Claims
- 1. In a drill bit having a plurality of cutting elements distributed over the profile of the bit, the improvement comprising:
- a facet in the bit profile adjacent each of said cutting elements located in an otherwise curved area of the bit profile, and wherein a number of said cutting elements are mounted in raised wings in said bit profile and said wings are faceted.
- 2. The drill bit of claim 1, wherein said drill bit is a full bore matrix body drag bit.
- 3. In a drill bit having a body defining a cutting face with openings extending into said body for supporting a cutting element in each opening, the improvement comprising:
- a plurality of facets in said body, each of said faces surrounding a corresponding opening for receiving a cutting element, wherein each of said facets is oriented perpendicular to the longitudinal axis of its corresponding opening, and wherein said facets and openings are located in raised cutter supporting wings in said bit body.
- 4. The drill bit of claim 3, wherein said drill bit is a full bore matrix body drag bit.
- 5. In a method of producing a matrix body bit including the steps of forming a pattern, placing the pattern in a setable mud, removing the pattern, hardening the mud to form a bit mold, attaching a plurality of cores to the mold surface to create openings in the resultant matrix bit body for mounting cutter elements, forming a matrix bit body in said mold using an infiltration process, and mounting cutter elements in the openings formed by said cores, the improvement comprising the step of:
- forming a plurality of small flat surfaces in the exterior of said pattern with each of said flat surfaces corresponding to the location whereat at least one of said cores is to be attached to said mold.
- 6. The method of claim 5, wherein each of said small flat surfaces is perpendicular to the longitudinal axis of the corresponding core.
- 7. The method of claim 6, wherein said cutter elements are located in raised wings in said bit body and said small flat surfaces lead to the formation of facets in said wings.
- 8. A pattern formed in accordance with the method of claim 5.
- 9. A mold formed in accordance with the method of claim 5.
- 10. A matrix bit formed in accordance with the method of claim 5.
- 11. A method of forming a plurality of small surfaces in a bit pattern comprising the steps of:
- scribing a cutter location point on the pattern surface,
- rotating the pattern to the angle of the flat surface,
- centering over the scribed cutter location,
- replacing the scribing tool with a mill tool,
- touching off of the pattern surface to determine zero depth, and
- plunging the mill tool to about 0.095 of an inch and running it out in all directions.
- 12. The method of claim 11, wherein inner flat surfaces are cut before outer flat surfaces to prevent removal of location points prior to machining.
- 13. In a pattern for forming a mold for a matrix body bit having one or more raised wings for supporting a plurality of cutter elements, the improvement comprising:
- a plurality of facets in said wings, each of said facets corresponding to the location of at least one of said cutter elements.
- 14. The pattern of claim 13, wherein said cutter elements are stud mounted and each of said facets is perpendicular to the longitudinal axis of the stud of the corresponding cutter element.
- 15. In a mold for forming a matrix body bit having one or more raised wings for supporting a plurality of cutter elements, the improvement comprising:
- a plurality of flats in the wing forming surfaces, each of said flats corresponding to the location for attachment of at least one core.
- 16. The mold of claim 15, wherein each of said flats is at a common angle with respect to the longitudinal axis of its corresponding core.
- 17. In a method of producing a matrix body bit, the improvement comprising the step of:
- using a bit pattern having faceted wings.
- 18. In a method of producing a matrix body bit, the improvement comprising the step of:
- using a mold having flats for producing a bit body having faceted wings.
- 19. In a matrix body bit having one or more raised wings for supporting a plurality of cutter elements, the improvement comprising:
- a plurality of facets in said wings, each of said facets corresponding to the location of at least one of said cutter elements.
- 20. The matrix body bit of claim 19, wherein said bit is a full bore drag bit and said cutter elements are stud mounted PDC cutters.
- 21. In a method of producing a matrix body bit including the steps of forming a bit mold, attaching a plurality of cores to the inner mold surface to create openings in the resultant matrix bit body for mounting cutter elements, forming a matrix bit body in said mold using an infiltration process, and mounting cutter elements in the openings formed by said cores, the improvement comprising the step of:
- forming a plurality of small flat surfaces in the inner surface of said mold with each of said flat surfaces corresponding to the location whereat at least one of said cores is to be attached to said mold.
- 22. The method of claim 21, wherein each of said small flat surfaces is perpendicular to the longitudinal axis of the corresponding core.
- 23. The method of claim 21, wherein said cutter elements are located in raised wings in said bit body and said small flat surfaces lead to the formation of facets in said wings.
- 24. The method of claim 21, wherein said mold is a hard mold and said step of forming a plurality of flat surfaces includes machining said flat surfaces.
- 25. The method of claim 21, wherein said mold is a soft mold and said step of forming a plurality of flat surfaces includes using a pattern having corresponding flat surfaces to form said mold.
- 26. A mold formed in accordance with the method of claim 21.
- 27. A matrix body bit formed in accordance with the method of claim 21.
CROSS-REFERENCE TO RELATED APPLICATIONS
This application is a continuation-in-part of application Ser. No. 07/523,235, filed on May 11, 1990, now abandoned.
US Referenced Citations (14)
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
523235 |
May 1990 |
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