In various fields such as earth-boring, road milling, mining and trenching it is often desirable to engage and degrade tough materials such as rock, asphalt, or concrete. To do so, cutting elements may be coupled to a movable body that may bring the cutting elements into contact with a material to be degraded as the body moves. For example, when exploring for or extracting subterranean oil, gas, or geothermal energy deposits, a plurality of cutting elements can be secured to a drill bit attached to the end of a drill sting. As the drill bit is rotated, the cutting elements may degrade a subterranean formation forming a wellbore, which allows the drill bit to advance through the formation. In another example, when preparing an asphalt road for resurfacing, cutting elements can be coupled to tips of picks that may be connected to a rotatable drum. As the drum is rotated, the cutting elements may degrade the asphalt leaving a surface ready for application of a fresh layer.
The cutting elements used in such applications often include super-hard materials, such as polycrystalline diamond, sintered to a substrate material in a high-pressure, high-temperature environment. These cutting elements, like those described in U.S. Pat. No. 7,726,420 to Shen et al., may include a cutting edge formed in the super-hard material designed to scrape against and shear away a surface. While effective in cutting formation or other materials, such cutting elements may be susceptible to chipping, cracking, or partial fracturing when subjected to high forces.
In accordance with some embodiments, a cutting element includes a substrate that is axially symmetric about a central axis thereof. The substrate has a radius perpendicular to the central axis and which extends from the central axis to an outer surface of the substrate. A super-hard material is coupled to the substrate, and the central axis passes through the super-hard material. The super-hard material has an external surface defining at least one ridge protruding from a remainder of the external surface. A central point on the central axis is offset from the external surface of the super-hard material by a distance equal to the radius of the substrate. A distance measured from the external surface of the super-hard material to the central point is greatest at a position between 25° and 45° from the central axis of the substrate.
According to some embodiments, a cutting element may include a substrate that is axially symmetric about its central axis. A super-hard material may be bonded to a side of the substrate such that the central axis passes through the super-hard material. An external surface of the super-hard material may include a geometry designed to increase the cutting element's resistance to high forces. Specifically, a distance, measured from the external surface of the super-hard material to a central point, may be greatest at an angle from the central axis of the substrate. The central point may be located on the central axis and sit a length from the external surface along the central axis equal to a radius of the substrate.
In further example embodiments, an external surface of the super-hard material may include a ridge protruding from a remainder of the external surface. In various embodiments, the ridge may intersect the central axis of the substrate, be generally perpendicular to the central axis of the substrate, or be generally convex over a maximum length thereof. In some embodiments, a plurality of ridges may extend from a common center that may fall on the central axis of the substrate with the ridges equally spaced around the common center. In some embodiments, the distance measured from the external surface of the super-hard material to the central point is greatest at more than one positions optionally between 25° and 45° from the central axis of the substrate.
A thickness of the super-hard material may also be designed to increase the cutting element's resistance to high forces. For instance, a thickness, measured from the external surface of the super-hard material to an interface between the super-hard material and the substrate along a line passing through the central point, may be greatest at a position between 25° and 45° from the central axis of the substrate. Beyond this position between 25° and 45° from the central axis of the substrate, a portion of the external surface may take the form of part of a cone shape or ogive shape. Additionally, a boundary between the ridge and the cone shape or ogive shape may include a chamfer.
In some embodiments, the substrate may have an elevated portion protruding into the super-hard material and extending radially to a position between 25° and 45° from the central axis of the substrate from the central point. In some embodiments, a thickness of a transition region between the super-hard material and the substrate may have a substantially constant thickness regardless of thickness of the super-hard material.
A cutting element of the present disclosure may be coupled to a drill bit or pick. When secured to a drill bit or pick, to control the aggressiveness of each cutting element, a ridge on each cutting element may be positioned between 0° and 70° relative to a formation. Further, the ridge on each cutting element may be positioned parallel, non-parallel, or perpendicular to a direction of rotation.
In some embodiments, an external surface of the super-hard material 363 may include or define a ridge 370 or other feature that is generally perpendicular to the axis 362. A central point 364 may be identified at a position along the axis 362 at a distance from an external surface of the super-hard material 363 that is equal to the distance between the axis 362 and the outer surface of the substrate 361. For instance, the central point 364 may be on the axis 362 and axially offset from the ridge 370 by a distance equal to the radius (or half-width) of the substrate 361. In some embodiments, a greatest distance 365 measured from an external surface of the super-hard material 363 to the central point 364 may be oriented at an angle 366 from the axis 362. In some embodiments, the angle 366 may be between 10° and 60°. For instance, the angle 366 may be within a range having lower, upper, or both lower and upper limits including any of 10°, 20°, 25°, 30°, 40°, 45°, 50°, 60°, and values therebetween. In particular examples, the angle 366 may be between 20° and 50°, between 25° and 45°, or between 30° and 40°. In still other embodiments, the angle 366 may be less than 25° or greater than 45°.
As can be seen in the illustrated embodiment, the greatest distance 365 may optionally be found at more than one point around a perimeter of the super-hard material 363. In at least some embodiments, including multiple locations at which the greatest distance 365 is present may allow for the super-hard material 363 to have one, two, or more axes of symmetry, or otherwise be re-usable. For instance, the cutting element 360 may be used to degrade a material with the cutting element 360 in an orientation that primarily uses a portion of the cutting element 360 associated with one point having the greatest distance 365. Thereafter, the cutting element 360, hardened tip 306, or pick 302 may be removed and rotated to expose a fresh section of the ridge 370 (e.g., in the event the first cutting portion chips, cracks, dulls, etc.).
The thickness of the super-hard material 363 may be measured from the external surface of the super-hard material 363 to an interface between the super-hard material 363 and the substrate 361, along a line passing through the central point 364. In some embodiments, the thickness of the super-hard material 363 may be constant within the super-hard material 363. In other embodiments, the thickness may vary. For instance, a thickness of the super-hard material 363 is optionally greatest along the line defining the greatest distance 365. In other embodiments, the thickness of the super-hard material 363 may be greatest along a line that is offset from the line defining the greatest distance 365. In at least some embodiments, the thickness of the super-hard material 363 is greatest along a line between 0° and 90° from the axis 362. For instance, the angle of the line associated with the greatest thickness may be within a range having lower, upper, or both lower and upper limits including any of 0°, 15°, 25°, 35°, 45°, 55°, 60°, 75°, 90°, and values therebetween. In particular examples, such an angle may be between 15° and 75°, between 25° and 45°, or between 30° and 40°.
In some embodiments, the ridge 370 may have a generally constant height, such that the outer edge in the cross-sectional view in
As can also be seen in the embodiment shown in
In some embodiments, the substrate 361 may include an elevated portion 368. The elevated portion 368 may protrude into the super-hard material 363, such that a radial line perpendicular to the axis 362 would extend through at least a portion of the super-hard material 363. In some embodiments, the elevated portion 368 extends radially to a position between 0° and 90° from the axis 362 of the substrate 361 as measured from the central point 364. For instance, the elevated portion 368 may extend radially to an angular position that is within a range having lower, upper, or both lower and upper limits including any of 0°, 15°, 25°, 35°, 45°, 55°, 60°, 75°, 90° and values therebetween, from the axis 362 of the substrate 361, as measured from the central point 364. In particular examples, such an angle may be between 15° and 75°, between 25° and 45°, or between 30° and 40°.
In the illustrated embodiment, an external surface of the super-hard material 463 includes a ridge 470 that protrudes from the substrate 461 and which is optionally tapered or otherwise contoured over its length across a width of the cutting element 460. For instance, the ridge 470 may be generally convex over its maximum length. As can be seen in
Additionally, in the illustrated embodiment, the substrate 461 optionally includes an elevated portion 468 having a depression 469 therein. The depression 469 may be centered along the axis 462 in some embodiments, and may be symmetrical such that the substrate 461 is symmetrical about the axis 462. In other embodiments, the depression 469 may be asymmetric.
The substrate 761, 961 may have a substantially cylindrical shape, such that the common center 771, 871 lies on a central axis 962 of the cylindrical shape. The ridges 770, 870 may intersect the axis 962 and may be equally or unequally angularly spaced around the common center 771, 871. In some embodiments, the ridges 770, 870 may be generally perpendicular to the axis 962, angled at a non-perpendicular angel relative to the axis 962, or generally convex or concave over a maximum length thereof. Each of the ridges 770, 870 may have a radius of curvature 951. In some embodiments, the radius of curvature 951 may be between 0.02 inch (0.51 mm) to 0.35 inch (8.89 mm) when viewed along a length of the corresponding ridge (e.g., perpendicular to the axis 962). For instance, the radius or curvature 951 of a ridge may be within a range having a lower, upper, or both lower and upper limits including any of 0.02 inch (0.51 mm), 0.05 inch (1.27 mm), 0.10 inch (2.54 mm), 0.20 inch (5.08 mm), 0.25 inch (6.35 mm), 0.30 inch (7.62 mm), 0.35 inch (8.89 mm), or values therebetween. For instance, in some embodiments, the radius of curvature 951 of a ridge may be less than 0.25 inch (6.35 mm), greater than 0.05 inch (1.27 mm), between 0.03 inch (0.76 mm) and 0.30 inch (7.72 mm), between 0.05 inch (1.27 mm) and 0.25 inch (6.35 mm), or may be 0.105 inch (2.67 mm). In other embodiments, the radius or curvature 951 of a ridge may be less than 0.02 inch (0.51 mm) or greater than 0.35 inch (8.89 mm).
In some embodiments, one or more ridges 770, 870 may further have an additional radius of curvature 952 when viewed perpendicular to the length of the ridge 770, 879, and perpendicular to the axis 952. The radius or curvature 952 may, in some embodiments, be convex or concave, and may be between 0 inch (0 mm) and 5 inches (127 mm). For instance, For instance, the radius or curvature 952 of a ridge may be within a range having a lower, upper, or both lower and upper limits including any of 0.000 inch (0.00 mm), 0.025 inch (0.64 mm), 0.050 inch (1.27 mm), 0.075 inch (1.91 mm), 0.100 inch (2.54 mm), 0.200 inch (5.08 mm), 0.500 inch (12.7 mm), 1.000 inch (25.4 mm), 2.500 inches (63.5 mm), 5.000 inches (127 mm), or values therebetween. For instance, in some embodiments, the radius of curvature 952 of a ridge may be less than 3.000 inches (76.2 mm), greater than 0.075 inch (1.91 mm), between 0.050 inch (1.27 mm) and 4.000 inches (101.6 mm), between 0.075 inch (1.91 mm) and 3.000 inches (76.2 mm), or may be 1.790 inches (45.47 mm). In other embodiments, the radius or curvature 952 of a ridge may greater than 5 inches (127 mm).
In some embodiments, the super-hard material 763, 863, 963 may include a generally conical or ogive periphery 748, 848. The periphery 748, 848 may be positioned, for instance, radially beyond a position between 25° and 45° from the axis 962, although the periphery 748, 848 may be positioned less than 25° or greater than 45° from the axis 962 in other embodiments. The periphery 748, 848 may narrow in a direction extending from adjacent the interface between the substrate 761, 961 and the super-hard material 763, 863, 963 toward a distal end of the super-hard material 763, 863, 963. A boundary between each of the ridges 770, 870 and the periphery 748, 848 may, in some embodiments, include a transition such as a fillet, round, or chamfer 773, 873. One or more, and potentially each, of the ridges 770, 870 may optionally include an arched exterior culminating at a generally planar surface or linear edge, and curving on either side of each ridge toward the substrate 761, 961. Further, each arched exterior may include a similar radius of curvature relative to the radius of curvature of each other arched exterior. The ridges 770, 870 may extend from the common center 771, 871 to the periphery 748, 848 where a transition may connect each of the ridges 770, 879. The transition between each of the ridges 770, 870 and the periphery 748, 848 may include a chamfer, although in some embodiments the transition may be curved. For instance, a radius of curvature 953 between a ridge 770, 870 and the periphery 748, 848 may be between 0.020 inch (0.51 mm) and 0.150 inch (3.81 mm) when viewed perpendicular to a ridge and perpendicular to the axis 962, as shown in
The periphery 748, 848 itself may be linear, or may include a concave or convex radius of curvature 954. In some embodiments, the radius of curvature may be convex and may be between 0.075 inch (1.91 mm) to 3.000 inches (76.2 mm) when viewed perpendicular to a ridge and perpendicular to the axis 962, as shown in
Further, when viewed in cross-section or as a side view, the periphery 748, 848 may extend at an angle 955 relative to the axis 962, as seen in
In the embodiments shown in
In some embodiments, the surfaces 749, 849 leading up to each of the adjacent ridges 770, 870 may define or have a radius of curvature 956 when viewed along a ridge perpendicular to the axis 962. According to at least some embodiments, the radius of curvature 956 may be between 0.050 inch (1.27 mm) and 3.000 inches (76.2 mm), or between 0.500 inch (12.7 mm) and 2.000 inches (50.8 mm). For instance, the radius of curvature 956 may be 1.000 inch (25.4 mm). In other embodiments, the radius of curvature 956 may be less than 0.05 inch (1.27 mm) or greater than 3.000 inches (76.2 mm).
In some further embodiments, the surfaces 749, 849 on either side of a furrow 747, 847 may form an angle 957 with a surface opposite each of the ridges 770, 870 when viewed along the ridge and perpendicular to the axis 962, as shown in
As shown, each of the depressions 772, 872 may diverge from adjacent ridges 770, 870 and extend a similar depth toward the substrate 761, 961. In addition, each of the furrows 747, 847 may extend radially outwardly from the common center 771, 871 and extend further toward the substrate 761, 961 in a radially outward direction. In other embodiments, one or more depressions 772, 872 may have a different depth, or a furrow 747, 847 may extend radially inwardly at one or more locations along a length thereof.
Any number of cutting elements or inserts 1220, 1230, and 1240 may be coupled to, or otherwise disposed on the bit face 1214, and the elements 1220, 1230, and 1240 may be arranged in any number of manners, configurations, patterns, and the like. Moreover, the inserts 1220, 1230, and 1240 themselves may have any number of different shapes, forms, constructions, or other characteristics. In some embodiments, the inserts 1220 are chisel-type inserts. Embodiments of chisel-type cutters 1220 are shown in and described with respect to
In some embodiments, inserts 1230 are pointed-type (e.g., conical) cutting elements.
In some embodiments, inserts 1240 are domed inserts.
In some embodiments, the center region 1220 of the bit 1210 includes at least one pointed cutting element 1230. A pointed cutting element in the center region may bear on-axis impact on the small-radius cutting tip to crush and gouge the formation. Domed-type inserts 1240 may be found within the center region, the gage region, both, or neither.
In some embodiments, gage region 1218 may include at least one chisel-type cutting element 1220. A chisel-type cutting element may have durability similar to domed inserts, but with increased crushing, penetration, and cutting efficiency. A chisel-type insert may allow for a sharper radius to cut in the forward direction of the bit, and may further have a sharp radius to cut the gage or at the side of the bit. In addition, a chisel-type cutting element may exhibit increased resistance to off-axis impact forces, such as those that may be experienced in the gage region, as compared to pointed-type cutting elements.
The cutting element(s) 1220 may be oriented within the gage region for maximum impact resistance and rock fragmentation. For example, the cutting element 1220 may be rotated to orient the ridge or chisel feature perpendicular to the direction of rotation of the drill bit. In other embodiments, the chisel/ridge may be oriented at an angle that is not perpendicular to the direction of rotation, such as at +/−45° relative to the direction of rotation and/or the formation hole wall. Combinations of orientations of multiple chisel-type cutters in the gage region may help promote crack formation or cause larger chip to be removed by the cutters. For example, chisel-type cutters may be oriented at alternating +θ degrees/−θ degrees, where 0<θ<90 (forming a “W” type pattern), which may facilitate more efficient crack formation and crack propagation with the crack tips intersecting to form large chips.
In the same or other embodiments, a ridge or chisel type insert 1220 may be tilted so that the axis of the insert is not parallel to the bit axis.
In some embodiments, the center region of the bit face includes a plurality of pointed-type elements, and the gage region includes a plurality of chisel-type elements. This configuration may provide increased rate of penetration (ROP) relative to using smaller-radius pointed inserts or larger-radius domed inserts, as crushing and penetration can be increased while durability can be maintained by including chisel cutters in regions where inserts may experience greater off-axis loads. In some embodiments, pointed-type cutters are used in areas that experience primarily on-axis loads, while chisel-type cutters are used in areas that experience off-axis loads.
While embodiments of cutting elements and cutting tools have been primarily described with reference to drilling, road milling, and mining operations, the devices described herein may be used in applications other than the drilling, mining, or road milling. In other embodiments, cutting elements and cutting tools according to the present disclosure may be used outside a wellbore, mining, or road milling environment. For instance, tools and assemblies of the present disclosure may be used in a wellbore used for placement of utility lines, in a medical procedure (e.g., to clear blockages within an artery), in a manufacturing industry (e.g., to expand a diameter of a bore within a component), in other industries (e.g., aquatic, automotive, etc.), or in a wellbore enlargement application (e.g., with an underreamer).
The articles “a,” “an,” and “the” are intended to mean that there are one or more of the elements in the preceding descriptions. The terms “comprising,” “including,” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements. Additionally, it should be understood that references to “one embodiment” or “an embodiment” of the present disclosure are not intended to be interpreted as excluding the existence of additional embodiments that also incorporate the recited features. Numbers, percentages, ratios, or other values stated herein are intended to include that value, and also other values that are “about” or “approximately” the stated value, as would be appreciated by one of ordinary skill in the art encompassed by embodiments of the present disclosure. A stated value should therefore be interpreted broadly enough to encompass values that are at least close enough to the stated value to perform a desired function or achieve a desired result. The stated values include at least the variation to be expected in a suitable manufacturing or production process, and may include values that are within 5%, within 1%, within 0.1%, or within 0.01% of a stated value. Where a range of values includes various lower or upper limits, any two values may define the bounds of the range, or any single value may define an upper limit (e.g., up to 50%) or a lower limit (at least 50%).
A person having ordinary skill in the art should realize in view of the present disclosure that equivalent constructions do not depart from the spirit and scope of the present disclosure, and that various changes, substitutions, and alterations may be made to embodiments disclosed herein without departing from the spirit and scope of the present disclosure. Equivalent constructions, including functional “means-plus-function” clauses are intended to cover the structures described herein as performing the recited function, including both structural equivalents that operate in the same manner, and equivalent structures that provide the same function. It is the express intention of the applicant not to invoke means-plus-function or other functional claiming for any claim except for those in which the words ‘means for’ appear together with an associated function. Each addition, deletion, and modification to the embodiments that falls within the meaning and scope of the claims is to be embraced by the claims.
The terms “approximately,” “about,” and “substantially” as used herein represent an amount close to the stated amount that still performs a desired function or achieves a desired result. For example, the terms “approximately,” “about,” and “substantially” may refer to an amount that is within less than 5% of, within less than 1% of, within less than 0.1% of, and within less than 0.01% of a stated amount. Further, it should be understood that any directions or reference frames in the preceding description are merely relative directions or movements. For example, any references to “up” and “down” or “above” or “below” are merely descriptive of the relative position or movement of the related elements. It should be understood that “proximal,” “distal,” “uphole,” and “downhole” are relative directions. As used herein, “proximal” and “uphole” should be understood to refer to a direction toward the surface, rig, operator, or the like. “Distal” or “downhole” should be understood to refer to a direction away from the surface, rig, operator, or the like. When the word “may” is used herein, such term should be interpreted as meaning that the identified feature, function, characteristic, or the like is present in some embodiments, but is optional and not present in other embodiments.
The present disclosure may be embodied in other specific forms without departing from its spirit or characteristics. The described embodiments are to be considered as illustrative and not restrictive. The scope of the disclosure is, therefore, indicated by the appended claims rather than by the foregoing description. Changes that come within the meaning and range of equivalency of the claims are to be embraced within their scope. Features of various embodiments described herein may be used in combination, except to the extent such features are mutually exclusive.
This application claims the benefit of, and priority to, U.S. Patent Application No. 62/278,116, filed Jan. 13, 2016 and to U.S. Patent Application No. 62/338,713, filed May 19, 2016, which applications are expressly incorporated herein by this reference in their entireties.
Filing Document | Filing Date | Country | Kind |
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PCT/US2017/012895 | 1/11/2017 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2017/123562 | 7/20/2017 | WO | A |
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