This disclosure relates generally to earth boring tools having rotatable cutting structures. This disclosure also relates to earth-boring tools having blades with fixed cutting elements as well as rotatable cutting structures.
Oil wells (wellbores) are usually drilled with a drill string. The drill string includes a tubular member having a drilling assembly that includes a single drill bit at its bottom end. The drilling assembly may also include devices and sensors that provide information relating to a variety of parameters relating to the drilling operations (“drilling parameters”), behavior of the drilling assembly (“drilling assembly parameters”) and parameters relating to the formations penetrated by the wellbore (“formation parameters”). A drill bit and\or reamer attached to the bottom end of the drilling assembly is rotated by rotating the drill string from the drilling rig and/or by a drilling motor (also referred to as a “mud motor”) in the bottom hole assembly (“BHA”) to remove formation material to drill the wellbore.
Some embodiments of the present disclosure include earth-boring tools. The earth-boring tools may include a body, at least one rotatable cutting structure assembly coupled to the body, at least five blades attached to the body and extending at least from a nose region of the earth-boring tool and throughout a gage region of the earth-boring tool, and at least three blades attached to the body and extending from a center longitudinal axis of the body to at least the nose region of the earth-boring tool. In some instances, the at least one rotatable cutting structure assembly may include a leg extending from a gage region of the earth-boring tool, and a rotatable cutting structure rotatably coupled to the leg.
In additional embodiments, the earth-boring tool may include a body, two rotatable cutting structure assemblies coupled to the body, and a plurality of blades coupled to the body. Each rotatable cutting structure assembly may include a leg extending from a gage region of the body and a rotatable cutting structure rotatably coupled to the leg. The plurality of blades may include a first set of five blades attached to the body, wherein three blades of the first set of five blades are disposed angularly between the two rotatable cutting structure assemblies on a first lateral side of the body of the earth-boring tool, and wherein two blades of the first set of five blades are disposed angularly between the two rotatable cutting structure assemblies on an opposite, second lateral side of the body of the earth-boring tool, and a second set of three blades attached to the body and extending from a center longitudinal axis of the body to at least a nose region of the body.
Some embodiments of the present disclosure include a method of forming an earth-boring tool. The method may include forming a first set of at least five blades on a body of the earth-boring tool, and forming each blade of the first set of at least five blades to extend from a nose region of the earth-boring tool to at least a gage region of the earth-boring tool, forming a second set of at least three blades on the body, and forming each blade of the second set of at least three blades to extend from a center longitudinal axis of the earth-boring tool to at least the nose region of the earth-boring tool, and coupling at least one rotatable cutting structure assembly to the body.
For a detailed understanding of the present disclosure, reference should be made to the following detailed description, taken in conjunction with the accompanying drawings, in which like elements have generally been designated with like numerals, and wherein:
The illustrations presented herein are not actual views of any drill bit, roller cutter, or any component thereof, but are merely idealized representations, which are employed to describe the present invention.
As used herein, the terms “bit” and “earth-boring tool” each mean and include earth-boring tools for forming, enlarging, or forming and enlarging a borehole. Non-limiting examples of bits include fixed cutter (drag) bits, fixed cutter coring bits, fixed cutter eccentric bits, fixed cutter bi-center bits, fixed cutter reamers, expandable reamers with blades bearing fixed cutters, and hybrid bits including both fixed cutters and rotatable cutting structures (roller cones).
As used herein, the term “cutting structure” means and include any element that is configured for use on an earth-boring tool and for removing formation material from the formation within a wellbore during operation of the earth-boring tool. As non-limiting examples, cutting structures include rotatable cutting structures, commonly referred to in the art as “roller cones” or “rolling cones.”
As used herein, the term “cutting elements” means and includes, for example, superabrasive (e.g., polycrystalline diamond compact or “PDC”) cutting elements employed as fixed cutting elements, as well as tungsten carbide inserts and superabrasive inserts employed as cutting elements mounted to rotatable cutting structures, such as roller cones.
As used herein, any relational term, such as “first,” “second,” “top,” “bottom,” etc., is used for clarity and convenience in understanding the disclosure and accompanying drawings, and does not connote or depend on any specific preference or order, except where the context clearly indicates otherwise. For example, these terms may refer to an orientation of elements of an earth-boring tool when disposed within a borehole in a conventional manner. Furthermore, these terms may refer to an orientation of elements of an earth-boring tool when as illustrated in the drawings.
As used herein, the term “substantially” in reference to a given parameter, property, or condition means and includes to a degree that one skilled in the art would understand that the given parameter, property, or condition is met with a small degree of variance, such as within acceptable manufacturing tolerances. For example, a parameter that is substantially met may be at least about 90% met, at least about 95% met, or even at least about 99% met.
Some embodiments of the present disclosure include a hybrid earth-boring tool having both blades and rotatable cutting structures. In particular, the earth-boring tool may include a first set of at least five blades and a second set of at least three blades. In some embodiments, the earth-boring tool may include at least five blades extending to a gage region of the earth-boring tool. Moreover, the earth-boring tool may include at least three blades extending to the center (i.e., a center longitudinal axis) of the earth-boring tool. In some instances, the first set of at least five blades may include two pairs of connected blades and a single distinct blade. For example, the first set of at least five blades may include a first pair of blades that are connected together via a first connector portion (e.g., a webbing between the pair of blades). The first set of at least five blades may further include a second pair of blades that are connected together via a second connector portion. Additionally, in one or more embodiments, at least one cutting element structure assembly may be disposed angularly between the first and second pairs of blades. In other words, the at least one cutting element structure assembly may be disposed between the first and second pairs of blades along a rotational direction of the earth-boring tool.
The drill string 110 may extend to a rig 120 at surface 122. The rig 120 shown is a land rig 120 for ease of explanation. However, the apparatuses and methods disclosed equally apply when an offshore rig 120 is used for drilling boreholes under water. A rotary table 124 or a top drive may be coupled to the drill string 110 and may be utilized to rotate the drill string 110 and to rotate the drilling assembly 114, and thus the drill bit 116 to drill the borehole 102. A drilling motor 126 may be provided in the drilling assembly 114 to rotate the drill bit 116. The drilling motor 126 may be used alone to rotate the drill bit 116 or to superimpose the rotation of the drill bit 116 by the drill string 110. The rig 120 may also include conventional equipment, such as a mechanism to add additional sections to the tubular member 112 as the borehole 102 is drilled. A surface control unit 128, which may be a computer-based unit, may be placed at the surface 122 for receiving and processing downhole data transmitted by sensors 140 in the drill bit 116 and sensors 140 in the drilling assembly 114, and for controlling selected operations of the various devices and sensors 140 in the drilling assembly 114. The sensors 140 may include one or more of sensors 140 that determine acceleration, weight on bit, torque, pressure, cutting element positions, rate of penetration, inclination, azimuth formation/lithology, etc. In some embodiments, the surface control unit 128 may include a processor 130 and a data storage device 132 (or a computer-readable medium) for storing data, algorithms, and computer programs 134. The data storage device 132 may be any suitable device, including, but not limited to, a read-only memory (ROM), a random-access memory (RAM), a flash memory, a magnetic tape, a hard disk, and an optical disk. During drilling, a drilling fluid from a source 136 thereof may be pumped under pressure through the tubular member 112, which discharges at the bottom of the drill bit 116 and returns to the surface 122 via an annular space (also referred as the “annulus”) between the drill string 110 and an inside sidewall 138 of the borehole 102.
The drilling assembly 114 may further include one or more downhole sensors 140 (collectively designated by numeral 140). The sensors 140 may include any number and type of sensors 140, including, but not limited to, sensors generally known as the measurement-while-drilling (MWD) sensors or the logging-while-drilling (LWD) sensors, and sensors 140 that provide information relating to the behavior of the drilling assembly 114, such as drill bit rotation (revolutions per minute or “RPM”), tool face, pressure, vibration, whirl, bending, and stick-slip. The drilling assembly 114 may further include a controller unit 142 that controls the operation of one or more devices and sensors 140 in the drilling assembly 114. For example, the controller unit 142 may be disposed within the drill bit 116 (e.g., within a shank 208 and/or crown 210 of a bit body of the drill bit 116). The controller unit 142 may include, among other things, circuits to process the signals from sensor 140, a processor 144 (such as a microprocessor) to process the digitized signals, a data storage device 146 (such as a solid-state-memory), and a computer program 148. The processor 144 may process the digitized signals, and control downhole devices and sensors 140, and communicate data information with the surface control unit 128 via a two-way telemetry unit 150.
The earth-boring tool 200 may comprise a body 202 including a neck 206, a shank 208, and a crown 210. In some embodiments, the bulk of the body 202 may be constructed of steel, or of a ceramic-metal composite material including particles of hard material (e.g., tungsten carbide) cemented within a metal matrix material. The body 202 of the earth-boring tool 200 may have an axial center 204 defining a center longitudinal axis 205 that may generally coincide with a rotational axis of the earth-boring tool 200. The center longitudinal axis 205 of the body 202 may extend in a direction hereinafter referred to as an “axial direction.”
The body 202 may be connectable to a drill string 110 (
Each blade 214 of the plurality of blades 214 of the earth-boring tool 200 may include a plurality of cutting elements 230 fixed thereto. The plurality of cutting elements 230 of each blade 214 may be located in a row along a profile of the blade 214 proximate a rotationally leading face 232 of the blade 214. In some embodiments, the plurality of cutting elements 220 of the plurality of rotatable cutting structures 218 (e.g., roller cutters) and plurality of cutting elements 230 of the plurality of blades 214 may include PDC cutting elements 230. Moreover, the plurality of cutting elements 230 of the plurality of rotatable cutting structures 218 and plurality of cutting elements 230 of the plurality of blades 214 may include any suitable cutting element configurations and materials for drilling and/or enlarging boreholes.
The plurality of rotatable cutting structure assemblies 212 may include a plurality of legs 216 and a plurality of rotatable cutting structures 218, each respectively mounted to a leg 216. The plurality of legs 216 may extend from an end of the body 202 opposite the neck 206 and may extend in the axial direction. The plurality of blades 214 may also extend from the end of the body 202 opposite the neck 206 and may extend in both the axial and radial directions. Each blade 214 may have multiple profile regions as known in the art (cone, nose, shoulder, gage). In some embodiments, two or more blades 214 of the plurality of blades 214 may be located between adjacent legs 216 of the plurality of legs 216. In some embodiments, the plurality of rotatable cutting structure assemblies 212 may not include a plurality of legs 216 but may be mounted directed to the crown 210 on the body 202 of the earth-boring tool 200.
Fluid courses 234 may be formed between adjacent blades 214 of the plurality of blades 214 and may be provided with drilling fluid by ports located at the end of passages leading from an internal fluid plenum extending through the body 202 from a tubular shank 208 at the upper end of the earth-boring tool 200. Nozzles 238 may be secured within the ports for enhancing direction of fluid flow and controlling flow rate of the drilling fluid. The fluid courses 234 extend to junk slots 240 extending axially along the longitudinal side of earth-boring tool 200 between blades 214 of the plurality of blades 214.
In one or more embodiments, each blade of the second set of at least three blades 304 may extend from the center longitudinal axis 205 of the earth-boring tool 200, through a cone region 306 of the earth-boring tool 200, and into the nose region 308 of the earth-boring tool 200. Furthermore, a cutting profile 314 of each blade of second set of at least three blades 304 may extend from the cone region 306 of the earth-boring tool 200 and at least into the nose region 308 of the earth-boring tool 200. In view of the foregoing, earth-boring tool 200 may include at least three blades extending to the center (i.e., the center longitudinal axis 205) of the earth-boring tool 200. Furthermore, in some embodiments, one of the blades of the second set of at least three blades 304 may be part of (e.g., a portion) of one of the blades of the first set of at least five blades 302. For example, one of the blades of the second set of at least three blades 304 and one of the blades of the first set of at least five blades 302 may form a continuous blade extending from the center longitudinal axis 205 of the earth-boring tool 200 to the gage region 312 of the earth-boring tool 200.
Because the earth-boring tool 200 includes at least three blades extending to the center of the earth-boring tool 200, and because the earth-boring tool 200 include at least five blades extending to the gage region 312 of the earth-boring tool 200, the earth-boring tool 200 of the present disclosure may provide higher cutting element densities in comparison to conventional earth-boring tools or hybrid drill bits. The cutting element densities of the earth-boring tool 200 are described in greater detail below in regard to
In some instances, the first set of at least five blades 302 may include two pairs of connected blades 316, 318 and a single distinct blade 324. For example, the first set of at least five blades 302 may include a first pair of blades 316 that are connected together via a first connector portion 320 (e.g., a webbing between the pair of blades). In some embodiments, the first connector portion 320 may connect ends of the first pair of blades 316 proximate the cone region 306 of the earth-boring tool 200. In particular, the first connector portion 320 may extend between the blades of the first pair of blades 316 such that the first pair of blades 316 form a generally V-shape. The first set of at least five blades 302 may further include a second pair of blades 318 that are connected together via a second connector portion 322. In some embodiment, the second connector portion 322 may also connect ends of the second pair of blades 318 proximate the cone region 306 of the earth-boring tool 200. In particular, the second connector portion 322 may extend between the blades of the second pair of blades 318 such that the second pair of blades 318 also form a generally V-shape. In some embodiments, the first and second pairs of blades 316, 318 may be pointed toward each other laterally across the earth-boring tool 200. For example, points of the V-shapes formed by the first and second pairs of blades 316, 318 may generally point toward each other.
In some embodiments, the first pair of blades 316 may include at least one blade of the second set of three blades 304. For example, one blade of the first pair of blades 316 may extend from the center longitudinal axis 205 to the gage region 312 of the earth-boring tool 200. Furthermore, in some embodiments, the first and second pairs of blades 316, 318 may be disposed on opposite lateral sides of the earth-boring tool 200. In some instances, the second pair of blades 318 may extend from the gage region 312 of the earth-boring tool 200 through the nose region 308 of the earth-boring tool 200. For example, the second pair of blades 318 may not substantially extend into the cone region 306 of the earth-boring tool 200. Moreover, the cutting profiles of the second pair of blades 318 may extend from the gage region 312 of the earth-boring tool 200 through the nose region 308 of the earth-boring tool 200 and may not substantially extend into the cone region 306 of the earth-boring tool 200.
As noted above, in some embodiments, the first set of at least five blades 302 may include the single distinct blade 324. The single distinct blade 324 may be disposed angularly adjacent to the first pair of blades 316. For example, the single distinct blade 324 may lead the first pair of blades 316 in a direction of rotation of the earth-boring tool 200. Furthermore, the single distinct blade 324 may extend from the gage region of the earth-boring tool 200 through the nose region 308 of the earth of the earth-boring tool 200. For example, the single distinct blade 324 may not substantially extend into the cone region 306 of the earth-boring tool 200. Moreover, the cutting profiles of the single distinct blade 324 may extend from the gage region 312 of the earth-boring tool 200 through the nose region 308 of the earth-boring tool 200 and may not substantially extend into the cone region 306 of the earth-boring tool 200.
Additionally, in one or more embodiments, at least one rotatable cutting structure assembly 212 may be disposed angularly between the first and second pairs of blades 316, 318. In other words, the at least one rotatable cutting structure assembly 212 may be disposed between the first and second pairs of blades 316, 318 along a rotational direction of the earth-boring tool 200. Each rotatable cutting structure 218 may be rotatably mounted to a respective leg 216 of the body 202. For example, each rotatable cutting structure 218 may be mounted to a respective leg 216 with one or more of a journal bearing and rolling-element bearing. Many such bearing systems are known in the art and may be employed in embodiments of the present disclosure
Each rotatable cutting structure 218 may have a plurality of cutting elements 220 thereon. In some embodiments, the plurality of cutting elements 220 of each rotatable cutting structure 218 may be arranged in generally circumferential rows on an outer surface 222 of the rotatable cutting structure 218. In other embodiments, the cutting elements 220 may be arranged in an at least substantially random configuration on the outer surface 222 of the rotatable cutting structure 218. In some embodiments, the cutting elements 220 may comprise preformed inserts that are interference fitted into apertures formed in each rotatable cutting structure 218. In other embodiments, the cutting elements 220 of the rotatable cutting structure 218 may be in the form of teeth integrally formed with the material of each rotatable cutting structure 218. The cutting elements 220, if in the form of inserts, may be formed from tungsten carbide, and optionally have a distal surface of polycrystalline diamond, cubic boron nitride, or any other wear-resistant and/or abrasive or superabrasive material.
In some embodiments, each rotatable cutting structure 218 of the plurality of rotatable cutting structures 218 may have a general conical shape, with a base end 224 (e.g., wide end and radially outermost end 224) of the conical shape being mounted to a respective leg 216 and a tapered end 226 (e.g., radially innermost end 226) being proximate (e.g., at least substantially pointed toward) the axial center 204 of the body 202 of the earth-boring tool 200. In other embodiments, each rotatable cutting structure 218 of the plurality of rotatable cutting structures 218 may not have a generally conical shape but may have any shape appropriate for rotatable cutting structures 218.
Each rotatable cutting structure 218 of the plurality of rotatable cutting structures 218 may have a rotational axis 228a, 228b about which each rotatable cutting structure 218 may rotate during use of the earth-boring tool 200 in a drilling operation. In some embodiments, the rotational axis 228a, 228b of each rotatable cutting structure 218 of the plurality of rotatable cutting structures 218 may intersect the axial center 204 of the earth-boring tool 200. In other embodiments, the rotational axis 228a, 228b of one or more rotatable cutting structures 218 of the plurality of rotatable cutting structures 218 may be offset from the axial center 204 of the earth-boring tool 200. For example, the rotational axis 228a, 228b of one or more rotatable cutting structures 218 of the plurality of rotatable cutting structures 218 may be laterally offset (e.g., angularly skewed) such that the rotational axis 228a, 228b of the one of more rotatable cutting structures 218 of the plurality of rotatable cutting structures 218 does not intersect the axial center 204 of the earth-boring tool 200. In some embodiments, the radially innermost end 226 of each rotatable cutting structure 218 of the plurality of rotatable cutting structures 218 may be radially spaced from the axial center 204 of the earth-boring tool 200.
In some embodiments, the plurality of rotatable cutting structures 218 may be angularly spaced apart from each other around the center longitudinal axis 205 of the earth-boring tool 200. For example, a first rotational axis 228a of a first rotatable cutting structure 218 of the plurality of rotatable cutting structures 218 may be circumferentially angularly spaced apart from a second rotational axis 228b of a second rotatable cutting structure 218 by about 75° to about 180°. In some embodiments, the rotatable cutting structures 218 may be angularly spaced apart from one another by an acute angle. For example, in some embodiments, the rotatable cutting structures 218 may be angularly spaced apart from one another by about 120°. In other embodiments, the rotatable cutting structures 218 may be angularly spaced apart from one another by about 150°. In other embodiments, the rotatable cutting structures 218 may be angularly spaced apart from one another by about 180°. Although specific degrees of separation of rotational axes (i.e., number of degrees) are disclosed herein, one of ordinary skill in the art would recognize that the rotatable cutting structures 218 may be angularly spaced apart from one another by any suitable amount.
Referring still to
In some embodiments, one or more rows of cutting elements 220 of the first rotatable cutting structure 218a may be recessed relative to other rows of cutting elements 220. For example, each cutting element 220 of a respective row of cutting elements 220 may be disposed in a recess 402. In some instances, a row of cutting elements 220 most proximate the base end 224 of the first rotatable cutting structure 218 may be recessed relative to other rows of cutting elements 220. Conversely, the second rotatable cutting structure 218b may not include one or more recessed rows of cutting elements 220. Furthermore, in some instances, each cutting element 220 of the plurality of cutting elements 220 of both of the first and second rotatable cutting structures 218a, 218b may have a generally conical shape. For example, the plurality of cutting elements 220 of both of the first and second rotatable cutting structures 218a, 218b may not include wedge shapes.
In one or more embodiments, the base end 224 of both of the first and second rotatable cutting structures 218a, 218b may include a frusto-conical surface 404. Furthermore, both of the first and second rotatable cutting structures 218a, 218b may include a plurality of impact inserts 406 disposed on the frusto-conical surface 404 (e.g., inserted into a portion of the rotatable cutting structure 218 defining the frusto-conical surface 404).
Furthermore, in some embodiments, the second rotatable cutting structure 218b may have a greater height than the first rotatable cutting structure 218a along the rotational axes 228a, 228b of the first and second rotatable cutting structures 218a, 218b. For example, in some embodiments, the first rotatable cutting structure 218a may have a height H1 within a range of about 2.8 inches and about 3.2 inches, and the second rotatable cutting structure 218b may have a height H2 within a range of about 3.1 inches and about 3.5 inches. For instance, the first rotatable cutting structure 218a may have a height H1 of about 3.0 inches, and the second rotatable cutting structure 218b may have a height H2 of about 3.3 inches. Furthermore, both of the first and second rotatable cutting structures 218a, 218b may have a width W within a range of about 5.5 inches to about 6.5 inches. For example, both of the first and second rotatable cutting structures 218a, 218b may have a width W of about 6.0 inches. Moreover, the frusto-conical surface 404 of a respective rotatable cutting structure may define an angle β with a plane orthogonal to the axis of rotation of a respective rotatable cutting structure. In some embodiments, the angle β may be within a range of about 30° and about 40°. For example, the angle β may be about 36°. Additionally, the base end 224 of both of the first and second rotatable cutting structures 218a, 218b may have a diameter D within a range of about 3.5 inches and about 4.0 inches. For instance, the base end 224 may have a diameter of about 3.7 inches. In some embodiments, both the first and second rotatable cutting structures 218a, 218b may be coupled to a leg 216 (
In view of the foregoing, the rotatable cutting structures (e.g., rotatable cutting structures 218a, 218b) of the present disclosure may provide advantages over conventional rotatable cutting structures. For example, the rotatable cutting structures of the present disclosure may exhibit a roll ratio within a range of 1.85 and 1.90 when used in an earth-boring tool (e.g., earth-boring tool 200). As used herein, the term “roll ratio” may refer to a number of times a rotatable cutting structure rotates relative to a full rotation of an earth-boring tool upon which the rotatable cutting structure is being used. Reducing the roll ratio may reduce wear on the cutting elements 220 of the rotatable cutting structure and may increase a life span of the cutting elements 220 and, as a result, the rotatable cutting structure.
Due to the cutting elements 220 defining the cutter profile 500 being aligned along the foregoing described lines of curvature, the rotatable cutting structures (e.g., the first and second rotatable cutting structures 218a, 218b (
With reference to
In some embodiments, each blade of the seven blades may be spaced apart from each other angularly around the longitudinal axis of the earth-boring tool 200 by certain angles. For example, a plane 602 extending radially outward from the center longitudinal axis 205 and intersecting a leading face of blade No. 1 (referred to hereinafter as “leading plane”) may be circumferentially angularly spaced apart from a leading plane 604 of blade No. 2 by about 40° to about 60°. For instance, in some embodiments, blade No. 1 and blade No. 2 may be angularly spaced apart from one another by about 54°. Additionally, the leading plane 604 of blade No. 2 may be circumferentially angularly spaced apart from a leading plane 606 of blade No. 3 by about 40° to about 60°. In particular, in some embodiments, blade No. 2 and blade No. 3 may be angularly spaced apart from one another by about 56°. Moreover, the leading plane 606 of blade No. 3 may be circumferentially angularly spaced apart from a leading plane 608 of blade No. 4 by about 40° to about 60°. For instance, in some embodiments, blade No. 3 and blade No. 4 may be angularly spaced apart from one another by about 55°. Furthermore, the leading plane 608 of blade No. 4 may be circumferentially angularly spaced apart from a leading plane 610 of blade No. 5 by about 40° to about 60°. For example, in some embodiments, blade No. 4 and blade No. 5 may be angularly spaced apart from one another by about 50°. Likewise, the leading plane 610 of blade No. 5 may be circumferentially angularly spaced apart from a leading plane 612 of blade No. 6 by about 40° to about 60°. For instance, in some embodiments, blade No. 5 and blade No. 6 may be angularly spaced apart from one another by about 58°. Also, the leading plane 612 of blade No. 6 may be circumferentially angularly spaced apart from a leading plane 614 of blade No. 7 by about 35° to about 50°. For example, in some embodiments, blade No. 6 and blade No. 7 may be angularly spaced apart from one another by about 42°. Although specific degrees of separation of leading planes (i.e., number of degrees) are disclosed herein, one of ordinary skill in the art would recognize that blades No. 1-7 may be angularly spaced apart from one another by any suitable amount.
As mentioned above in regard to
In some embodiments, the secondary junk slot 706 may include a curved portion 712 have a radius of curvature R3 within a range of about 1.3 inches and about 1.7 inches. For example, the curved portion 712 of the secondary junk slot 706 may have radius of curvature R3 of about 1.5 inches. Additionally, both the secondary junk slot 706 and the sub-assembly junk slot 704 may have a planar portion 714 proximate the nose region 308 and cone region 306 of the earth-boring tool 200. In some embodiments, a surface of the planar portion 714 may form an angle α with respect to the center longitudinal axis 205 of the earth-boring tool 200 (
Furthermore, as shown in graph 1000, the earth-boring tool (e.g., earth-boring tool 200 (
By reducing imbalance percentages, the earth-boring tool of the present disclosure may provide more reliable drilling. Furthermore, reducing imbalance percentages may result in increased lifespans of earth-boring tools. Moreover, reducing imbalance percentages may reduce imbalanced wear on the earth-boring tools and cutting elements.
The embodiments of the disclosure described above and illustrated in the accompanying drawings do not limit the scope of the disclosure, which is encompassed by the scope of the appended claims and their legal equivalents. Any equivalent embodiments are within the scope of this disclosure. Indeed, various modifications of the disclosure, in addition to those shown and described herein, such as alternate useful combinations of the elements described, will become apparent to those skilled in the art from the description. Such modifications and embodiments also fall within the scope of the appended claims and equivalents.
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