This relates drill bits, and methods of dressing drill bits with hard surfaces.
PDCs are used to provide a hard working surface on drill bits or mills that may be used in downhole operations. Poly-crystalline diamond cutters (PDCs) are well known and often used in the manufacture of drill bits suitable for the above mentioned applications.
Due to the immense stress forces encountered during drilling, PDCs installed on drill bits typically become irreparably damaged during use and must be replaced to ensure the efficacy of drill bits. Installing PDCs on a drill bit, whether the first time or when refreshing the drill bit, may be referred to as dressing the drill bit. The PDCs are installed to enhance the strength of the bond between the PDCs and the drill bit in order to prevent their breakage or removal during use, taking into consideration the time required to install the PDCs.
An example of a drill bit that uses PDCs is depicted in U.S. Pat. No. 9,811,630 entitled “Multilevel force balanced downhole drilling tools and methods”.
According to an aspect, there is provided a method of installing cutters on a drill bit, the method comprising the steps of providing a drill bit body having an outer surface, the outer surface comprising a surface profile that is adapted to receive and support a plurality of cutting elements, installing cutting elements on the outer surface of the drill bit body such that the surface profile supports the plurality of cutting elements in a desired orientation, each cutting element comprising a substrate comprising a rear end, a leading end that carries a cutting portion, and a cylindrical surface that extends between the rear end and the leading end, the cutting elements being installed such that a portion of the substrate is exposed and the leading end leads the cutting element in a direction of rotation of the drill bit body, binding the cutting elements on the outer surface of the drill bit body by applying a composite to the outer surface and to the portion of the substrate that is exposed, the composite comprising a mixture of a matrix and cutting fragments and wherein the composite is in direct contact with about 40-75%% of a surface area of the substrate.
According to other aspects, the method may comprise one or more of the following features, alone or in combination: wherein the surface profile may comprise a plurality of indents, and the step of installing cutting elements on the outer surface may comprise placing the cutting elements within the plurality of indents; the composite may be applied between adjacent cutting elements; the cutting fragments may comprise cutting portion fragments carried by substrate fragments; the substrate may comprise carbide and the cutting portion comprises poly-crystalline diamond; and the composite may be in direct contact with about 45-55% of the surface area of the substrate.
According to an aspect, there is provided a drill bit, comprising a drill bit body having an outer surface, the outer surface comprising a surface profile that is adapted to receive and support a plurality of cutting elements, cutting elements installed on the outer surface of the drill bit body such that the surface profile supports each cutting element in a desired orientation, each cutting element comprising a substrate comprising a rear end, a leading end that carries a cutting portion, and a cylindrical surface that extends between the rear end and the leading end, the cutting elements being installed such that the a portion of the substrate is exposed and the leading end leads the cutting element in a direction of rotation of the drill bit body, and a composite applied to the outer surface and to the portion of the substrate that is exposed, the composite comprising a mixture of a matrix and cutting fragments, wherein the composite binds the cutting elements to the outer surface of the drill bit body and the composite is in direct contact with about 40-75% of a surface area of the substrate.
According to other aspects, the drill bit may comprise one or more of the following features, alone or in combination: the surface profile may comprise a plurality of indents sized to receive one cutting element; the composite may be applied between adjacent cutting elements; the cutting fragments may comprise cutting portion fragments carried by substrate fragments; the substrate may comprise carbide and the cutting portion comprises poly-crystalline diamond; and the composite may be in direct contact with about 45-55% of the surface area of the substrate.
According to an aspect, there is provided a method of replacing cutting elements on a drill bit, the method comprising the steps of heating a drill bit body that has used cutting elements bound to an outer surface of the drill bit body by a composite, the used cutting elements engaging the outer surface such that a surface profile of the outer surface of the drill bit body supports each cutting element, the composite comprising a mixture of a matrix and cutting fragments, wherein at least a portion of the cutting elements are spent cutting elements, removing the composite from the spent cutting elements to unbind spent cutting elements, installing replacement cutting elements to replace the removed spent cutting elements, and binding the replacement cutting elements to the outer surface by applying composite to about 40-75% of a substrate of the replacement cutting elements.
According to other aspects, the method may comprise one or more of the following features, alone or in combination: the replacement cutting elements may be cylindrical and may comprise a substrate having a rear end and a leading end that carries a cutting portion, the replacement cutting elements being installed such that the substrate engages the outer surface with a portion of the substrate exposed and the leading end leads the replacement cutting element in a direction of rotation of the drill bit body; and composite may be applied to about 45-55% of the surface area of the substrate of the replacement cutting elements.
In other aspects, the features described above may be combined together in any reasonable combination as will be recognized by those skilled in the art.
These and other features will become more apparent from the following description in which reference is made to the appended drawings, the drawings are for the purpose of illustration only and are not intended to be in any way limiting, wherein:
A drill bit, generally identified by reference numeral 10, will now be described with reference to
Referring to
Referring to
When installed in indent 16, a portion of the surface area of cutter 20 is exposed, which includes a portion of the sidewall, and may include a portion of rear end 25. Surface profile 18 may be configured such that cutting elements 20 are oriented at a specific angle relative to a rotational axis of drill bit 10, or positioned at a specific distance from the rotational axis. In this manner, the cutting action of drill bit 10 may be defined based on the portion of drill bit 10 that engages the material being drilled. For example, the leading face of drill bit 10 may have a different cutting action than on the sides of drill bit 10.
As shown, cutting portions 22 may have flat front faces on leading end 26 that cooperate with adjacent cutting elements 20 to act as a cutting edge 28 on drill bit 10. Cutting edge 28 may be adjacent to a channel 30 formed in outer surface 14 that allows drilled materials to flow out of the way of drill bit 10. Channels 30 may include ports 32 that allow drilling fluid to be circulated during a drilling or milling operation. Cutting elements 20 may have different shapes and sizes on the same drill bit 10, and may have different orientations relative to outer surface 14 or axis rotation of drill bit body 12. Cutting portion 22 and substrate 24 may be made from poly-crystalline diamond and a carbide such a tungsten carbide, respectively. Other suitable materials know in the art may be used.
Referring to
Referring to
Installing composite 40 may involve heating composite 40 until matrix 42 melts and then applying it to outer surface 14 such that composite 40 sufficiently coats outer surface 14 and the exposed portions of substrate 24. Once cooled composite 40 binds cutting elements 20 to outer surface 14. Composite 40 may be applied such that it is in direct contact with around 50% of a surface area of the substrate of cutting elements 20. Composite may be applied such that it is in direct contact with up to about 75% of the surface area of substrate 24, or as little as 40%. The surface area of substrate 24 may be considered to be the rear face of substrate 24 and the sidewall, and typically does not include cutting portion 22. Composite 40 may be localized around cutting elements 20, or it may be applied to the entire outer surface 14 of drill bit 10. Cutting fragments 44 strengthen matrix 42 and allows a thicker layer of composite 40 to be applied relative to matrix alone.
Referring to FIG, composite 40 may be applied so that some or all of cutting portion 22 of cutting elements 20 is exposed. If cutting portion 22 is covered during manufacturing, it will typically wear off to expose cutting portion 22 during use. The thickness of composite 40 may be vary depending on the location on outer surface 14, but is applied thinly enough that it does not interfere with operation of cutting element 20 while acting as a secondary cutting surface.
Drill bit 10 may have different zones on it with different binding conditions for cutting elements 20 within each zone. This may include the position and orientation of cutting elements 20, the type and/or thickness of composite 40. For example, cutting elements 20 may be mounted to indents 16 and bound by composite 40 in certain zones, while in other zones, cutting elements 20 may be oriented such that the plane of cutting portions 22 are aligned with the cutting surface of drill bit 10, such as to act as a bearing surface to center drill bit 10, in which case cutting elements 20 may not be bound to indent 16 using composite 40.
Methods of installing cutter elements 20 and replacing spent cutting elements 20 will now be described.
Referring to
Once cutting elements 20 are installed, composite 40 is applied to outer surface 14 and the exposed portion of substrate 24 of cutting elements 20 to bind cutting elements on outer surface 14, where composite 40 may be heated above a melting point of matrix 42, such as in the range of 400° C.-700° C., which may depend on the melting point of composite 40, and then applied. This may be done such that composite 40 is in direct contact with about 50% of the surface area of substrate 24, or between about 25-60% of the surface area.
During operations, cutting elements 20 may become spent and lose their cutting efficacy, cutting surface 22 may break away from cutting element 20, or cutting element 20 may break away from drill bit 10. Spent or broken cutting elements 20 may be refreshed or replaced by dressing drill bit 10.
To unbind spent cutting elements, drill bit 10 may be heated to a temperature sufficient to allow removal of composite 40 from substrate 24 of cutting elements 20. All of drill bit 10 may be heated, such as with an induction oven, or only small portions of composite 40 and/or outer surface 14 may be heated, such as with torches, to remove the portion that binds cutting elements 20 to drill bit 10. Once composite 40 has been removed, spent cutting elements 20 may be removed from outer surface 14 and refreshed. Refreshing cutting elements 20 may include completely replacing cutting elements 20 or rotating cutting elements such that an unworn edge of cutting portion 22 becomes the working edge of cutting element 20. This may be done multiple times. For example, cutting elements may be refreshed in this way 2 or more times. Other cutting elements 20 that remain functional and are not spent may be left alone. Composite 40 is then reapplied to bind the new cutting elements 20 within to outer surface 14. Heating only composite 40 to refresh cutting elements 20 may extend the life of drill bit body 12 by reducing the frequency and severity of heating cycles when changing cutting elements 20.
Composite 40 may be the primary holding force for cutting elements 20 and any solder applied to tack cutting elements 20 in place may be insufficient alone to support cutting element during normal operation. In addition, composite 40 acts as a wear surface and protective layer for drill bit body 12. By providing a thick layer of composite 40, or by having cutting elements 20 extend further out from indents 16, the amount of wear experienced by drill bit body 12 and indents 16 may be reduced or avoided, such that the amount of redressing required to build up drill bit body 12 around new cutting elements 20 is also reduced or avoided.
Some pockets may receive less than half the radius of the back of the cutter substrate; preferably less than half the surface area, depending on orientation of the pocket. This may apply to be some, but not all, cutters.
In this patent document, the word “comprising” is used in its non-limiting sense to mean that items following the word are included, but items not specifically mentioned are not excluded. A reference to an element by the indefinite article “a” does not exclude the possibility that more than one of the elements is present, unless the context clearly requires that there be one and only one of the elements.
The scope of the following claims should not be limited by the preferred embodiments set forth in the examples above and in the drawings, but should be given the broadest interpretation consistent with the description as a whole.
Number | Date | Country | Kind |
---|---|---|---|
CA 3161043 | May 2022 | CA | national |
Number | Name | Date | Kind |
---|---|---|---|
3187739 | Du Fresne | Jun 1965 | A |
3666185 | Williams | May 1972 | A |
4721356 | Lyman | Jan 1988 | A |
4962893 | Bochmann et al. | Oct 1990 | A |
5049164 | Horton et al. | Sep 1991 | A |
5385307 | Azar | Jan 1995 | A |
6824086 | Mazurkiewicz et al. | Nov 2004 | B1 |
7234550 | Azar et al. | Jun 2007 | B2 |
7297418 | Watson | Nov 2007 | B2 |
7416141 | Dobbs | Aug 2008 | B2 |
8079428 | Lyons et al. | Dec 2011 | B2 |
20040110395 | Ueda et al. | Jun 2004 | A1 |
20060217258 | Zhao | Sep 2006 | A1 |
20080029625 | Talton | Feb 2008 | A1 |
20090170414 | Ferrell et al. | Jul 2009 | A1 |
20110000715 | Lyons | Jan 2011 | A1 |
20140246249 | Cheng | Sep 2014 | A1 |
20200291726 | Lyles et al. | Sep 2020 | A1 |
Number | Date | Country |
---|---|---|
2276473 | Dec 2000 | CA |
2005562 | Apr 1979 | GB |
2073048 | Oct 1981 | GB |
2009061353 | May 2009 | WO |
Number | Date | Country | |
---|---|---|---|
20230265717 A1 | Aug 2023 | US |
Number | Date | Country | |
---|---|---|---|
63311860 | Feb 2022 | US |