U.S. patent application number 16/433400 was filed with the patent office on 2019-09-19 for earth-boring tools and methods of forming earth-boring tools.
The applicant listed for this patent is Baker Hughes, a GE company, LLC. Invention is credited to Kenneth R. Evans, David Gavia, Bibek Ghimire.
Application Number | 20190284877 16/433400 |
Document ID | / |
Family ID | 61011780 |
Filed Date | 2019-09-19 |
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United States Patent
Application |
20190284877 |
Kind Code |
A1 |
Gavia; David ; et
al. |
September 19, 2019 |
EARTH-BORING TOOLS AND METHODS OF FORMING EARTH-BORING TOOLS
Abstract
An earth-boring tool comprises a body, a plurality of blades,
and cutting elements. The body has a face at a leading end thereof
and comprises a cone region, a nose region, a flank region, a
shoulder region, and a gage region. The plurality of blades extends
longitudinally and radially over the face. The cutting elements are
disposed within the shoulder region of the body on different blades
of the plurality of blades than one another, a first of the cutting
elements exhibiting a different size than a second of the cutting
elements. A method of forming an earth-boring tool and a method of
forming a borehole in a subterranean formation are also
described.
Inventors: |
Gavia; David; (The
Woodlands, TX) ; Evans; Kenneth R.; (Spring, TX)
; Ghimire; Bibek; (The Woodlands, TX) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
Baker Hughes, a GE company, LLC |
Houston |
TX |
US |
|
|
Family ID: |
61011780 |
Appl. No.: |
16/433400 |
Filed: |
June 6, 2019 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
|
15222508 |
Jul 28, 2016 |
10344537 |
|
|
16433400 |
|
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Current U.S.
Class: |
1/1 |
Current CPC
Class: |
E21B 10/43 20130101;
E21B 10/54 20130101 |
International
Class: |
E21B 10/43 20060101
E21B010/43; E21B 10/54 20060101 E21B010/54 |
Claims
1. An earth-boring tool, comprising: a body having a face at a
leading end thereof and comprising a cone region, a nose region, a
flank region, a shoulder region, and a gage region; a plurality of
blades extending longitudinally and radially over the face; and
cutting elements disposed within the shoulder region of the body on
different blades of the plurality of blades than one another, a
first of the cutting elements provided in a rotationally leading
position relative to a second of the cutting elements and
exhibiting a smaller size than the second of the cutting
elements.
2. (canceled)
3. The earth-boring tool of claim 1, wherein a third of the cutting
elements is provided in a rotationally trailing position relative
to the second of the cutting elements and exhibits a larger size
than the second of the cutting elements.
4. A method of forming an earth-boring tool, comprising: forming a
body having a face at a leading end thereof and comprising a cone
region, a nose region, a flank region, a shoulder region, and a
gage region; disposing a first cutting element within the shoulder
region of the body on a first blade extending longitudinally and
radially over the face; and disposing a second cutting element
within the shoulder region of the body on a second blade extending
longitudinally and radially over the face and rotationally trailing
the first blade, the second cutting element exhibiting a larger
diameter than the first cutting element.
5. (canceled)
6. The method of claim 4, further comprising disposing the second
cutting element directly radially adjacent the first cutting
element.
7. The method of claim 4, further comprising disposing additional
cutting elements within one or more of the cone region, the nose
region, the flank region, and the gage region of the body, one or
more of the first cutting element and the second cutting element
exhibiting a larger size than any of the additional cutting
elements.
8. The method of claim 7, further comprising selecting the first
cutting element and the second cutting element to each individually
exhibit a larger cutting face than any of the additional cutting
elements.
9. The method of claim 7, further comprising selecting each of the
additional cutting elements to exhibit substantially the same size
as one another.
10. The method of claim 4, further comprising disposing a third
cutting element within the shoulder region of the body on a third
blade extending longitudinally and radially over the face and
rotationally trailing the second blade, the third cutting element
exhibiting a larger diameter than each of the first cutting element
and the second cutting element.
11. The method of claim 10, further comprising disposing the third
cutting element directly radially adjacent the second cutting
element.
12. The method of claim 4, wherein disposing a second cutting
element within the shoulder region of the body on a second blade
comprises positioning the second cutting element to be underexposed
relative to the first cutting element.
13. The method of claim 4, wherein disposing a second cutting
element within the shoulder region of the body on a second blade
comprises disposing the second cutting element at a different
radial position within the shoulder region of the body than the
first cutting element.
14. An earth-boring tool, comprising: a body having a face at a
leading end thereof and comprising a cone region, a nose region, a
flank region, a shoulder region, and a gage region; a first cutting
element located within the shoulder region of the body on a first
blade extending longitudinally and radially over the face of the
body; and a second cutting element located within the shoulder
region of the body on a second blade extending longitudinally and
radially over the face of the body and rotationally trailing the
first blade, the second cutting element exhibiting a larger
diameter than the first cutting element.
15. The earth-boring tool of claim 14, further comprising
additional cutting elements located within one or more of the cone
region, the nose region, the flank region, and the gage region of
the body on one or more of the first blade and the second blade,
the additional cutting elements exhibiting a smaller diameter than
one or more of the first cutting element and the second cutting
element.
16. The earth-boring tool of claim 14, wherein the first blade is
positioned circumferentially adjacent the second blade.
17. The earth-boring tool of claim 14, wherein a ratio between a
diameter of the first cutting element and a diameter of the second
cutting element is within a range of from about 0.32:1 to about
0.84:1.
18. The earth-boring tool of claim 14, further comprising a third
cutting element located within the shoulder region of the body on
third blade extending longitudinally and radially over the face of
the body and rotationally trailing the second blade, the third
cutting element exhibiting a larger diameter than the second
cutting element.
19. The earth-boring tool of claim 18, wherein: the second cutting
element is underexposed relative to the first cutting element; and
the third cutting element is underexposed relative to the second
cutting element.
20. The earth-boring tool of claim 14, wherein the first cutting
element and the second cutting element are radially positioned
relative to one another such that rotational paths for the first
cutting element and the second cutting element overlap one another
proximate outermost lateral boundaries of the rotational paths.
21. The earth-boring tool of claim 14, wherein the first cutting
element and the second cutting element are radially positioned
relative to one another such that rotational paths for the first
cutting element and the second cutting element overlap one another
proximate lowermost longitudinal boundaries of the rotational
paths.
22. The earth-boring tool of claim 14, wherein the first cutting
element and the second cutting element are radially positioned
relative to one another such that rotational paths for the first
cutting element and the second cutting element overlap one another
a location intermediate between outermost lateral boundaries and
lowermost longitudinal boundaries of the rotational paths.
Description
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application is a divisional of U.S. patent application
Ser. No. 15/222,508, filed Jul. 28, 2016, pending, the disclosure
of which is hereby incorporated herein in its entirety by this
reference.
TECHNICAL FIELD
[0002] The disclosure relates generally to earth-boring tools, to
methods of forming earth-boring tools, and to methods of forming a
borehole in a subterranean formation. More particularly,
embodiments of the disclosure relate to earth-boring tools
exhibiting favorable cutting efficiency, force distribution, and
damage distribution during drilling operations, and to methods of
forming and using such earth-boring tools.
BACKGROUND
[0003] Boreholes are formed in subterranean formations for various
purposes including, for example, extraction of oil and gas from the
subterranean formations and extraction of geothermal heat from the
subterranean formations. A borehole may be formed in a subterranean
formation using a drilling assembly including an earth-boring tool,
such as a rotary drill bit, coupled to a distal end of a drill
string that includes a series of elongated tubular segments
connected end-to-end and extending into the wellbore from the
surface of the subterranean formation.
[0004] Non-limiting examples of rotary drill bits include
fixed-cutter drill bits (also known in the art as "drag" bits),
roller cone drill bits (also known in the art as "rock" bits),
diamond-impregnated bits, and hybrid bits (which may include, for
example, both fixed-cutters and roller cone cutters). The rotary
drill bit can, for example, be a fixed-cutter drill bit, which
typically includes a plurality of blades each carrying multiple
cutting elements configured and positioned to cut, crush, shear,
and/or abrade away material of the subterranean formation as the
rotary drill bit is rotated under an applied axial force (known in
the art as "weight-on-bit" (WOB)) to form a borehole therein.
Fixed-cutter drill bits have proven very effective in achieving
high rates of penetration (ROP) in drilling subterranean formations
exhibiting low to medium hardness.
[0005] Cutting elements are typically laid out on a fixed-cutter
drill bit in a configuration resulting in the formation of
progressively smaller helical grooves in a radially outwardly
extending direction as the fixed-cutter drill bit is used to form a
borehole in the subterranean formation. The geometric
configurations (e.g., sizes, shapes) and layout (e.g., positions,
spacing) of the cutting elements within at least a shoulder region
of a conventional fixed-cutter drill bit frequently results in a
single cutting element performing substantially all of the work of
forming the outermost diameter of the borehole. Such geometric
configurations and layouts can be inefficient to produce boreholes
exhibiting desirable outermost diameters, and can result in an
undesirably short operational life of the fixed-cutter drill
bit.
[0006] Accordingly, it would be desirable to have earth-boring
tools (e.g., rotary drill bits), methods of forming earth-boring
tools, and methods of forming a borehole in a subterranean
formation facilitating enhanced efficiency, and prolonged
operational life during drilling operations as compared to
conventional earth-boring tools, methods of forming earth-boring
tools, and methods of forming a borehole in a subterranean
formation.
BRIEF SUMMARY
[0007] In some embodiments, an earth-boring tool comprises a body,
a plurality of blades, and cutting elements. The body has a face at
a leading end thereof and comprises a cone region, a nose region, a
flank region, a shoulder region, and a gage region. The plurality
of blades extends longitudinally and radially over the face. The
cutting elements are disposed within the shoulder region of the
body on different blades of the plurality of blades than one
another, a first of the cutting elements exhibiting a different
size than a second of the cutting elements.
[0008] In additional embodiments, a method of forming an
earth-boring tool comprises forming a body having a face at a
leading end thereof and comprising a cone region, a nose region, a
flank region, a shoulder region, and a gage region. A first cutting
element is disposed within the shoulder region of the body on a
first blade extending longitudinally and radially over the face. A
second cutting element is disposed within the shoulder region of
the body on a second blade extending longitudinally and radially
over the face and rotationally trailing the first blade, the second
cutting element exhibiting a different size than the first cutting
element.
[0009] In further embodiments, a method of forming a borehole in a
subterranean formation comprises disposing an earth-boring tool at
a distal end of a drill string in a borehole in a subterranean
formation, the earth-boring tool comprising a body, a plurality of
blades, and cutting elements. The body has a face at a leading end
thereof and comprises a cone region, a nose region, a flank region,
a shoulder region, and a gage region. The plurality of blades
extends longitudinally and radially over the face. The cutting
elements are disposed within the shoulder region of the body on
different blades of the plurality of blades than one another, a
first of the cutting elements exhibiting a different size than a
second of the cutting elements. Weight on bit is applied to the
earth-boring tool through the drill string to contact the formation
while rotating the earth-boring tool. The subterranean formation is
engaged with the cutting elements of the rotating earth-boring
tool.
BRIEF DESCRIPTION OF THE DRAWINGS
[0010] FIG. 1A is a face view of a rotary drill bit, in accordance
with an embodiment of the disclosure.
[0011] FIG. 1B is a cutter and blade profile for the rotary drill
bit shown in FIG. 1A.
[0012] FIG. 2 is a cutter and blade profile of a rotary drill bit,
in accordance with another embodiment of the disclosure.
[0013] FIGS. 3 through 5 are schematic views of different cutting
element exposure configurations, in accordance with embodiments of
the disclosure.
[0014] FIG. 6 is a cutter and blade profile of a rotary drill bit,
in accordance with a further embodiment of the disclosure.
[0015] FIG. 7 is a perspective view of a segment of a borehole
formed in a subterranean formation using a rotary drill bit having
the cutter and blade profile shown in FIG. 1B.
[0016] FIG. 8 is a perspective view of a segment of a borehole
formed in a subterranean formation using a rotary drill bit having
the cutter and blade profile shown in FIG. 6.
DETAILED DESCRIPTION
[0017] Earth-boring tools are disclosed, as are methods of forming
earth-boring tools, and methods of forming a borehole in a
subterranean formation. In some embodiments, an earth-boring tool
includes a body (e.g., bit body) having a face (e.g., bit face) at
a leading end thereof, and a plurality of blades extending
longitudinally and radially over the face of the body. The body may
include a rotational axis, a cone region outwardly radially
adjacent the rotational axis, a nose region outwardly radially
adjacent the cone region, a flank region outwardly radially
adjacent the nose region, a shoulder region outwardly radially
adjacent the flank region, and a gage region outwardly radially
adjacent the shoulder region. Cutting elements are disposed within
the shoulder region of the body on different blades than one
another. At least one of the cutting elements exhibits a different
size (e.g., a different diameter, a different lateral extent) and a
different radial position within the shoulder region of the body
than at least one other of the cutting elements. The configurations
(e.g., sizes, shapes, material compositions) and layout (e.g.,
positions, spacing) of the cutting elements may facilitate the more
efficient formation of a borehole in a subterranean formation as
compared to conventional cutting element configurations and layouts
employed in conventional earth-boring tools.
[0018] The following description provides specific details, such as
material types and processing conditions in order to provide a
thorough description of embodiments of the disclosure. However, a
person of ordinary skill in the art will understand that the
embodiments of the disclosure may be practiced without employing
these specific details. Indeed, the embodiments of the disclosure
may be practiced in conjunction with conventional fabrication
techniques employed in the industry. In addition, the description
provided below does not form a complete process flow for
manufacturing a structure (e.g., cutting element), tool, or
assembly. Only those process acts and structures necessary to
understand the embodiments of the disclosure are described in
detail below. Additional acts to form the complete structure, the
complete tool, or the complete assembly from various structures may
be performed by conventional fabrication techniques. The drawings
accompanying the present application are for illustrative purposes
only, and are not drawn to scale. Additionally, elements common
between figures may retain the same numerical designation.
[0019] As used herein, the terms "comprising," "including,"
"containing," and grammatical equivalents thereof are inclusive or
open-ended terms that do not exclude additional, unrecited elements
or method steps, but also include the more restrictive terms
"consisting of" and "consisting essentially of" and grammatical
equivalents thereof. As used herein, the term "may" with respect to
a material, structure, feature, or method act indicates that such
is contemplated for use in implementation of an embodiment of the
disclosure and such term is used in preference to the more
restrictive term "is" so as to avoid any implication that other,
compatible materials, structures, features and methods usable in
combination therewith should or must be, excluded.
[0020] As used herein, spatially relative terms, such as "beneath,"
"below," "lower," "bottom," "above," "upper," "top," "front,"
"rear," "left," "right," and the like, may be used for ease of
description to describe one element's or feature's relationship to
another element(s) or feature(s) as illustrated in the figures.
Unless otherwise specified, the spatially relative terms are
intended to encompass different orientations of the materials in
addition to the orientation depicted in the figures. For example,
if materials in the figures are inverted, elements described as
"below" or "beneath" or "under" or "on bottom of" other elements or
features would then be oriented "above" or "on top of" the other
elements or features. Thus, the term "below" can encompass both an
orientation of above and below, depending on the context in which
the term is used, which will be evident to one of ordinary skill in
the art. The materials may be otherwise oriented (e.g., rotated 90
degrees, inverted, flipped) and the spatially relative descriptors
used herein interpreted accordingly.
[0021] As used herein, the singular forms "a," "an," and "the" are
intended to include the plural forms as well, unless the context
clearly indicates otherwise.
[0022] As used herein, the term "and/or" includes any and all
combinations of one or more of the associated listed items.
[0023] As used herein, the term "configured" refers to a size,
shape, material composition, and arrangement of one or more of at
least one structure and at least one apparatus facilitating
operation of one or more of the structure and the apparatus in a
pre-determined way.
[0024] As used herein, the term "substantially" in reference to a
given parameter, property, or condition means and includes to a
degree that one of ordinary skill in the art would understand that
the given parameter, property, or condition is met with a degree of
variance, such as within acceptable manufacturing tolerances. By
way of example, depending on the particular parameter, property, or
condition that is substantially met, the parameter, property, or
condition may be at least 90.0% met, at least 95.0% met, at least
99.0% met, or even at least 99.9% met.
[0025] As used herein, the term "about" in reference to a given
parameter is inclusive of the stated value and has the meaning
dictated by the context (e.g., it includes the degree of error
associated with measurement of the given parameter).
[0026] As used herein, the terms "earth-boring tool" and
"earth-boring drill bit" mean and include any type of bit or tool
used for drilling during the formation or enlargement of a wellbore
in a subterranean formation and include, for example, fixed-cutter
bits, roller cone bits, percussion bits, core bits, eccentric bits,
bicenter bits, reamers, mills, drag bits, hybrid bits (e.g.,
rolling components in combination with fixed cutting elements), and
other drilling bits and tools known in the art.
[0027] FIG. 1A is a face view of a rotary drill bit 100 in the form
of a fixed cutter or so-called "drag" bit, according to an
embodiment of the disclosure. The rotary drill bit 100 includes a
body 102 exhibiting a face 104 defined by external surfaces of the
body 102 that contact a subterranean formation during drilling
operations. The body 102 may comprise, by way of example and not
limitation, an infiltrated tungsten carbide body, a steel body, or
a sintered particle matrix body, and may include a plurality of
blades 106 extending longitudinally and radially over the face 104
in a spiraling configuration relative to a rotational axis 112 of
the rotary drill bit 100. The blades 106 may receive and hold
cutting elements 114 (numbered from 1 to 31), and may define fluid
courses 108 there between extending into junk slots 110 between
gage sections of circumferentially adjacent blades 106. In some
embodiments, the body 102 includes an even number of the blades
106, such as greater than or equal to four of the blades 106 (e.g.,
four of the blades 106, six of the blades 106, eight of the blades
106). For example, as depicted in FIG. 1A, the body 102 may include
six (6) of the blades 106. In additional embodiments, the body 102
includes a different quantity (e.g., number, amount) of the blades
106. The body 102 may include, for example, an odd number of the
blades 106 (e.g., five of the blades 106; seven of the blades 106).
Accordingly, while various embodiments herein describe or
illustrate the body 102 as including the six (6) blades 106A-106F,
the body 102 may, alternatively, include a different number of the
blades 106.
[0028] As shown in FIG. 1A, the blades 106 may include primary
blades 106A, 106C, 106E, and secondary blades 106B, 106D, 106F. At
least a portion (e.g., each) of the primary blades 106A, 106C, 106E
may be circumferentially separated from one another by the
secondary blades 106B, 106D, 106F, and may each include a first end
located radially proximate the rotational axis 112 of the rotary
drill bit 100. In addition, at least a portion (e.g., each) of the
secondary blades 106B, 106D, 106F may be circumferentially
separated from one another primary blades 106A, 106C, 106E, and may
each include a first end located more radially distal from the
rotational axis 112 of the rotary drill bit 100 than the first end
of each of the primary blades 106A, 106C, 106E. As shown in FIG.
1A, the primary blades 106A, 106C, 106E may circumferentially
alternate with the secondary blades 106B, 106D, 106F around the
face 104 of the rotary drill bit 100. A first primary blade 106A
may be circumferentially separated from a second primary blade 106C
by a first secondary blade 106B, the second primary blade 106C may
be circumferentially separated from a third primary blade 106E by a
second secondary blade 106D, and the third primary blade 106E may
be circumferentially separated from the first primary blade 106A by
a third secondary blade 106F. In additional embodiments, such as in
embodiments wherein the body 102 exhibits a different number of the
blades 106, the body 102 may exhibit a different quantity and/or a
different circumferential sequence (e.g., circumferential pattern)
of primary blades and secondary blades. The body 102 may include,
for example, an even number of primary blades circumferentially
alternating with an even number of secondary blades (e.g., two
primary blades circumferentially alternating with two secondary
blades, four primary blades circumferentially alternating with four
secondary blades), an odd number of primary blades at least
partially circumferentially alternating with an even number of
secondary blades (e.g., three primary blades circumferentially
alternating with two secondary blades, three primary blades
partially circumferentially alternating with four secondary
blades), or an even number of primary blades at least partially
circumferentially alternating with an odd number of secondary
blades (e.g., two primary blades circumferentially alternating with
three secondary blades, four primary blades partially
circumferentially alternating with three secondary blades).
Accordingly, while various embodiments herein describe or
illustrate the body 102 as including three (3) primary blades 106A,
106C, 106E circumferentially alternating with three (3) secondary
blades 106B, 106D, 106F, the body 102 may, alternatively, include a
different quantity and/or a different sequence of primary blades
and secondary blades.
[0029] The cutting elements 114 may comprise a superabrasive (e.g.,
diamond) mass bonded to a supporting substrate. For example, at
least some of the cutting elements 114 may be formed of and include
a disc-shaped diamond "table" having a cutting face formed on and
bonded under an ultra-high-pressure and high-temperature (HPHT)
process to a supporting substrate formed of cemented tungsten
carbide. Other known cutting face configurations may also be
employed in implementation of embodiments of the disclosure. The
cutting elements 114 may be affixed to the blades 106 through
brazing, welding, or any other suitable means. The cutting elements
114 may be backraked at a common angle, or at varying angles. In
addition, the cutting elements 114 may independently be formed of
and include suitably mounted and exposed natural diamonds,
thermally stable polycrystalline diamond compacts, cubic boron
nitride compacts, tungsten carbide, diamond grit-impregnated
segments, or combinations thereof. The material composition of the
cutting elements 114 may be selected at least partially based on
the hardness and abrasiveness of the subterranean formation to be
drilled.
[0030] The cutting elements 114 are positioned and sized on the
blades 106 to provide enhanced cutting efficiency, to more evenly
distribute damage (e.g., dulling) across the cutting elements 114,
and to extend the life of the rotary drill bit 100 during drilling
operations (e.g., drilling of a homogeneous subterranean formation;
drilling of a heterogeneous subterranean formation, such as a
subterranean formation including transitions between a soft
material and a hard material) as compared to conventional cutting
element layouts. FIG. 1B shows a cutter and blade profile of the
rotary drill bit 100 (FIG. 1A) as if each of the cutting elements
114 disposed on the various blades 106 was rotated about the
rotational axis 112 onto a single blade 106. As shown in FIG. 1B,
the cutting elements 114 are positioned on the blades 106 and are
numbered from 1 to 31 sequentially in the radial direction. The
numbering scheme shown correlates to the radial position of the
cutting elements 114 with relation to the rotational axis 112 of
the rotary drill bit 100. For example, the cutting element 114
identified by the number one (1) is the cutting element 114 closest
to the rotational axis 112, while the cutting element 114
identified by the number 31 is positioned farthest from the
rotational axis 112. In additional embodiments, the blades 106 may
include a different quantity of the cutting elements 114, such as
greater than 31 of the cutting elements 114, or less than 31 of the
cutting elements 114. Furthermore, in FIG. 1B, the subscript number
provided on the number identifying each of the cutting elements 114
correlates to the blade 106 upon which a particular cutting element
114 is located. The subscript number 1 corresponds to the first
primary blade 106A, the subscript number 2 corresponds to the first
secondary blade 106B, the subscript number 3 corresponds to the
second primary blade 106C, the subscript number 4 corresponds to
the second secondary blade 106D, the subscript number 5 corresponds
to the third primary blade 106E, and the subscript number 6
corresponds to the third secondary blade 106F. For example,
"1.sub.1" indicates that the cutting element 114 identified by the
number 1 is located on the first primary blade 106A, "2.sub.5"
indicates that the cutting element 114 identified by the number 2
is located on the third primary blade 106E, "3.sub.3" indicates
that the cutting element 114 identified by the number 3 is located
on the second primary blade 106C, "9.sub.4" indicates that the
cutting element 114 identified by the number 10 is located on the
second secondary blade 106D, "11.sub.2" indicates that the cutting
element 114 identified by the number 11 is located on the first
secondary blade 106B, "13.sub.6" indicates that the cutting element
114 identified by the number 12 is located on the third secondary
blade 106F, etc.
[0031] Referring to FIG. 1B, the cutting elements 114 may be
positioned (e.g., disposed, located) within different regions of
the body 102 (FIG. 1A). A first portion of the cutting elements 114
may be positioned within a cone region 116 outwardly radially
adjacent the rotational axis 112, a second portion of the cutting
elements 114 may be positioned within a nose region 118 outwardly
radially adjacent the cone region 116, a third portion of the
cutting elements 114 may be positioned within a flank region 120
outwardly radially adjacent the nose region 118, a fourth portion
of the cutting elements 114 may be positioned within a shoulder
region 122 outwardly radially adjacent the flank region 120, and a
fifth portion of the cutting elements 114 may be positioned within
a gage region 124 outwardly radially adjacent the shoulder region
122. By way of non-limiting example, as shown in FIG. 1B, the
cutting elements 114 identified by numbers 1 through 6 may be
positioned within the cone region 116; the cutting elements 114
identified by numbers 7 through 15 may be positioned within the
nose region 118; the cutting elements 114 identified by numbers 16
through 22 may be positioned within the flank region 120; the
cutting elements 114 identified by numbers 23 through 25 may be
positioned within the shoulder region 122; and the cutting element
114 identified by numbers 26 through 31 may be positioned within
the gage region 124.
[0032] In additional embodiments, the body 102 (FIG. 1A) may
exhibit one or more of a different quantity and a different
arrangement of the cutting elements 114 in one or more of the
different regions thereof. One or more of the different regions
may, for example, exhibit a greater quantity of the cutting
elements 114, a lower quantity of cutting elements 114, closer
radial spacing (e.g., separation) between at least some of the
cutting elements 114, and/or farther radial spacing between at
least some of the cutting elements 114. By way of non-limiting
example, the shoulder region 122 may exhibit greater than three (3)
cutting elements 114 therein, or less than three (3) cutting
elements 114 therein. The quantity of cutting elements 114 included
in the shoulder region 122 may be within a range of from one (1) to
a number corresponding to (e.g., the same as) the total number of
blades 106 included in the body 102. For example, in embodiments
where the body 102 includes six (6) blades 106, the shoulder region
122 may include from one (1) cutting element 114 to six (6) cutting
elements 114. As another example, in embodiments where the body 102
includes four (4) blades 106, the shoulder region 122 may include
from one (1) cutting element 114 to four (4) cutting elements 114.
Accordingly, while various embodiments herein describe or
illustrate the different regions of the body 102 as including
particular quantities and particular arrangements of the cutting
elements 114, one or more of the different regions (e.g., the
shoulder region 122) of the body 102 may, alternatively, include
one or more of a different quantity and different arrangement of
the cutting elements 114 therein.
[0033] Referring collectively to FIGS. 1A and 1B, the cutting
elements 114 in one or more of the different regions of the body
102 (FIG. 1A) may independently be disposed on any desired
combination of the primary blades 106A, 106C, 106E (FIG. 1A) and
the secondary blades 106B, 106D, 106F (FIG. 1A). For example, if
the shoulder region 122 (FIG. 1B) includes three (3) of the cutting
elements 114 (e.g., the cutting elements 114 identified by numbers
23, 24, and 25), one (1) of the cutting elements 114 (e.g., the
cutting element 114 identified by the number 24) may be located on
one of the primary blades 106A, 106C, 106E (e.g., the first primary
blade 106A), and two (2) of the cutting elements 114 (e.g., the
cutting elements 114 identified by the numbers 23 and 25) may be
located on two (2) of the secondary blades 106B, 106D, 106F (e.g.,
the first secondary blade 106B and the third secondary blade 106F)
circumferentially adjacent the one (1) of the primary blades 106A,
106C, 106E. In additional embodiments, one (1) of the cutting
elements 114 may be located on one (1) of the secondary blades
106B, 106D, 106F, and two (2) of the cutting elements 114 may be
located on two (2) of the primary blades 106A, 106C, 106E
circumferentially adjacent the one (1) of the secondary blades
106B, 106D, 106F. In further embodiments, such as in embodiments
within the body 102 includes a different quantity of the blades 106
(e.g., e.g., a different quantity of primary blades and/or a
different quantity of secondary blades) and/or a different quantity
of the cutting elements 114 in the shoulder region 122, the cutting
elements 114 within the shoulder region 122 may be disposed on
primary blades (e.g., the primary blades 106A, 106C, 106E) and/or
secondary blades (e.g., the secondary blades 106B, 106D, 106F) in a
different arrangement that that depicted in FIGS. 1A and 1B.
[0034] The cutting elements 114 may be provided on the blades 106
in any desired spiral configuration, such as a reverse spiral
configuration, a forward spiral configuration, or a combination
thereof. As used herein, the term "reverse spiral configuration"
means and includes a configuration wherein neighboring cutting
elements are positioned on an earth-boring tool (e.g., a rotary
drill bit) so as to form an arcuate (e.g., curved) path extending
from a cutting element more radially proximate a rotational axis of
the earth-boring tool to another cutting element more radially
distal from the rotational axis in the rotational direction of the
earth-boring tool. For example, a first cutting element may be
positioned on a first of the blades 106, and a second cutting
element radially adjacent the first cutting element, but radially
distal from the rotational axis 112 of the rotary drill bit 100
relative to the first cutting element, may be positioned on a
second of the blades 106 that rotationally leads the first of the
blades 106. Conversely, as used herein, the term "forward spiral
configuration" means and includes a configuration wherein
neighboring cutting elements are positioned on an earth-boring tool
(e.g., a rotary drill bit) so as to form an arcuate path extending
from a cutting element more radially proximate a rotational axis of
the earth-boring tool bit to another cutting element more radially
distal from the rotational axis in a direction opposite (e.g.,
against) the rotational direction of the earth-boring tool. For
example, a first cutting element may be positioned on a first of
the blades 106, and a second cutting element radially adjacent the
first cutting element, but radially distal from the rotational axis
112 of the rotary drill bit 100 relative to the first cutting
element, may be positioned on a second of the blades 106 that
rotationally trails the first of the blades 106. In some
embodiments, some of the cutting elements 114 are provided on the
blades 106 in a reverse spiral configuration, and other of the
cutting elements 114 are provided on the blades 106 in a forward
spiral configuration. For example, at least some of the cutting
elements 114 provided within one or more of the different regions
of the body 102 (e.g., one or more of the cone region 116, the nose
region 118, the flank region 120, the shoulder region 122, and the
gage region 124 shown in FIG. 1B) may be provided on the blades 106
in a first spiral configuration, and at least some other of the
cutting elements 114 provided within one or more other of the
different regions of the body 102 (e.g., one or more other of the
cone region 116, the nose region 118, the flank region 120, the
shoulder region 122, and the gage region 124 shown in FIG. 1B) may
be provided on the blades 106 in a second, opposite spiral
configuration. As shown in FIGS. 1A and 1B, in some embodiments,
the cutting elements 114 (e.g., the cutting elements 114 identified
by numbers 23 through 25) within the shoulder region 122 (FIG. 1B)
of the body 102 are provided in a forward spiral configuration, and
the cutting elements 114 (e.g., the cutting elements 114 identified
by numbers 1 through 22 and 26 through 31) within the other regions
(e.g., the cone region 116, the nose region 118, the flank region
120, and the gage region 124) of the body 102 are provided in a
reverse spiral configuration.
[0035] With continued reference to FIGS. 1A and 1B, at least some
of the cutting elements 114 located within the shoulder region 122
of the body 102 may exhibit a different size (e.g., diameter,
lateral extent) than at least some other of the cutting elements
114 located within the other regions of the body 102. As a
non-limiting example, at least a portion (e.g., each) of the
cutting elements 114 (e.g., the cutting elements 114 identified by
the numbers 23 through 25) located within the shoulder region 122
of the body 102 may exhibit a larger size (e.g., a larger diameter,
a larger lateral extent) than at least a portion (e.g., each) of
the cutting elements 114 (e.g., the cutting elements 114 identified
by the numbers 1 through 22 and 26 through 31) in one or more
(e.g., each) of the cone region 116, the nose region 118, the flank
region 120, and the gage region 124 of the body 102. In some
embodiments, the cutting elements 114 in each of the cone region
116, the nose region 118, the flank region 120, and the gage region
124 of the body 102 exhibit substantially the same size as one
another, and at least one of the cutting elements 114 in the
shoulder region 122 of the body 102 exhibits at least one size
larger than the substantially uniform size of the cutting elements
114 within the other regions of the body 102. As described in
further detail below, the sizes and arrangements of the cutting
elements 114 within the shoulder region 122 may be selected to
control how the cutting elements 114 engage surfaces of a
subterranean formation to form a borehole exhibiting desirable
dimensions (e.g., a desirable outermost diameter) and to control
work rates of the cutting elements 114 within the shoulder region
122.
[0036] At least some of the cutting elements 114 within the
shoulder region 122 of the body 102 (FIG. 1A) exhibit a different
size (e.g., diameter, lateral extent) than at least some other of
the cutting elements 114 within the shoulder region 122. For
example, as shown in FIG. 1B, the cutting element 114 identified by
the number 23 may exhibit a larger diameter than the cutting
element 114 identified by the number 24, and the cutting element
114 identified by the number 24 may have a larger diameter than the
cutting element 114 identified by the number 23. The size of each
of the cutting elements 114 within the shoulder region 122 may be
selected at least partially based on a desired engagement of a
subterranean formation by the cutting elements 114 during use and
operation of the rotary drill bit 100 (FIG. 1A). The sizes of the
cutting elements 114 within the shoulder region 122 may be selected
relative to one another to facilitate the more efficient formation
of a borehole exhibiting a larger outer diameter than would
otherwise be formed if the cutting elements 114 within the shoulder
region 122 exhibited the substantially the same size as one another
and/or substantially the same size as the cutting elements 114
within the other regions of the body 102. A ratio between a size of
a first, relatively smaller cutting element 114 within the shoulder
region 122 and a size of a second, relatively larger cutting
element 114 within the shoulder region 122 may, for example, be
within a range of from about 0.32:1 to about 0.84:1. The cutting
elements 114 within the shoulder region 122 may exhibit two (2) or
more different sizes than one another within a range of about 8
millimeters (mm) to about 25 mm. For example, at least one of the
cutting elements 114 within the shoulder region 122 may exhibit a
size selected from the group consisting of 8 mm, 11 mm, 13 mm, 16
mm, 19 mm, and 25 mm; and at least one other of the cutting
elements 114 within the shoulder region 122 may exhibit a different
size selected from the group consisting of 8 mm, 11 mm, 13 mm, 16
mm, 19 mm, and 25 mm. In some embodiments, a first of the cutting
elements 114 within the shoulder region 122 exhibits a size of
about 16 mm, a second of the cutting elements 114 within the
shoulder region 122 exhibits a size of about 19 mm, and a third of
the cutting elements 114 within the shoulder region 122 exhibits a
size of about 25 mm. In additional embodiments, one or more of the
cutting elements 114 within the shoulder region 122 may exhibit a
different size within the range of from about 8 mm to about 25 mm
so long as at least two (2) of the cutting elements 114 within the
shoulder region 122 exhibit different sizes than one another. Table
1 below presents a non-limiting list of cutting element sizes and
cutting element size ratios that may be employed in combination
within the shoulder region 122 of the body 102.
TABLE-US-00001 TABLE 1 Exemplary Cutting Element Sizes and Cutting
Element Size Ratios Ratio Cutting Element Size 11 13 16 19 25 8
0.73 0.62 0.50 0.42 0.32 11 X 0.85 0.69 0.58 0.44 13 X X 0.81 0.68
0.52 16 X X X 0.84 0.64 19 X X X X 0.76 25 X X X X X
[0037] Each of the cutting elements 114 within the shoulder region
122 of the body 102 may exhibit a different size than each other of
the cutting elements 114 within the shoulder region 122 of the body
102. For example, each of the cutting elements 114 identified by
the numbers 23 through 25 may exhibit a different size than each
other of the cutting elements 114 identified by the numbers 23
through 25. Alternatively, at least one of the cutting elements 114
within the shoulder region 122 of the body 102 may exhibit
substantially the same size as at least one other of the cutting
elements 114 within the shoulder region 122 of the body 102, so
long as at least two (2) of the cutting elements 114 within the
shoulder region 122 of the body 102 exhibit different sizes than
one another. For example, one (1) of the cutting elements 114
identified by the numbers 23 through 25 may exhibit substantially
the same size as one (1) other of the cutting elements 114
identified by the numbers 23 through 25. In some embodiments, each
of the cutting elements 114 within the shoulder region 122 of the
body 102 exhibits a different size than each other of the cutting
elements 114 within the shoulder region 122.
[0038] The cutting elements 114 within the shoulder region 122 of
the body 102 may each independently exhibit any desired shape, such
as a cylindrical shape, a conical shape, a frustoconical shape,
truncated versions thereof, or an irregular shape. As shown in FIG.
1A, in some embodiments, each of the cutting elements 114 within
the shoulder region 122 (FIG. 1B) independently exhibits a
generally cylindrical shape (e.g., a circular cylinder shape).
Accordingly, as shown in FIG. 1B, each of the cutting elements 114
within the shoulder region 122 may exhibit a substantially circular
cross-sectional shape. In additional embodiments, at least one of
the cutting elements 114 within the shoulder region 122 exhibits a
different shape. By way of non-limiting example, FIG. 2 shows a
cutter and blade profile for a rotary drill bit in accordance with
additional embodiments of the disclosure. To avoid repetition, not
all features shown in FIG. 2 are described in detail herein.
Rather, unless described otherwise below, features designated by a
reference numeral that is a 100 increment of the reference numeral
of a feature described previously in relation to one or more of
FIGS. 1A and 1B will be understood to be substantially similar to
the feature described previously. As shown in FIG. 2, at least one
of the cutting elements 214 within the shoulder region 222 may
exhibit a non-cylindrical shape (e.g., a conical shape, a
frustoconical shape, truncated versions thereof, an irregular
shape). One or more of the cutting elements 214 within the shoulder
region 222 (e.g., the cutting element 214 identified by the number
25) may, for example, exhibit a generally frustoconical shape. In
such embodiments, the non-cylindrical shape of one or more of the
cutting elements 214 within the shoulder region 222 may facilitate
a different type of engagement with a subterranean formation than
would otherwise be provided by cutting elements 214 exhibiting
generally cylindrical shapes. For example, one or more of the
cutting elements 214 exhibiting a non-cylindrical shape may
facilitate one or more of crushing and gouging a subterranean
formation when the rotary drill bit is rotated under applied force
to form or enlarge a borehole, whereas one or more of the cutting
elements 214 exhibiting a cylindrical shape may facilitate shearing
the subterranean formation when the rotary drill bit is rotated
under the applied force.
[0039] With returned reference to FIGS. 1A and 1B, the cutting
elements 114 within the shoulder region 122 of the body 102 may be
provided in any desired arrangement relative to one another. The
arrangement of the cutting elements 114 within the shoulder region
122 of the body 102 at least partially depends on a desired work
rate of each of the cutting elements 114 within the shoulder region
122 during use and operation of the rotary drill bit 100. For
example, the cutting elements 114 within the shoulder region 122
may be radially and circumferentially positioned relative to one
another along the body 102 (FIG. 1A) such that each of the cutting
elements 114 within the shoulder region 122 at least partially cuts
(e.g., shears, gouges, crushes, abrades) a different portion of a
subterranean formation to define an outermost diameter of a
borehole in the subterranean formation. Put another way, the
cutting elements 114 within the shoulder region 122 may be radially
and circumferentially positioned relative to one another so as to
share the work of forming or enlarging the outermost diameter of
the borehole.
[0040] In some embodiments, at least one of the cutting elements
114 within the shoulder region 122 exhibiting a relatively larger
size (e.g., a relatively larger diameter, a relatively larger
lateral extent) is provided at a position that rotationally leads a
position of at least one other of the cutting elements 114 within
the shoulder region 122 exhibiting a relatively smaller size (e.g.,
a relatively smaller diameter, a relatively smaller lateral extent)
during use and operation of the rotary drill bit 100 (FIG. 1A). By
way of non-limiting example, the cutting element 114 identified by
the number 23 may be relatively larger than and may rotationally
lead the cutting element 114 identified by the number 24, and the
cutting element 114 identified by the number 24 may be relatively
larger than and may rotationally lead the cutting element 114
identified by the number 25. Each relatively larger cutting element
114 within the shoulder region 122 may be positioned directly
radially adjacent a relatively smaller cutting element 114
rotationally trailing the relatively larger cutting element 114; or
at least one relatively larger cutting element 114 within the
shoulder region 122 may be radially separated from at least one
relatively smaller cutting element 114 rotationally trailing the
relatively larger cutting element 114 by at least one other cutting
element 114 exhibiting a size greater than or equal to that of the
relatively larger cutting element 114. As used herein, cutting
elements that are "directly radially adjacent" one another refers
to cutting elements radially neighboring one another on a face
profile of a rotary drill bit without another cutting element
radially positioned there between. In some embodiments, each
relatively larger cutting element 114 within the shoulder region
122 is positioned directly radially adjacent a relatively smaller
cutting element 114 rotationally trailing the relatively larger
cutting element 114. For example, as shown in FIG. 1B, the cutting
element 114 identified by the number 23 may be relatively larger
than and may be positioned directly radially adjacent the cutting
element 114 identified by the number 24, and the cutting element
114 identified by the number 24 may be relatively larger than and
may be positioned directly radially adjacent cutting element 114
identified by the number 25.
[0041] As shown in FIG. 1B, one or more of the relatively smaller,
rotationally trailing cutting elements 114 within the shoulder
region 122 may be underexposed with respect to one or more of the
relatively larger, rotationally leading cutting elements 114 within
the shoulder region 122. By way of non-limiting example, the
cutting element 114 identified by the number 24 may be underexposed
with respect to the cutting element 114 identified by the number
23, and the cutting element 114 identified by the number 25 may be
underexposed with respect to the cutting element 114 identified by
the number 24. The degree to which relatively smaller, rotationally
trailing cutting elements 114 within the shoulder region 122 are
underexposed with respect to relatively larger, rotationally
leading cutting elements 114 within the shoulder region 122 at
least partially depends on the properties of the subterranean
formation to be acted upon by the rotary drill bit 100 (FIG. 1A); a
desired ROP for the rotary drill bit 100; the relative sizes,
shapes, and spacing (e.g., radial and circumferential separation)
of the cutting elements 114 within the shoulder region 122; the
quantity of cutting elements 114 within the shoulder region 122;
the presence or absence of chamfers on cutting faces of the cutting
elements 114 within the shoulder region 122; and backrake angles of
the cutting elements 114 within the shoulder region 122. The
relatively larger, more highly exposed cutting elements 114 within
the shoulder region 122 may apply focused energy applied to the
rotary drill bit 100 (FIG. 1A) from weight on bit (WOB) and bit
rotation to fracture the subterranean formation, and the relatively
smaller, less exposed cutting elements 114 within the shoulder
region 122 may clear and widen grooves made in the subterranean
formation by the relatively larger, more highly exposed cutting
elements 114 within the shoulder region 122. In additional
embodiments, one or more rotationally trailing cutting elements 114
within the shoulder region 122 may have the same exposure as one or
more rotationally leading cutting elements 114 within the shoulder
region 122.
[0042] FIGS. 3 through 5 are schematic views showing non-limiting
examples of different cutting element exposure configurations that
may be present in a shoulder region (e.g., the shoulder region 122
shown in FIG. 1B) of a body (e.g., the body 102 shown in FIG. 1A)
of a rotary drill bit (e.g., the rotary drill bit 100 shown in FIG.
1A) according to embodiments of the disclosure. As shown in FIG. 3,
in some embodiments, at least one relatively larger cutting element
302 (e.g., corresponding to the cutting element 114 identified by
the number 23 in FIG. 1B) and at least one relatively smaller
cutting element 304 (e.g., corresponding to the cutting element 114
identified by the number 24 in FIG. 1B) are radially positioned
relative to one another such that rotational paths for the
relatively larger cutting element 302 and the relatively smaller
cutting element 304 during drilling in the direction D overlap one
another proximate outermost lateral boundaries of the rotational
paths. As shown in FIG. 4, in additional embodiments, at least one
relatively larger cutting element 402 (e.g., corresponding to the
cutting element 114 identified by the number 23 in FIG. 1B) and at
least one relatively smaller cutting element 404 (e.g.,
corresponding to the cutting element 114 identified by the number
24 in FIG. 1B) are radially positioned relative to one another such
that rotational paths for the larger cutting element 402 and the
smaller cutting element 404 during drilling in the direction D
overlap one another proximate lowermost longitudinal boundaries of
the rotational paths. As shown in FIG. 5, in further embodiments,
at least one relatively larger cutting element 502 (e.g.,
corresponding to the cutting element 114 identified by the number
23 in FIG. 1B) and at least one relatively smaller cutting element
504 (e.g., corresponding to the cutting element 114 identified by
the number 24 in FIG. 1B) are radially positioned relative to one
another within the shoulder region such that rotational paths for
the larger cutting element 502 and the smaller cutting element 504
during drilling in the direction D overlap one another at a
location intermediate between outermost lateral boundaries and
lowermost longitudinal boundaries of the rotational paths.
[0043] Returning briefly to FIGS. 1A and 1B, in additional
embodiments, at least one relatively larger cutting element 114
within the shoulder region 122 (FIG. 1B) is provided at a position
that rotationally trails at least one relatively smaller cutting
element 114 within the shoulder region 122 during use and operation
of the rotary drill bit 100 (FIG. 1A). By way of non-limiting
example, FIG. 6 shows a cutter and blade profile for a rotary drill
bit in accordance with additional embodiments of the disclosure. To
avoid repetition, not all features shown in FIG. 6 are described in
detail herein. Rather, unless described otherwise below, features
designated by a reference numeral that is a 100 increment of the
reference numeral of a feature described previously in relation to
one or more of FIGS. 1A and 1B will be understood to be
substantially similar to the feature described previously. As shown
in FIG. 6, in some embodiments, at least one cutting element 614
within a shoulder region 622 exhibiting a relatively smaller size
(e.g., a relatively smaller diameter, a relatively smaller lateral
extent) is provided at a position that rotationally leads a
position of at least one other of the cutting elements 614 within
the shoulder region 622 exhibiting a relatively larger size (e.g.,
a relatively larger diameter, a relatively larger lateral extent).
By way of non-limiting example, the cutting element 614 identified
by the number 22 may be relatively smaller than and may
rotationally lead the cutting element 614 identified by the number
24, and the cutting element 614 identified by the number 24 may be
relatively smaller than and may rotationally lead the cutting
element 614 identified by the number 25. Each relatively smaller
cutting element 614 within the shoulder region 622 may be
positioned directly radially adjacent a relatively larger cutting
element 614 rotationally trailing the relatively smaller cutting
element 614; or at least one relatively smaller cutting element 614
within the shoulder region 622 may be radially separated from at
least one relatively larger cutting element 614 rotationally
trailing the relatively smaller cutting element 614 by at least one
other cutting element 614 exhibiting a size less than or equal to
that of the relatively smaller cutting element 614.
[0044] With continued reference to FIG. 6, one or more of the
relatively larger, rotationally trailing cutting elements 614
within the shoulder region 622 may be underexposed with respect to
one or more of the relatively smaller, rotationally leading cutting
elements 614 within the shoulder region 622. By way of non-limiting
example, the cutting element 614 identified by the number 24
rotationally trailing and relatively larger than the cutting
element 614 identified by the number 22 may be underexposed with
respect to the cutting element 614 identified by the number 22, and
the cutting element 614 identified by the number 25 rotationally
trailing and relatively larger than the cutting element 614
identified by the number 24 may be underexposed with respect to the
cutting element 614 identified by the number 24. The degree to
which relatively larger, rotationally trailing cutting elements 614
within the shoulder region 622 are underexposed with respect to
relatively smaller, rotationally leading cutting elements 614
within the shoulder region 622 at least partially depends on the
properties of the subterranean formation to be acted upon by the
rotary drill bit; a desired ROP for the rotary drill bit; the
relative sizes, shapes, and spacing (e.g., radial and
circumferential separation) of the cutting elements 614 within the
shoulder region 622; the quantity of cutting elements 614 within
the shoulder region 622; the presence or absence of chamfers on
cutting faces of the cutting elements 614 within the shoulder
region 622; and backrake angles of the cutting elements 614 within
the shoulder region 622. The relatively smaller, more highly
exposed cutting elements 614 within the shoulder region 622 may
apply focused energy applied to the rotary drill bit from WOB and
bit rotation to fracture the subterranean formation, and the
relatively larger, less exposed cutting elements 614 within the
shoulder region 622 may clear and widen grooves made in the
subterranean formation by the relatively smaller, more highly
exposed cutting elements 614 within the shoulder region 622. In
additional embodiments, one or more rotationally trailing cutting
elements 614 within the shoulder region 622 may have the same
exposure as one or more rotationally leading cutting elements 614
within the shoulder region 622.
[0045] In use and operation, a rotary drill bit according to an
embodiment of the disclosure (e.g., the rotary drill bit 100) may
be rotated about its rotational axis (e.g., the rotational axis
112, 212, 612) in a borehole extending into a subterranean
formation. As the rotary drill bit rotates under applied WOB, at
least some of the cutting elements thereof (e.g., at least some of
the cutting elements 114, 214, 614) provided in rotationally
leading positions across the body of the rotary drill bit engage
surfaces of the borehole and cut e.g., shear, gouge, crush, abrade)
portions of the subterranean formation, forming grooves in the
subterranean formation. Additional cutting elements provided in
rotationally trailing positions may then follow and enlarge the
grooves formed by the rotationally leading cutting elements. The
cutting elements provided in the shoulder region (e.g., the
shoulder region 122, 222, 622) of the body of the rotary drill bit
may share the work of forming and/or enlarging the outermost
diameter of the borehole through the formation and/or enlargement
of such grooves.
[0046] FIG. 7 shows a perspective view of a segment of a borehole
700 that may be formed in a subterranean formation using a rotary
drill bit according to embodiments of the disclosure. The borehole
700 may, for example, be formed in the subterranean formation using
a rotary drill bit (e.g., the rotatory drill bit 100 shown in FIG.
1A) having the cutter and blade profile shown in FIG. 1B. As shown
in FIG. 7, the borehole 700 may exhibit an overall lateral groove
701 at least partially defining an outmost diameter of the borehole
700 and formed from a first groove 702, a second groove 704, and a
third groove 706. The second groove 704 may overlap the first
groove 702, and the third groove 706 may overlap one or more of the
first groove 702 and the second groove 704. Referring collectively
to FIGS. 1B and 7, the first groove 702, the second groove 704, and
the third groove 706 may respectively be formed by the cutting
elements 114 (FIG. 1B) identified by the numbers 23, 24, and 25
(FIG. 1B) within the shoulder region 122 (FIG. 1B) of the body 102
(FIG. 1A) of the rotary drill bit 100 (FIG. 1A). During the
formation of the borehole 700, the relatively larger, rotationally
leading cutting element 114 identified by the number 23 may
fracture the subterranean formation to form the first groove 702,
the relatively smaller cutting element 114 identified by the number
24 may fracture a remaining portion of the subterranean formation
surrounding the first groove 702 to form the second groove 704, and
then the even relatively smaller cutting element 114 identified by
the number 25 may fracture a further remaining portion of the
subterranean formation surrounding the first groove 702 and/or the
second groove 704 to form the third groove 706. Accordingly, the
second groove 704 may widen and refine the first groove 702, and
the third groove 706 may further widen and refine the widened
groove formed from the first groove 702 and the second groove 704
to form the overall lateral groove 701.
[0047] FIG. 8 shows a perspective view of a segment of a borehole
800 that may be formed in a subterranean formation using a rotary
drill bit according to additional embodiments of the disclosure.
The borehole 800 may, for example, be formed in the subterranean
formation using a rotary drill bit having the cutter and blade
profile shown in FIG. 6. As shown in FIG. 8, the borehole 800 may
exhibit an overall lateral groove 801 at least partially defining
an outmost diameter of the borehole 800 and formed from a first
groove 802, a second groove 804, and a third groove 806. The second
groove 804 may overlap the first groove 802, and the third groove
806 may overlap one or more of the first groove 802 and the second
groove 804. Referring collectively to FIGS. 6 and 8, the first
groove 802, the second groove 804, and a third groove 806 may
respectively be formed by the cutting elements 614 (FIG. 6)
identified by the numbers 22, 24, and 25 (FIG. 6) within the
shoulder region 622 (FIG. 6) of a body of the rotary drill bit.
During the formation of the borehole 800, the relatively smaller,
rotationally leading cutting element 614 identified by the number
22 may fracture the subterranean formation to form the first groove
802, the relatively larger cutting element 614 identified by the
number 24 may fracture a remaining portion of the subterranean
formation surrounding the first groove 802 to form the second
groove 804, and then even relatively larger cutting element 614
identified by the number 25 may fracture a further remaining
portion of the subterranean formation surrounding the first groove
802 and/or the second groove 804 to form the third groove 806.
Accordingly, the second groove 804 may widen and refine the first
groove 802, and the third groove 806 may further widen and refine
the widened groove formed from the first groove 802 and the second
groove 804 to form the overall lateral groove 801.
[0048] The apparatuses and methods according to embodiments of the
disclosure advantageously facilitate the efficient formation of
boreholes exhibiting desirable outer diameters in a subterranean
formation. The cutting element configurations (e.g., sizes, shapes,
material compositions) and layouts (e.g., positions, spacing) of
the disclosure permit cutting elements (e.g., the cutting elements
114, 214, 614) positioned within a shoulder region (e.g., the
shoulder regions 122, 222, 622) of a body of a rotary drill bit
(e.g., the rotary drill bit 100) to share the work of forming the
outer diameter of a borehole, more evenly distributing damage
across the cutting elements, and extending operational life of the
rotary drill bit as compared to conventional rotary drill bits
including conventional cutting element configurations and
layouts.
[0049] While certain embodiments have been described and shown in
the accompanying drawings, such embodiments are merely illustrative
and not restrictive of the scope of the disclosure, and this
disclosure is not limited to the specific constructions and
arrangements shown and described, since various other additions and
modifications to, and deletions from, the described embodiments
will be apparent to one of ordinary skill in the art. The scope of
the invention, as exemplified by the various embodiments of the
present disclosure, is limited only by the claims which follow, and
their legal equivalents.
* * * * *