Hybrid drill bit having increased service life
View Patent ↗A method of improving the service life of a drill bit comprises creating a weldment between load bearing portions of the drill bit where the weldment has a preselected root gap greater than about 25 mils and a preselected root face greater than about 25 mils, and where the weldment has a material property greater than the materials being joined.
1. A method of manufacturing a drill bit, comprising:
selecting a root gap dimension of between about 25 mils and about 60 mils;
selecting a root face dimension about equal to or less than the selected root gap;
establishing a root gap having the selected root gap dimension between a drill bit module and a drill bit body; and creating a multi-pass weldment between the module and the body having the selected root gap and root face dimensions and from weldment material having at least one material property greater in value than the same material property of the materials being joined; wherein the root face dimension is less than a dimension between the drill bit module and the drill bit body.
2. The method of claim 1 , wherein the root gap is between about 30 mils and about 50 mils.
3. The method of claim 1 , wherein the root face is between about 25 mils and 60 mils and is about equal to or less than the root gap.
4. The method of claim 1 , wherein the material property is tensile strength.
5. The method of claim 1 , wherein the material property is fatigue strength.
6. The method of claim 1 , further comprising forming in the body a cavity configured to receive the module and establish the selected root gap and root face.
7. The method of claim 6 , further comprising locating the module in the body prior to creating the weldment, adjusting the module in the cavity to establish a desired projection and attaching the module to the body with at least one threaded fastener.
8. The method of claim 6 , further comprising
placing the drill bit module in the cavity; and
positioning the module in the cavity to establish the root gap.
9. The method of claim 8 , wherein positioning the module in the cavity to establish the root gap comprises moving the module in an axial direction, or in a radial direction, or in both axial and radial directions.
10. The method of claim 1 , further comprising maintaining a weldment interpass temperature of less than about 400° F.
11. The method of claim 10 , further comprising maintaining a weldment interpass temperature of about 300° F.
12. A modular drill bit, comprising:
a weldment joining at least one module to a drill bit body; the weldment having a preselected root gap dimension of between about 25 mils and about 60 mils and a preselected root face dimension greater than about 25 mils and equal to or less than the selected root gap dimension; and the weldment having at least one material property greater in value than a material property of the materials being joined; wherein the root face dimension is less than a dimension between the at least one module and the drill bit body.
13. The bit of claim 12 , wherein the root gap is between about 30 mils and about 50 mils.
14. The bit of claim 12 , wherein the root face is between about 25 mils and 60 mils.
15. The bit of claim 12 , wherein the material property is tensile strength.
16. The bit of claim 12 , wherein the material property is fatigue strength.
17. The bit of claim 12 , further comprising a cavity formed in the body and configured to receive the module and establish the selected root gap and root face.
18. The bit of claim 17 , wherein the cavity is configured to allow axial, or radial, or axial and radial positioning of the drill bit module prior to creating the weldment.
19. The bit of claim 12 , further comprising a weldment interpass temperature of less than about 400° F.
20. The bit of claim 19 , further comprising a weldment interpass temperature of about 300° F.
21. A hybrid drill bit, comprising:
a bit body having at least one cutter blade and at least one portion formed in the bit body and configured to receive a roller cutter assembly leg;
a roller cutter assembly leg attached to the bit body at the body portion with at least one threaded fastener;
a multi-pass weldment joining the roller cutter assembly to the bit body and formed with a weldment interpass temperature of about 300° F. or less;
the weldment having a preselected root gap dimension greater than about 25 mils and a preselected root face dimension greater than about 25 mils and equal to or less than the selected root gap dimension; and
the weldment having a tensile strength greater than a tensile strength of either the bit body material or the roller cutter assembly material.