Rotary drill bit including a heat-absorbing material for increasing thermal stability of a superabrasive compact
View Patent ↗In an embodiment, a superabrasive compact is disclosed in which a heat-absorbing material having a phase-transition temperature lower than a peak operating temperature of a superabrasive table of the superabrasive compact is positioned in the superabrasive compact. In some embodiments, the heat-absorbing material positioned between the substrate and the superabrasive table. In another embodiment, a rotary drill bit is also disclosed including a bit body and at least one cutting element including a substrate and a superabrasive table bonded to the substrate. At least one heat-absorbing material is positioned within the bit body at least proximate to the at least one cutting element.
1. A rotary drill bit, comprising:
a bit body configured to engage a subterranean formation;
a plurality of superabrasive cutting elements affixed to the bit body, at least one of the plurality of superabrasive cutting elements including:
a substrate;
a superabrasive table bonded to the substrate; and
a heat-absorbing material positioned within a cavity that is at least partially defined by the substrate and completely enclosed by the at least one of the plurality of superabrasive cutting elements, the heat-absorbing material having a phase-transition temperature greater than about 90° C. and less than a temperature at which the at least one of the plurality of superabrasive cutting elements fail.
2. The rotary drill bit of claim 1 wherein the at least one of the plurality of superabrasive cutting elements includes one or more heat pipes embedded therein that thermally couple the superabrasive table and the heat-absorbing material together.
3. The rotary drill bit of claim 2 wherein the one or more heat pipes include a wicking material.
4. The rotary drill bit of claim 1 wherein the cavity is completely enclosed and defined by the substrate and the superabrasive table of the at least one of the plurality of superabrasive cutting elements.
5. The rotary drill bit of claim 1 wherein the cavity is completely enclosed by and defined by the substrate.
6. The rotary drill bit of claim 1 wherein the phase-transition temperature is a liquid-to-gas transition temperature.
7. The rotary drill bit of claim 1 wherein the phase-transition temperature is a solid-to-liquid transition temperature.
8. The rotary drill bit of claim 1 wherein the phase-transition temperature is about 200° C. to about 800° C.
9. The rotary drill bit of claim 1 wherein the at least one of the plurality of superabrasive cutting elements is brazed to the bit body using a braze alloy, the phase-transition temperature of the heat-absorbing material is less than at least one of a solidus or a liquidus of the braze alloy.
10. The rotary drill bit of claim 1 wherein the heat-absorbing material has a heat of fusion of about 20 J/g to about 300 J/g.
11. The rotary drill bit of claim 1 wherein the heat-absorbing material includes at least one material selected from the group consisting of a salt, a hydroxide, a nitrate, a silicate, a metal, an alloy, and a semiconductor.
12. The rotary drill bit of claim 1 wherein the superabrasive table includes polycrystalline diamond.
13. A rotary drill bit, comprising:
a bit body configured to engage a subterranean formation, the bit body defining a plurality of pockets;
a plurality of superabrasive cutting elements, at least one of the plurality of superabrasive cutting elements partially occupying a corresponding one of the plurality of pockets, the at least one of the plurality of superabrasive cutting elements including:
a substrate;
a superabrasive table bonded to the substrate; and
a heat-absorbing material embedded therein and being completely enclosed by the at least one of the plurality of superabrasive cutting elements, the heat absorbing material having a phase-transition temperature greater than about 90° C. and less than a temperature at which the at least one of plurality of superabrasive cutting elements fail.
14. The rotary drill bit of claim 13 wherein the phase-transition temperature is a liquid-to-gas transition temperature.
15. The rotary drill bit of claim 13 wherein the phase-transition temperature is a solid-to-liquid transition temperature.
16. The rotary drill bit of claim 13 wherein the phase-transition temperature is about 200° C. to about 800° C.
17. The rotary drill bit of claim 13 wherein the phase-transition temperature is about 400° C. to about 800° C.
18. The rotary drill bit of claim 13 wherein the heat-absorbing material includes at least one material selected from the group consisting of a salt, a hydroxide, a nitrate, a silicate, a metal, an alloy, and a semiconductor.