizing elements do not extend beyond the most proximally disposed cutting elements on said reamer section.
- 3. The bi-center bit of claim 2 where the stabilizing elements comprise a gauge pad.
- 4. The bi-center bit of claim 1 where the backrake angle is between 45-85°.
- 5. The bi-center bit of claim 2 where the stabilizing elements extend to the pass-through gauge.
- 6. The bi-center bit of claim 1 where the body is adapted to rotate about one axis when operated in casing and a second, independent axis when operated free of casing.
- 7. The bi-center bit of claim 1 where the bit body is manufactured from steel.
- 8. The bi-center bit of claim 1 further defining a rotational axis “A” and a pass-through axis “B” where the cutting face of most of the cutting elements disposed on cutting blades situated between the rotational axis “A” and the pass-through axis “B” are oriented such that such elements are brought into at least partial contact with the material to be drilled when the bit is rotated about said axis “B.”
- 9. The bi-center bit of claim 1 where the cutting blades on the pilot and reamer include a primary and one or more secondary cutting blades, where both the rotational and pass-through axis are disposed about the primary cutting blade;
where each cutting element defines a cutting face; and where the cutting faces of most cutting elements disposed along the primary cutting blade not between the rotational axis “A” and pass-through axis “B” but between the pass-through axis and pass-through gauge are brought into at least partial contact with the material to be drilled when said bit is rotated about axis “B.”
- 10. The bi-center bit of claim 9 including cutting elements positioned on the secondary cutting blades such that at least a portion of the cutting face of most elements engages the material to be drilled when the bit is rotated about axis “A.”
- 11. The bi-center bit of claim 9 where the skew angle of said cutting elements positioned on the secondary blades is between 0-80°.
- 12. The bi-center bit of claim 1 where cutting elements disposed on cutting blades comprising the reamer section, other than those cutting elements disposed on cutting blades which extend to the pass-through gauge, define an angle formed between the line of contact on the cutting element and the material to be drilled of between 50-80°.
- 13. The bi-center bit of claim 1 where the bit body includes tungsten carbide matrix.
- 14. The bi-center bit of claim 6 where the cutting elements disposed about the pilot and reamer sections demonstrate substantially complete cutter overlap when the bit is rotated about either axis.
- 15. A method to fabricate a bi-center bit adapted to rotate about one of two axis where the bi-center bit comprises a bit body having a proximal and a distal end where the distal end defines a pilot bit and an intermediate reamer section, where each the pilot and reamer sections define a bit face including primary and secondary cutting blades and cutting elements disposed on said blades where each cutting element defines a cutting face, the method comprising the steps of:
fabricating a cutter profile for the bit about the rotational axis “A”; identifying the pass-through axis “B” of the bit; fabricating a cutter profile for the bit about the pass-through axis “B”; and situating cutting elements on the bit face of the pilot and reamer sections such that at least a portion of a cutting element is disposed about substantially all portions of said profiles when the bit is rotated about the rotational and pass-through axes.
- 16. The method of claim 15 further including the step of positioning the cutting blades so that the rotational and pass-through axes fall along a primary cutting blade.
- 17. The method of claim 15 further including the step of positioning cutting elements on the primary cutting blade between the rotational axis “A” and pass-through axis “B” such that substantially all of the cutting faces of said elements are brought into at least partial contact with the material to be drilled when the bit is rotated about said axis “B.”
- 18. The method of claim 15 further including the step of positioning cutting elements on the primary cutting blade opposite said rotational axis “A” and between said pass-through axis “B” and gauge such that the cutting faces of substantially all such elements are brought into at least partial contact with the material to be drilled when said bit is rotated about axis “A.”
- 19. The method of claim 15 where the skew angle of cutting elements of the secondary cutting blades is between 0-80°.
- 20. The method of claim 15 where the reamer section defines at least one cutting blade which extends to the pass-through gauge and including the additional step of positioning cutting elements along said cutting blade such that cutting elements proximate to the pass-through gauge at their line of contact with the material to be drilled define an angle of attack of between 5-45°.
- 21. A two stage drilling tool comprising:
a bit body defining a proximal end adapted for connection to a drill string and a distal end where said distal end terminates in a primary bit face and a secondary bit face spaced proximally from said primary bit face where said primary bit face includes a primary upset and secondary upsets and where one or more cutting elements are disposed about said upsets; said tool defining a rotational axis “A” and a pass-through axis “B”; where cutting elements disposed along said primary upset between said axis “A” and axis “B” define cutting faces where most of said cutter faces are brought into at least partial contact with the material to be drilled when said tool is rotated about said pass-through axis “B.”
- 22. The drilling tool of claim 21 where both of said axes “A” and “B” are disposed along the primary upset.
- 23. The tool of claim 21 where the cutting faces of most of the cutting elements disposed about the primary upset not between the rotational axis “A” and pass-through axis “B” but between said pass-through axis “B” and gauge are brought into at least partial contact with the material to be drilled when said bit is rotated about either axis “A” or “B.”
- 24. The tool of claim 21 further including the step of positioning the cutting elements on said secondary upsets such that they define a skew angle between 0-80°.
- 25. A bi-center bit comprising:
a bit body defining a proximal end for connection to a drill string and a distal end, where the distal end defines a pilot bit and an intermediate reamer section, where each said pilot and reamer sections each define a bit face; the bit face on said pilot being comprised of a primary upset and one or more secondary upsets; the bit body defining a rotational axis “A” and a pass-through axis “B”; and cutting elements disposed about said primary and secondary upsets where each of said cutting elements defines a cutting face, where most of the cutting elements disposed along the primary or secondary upsets between said rotational axis “A” and pass-through axis “B” are brought into contact with the material to be drilled when the bit is rotated about either the pass-through axis “B” or the rotational axis “A.”
- 26. The bi-center bit of claim 25 where most of the cutting elements disposed along said primary upset not between said axis “A” and “B” but between axis “B” and the pass-through gauge are brought into at least partial contact with the formation when the bit is rotated about the rotational axis “B.”
- 27. The bi-center bit of claim 26 where said reamer section defines leading and trailing upsets such that cutting elements positioned about said leading and trailing upsets and extending or proximate to the pass-through gauge define an effective backrake angle of between 45-85° where the effective backrake angle is equal to 180° minus the angle of contact between the cutter face and the material to be drilled and the angle of inclination of the contact surface of the cutting element.
- 28. The bi-center bit of claim 26 further including one or more stabilizer elements disposed opposite said reamer section where the proximal most portion of said elements does not extend beyond the proximal most cutting element on said reamer section.
- 29. A bit adapted to rotate about two or more rotational axes where such bit defines a pass-through gauge, said bit comprising:
a bit body defining a proximal end adapted for connection to a drill string and a distal end, where the distal end defines a pilot bit and an intermediate reamer section, where each the pilot and reamer section define a cutting face; the bit body defining a rotational axis “A” and a pass-through axis “B”; and a plurality of cutting elements situated on cutting blades disposed about the cutting face of the pilot and reamer sections, such that there is substantially complete cutter overlap when said bit is rotated about the rotational or pass-through axis.
- 30. The bit of claim 29 where the cutting elements disposed proximate the pass-through gauge define a high effective backrake angle.
- 31. A method to fabricate a bit which defines at least two axes of rotation, where the bit includes a bit body defining a proximal end adapted to be coupled to the drill string, a distal end, a pilot section and a reamer section, where both said pilot and reamer sections include one or more cutting blades, the method comprising:
defining a rotational axis and a pass-through axis of the bit; and positioning cutting elements on the cutting blades of the pilot and reamer sections such as to create substantially complete cutter overlap when the bit is rotated about either the rotational and pass-through axis.
- 32. The method of claim 31 further including the step of positioning one or more stabilizing elements opposite said reamer section such that the proximal most portion of said stabilizing elements do not extend beyond the most proximal cutting elements disposed on said reamer section.
- 33. The method of claim 31 where said stabilizing element includes a gauge pad.
- 34. The method of claim 31 further including the step of orienting the cutting elements which each define a cutting face such that the cutting face of most of said elements
on cutting blades situated between the rotational and pass-through axes are oriented such that they are brought into contact with the material to be drilled when the bit is rotated about the pass-through axis.
- 35. The method of claim 31 further including the step of orienting the cutting elements which each define a cutting face such that the cutting face of most of said elements on cutting blades situated between the rotational and pass-through axes are oriented such that they are brought into contact with the material to be drilled when the bit is rotated about the rotational axis.
- 36. The method of claim 31 further including the step of orienting the cutting elements which each define a cutting face such that the cutting face of most of said elements on cutting blades situated between the rotational and pass-through axes are oriented such that they are brought into contact with the material to be drilled when the bit is rotated about the rotational axis or the pass-through axis.
- 37. The method of claim 31 further including the step of orienting the cutting elements which each define a cutting face and where the cutting blades include primary and secondary blades, where the rotational and pass-through axes lie substantially along the primary blade such that the cutting faces of substantially all elements disposed along the primary cutting blade not between the rotational axis and pass-through axis but between the pass-through axis and gauge are brought into at least partial contact with the formation to be drilled when said bit is rotated about the rotational axis.
- 38. The method of claim 31 where the reamer section defines one or more blades which extend to pass-through gauge further including the step of positioning cutting
elements on said blades at or near the pass-through gauge so as to from an angle between the material to be drilled and the line of contact on the cutting element where said angle is between 5-45°.
- 39. The method of claim 37 further including the step of positioning the cutting elements on the secondary blades such that they define a skew angle of between 0-80°.
- 40. An eccentric drilling tool comprising:
a bit body defining a proximal end adapted for connection to a drill string a distal end and defining a pass-through gauge, where said distal end terminates in a primary bit face and a secondary bit face spaced proximally from said primary bit face where said primary bit face includes a primary upset and secondary upsets and where one or more cutting elements are disposed about said upsets; said tool defining a rotational axis “A” and a pass-through axis “B”; and where the cutting elements define substantially complete cutter overlap when said tool is rotated about the rotational or pass-through axes.
- 41. The eccentric tool of claim 40 where both of said axes “A” and “B” are disposed about the primary upset.
- 42. The eccentric tool of claim 40 where the cutting elements disposed proximate the pass-through gauge define a high effective backrake angle.
- 43. The eccentric tool of claim 40 where cutting elements disposed along said primary upset between said axis “A” and axis “B” define cutting faces where most of said cutter faces are brought into at least partial contact with the material to be drilled when either the tool is rotated about said pass-through axis “B” or rotational axis “A.”
- 44. A multi-center bit comprising:
a bit body defining a proximal end adapted for connection to a drill string and a distal end, where the distal end defines a pilot bit and an intermediate reamer section, where each the pilot and reamer section define a cutting face which include one or more cutting elements; the bit body defining a rotational axis and at least a second axis; and where said bit when in use defines two distinct bottom hole patterns when rotated about the rotational and the other axis.
- 45. The bit of claim 44 where the bit defines a pass-through gauge and where cutting elements disposed proximate said gauge define a high effective backrake angle.
- 46. The bit of claim 44 which is adapted to consecutively be used to cut through casing equipment and the underlying formation without being removed from the borehole.
- 47. The bit of claim 44 further including one or more stabilizing elements disposed opposite the reamer section such that the proximal most portion of said stabilizing elements do not extend beyond the most proximately disposed elements on the reamer section.
- 48. The bit of claim 44 which is adapted to rotate in casing about an axis separate from the rotational axis so as to not pierce said casing.
- 49. A multi-center bit comprising:
a bit body defining a proximal end adapted for connection to a drill string and a distal end, where the distal end defines a first and a second cutting section, where each said first and second sections define a cutting face; the bit body defining a first and second axis; a plurality of cutting elements situated on cutting blades disposed about the cutting face of the first and second sections; and said bit adapted to consecutively without removal rotate about said axis first within casing without cutting said casing and rotating about second axis within a borehole formed in formation.
- 50. The bit of claim 49 where the rotation of the bit about the first or the second axes defines substantially complete cutter overlap.
- 51. The bit of claim 46 where the rotation of the bit about the first and the second axes creates at least two distinct bottom hole patterns.
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This application depends from and incorporates the subject matter of provisional application Ser. No. 06/118,518 as filed on Feb. 3, 1999.
Provisional Applications (1)
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Number |
Date |
Country |
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60118518 |
Feb 1999 |
US |