U.S. patent application number 16/601257 was filed with the patent office on 2020-02-06 for methods of using elastomeric components.
The applicant listed for this patent is Schlumberger Technology Corporation. Invention is credited to Manuel Marya, Xiaohong Ren, Jushik Yun.
Application Number | 20200040692 16/601257 |
Document ID | / |
Family ID | 60675946 |
Filed Date | 2020-02-06 |
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United States Patent
Application |
20200040692 |
Kind Code |
A1 |
Yun; Jushik ; et
al. |
February 6, 2020 |
METHODS OF USING ELASTOMERIC COMPONENTS
Abstract
A method includes fitting an elastomeric component about a
perimeter surface of a tool that includes a longitudinal axis, the
elastomeric component including carbon-based nanoplatelets in an
elastomeric matrix; and tripping the tool into a bore in a geologic
formation.
Inventors: |
Yun; Jushik; (Sugar Land,
TX) ; Ren; Xiaohong; (Sugar Land, TX) ; Marya;
Manuel; (Rosharon, TX) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
Schlumberger Technology Corporation |
Sugar Land |
TX |
US |
|
|
Family ID: |
60675946 |
Appl. No.: |
16/601257 |
Filed: |
October 14, 2019 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
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15191090 |
Jun 23, 2016 |
10443339 |
|
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16601257 |
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Current U.S.
Class: |
1/1 |
Current CPC
Class: |
C08J 5/005 20130101;
C08J 2300/26 20130101; B82Y 30/00 20130101; C08K 3/04 20130101;
E21B 33/1208 20130101 |
International
Class: |
E21B 33/12 20060101
E21B033/12; C08K 3/04 20060101 C08K003/04; C08J 5/00 20060101
C08J005/00 |
Claims
1. A method comprising: fitting an elastomeric component about a
perimeter surface of a tool that comprises a longitudinal axis, the
elastomeric component comprising carbon-based nanoplatelets in an
elastomeric matrix; and tripping the tool into a bore in a geologic
formation.
2. The method of claim 1, wherein the carbon-based nanoplatelets
comprise chemically modified carbon-based nanoplatelets.
3. The method of claim 1, further comprising compressing the
elastomeric component to expand an outer perimeter of the
elastomeric component.
4. The method of claim 1, further comprising surface treating the
carbon-based nanoplatelets.
5. The method of claim 1, wherein the elastomeric component that
comprises carbon-based nanoplatelets in an elastomeric matrix
comprises the carbon-based nanoplatelets at less than approximately
10 percent by weight.
6. The method of claim 1, wherein the carbon-based nanoplatelets of
the elastomeric component comprise an average maximum platelet
dimension less than approximately 50 microns.
7. The method of claim 1, wherein the carbon-based nanoplatelets of
the elastomeric component comprise an average platelet thickness
dimension less than approximately 10 nanometers.
8. The method of claim 1, wherein the fitting step comprises
fitting the elastomeric component about an inner perimeter surface
of the tool.
9. The method of claim 8, further comprising, after the fitting
step, expanding the elastomeric component in a radial direction to
alter an inner perimeter surface of the elastomeric component, an
outer perimeter of the elastomeric component remaining relatively
constant and in contact with the inner perimeter surface of the
elastomeric component.
10. The method of claim 8, further comprising, after the fitting
step, expanding the elastomeric component in a radial direction to
alter an inner perimeter surface of the elastomeric component, an
outer perimeter of the elastomeric component remaining relatively
constant and in contact with the inner perimeter surface of the
elastomeric component.
11. The method of claim 8, further comprising, after the fitting
step, contracting the elastomeric component in a radial direction
to alter an inner perimeter surface of the elastomeric component,
an outer perimeter of the elastomeric component remaining
relatively constant and in contact with the inner perimeter surface
of the elastomeric component.
12. The method of claim 1, wherein the fitting step comprises
fitting the elastomeric component about an outer perimeter surface
of the tool.
13. The method of claim 1, wherein the tool comprises a bore packer
assembly.
14. The method of claim 1, wherein the tool comprises slips.
15. A method comprising: fitting a first elastomeric component
about a perimeter surface of a tool that comprises a longitudinal
axis, the first elastomeric component comprising carbon-based
nanoplatelets in an elastomeric matrix; fitting a second
elastomeric component about the tool with respect to the first
elastomeric component; and tripping the tool into a bore in a
geologic formation.
16. The method of claim 15, wherein the first elastomeric component
and the second elastomeric component contact each other.
17. The method of claim 15, wherein an axial gap exists between the
first elastomeric component and the second elastomeric
component.
18. The method of claim 15, wherein the first elastomeric component
that comprises the carbon-based nanoplatelets in an elastomeric
matrix comprises the carbon-based nanoplatelets at less than
approximately 10 percent by weight.
19. The method of claim 15, wherein the tool comprises a bore
packer assembly.
20. The method of claim 15, wherein the tool comprises slips.
Description
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application is a divisional of U.S. Patent Application
Publication No. 2017/0370174, which was filed on Jun. 23, 2016, and
is incorporated by reference herein in its entirety.
BACKGROUND
[0002] Equipment used in the oil and gas industry may be exposed to
high-temperature and/or high-pressure environments. Such
environments may also be chemically harsh, for example, consider
environments that may include chemicals such as hydrogen sulfide,
carbon dioxide, etc. Various types of environmental conditions can
damage equipment.
SUMMARY
[0003] A method according to one or more embodiments of the present
disclosure includes fitting an elastomeric component about a
perimeter surface of a tool that includes a longitudinal axis, the
elastomeric component including carbon-based nanoplatelets in an
elastomeric matrix; and tripping the tool into a bore in a geologic
formation.
[0004] A method according to one or more embodiments of the present
disclosure includes fitting a first elastomeric component about a
perimeter surface of a tool that includes a longitudinal axis, the
first elastomeric component including carbon-based nanoplatelets in
an elastomeric matrix, fitting a second elastomeric component about
the tool with respect to the first elastomeric component, and
tripping the tool into a bore in a geologic formation. Various
other apparatuses, systems, methods, etc., are also disclosed.
[0005] This summary is provided to introduce a selection of
concepts that are further described below in the detailed
description. This summary is not intended to identify key or
essential features of the claimed subject matter, nor is it
intended to be used as an aid in limiting the scope of the claimed
subject matter.
BRIEF DESCRIPTION OF THE DRAWINGS
[0006] Features and advantages of the described implementations can
be more readily understood by reference to the following
description taken in conjunction with the accompanying
drawings.
[0007] FIG. 1 illustrates examples of equipment in a geologic
environment;
[0008] FIG. 2 illustrates examples of equipment;
[0009] FIG. 3 illustrates an example of equipment;
[0010] FIG. 4 illustrates examples of a packer assemblies;
[0011] FIG. 5 illustrates examples of structures;
[0012] FIG. 6 illustrates examples of structures;
[0013] FIG. 7 illustrates an example of a method;
[0014] FIG. 8 illustrates an example of a method;
[0015] FIG. 9 illustrates an example of a plot;
[0016] FIG. 10 illustrates an example of a plot;
[0017] FIG. 11 illustrates an example of a plot;
[0018] FIG. 12 illustrates an example of a method;
[0019] FIG. 13 illustrates an example of equipment;
[0020] FIG. 14 illustrates examples of equipment;
[0021] FIG. 15 illustrates an example of a method;
[0022] FIG. 16 illustrates an example of a method;
[0023] FIG. 17 illustrates an example of a system; and
[0024] FIG. 18 illustrates example components of a system and a
networked system.
DETAILED DESCRIPTION
[0025] The following description includes the best mode presently
contemplated for practicing the described implementations. This
description is not to be taken in a limiting sense, but rather is
made merely for the purpose of describing the general principles of
the implementations. The scope of the described implementations
should be ascertained with reference to the issued claims.
[0026] An elastomeric material can include one or more types of
polymers that can be characterized by viscoelasticity (e.g.,
viscosity and elasticity) that results in a relatively low Young's
modulus (E) and a relatively high failure strain in comparison with
non-elastomeric materials. As an example, an elastomeric material
or elastomer may include or be rubber, which can be a vulcanisate.
As an example, monomers that link to form polymers can include
carbon and hydrogen and, for example, oxygen and/or silicon.
Elastomers tend to be amorphous polymers existing above their glass
transition temperature, which can allow for segmental motion. At
ambient temperatures, rubbers tend to be relatively soft (e.g., E
of the order of about 3 MPa) and deformable.
[0027] Elastomers that exist without reinforcing material (e.g.,
reinforcement) can be limited for use in high-performance
applications as their strength may be about ten times lower than in
a reinforced state (e.g., as an elastomeric material that includes
one or more elastomers and one or more other types of
material).
[0028] As an example, a reinforcing material can include silica or
carbon-black. Such reinforcing materials find use as fillers in
elastomeric materials, which may be used to form elastomeric seals
(e.g., packers, plugs, misc. seals, etc.).
[0029] Packer elastomers can lose mechanical properties as
temperature increases. For example, mechanical properties of
hydrogenated nitrile butadiene rubber (HNBR) can be decreased at
temperatures of about 160 degrees C. (e.g., about 325 degrees F.)
and mechanical properties of AFLAS.TM. fluororubber (Asahi Glass
Co., Ltd., Tokyo, Japan) can be decreased at temperatures of about
220 degrees C. (e.g., about 425 degrees F.).
[0030] As an example, an elastomeric component may be formed via
mixing one or more elastomers (e.g., in polymer and/or monomer
forms) together with one or more types of fillers as
reinforcements. As an example, a method for forming an elastomeric
component or components may include curing (e.g., polymerization,
cross-linking, etc.). As an example, an elastomeric component can
be formed according to a mechanical design. For example, consider
an arrangement of components that can include one or more
elastomeric components and optionally one or more non-elastomeric
components (e.g., metal, hard plastic, ceramic, etc.).
[0031] As an example, a method can include additional of one or
more reinforcements, mixing, processing to form one or more
elastomeric components. As an example, a method can include adding
one or more types of nanoscale reinforcements. For example,
consider nanoscale particulate material that may be referred to as
nanoparticles, noting that a nanoscale particulate material can
include one or more dimensions that may be greater than nanoscale
(e.g., consider nanofibers, nanoplates, etc.). As an example,
nanoparticles may be particles that include a dimension or
dimensions in a range from about 1 to about 100 nanometers. As an
example, in nanotechnology, a particle may be defined as a small
object that behaves as a unit with respect to its transport and
properties. As an example, particles may be classified according to
a dimension such as diameter and/or, for example, a maximum
dimension and a minimum dimension. As an example, ultrafine
particles can be particles that include a dimension (e.g.,
diameter) in a range of about 1 to about 100 nanometers; whereas,
fine particles may be larger (e.g., in a range of about 100 to
about 2,500 nanometers).
[0032] As an example, an elastomeric material may be utilized as
part of a packer. As an example, a packer can be a device or part
of a device, an assembly, a system, etc., that can be run into a
bore where the packer includes an initial outside dimension (e.g.,
diameter, radius, etc.) that can be expanded, for example, to form
a seal (e.g., with the bore). In such an example, a bore may be a
bore of tubing, casing, etc. or, for example, a bore may be an
earthen bore (e.g., a rock formation bore, etc.).
[0033] As an example, a packer can employ one or more elastomeric
components (e.g., elastomeric elements) that can be expanded. For
example, consider a production or test packer and an inflatable
packer. As to a production or test packer, expansion may be
accomplished by squeezing one or more elastomeric elements, which
may be somewhat doughnut shaped, between plates to thereby force
the one or more elastomeric elements to bulge (e.g., outwardly). As
to an inflatable packer, expansion may be accomplished by pumping a
fluid into a bladder where fluid pressure causes the packer to
expand. As an example, a production or test packer may be set in a
cased hole and an inflatable packer may be used in an open hole or
a cased hole. As an example, a packer may be run on wireline, pipe
and/or coiled tubing. As an example, a packer may be designed to be
removable and/or may be designed to be permanent. As an example, a
permanent packer may be constructed of one or more materials that
can be drilled and/or milled out.
[0034] As an example, a packer can be a downhole device that can be
used in a completion to isolate an annulus from production conduit,
which may allow for enabling controlled production, injection
and/or treatment. As an example, a packer assembly can include a
securing mechanism that can secure the packer against a casing
and/or a liner wall. For example, consider a slip arrangement and a
mechanism that can create a reliable hydraulic seal to isolate an
annulus, for example, via an expandable elastomeric element. As an
example, a packer may be classified by one or more types of
applications of use, one or more setting methods and/or
retrievability and/or permanence.
[0035] As an example, an elastomeric material may be utilized to
form a packer or one or more other types of elastomeric components.
As an example, such a component or components may be formulated
with one or more reinforcing materials to raise one or more
operational limits when compared to elastomers without such one or
more reinforcing materials (e.g., NBR, HNBR, AFLAS.TM.
fluororubber, EPDM (e.g., Ethylene-Propylene-Diene-Monomer rubber),
etc.). As an example, an elastomeric material may provide for use
in a greater H.sub.2S concentration environment.
[0036] As an example, a packer can be or include an elastomeric
ring that may be expanded radially in one or more of various
manners such as, for example, via mechanical manipulation (e.g.,
rotation, etc.), inflation, compression, etc. As an example, force
to compress an elastomeric ring may be provided by hydraulic
pressure, weight and/or other mechanism. As an example, a wellbore
operation being performed may dictate a type of packer to be
utilized (e.g., inflatable, hydraulically set, weight set, etc.)
and may dictate whether a packer is to be retrievable or
permanent.
[0037] As an example, one or more packers may be utilized in a
wellbore testing operation such as, for example, a drillstem
testing operation ("DST"). For example, for the purpose of
measuring a characteristic of a well (e.g., formation pressure,
flow rates, etc.) of a subterranean formation, a tubular test
string may be dispose in a wellbore that extends into the
formation. To test a particular region, or zone, of the formation
the test string may include a perforating gun that is used to form
perforation tunnels, or fractures, in portions of the formation
surrounding the wellbore, optionally via perforations through
casing. In such an example, to isolate a test zone (e.g., from a
surface of the well), the test string may carry a packer to be set
at the desired location in the well.
[0038] As an example, a geologic environment or downhole
environment may be a harsh environment and/or an environment that
may be classified as being a high-pressure and high-temperature
environment. A so-called HPHT environment may include pressures up
to about 138 MPa (e.g., about 20,000 psi) and temperatures up to
about 205 degrees C. (e.g., about 400 degrees F.), a so-called
ultra-HPHT environment may include pressures up to about 241 MPa
(e.g., about 35,000 psi) and temperatures up to about 260 degrees
C. (e.g., about 500 degrees F.) and a so-called HPHT-hc environment
may include pressures greater than about 241 MPa (e.g., about
35,000 psi) and temperatures greater than about 260 degrees C.
(e.g., about 500 degrees F.). As an example, an environment may be
classified based in one of the aforementioned classes based on
pressure or temperature alone. As an example, an environment may
have its pressure and/or temperature elevated, for example, through
use of equipment, techniques, etc. For example, a SAGD operation
may elevate temperature of an environment (e.g., by 100 degrees C.
or more).
[0039] As an example, an environment may be classified based at
least in part on its chemical composition. For example, where an
environment includes hydrogen sulfide (H.sub.2S), carbon dioxide
(CO.sub.2), etc., the environment may be corrosive to certain
materials. As an example, an environment may be classified based at
least in part on particulate matter that may be in a fluid (e.g.,
suspended, entrained, etc.). As an example, particulate matter in
an environment may be abrasive or otherwise damaging to equipment.
As an example, matter may be soluble or insoluble in an environment
and, for example, soluble in one environment and substantially
insoluble in another.
[0040] Conditions in a geologic environment may be transient and/or
persistent. Where equipment is placed within a geologic
environment, longevity of the equipment can depend on
characteristics of the environment and, for example, duration of
use of the equipment as well as function of the equipment. Where
equipment is to endure in an environment over a substantial period
of time, uncertainty may arise in one or more factors that could
impact integrity or expected lifetime of the equipment. As an
example, where a period of time may be of the order of decades,
equipment that is intended to last for such a period of time can be
constructed with materials that may be expected to endure
environmental conditions imposed thereon, whether imposed by an
environment or environments and/or one or more functions of the
equipment itself.
[0041] FIG. 1 is a schematic view of a packer assembly 10 that
includes one or more packers disposed in a bore 12 of a geologic
environment. In such an example, the packer assembly may be
referred to as a bore packer assembly, which may be a type of bore
tool (e.g., suitable for use in a bore formed in a geologic
environment). In the example of FIG. 1, the packer assembly 10 is
being utilized in well testing operation (e.g., drillstem testing).
As an example, the packer assembly 10 may be a hydraulically set,
retrievable packer that may be run downhole with a tubing, or test
string 14, and set (e.g., to form a test zone 16) by applying
hydraulic pressure via an annulus 18.
[0042] As an example, a packer assembly such as the packer assembly
10 may be placed in different configurations such as, for example,
a run-in-hole configuration, a set configuration, and a
pull-out-of-hole configuration. For example, the packer assembly 10
can be placed in a run-in-hole configuration before being lowered
into bore 12 on a conveyance, such as test string 14. Once the
packer assembly 10 is in a desired position in the bore 12,
pressure can be transmitted via fluid present in the annulus 18 to
place the packer assembly 10 in a set configuration in which one or
more packers of the packer assembly 10 secure (e.g., anchor)
themselves to a well casing 20 for isolating (e.g., sealing off)
the test zone 16 across the annulus 18. In such an example, this
permits the test string 14 to move through the packer assembly 10
while maintaining a seal between the interior of the one or more
packers of the packer assembly 10 and an exterior of the test
string 14. In the example of FIG. 1, after testing is complete, an
upward force may be applied to the test string 14 to place the
packer assembly 10 in a pull-out-of-hole configuration to disengage
the one or more packers of the packer assembly 10 from the casing
20.
[0043] As an example, the packer assembly 10 and the test string 14
may be allowed to linearly expand and contract without
implementation of one or more slip joints. As the test string 14 is
run downhole with the packer assembly 10, seals between the test
string 14 and the packer assembly 10 may remain protected as the
packer assembly 10 is lowered into and/or retrieved from the bore
12. In the example of FIG. 1, a perforating gun 22 can be
operatively coupled to the packer assembly 10, for example, to
create a perforation tunnel 7 through the casing 20 and into
portions of the subterranean formation 8. As an example, one or
more other tools may be included with the packer assembly 10, for
example, in addition to or replacing the perforating gun 22.
[0044] As shown in the example of FIG. 1, the packer assembly 10
includes a packer in the form of an annular, resilient elastomeric
seal element 24 that can be utilized to form an annular seal
between the exterior of the packer assembly 10 and the interior of
the casing 20 (e.g., in the set configuration of the packer
assembly 10). In such an example, the packer assembly 10 can be
configured to convert pressure exerted by fluid in the annulus 18
into a force to anchor the packer assembly 10 with the casing 20
and to compress the seal element 24. Such pressure may be a
combination of the hydrostatic pressure of a column of fluid in the
annulus 18 and, for example, pressure that is applied from the
surface 5 (e.g., pumped, etc.) via the annulus 18.
[0045] As an example, the packer assembly 10 can be structured to
transfer axial force (e.g., hydraulic force, etc.) across the
packer assembly 10, for example, to set slips 60 bypassing the
intervening elastomeric seal element 24 until the slips 60 are set
(e.g., engaging the casing 20). As an example, when compressed, the
seal element 24 can expand radially outward and form an annular
seal with the interior of the casing 20. As an example, the packer
assembly 10 can be constructed to hold the seal element 24 in a
compressed state until the packer assembly 10 is placed in a
pull-out-of-hole configuration, a configuration in which the packer
assembly 10 releases compressive forces on the seal element 24 and
allows the seal element 24 to assume a relaxed position.
[0046] In the example of FIG. 1, as an outer diameter of the seal
element 24, in the uncompressed state, may be closely matched to an
inner diameter of the casing 20, there may be a small annular
clearance between the seal element 24 and the casing 20 as the
packer assembly 10 is being retrieved from or lowered into the bore
12. As an example, to circumvent forces present as a result of a
small annular clearance, the packer assembly 10 may permit fluid to
flow through the packer assembly 10 (e.g., fluid bypass) when the
packer assembly 10 is being lowered into or retrieved from the bore
12. As an example, the packer assembly 10 may include one or more
radial bypass ports 26 that may be located above the seal element
24.
[0047] As an example, in a run-in-hole configuration, the packer
assembly 10 can be constructed to establish fluid communication
between one or more radial bypass ports 28 located below the seal
element 24 and one or more of the one or more radial ports 26. As
an example, in a pull-out-of-hole configuration, the packer
assembly 10 can be constructed to establish fluid communication
between one or more other radial ports 30, which may be located
below the seal element 24, and one or more of the one or more
radial ports 26. As an example, the one or more radial ports 26
above the seal element 24 may remain in an open state. However,
when the packer assembly 10 is set, the radial ports 30 and 28 can
be in a closed state. As an example, the packer assembly 10 can
include one or more radial ports 32 that may be used, for example,
to inject a kill fluid to halt production from a producing
formation. As shown, the one or more ports 32 can be located below
the seal element 24 in a lower housing 42 where each port may be a
part of a bypass valve.
[0048] FIG. 2 shows an example of a packer assembly 220 that
includes rings 221 and 223 disposed at ends of a packer 222
disposed about a tube 224, an example of a packer assembly 240 that
includes rings 241 and 243 disposed at ends of a first packer 242
and rings 245 and 247 disposed at ends of a second packer 246 where
the first and second packers 242 and 246 and the rings 241, 243,
245 and 247 are disposed about a tube 244, an example of a
multistage packer string 260 that includes packers 262 and 264,
slips 266 and a drag block 268 and examples of components of bore
tools and elastomeric components. As shown in the examples of FIG.
2, equipment that includes a tube or tubular portion can include
one or more packers. Such equipment may include one or more other
portions, for example, with slips, grips, etc.
[0049] As shown in FIG. 2, a packer can include rings, which may
be, for example, constructed at least in part from an elastomeric
material. As an example, rings can be seal rings that act to
maintain seals while a packer is in an expanded state and, for
example, in contact forcibly with a surface of a bore, which may be
an equipment bore (e.g., a casing bore, etc.) or an earthen bore
(e.g., a bore formed by a bore wall of a rock formation).
[0050] FIG. 2 shows an example of an assembly 282 that includes an
elastomeric component 283 disposed about an outer perimeter surface
of a component 284 of a bore tool that includes a longitudinal axis
(z) where the elastomeric component 283 may be expanded and/or
contracted in a radial direction as indicated by arrows, for
example, to alter an outer perimeter of the elastomeric component
283 (e.g., an outer perimeter surface), optionally at least in part
via altering a length of the elastomeric component 283. In such an
example, an inner perimeter of the elastomeric component 283 may
remain relatively constant and, for example, in contact with the
outer perimeter surface of the component 284.
[0051] FIG. 2 shows an example of an assembly 286 that includes an
elastomeric component 287 disposed about an inner perimeter surface
of a component 288 of a bore tool that includes a longitudinal axis
(z) where the elastomeric component 287 may be expanded and/or
contracted in a radial direction as indicated by arrows, for
example, to alter an inner perimeter of the elastomeric component
287 (e.g., an inner perimeter surface), optionally at least in part
via altering a length of the elastomeric component 287. In such an
example, an outer perimeter of the elastomeric component 287 may
remain relatively constant and, for example, in contact with the
inner perimeter surface of the component 288.
[0052] FIG. 2 shows an example of an assembly 292 that includes an
elastomeric component 293 disposed about an outer perimeter surface
of a component 294 of a bore tool that includes a longitudinal axis
(z) where the elastomeric component 293 may be expanded and/or
contracted in a radial direction as indicated by arrows, for
example, to alter an outer perimeter of the elastomeric component
293 (e.g., an outer perimeter surface), optionally at least in part
via altering a length of the elastomeric component 293. In such an
example, an inner perimeter of the elastomeric component 293 may
remain relatively constant and, for example, in contact with the
outer perimeter surface of the component 294.
[0053] FIG. 2 shows an example of an assembly 296 that includes an
elastomeric component 297 disposed about an inner perimeter surface
of a component 298 of a bore tool that includes a longitudinal axis
(z) where the elastomeric component 297 may be expanded and/or
contracted in a radial direction as indicated by arrows, for
example, to alter an inner perimeter of the elastomeric component
297 (e.g., an inner perimeter surface), optionally at least in part
via altering a length of the elastomeric component 297. In such an
example, an outer perimeter of the elastomeric component 297 may
remain relatively constant and, for example, in contact with the
inner perimeter surface of the component 298.
[0054] As an example, a bore tool can include a component that
includes a longitudinal axis and a perimeter surface disposed at
one or more radii from the longitudinal axis; and an elastomeric
component disposed about the perimeter surface where the
elastomeric component includes an elastomeric material that
includes, for example, carbon-based nanoplatelets. In such an
example, the perimeter surface of the component of the bore tool
may be an outer perimeter surface or an inner perimeter surface. As
an example, as to one or more radii, consider a substantially
cylindrical component that includes an outer perimeter disposed at
a substantially constant radius with respect to azimuthal angle
about a longitudinal axis and/or an inner perimeter disposed at a
substantially constant radius with respect to azimuthal angle about
a longitudinal axis (see, e.g., the assemblies 282 and 286); or,
for example, a component that may include an outer perimeter
defined by more than one radius and/or an inner perimeter defined
by more than one radius (see, e.g., the assemblies 292 and
296).
[0055] A method can include forming an elastomeric component that
includes carbon-based nanoplatelets in an elastomeric matrix;
fitting the elastomeric component about a perimeter surface of a
tool that includes a longitudinal axis; and tripping the tool into
a bore in a geologic formation. In such an example, the perimeter
surface of the tool may be an inner perimeter surface or an outer
perimeter surface. As an example, such a tool may be a bore tool as
it is suitable for tripping into a bore in a geologic formation
(e.g., geologic environment).
[0056] As an example, a bore packer assembly can include a first
end elastomeric element; an intermediate elastomeric element; and a
second end elastomeric element where at least one of the
elastomeric elements includes carbon-based nanoparticles. In such
an example, the bore packer assembly can include an outer perimeter
surface where the elastomeric elements are disposed about the outer
perimeter surface. As an example, one or more mechanisms may apply
force to the elastomeric elements such that outer perimeters of the
elastomeric elements change, for example, become greater or lesser
depending on the direction of the force. As an example, where force
acts to decrease the length of the elastomeric elements, the outer
perimeters of the elastomeric elements can increase radially
outwardly; whereas, where force acts to increase the length of the
elastomeric elements, the outer perimeters of the elastomeric
elements can decrease radially inwardly.
[0057] FIG. 3 shows a cutaway view of a sealing element mechanism
368 of a packer 310. In the example of FIG. 3, the sealing element
mechanism 368 includes an assembly 382 (e.g., a sliding shoe
assembly) that includes a seal element 324, a sliding shoe (e.g., a
sleeve) 374, a sliding shoe gage ring 376, a sliding shoe shear
member (e.g., a pin) 378, and a sliding shoe seal member 380.
[0058] As shown in the example of FIG. 3, the seal element 324 can
be a double fold back element stack, which can include a plurality
of elastomeric (e.g., rubber) packer elements (e.g., elastomeric
components). The seal element 324 can be connected to and can be
moveable with the sliding shoe 374, which can include a head
portion 384 and an elongated shelf 386. As shown in the example of
FIG. 3, the sliding shoe 374 substantially circumscribes a packer
mandrel 344.
[0059] In the example of FIG. 3, the seal element 324 can be
operationally connected with shelf 386. As an example, a head
portion 384 of the sliding shoe 374 can be oriented toward slips,
for example, when the sliding shoe 374 is disposed on the mandrel
344. As shown, a gage ring 376 can be connected with the sliding
shoe 374 via a shear member 378 and the gage ring 376 can be
connected to shelf 386 of shoe 374 distal from the head portion
384, where the seal element 324 is disposed at least in part
axially between the gage ring 376 and head portion 384 of the shoe
374. As an example, the assembled sliding shoe assembly 382 may be
positioned on the packer mandrel 344. The sliding shoe assembly 382
can be operatively coupled to the ratchet mechanism 346 and a
middle housing 340 (e.g., a pickup housing). In the example of FIG.
3, the head portion 384 of the sliding shoe 374 forms a box end
which is threadedly coupled to the middle housing 340. As an
example, an upper ratchet mandrel 388 may be threadedly coupled to
a pin end of the packer mandrel 344 and, for example, an outer
ratchet portion 390 may be disposed with an upper ratchet mandrel
388 (e.g., operatively coupled via threading to the gage ring
376).
[0060] As an example, a mechanism such as a sliding shoe assembly
(see, e.g., the sliding shoe assembly 382) can provide for
transferring axial force (see, e.g., "F" and arrows) from a setting
mechanism (see, e.g., the setting mechanism 366) to slips around
(e.g., bypassing, the seal element 324) a packer to set (e.g.,
actuate) the slips and, for example, anchor an assembly to casing
and, for example, to then facilitate application of axial force to
packer(s) (see, e.g., the seal elements 324) to compress and set
the packer(s). As an example, axial force transfer across a setting
mechanism (e.g., a housing) bypassing a packer can facilitate
setting slips through a packer, for example, without setting or
prematurely setting the packer until after the slip is set (e.g.,
delaying the setting of the seal element). Such a mechanism of
force transfer can reduce loss of energy in axial force that occurs
when acting through one or more packers (e.g., elastomeric
components) and thereby facilitate achieving a setting force as
desired at slips and minimizing an amount of actuating force at a
setting mechanism and/or at a wellbore annulus.
[0061] FIG. 4 shows various examples of some types of packers,
including a one piece packer 410, a fold back shoe packer 420, a
dual fold back shoe packer 430, an ECNER array packer 440, a garter
spring packer 450, a garter spring with wire mesh packer 460, a
three piece packer 470, a soft set array packer 480 and an
expandable ring packer 490. As an example, a packer can include an
elastomeric material or elastomeric materials. As an example, a
packer can include one or more metallic components (e.g., metal or
alloy). As an example, a packer can include one or more rings,
which may include a metal ring and/or an alloy ring. As an example,
a packer can include a mesh or meshes, which may include a metal
mesh and/or an alloy mesh. As an example, a packer can include one
or more springs, which may include a metal spring and/or an alloy
spring. As an example, a ring, a mesh, a spring, etc. may be an
anti-extrusion component.
[0062] As mentioned, an elastomeric material can include
reinforcing material, which may be a particulate material. As an
example, an elastomeric material can include a carbon-based
reinforcing material. As an example, an elastomeric material can
include graphene and/or graphene oxide where such graphene and/or
graphene oxide acts to reinforce one or more elastomers of the
elastomeric material. As an example, graphene can be a reinforcing
material. As an example, graphene oxide can be a reinforcing
material.
[0063] FIG. 5 shows examples of structures 501. While graphite is a
three-dimensional carbon-based material made of layers of graphene,
graphite oxide differs. By oxidation of graphite using one or more
oxidizing agents (e.g., sulfuric acid, sodium nitrate, potassium
permanganate, etc.), oxygenated functionalities can be introduced
in a graphite structure (e.g., hydroxyl, epoxide, etc.) that can
expand layer separation and impart hydrophilicity. The imparted
hydrophilicity can allow for exfoliation of graphite oxide in water
(e.g., via sonication assist, etc.) to produce single or few layer
graphene, which may be referred to as graphene oxide (GO); noting
that one or more other techniques for exfoliation may be
implemented, additionally or alternatively (e.g., other mechanical,
chemical, thermal, etc.). Thus, a difference between graphite oxide
and graphene oxide can be the number of layers. For example, a
dispersion of graphene oxide may include structures of a few layers
or less (e.g., flakes and monolayer flakes); whereas, structures of
graphite oxide include more layers. As an example, graphene oxide
(GO) may be reduced to form reduced graphene oxide (rGO). As an
example, graphene oxide may include surface charge, which may be
negative (e.g., consider presence of oxygen), depend on factors
such as pH, etc.
[0064] As an example, a material may include graphene and a metal
oxide bound via hydrogen bonds to the graphene. As an example, a
material may include graphene and one or more polymers that may be
capable of forming hydrogen bonds and/or other bonds to the
graphene. As an example, a material may include graphene, oxide(s)
and one or more polymers. As an example, a material may include
graphene as graphene oxide (GO).
[0065] In FIG. 5, the structures 501 include graphene where, for
example, carbon atoms may be arranged in a hexagonal manner, due to
sp.sup.2 bonding, as a crystalline allotrope of carbon (e.g., as a
large aromatic molecule). Graphene may be described as being a
one-atom thick layer of graphite and may be a basic structural
element of carbon allotropes such as, for example, graphite,
charcoal, carbon nanotubes and fullerenes.
[0066] As an example, a nanosheet (e.g., or nanoplatelet) may be
defined as including a two-dimensional nanostructure that may be
characterized in part by a thickness between a lower surface and an
upper surface of the nanostructure where the thickness is less than
about 100 nanometers. As an example, a graphene nanosheet may
include a thickness of the order of about 0.34 nm (e.g., consider a
single layer of carbon atoms with hexagonal lattices). As
mentioned, a nanosheet may be defined in part by an aspect ratio.
As an example, a graphene nanosheet may include an aspect ratio of
about 100 or more. As an example, graphene nanosheets that include,
on average, an aspect ratio of the order of about 100 or more
(e.g., optionally of about 1000 or more) may be used to form one or
more types of composite materials. As an example, a larger
dimension of a graphene nanosheet (e.g., that may define in part an
aspect ratio) may be, for example, of the order of about 100
nanometers or more. As an example, a larger dimension of a graphene
nanosheet (e.g., that may define in part an aspect ratio) may be,
for example, of the order of about 1 micron or more. As an example,
a larger dimension of a graphene nanosheet (e.g., that may define
in part an aspect ratio) may be, for example, of the order of about
10 microns or more. As an example, graphene nanosheets may be made
and/or provided in a range of dimensions and/or aspect ratios.
[0067] As illustrated in FIG. 5, the structures 501 may include a
layer of graphene or layers of graphene, which may be described,
for example, with respect to a Cartesian coordinate system (x, y,
z). As an example, a layer may be bonded to another layer, for
example, via interactions that may involve epoxide and hydroxyl
groups. As an example, one or more layers may include one or more
of epoxide, carbonyl (C.dbd.O), hydroxyl (--OH), and phenol groups,
which may optionally participate in bond formation. For example,
see an approximate representation of a single graphene sheet in the
structures 501, which includes various oxygen groups (e.g., a GO
sheet).
[0068] As an example, layers of graphene may be bonded via one or
more metal oxides and hydrogen, for example, magnesium oxide may
bind to graphene via hydrogen atoms; and/or layers of graphene may
be bonded via one or more polymers and hydrogen (e.g., and/or other
group).
[0069] As an example, a material may exhibit one or more regions
that deviate from planarity (e.g., a buckling like structure). As
an example, a material may include disorder and/or irregular
packing of layers.
[0070] FIG. 6 shows examples of structures 601 and 603. As an
example, a structure can be a graphene or a graphene-based
structure. As an example, a structure can include a 2-dimensional
hexagonal lattice of carbon sp.sup.2 hybridized carbon atoms. As an
example, a structure can be a "ball" (e.g., 3D structure) such as,
for example, a C-60 "bucky ball". As an example, a structure can be
a nanotube. As an example, a structure can be graphite. As shown,
the structure 603 is plate-like and may be referred to as a
nanoplate or nanoplatelet where a plurality may be referred to as
nanoplatelets. As an example, nanoplatelets can include oxygen
and/or nitrogen atoms. As an example, one or more functional groups
may be bonded to a nanoplatelet.
[0071] FIG. 7 shows an example of a method 710 that includes
providing graphite, oxidizing 730 at least a portion of the
graphite 720 to form graphite oxide 740 and sonicating 750 at least
a portion of the graphite oxide 740 to form graphene oxide (GO)
760.
[0072] As an example, a polymeric material may be an EPDM (e.g.,
Ethylene-Propylene-Diene-Monomer rubber), for example, manufactured
from ethylidenenorbornene (ENB), which is a bicyclic monomer and
intermediate that includes two double bonds, each with a different
reactivity. ENB can be a diene monomer in the manufacture of EPDM
(Ethylene-Propylene-Diene-Monomer) rubber.
[0073] FIG. 8 shows an example of a method 810 that includes
reacting ENB-EPDM with maleic anhydride (MAH) to graft the MAH onto
the ENB-EPDM. As shown, various functional groups of the MAH can
hydrogen bond with various groups of graphene oxide. The method 810
of FIG. 8 is provided as an example of a modification that can be
utilized to bond a polymeric material to a carbon-based material
such as, for example, graphene oxide.
[0074] As mentioned, graphene is a layered material that, for
example, can be provided with a relatively high aspect ratio in an
exfoliated state. Graphene tends to be strong on a per unit weight
basis. Graphene includes functional properties in that it may be
bonded to one or more other chemicals.
[0075] As an example, graphene nanoplatelets (e.g., nano-graphite)
can be of lesser cost than carbon-based nanotubes (CNTs). As an
example, graphene can provide gas impermeable characteristic and
may improve rapid gas decompression resistance characteristics.
[0076] As an example, an elastomeric material can include graphene
and can be formed as an elastomeric component (e.g., elastomeric
element) as part of one or more types of downhole tools (e.g.,
packer assemblies, etc.).
[0077] As an example, graphene nanoplatelets may be dispersed in a
mixture of monomers and/or polymers. For example, consider
polypropylene (PP) where chains can adhere to a graphene basal
plane. As an example, functional groups on edges of graphene
nanoplatelets may be considered. As an example, graphene
nanoplatelets can include, for example, the nanoplatelets xGnP.TM.
(XG Sciences, Lansing, Mich.).
[0078] As an example, particle size of graphene nanoplatelets can
be characterized by a diameter as a dimension (e.g., an effective
diameter), which may be, for example, in a range of about 1 micron
to about 25 microns, and include surface characteristics in a range
of about 120 m.sup.2/g to about 750 m.sup.2/g. In such examples, a
nanoplatelet may be characterized in a thickness or depth
dimension. For example, consider nanoplatelets with an average
thickness of approximately 2 nanometers.
[0079] As an example, graphene nanoplatelets may be utilized with
polyethylene (PE), for example, to form one or more types of
multifunctional high density polyethylene nanocomposites. Such an
approach can include incorporation of exfoliated graphite
nanoplatelets.
[0080] As an example, a linear low density PE based elastomeric
material can be formed via paraffin coating on exfoliated graphite
nanoplatelets.
[0081] As an example, as to Nylon 6, one or more types of
surfactants may be included in a mixture to enhance compatibility
with graphene nanoplatelets as the surface energy level of Nylon 6
tends to be similar to that of the aforementioned xGnP.TM.
nanoplatelets (e.g., consider polar contribution due the amide
groups of Nylon 6).
[0082] As an example, an elastomeric material can include
polycarbonate (PC) and graphene (e.g., consider polyurethane
elastomers types polymers that may include polycarbonate diols,
etc.).
[0083] As an example, an epoxy can include graphene. As an example,
such an epoxy may be utilized with one or more other types of
materials (e.g., elastomeric materials that may include one or more
types of carbon-based nanoparticles, etc.).
[0084] As an example, a material can include reduced graphene oxide
and natural rubber to form a nanocomposite material. In such an
example, a method can include dispersion of reduced graphene oxide
(RG-O) into natural rubber (NR), which can enhance mechanical,
electrical, and thermal properties of the natural rubber (NR).
[0085] As an example, a method can include modification of graphene
and fabrication of graphene-based polymer nanocomposites.
[0086] As an example, functionalized graphene sheets (FGSs) can be
utilized as a reinforcement material in an elastomeric material. In
such an example, the FGSs can be predominantly single sheets of
graphene with a lateral size of several hundreds of nanometers and
a thickness of about 1.5 nm.
[0087] As an example, graphite nanoplatelets of expanded graphite
can be utilized to form one or more types of polymer composites. As
an example, graphite may be expanded from intercalated graphite by
microwaves or radiofrequency waves in the presence of a gaseous
atmosphere. Such polymer composites can exhibit barrier and/or
conductive properties due to the presence of expanded graphite.
[0088] As an example, an elastomeric material can include one or
more lubricant additives. For example, consider a lubricant
additive in at least dynamic seal surface portion of an elastomeric
material that can reduce the coefficient of friction and stick-slip
amplitude at the surface.
[0089] As an example, a rubber composite material can include
graphene oxide. For example, consider materials in parts by weight
of: 100 parts of chlorosulfonated polyethylene, 10-15 parts of
ethylene-vinyl acetate rubber (EVM), 20-25 parts of hydrogenated
butadiene-acrylonitrile rubber (HNBR), 0.5-5 parts of graphene
oxide, 30-70 parts of hard carbon black with mean grain size of
15-25 nm, 1-10 parts of dioctyl sebacate (DOS), 3-6 parts of zinc
oxide, 3-6 parts of stearic acid, 0.5-4 parts of N,N-nickel dibutyl
dithiocarbamate, 1-4 parts of dipentamethylenethiuram hexasulfide,
0.5-4 parts of PbO and 1-6 parts of insoluble sulfur. Such a rubber
composite can, via chlorosulfonated polyethylene, EVM and HNBR with
low acrylonitrile content, balance fuel oil resistance and low
temperature resistance.
[0090] As an example, a method can include forming a graphene
reinforced elastomer composite material for one or more
applications such as, for example, downhole seal, packer for
downhole use, a blowout protector (BOP), etc. As an example, an
elastomeric material can be or include swellable elastomer, which
may exhibit high temperature and/or sour gas resistance. As an
example, consider EPDM as an oil swellable elastomeric
material.
[0091] As an example, one or more types of nano-scale reinforcement
material can be used to enhance rheological, mechanical and/or
physical properties of one or more types of polymers. As an
example, a nano-scale material may improve processability,
functionality and/or end-use performance of an elastomeric
material. As an example, graphite (e.g., graphene nanoplatelets)
can be utilized as reinforcement where relatively large specific
surface area, high strength and high surface reactivity can be
beneficial to modify properties of one or more types of
elastomers.
[0092] As an example, graphite (e.g., graphene nanoplatelets) can
be used as a single-reinforcement filler or alternatively with one
or more other filler materials such as, for example, silica, carbon
black, etc.
[0093] As to types of polymers, a polymeric material can include,
for example, one or more types of carboxylated nitrile rubber
compounds (XNBR), which may provide better strength properties,
especially abrasion resistance, when compared to NBR (e.g., without
carboxylation). As an example, carboxylated nitriles may be
produced by inclusion of carboxylic acid groups (e.g., as polymer
groups during polymerization). In such an example, carboxylic acid
groups can provide extra crosslinks (e.g., pseudo or ionic
crosslinks) and thereby produce harder, tougher compounds with
higher abrasion resistance, modulus, and tensile strength than
standard nitriles.
[0094] As an example, a polymeric material can include, for
example, one or more types of HNBR. HNBR can include so-called
highly saturated hydrocarbons and acrylonitrile (ACN) where, for
example, increased saturation is achieved via hydrogenation of
unsaturated bonds. As an example, increased saturation can impart
(e.g., improve) heat, chemical, and ozone resistance. As an
example, ACN content of HNBR can impart toughness, as well as
resistance to hydrocarbons. Where unsaturated butadiene segments
exist (e.g., less than about 10 percent), such sites may facilitate
peroxide curing and/or vulcanization. As an example, a
peroxide-cured HNBR may exhibit improved thermal properties without
further vulcanization (e.g., as with sulfur-cured nitriles).
[0095] As an example, a polymeric material can include, for
example, one or more types of fluoroelastomers, which may be
abbreviated as FKMs. FKM (FPM by ISO) is a designation for about 80
percent of fluoroelastomers as defined in ASTM D1418. FKMs may
exhibit heat and fluid resistance. For example, in FKMs, bonds
between carbon atoms of the polymer backbone and attached (pendant)
fluorine atoms tend to be resistant to chain scission and
relatively high fluorine-to-hydrogen ratios can provide stability
(e.g., reduced risk of reactions or environmental breakdown).
Further, FKMs tend to include a carbon backbone that is saturated
(e.g., lacking covalent double bonds, which may be attack sites).
Elastomers such as one or more of the VITON.TM. class of FKM
elastomers (E. I. du Pont de Nemours & Co., Wilmington, Del.)
may be used (e.g., VITON.TM. A, VITON.TM. B, VITON.TM. F, VITON.TM.
GF, VITON.TM. GLT, VITON.TM. GFLT, etc.).
[0096] On the basis of their chemical composition various FKMs may
be divided into the following types: Type 1 FKMs are composed of
vinylidene fluoride (VDF) and hexafluoropropylene (HFP); Type 2
FKMs are composed of VDF, HFP, and tetrafluoroethylene (TFE); Type
3 FKMs are composed of VDF, HFP, TFE, perfluoromethylvinylether
(PMVE); Type 4 FKMs are composed of propylene, TFE, and VDF; Type 5
FKMs are composed of VDF, HFP, TFE, PMVE, and ethylene. Other
categories of polymers can include FFKM and FEPM.
[0097] As an example, a polymeric material can include, for
example, one or more types of a polyvinylidene fluoride (PVDF),
which may be a relatively non-reactive and thermoplastic
fluoropolymer produced at least in part by polymerization of
vinylidene difluoride. As an example, a PVDF may be melt processed,
for example, depending on melting point (e.g., due to modifiers,
fillers, etc.). As an example, a PVDF may have a density of about
1.78. As an example, a material may include a co-polymer of PVDF
and HFP (e.g., poly(vinylidene fluoride-co-hexafluoropropylene),
which may be abbreviated as PVDF-HFP).
[0098] FIG. 9 shows an example of a plot 900 for elastomeric
materials that include graphite (e.g., graphene nanoplatelets) as
reinforcing filler. The plot 900 shows data as to storage modulus
as well as thermal resistance of an HNBR elastomer. The data in the
plot 900 indicate enhancement of modulus at temperatures in a range
of about 150 degrees C. to about 200 degrees C. when compared to
carbon black filled HNBR. The plot 900 also shows graphite (e.g.,
graphene nanoplatelets) filled FKM as having the highest thermal
stability, up to about 300 degrees C. As shown for various example
elastomeric materials corresponding to data in the plot 900,
enhancements to properties can be achieved at filler concentrations
at less than approximately 10 percent by weight.
[0099] FIG. 10 shows an example of a plot 1000 as to property
comparisons with a control (HNBR-carbon black) and two graphene
nanoplatelets reinforced HNBRs. For G1 compounds, the data indicate
an enhancement of modulus at about 50 percent and at about 100
percent and a slight increase in elongation at break and with a
relatively similar level of tear strength.
TABLE-US-00001 TABLE 1 Data of Plot 1000 Tear Storage Modulus
Modulus Elongation Strength Modulus Material 50% (psi) 100% (psi)
(percent) (lb/in) (300 C., psi) Control 416 800 351 182 860 G1 817
1312 443 193 1465 G2 689 1041 512 190 1401
[0100] FIG. 11 shows an example of a plot 1100 that includes data
for gas permeability as to the control, G1 and G2. As shown in the
plot 1100, CO.sub.2 permeability is less in G1 and G2 polymeric
materials than in the control polymeric material.
[0101] As demonstrated via the example polymeric materials (e.g.,
elastomeric materials), inclusion of carbon-based nanoparticles
such as, for example, graphene nanoplatelets, can reinforce a
polymeric matrix. For example, such reinforcement can enhance
mechanical properties, particularly at temperatures of interest for
various applications, and, for example, can decrease permeability
as to gas. As to the latter, decreased gas permeability can be
characterized as a gas barrier property. As an example, a polymeric
material that includes one or more types of carbon-based
nanoparticles (e.g., graphene nanoplatelets, etc.) can exhibit
decreased permeability as to one or more gasses, which can be
beneficial for one or more types of downhole applications.
[0102] As an example, a method can include mixing graphite (e.g.,
graphene nanoplatelets) with one or more types of polymers such as,
for example, one or more of HNBR, NBR, VITON.TM. polymer, VITON.TM.
Extreme polymer, AFLAS.TM. fluororubber, FFKM rubber, etc. where
the graphite can be dispersed within a matrix formed by the one or
more types of polymers. As an example, a component made at least in
part from such a resulting polymeric material may be suitable for
one or more types of downhole seal applications such as, for
example, as a portion of a packer assembly (e.g., a packer or seal
element). As an example, equipment that includes a packer may
itself be referred to as a "packer" (see, e.g., the multistage
packer 260 of FIG. 2). As an example, equipment such as a blowout
protector (BOP), etc., may include one or more types of polymeric
materials that include one or more forms of carbon-based material
(e.g., carbon ring based materials such as, for example, graphite,
etc.).
[0103] As an example, a method can include dispersing graphite
(e.g., graphene nanoplatelets) in an elastomeric fluid in a manner
that acts to reduce aggregation of the graphite (e.g.,
nanoparticles) in the elastomeric fluid.
[0104] As an example, nano-scale graphite can be dispersed in a dry
form of additives to provide a nanoparticle pre-blend and then
mixed with base elastomer such as, for example, one or more of
HNBR, FKM, AFLAS.TM. fluororubber (FEPM), and FFKM, to form a
relatively homogenous elastomer composite.
[0105] As an example, nano-scale graphite can be dispersed in a
liquid form polymer such as, for example, liquid NBR to provide a
nanoparticle pre-blended "master" batch that can be mixed with a
base resin such as, for example, one or more of HNBR, FKM to form a
relatively homogenous elastomer composite material.
[0106] As an example, graphene nanoplatelets can be surface treated
by carboxy-terminated butadiene-acroylonitrile (CTBN) to promote
dispersion. As an example, CTBN can be used for modification of
surface of carbon materials including carbon nanotubes.
[0107] As an example, carboxyl-modified multi-walled carbon
nanotubes (MWCNT-COOHs) (e.g., suitable for use as nano-scale
particles) can be incorporated into diglycidyl ether of bisphenol A
(DGEBA) toughened with carboxyl-terminated butadiene-acrylonitrile
(CTBN). As an example, addition of MWCNT-COOHs can accelerate
curing reaction of a rubber-toughened epoxy resin (e.g., as may be
shown via differential scanning calorimetry). As an example, Tg of
rubber-toughened epoxy nanocomposites may be lowered with inclusion
of MWCNT-COOH. As an example, tensile strength, elongation at
break, flexural strength and flexural modulus of
DGEBA/CTBN/MWCNT-COOHs nanocomposites can be increased in
relationship to MWCNT-COOH concentration. As an example, a
relatively homogenous dispersion of nanocomposites can be achieved
via use of MWCNT-COOH.
[0108] FIG. 12 shows an example of a method 1210 of modifying
carbon nanotubes (CNTs) via carboxyl groups. In particular, FIG. 12
shows the method 1210 as including a reaction scheme between
carboxyl groups in CTBN and MWCNT-COOHs and epoxy groups in
DGEBA.
[0109] As an example, one or more types of graphene reinforced
elastomeric materials can exhibit relatively high temperature
resistant and/or gas resistance. Such materials may be suitable for
one or more types of downhole oilfield applications.
[0110] As an example, an application may be a seal application
where one or more seal elements are made at least in part from a
graphene reinforced elastomer. As an example, consider an
HNBR-based elastomeric material for drilling mud motor for better
solvent resistance and fatigue. As an example, consider a swellable
elastomeric material for one or more types of downhole applications
that can include use of a packer or packers. As an example, an
elastomeric material can be utilized in a surface BOP packer
assembly as a seal element.
[0111] FIG. 12 shows an example of a system 1300 that includes a
casing 1302 (e.g., a tube or tubular) and equipment 1310 disposed
at least in part in a bore of the casing 1302. As shown, the
equipment 1310 includes components 1320 and 1330 that define axial
limits (e.g., axial stop surfaces) between which exist a packer
1360 that can include portions such as portions 1362, 1364 and
1366. As an example, one or more of the components 1320 and 1330
can move axially to apply force to the packer 1360. In such an
example, the packer 1360 may expand at least in part radially such
that the packer 1360 contacts an inner surface of the casing 1302.
In such an example, as indicated by pressures P1 and P2, a pressure
differential may be developed where the packer 1360 forms a seal
between, for example, the component 1320 and the inner surface of
the casing 1302.
[0112] With reference to the portions 1362, 1364 and 1366 of the
packer 1360, these may be made of the same elastomeric material or
made of one or more different types of elastomeric materials. As an
example, such materials may be formed via a compression modeling
process.
[0113] As an example, one or more elastomeric materials may be
selected at least in part based on friction coefficient. As an
example, one or more elastomeric materials may be bonded with one
or more components, which can include, for example, one or more
metal, alloy, ceramic and/or hard plastic materials.
[0114] As an example, a packer may be utilized to seal a tool or
tubing with respect to another tool or tubing. As an example, a
packer shaped as a ring or other annular shape may include an outer
diameter that is in a range of about 5 cm to about 50 cm. As an
example, a packer can be shaped as a ring or other type of annular
shape may include an inner diameter that is sized to fit about an
outer surface of a tool or tubing. As an example, an inner diameter
may be in a range of about 0.5 cm to about 49.5 cm.
[0115] FIG. 14 shows some examples of arrangements of packers 1410,
1420, 1430, 1440, 1450, 1460, 1470 and 1480.
[0116] As an example, for the packer 1410, portions 1412 and 1416
can be made of 90/95 duro elastomeric graphene filled material with
a temperature rating to about 200 degrees C. (e.g., about 400
degrees F.) and a portion 1414 may be made of 70/75 duro
elastomeric graphene filled material with a temperature rating to
about 200 degrees C. (e.g., about 400 degrees F.).
[0117] As an example, for the packer 1420, portions 1422 and 1426
can be made of 90/95 duro elastomeric graphene filled material with
a temperature rating to about 200 degrees C. (e.g., about 400
degrees F.) and a portion 1424 may be made of 70/75 duro
elastomeric graphene filled material with a temperature rating to
about 200 degrees C. (e.g., about 400 degrees F.).
[0118] As an example, for the packer 1430, portions 1432 and 1436
can be made of 90/95 duro elastomeric graphene filled material with
a temperature rating to about 200 degrees C. (e.g., about 400
degrees F.) and a portion 1434 may be made of 70/75 duro
elastomeric graphene filled material with a temperature rating to
about 200 degrees C. (e.g., about 400 degrees F.). As shown, the
packer 1430 can include one or more anti-extrusion components 1437
and 1439 such as, for example, one or more anti-extrusion meshes,
springs, etc. In such an example, one or more of the one or more
anti-extrusion components 1437 and 1439 may be bonded to the
elastomeric material of a portion or portions of the packer
1430.
[0119] As an example, for the packer 1440, portions 1442 and 1446
can be made of 90/95 duro elastomeric graphene filled material with
a temperature rating to about 200 degrees C. (e.g., about 400
degrees F.) and a portion 1444 may be made of 70/75 duro
elastomeric graphene filled material with a temperature rating to
about 200 degrees C. (e.g., about 400 degrees F.). As shown, the
packer 1440 can include one or more anti-extrusion components 1447
and 1449 such as, for example, one or more anti-extrusion meshes,
springs, etc. In such an example, one or more of the one or more
anti-extrusion components 1447 and 1449 may be bonded to the
elastomeric material of a portion or portions of the packer
1440.
[0120] As an example, for the packer 1450, portions 1452 and 1456
can be made of 90/95 duro elastomeric graphene filled material with
a temperature rating to about 200 degrees C. (e.g., about 400
degrees F.) and a portion 1454 may be made of 80/85 duro
elastomeric graphene filled material with a temperature rating to
about 200 degrees C. (e.g., about 400 degrees F.).
[0121] As an example, for the packer 1460, portions 1462 and 1466
can be made of 90/95 duro elastomeric graphene filled material with
a temperature rating to about 200 degrees C. (e.g., about 400
degrees F.) and a portion 1464 may be made of 80/85 duro
elastomeric graphene filled material with a temperature rating to
about 200 degrees C. (e.g., about 400 degrees F.).
[0122] As an example, for the packer 1470, portions 1472 and 1476
can be made of 90/95 duro elastomeric graphene filled material with
a temperature rating to about 200 degrees C. (e.g., about 400
degrees F.) and a portion 1474 may be made of 80/85 duro
elastomeric graphene filled material with a temperature rating to
about 200 degrees C. (e.g., about 400 degrees F.). As shown, the
packer 1470 can include one or more anti-extrusion components 1477
and 1479 such as, for example, one or more anti-extrusion meshes,
springs, etc. In such an example, one or more of the one or more
anti-extrusion components 1477 and 1479 may be bonded to the
elastomeric material of a portion or portions of the packer
1470.
[0123] As an example, for the packer 1480, portions 1482 and 1486
can be made of 90/95 duro elastomeric graphene filled material with
a temperature rating to about 200 degrees C. (e.g., about 400
degrees F.) and a portion 1484 may be made of 80/85 duro
elastomeric graphene filled material with a temperature rating to
about 200 degrees C. (e.g., about 400 degrees F.). As shown, the
packer 1480 can include one or more anti-extrusion components 1487
and 1489 such as, for example, one or more anti-extrusion meshes,
springs, etc. In such an example, one or more of the one or more
anti-extrusion components 1487 and 1489 may be bonded to the
elastomeric material of a portion or portions of the packer
1480.
[0124] FIG. 15 shows an example of a method 1500 that shows stress
profiles for a packer 1510 that includes three portions 1512, 1514
and 1516 with respect to time during a setting operation where the
packer 1510 is disposed between two surfaces. As an example, the
method 1500 can be a single step setting for the packer 1510;
noting that, for example, a method may include a shear-slip setting
for a packer.
[0125] As shown in FIG. 15, a location of maximum stress can change
during a setting process where, for example, it may be located at a
boundary between portions 1514 and 1516, then within the portion
1514, then at a boundary with a component that acts to retain the
portion 1512, etc.
[0126] As an example, a middle portion of a packer (e.g., a middle
element) may deform more than an end portion of a packer (e.g., an
end element). As an example, where a packer includes multiple
elements, the materials of construction of the elements may be
selected based at least in part on evolution of shapes, stresses,
etc., with respect to time. For example, as explained with respect
to various examples of FIG. 14, a material of construction of an
end portion (e.g., end element) may differ from a material of
construction of a portion that is not at an end (e.g., an
intermediate element).
[0127] As an example, a geologic environment or downhole
environment may be a harsh environment and/or an environment that
may be classified as being a high-pressure and high-temperature
environment (e.g., a HPHT environment). As an example, an
environment may be classified based at least in part on its
chemical composition. For example, where an environment includes
hydrogen sulfide (H.sub.2S), carbon dioxide (CO.sub.2), etc., the
environment may be corrosive to certain materials. As an example,
an environment may be classified based at least in part on
particulate matter that may be in a fluid (e.g., suspended,
entrained, etc.). As an example, particulate matter in an
environment may be abrasive or otherwise damaging to equipment. As
an example, conditions in a geologic environment may be transient
and/or persistent.
[0128] As an example, an elastomeric material or elastomeric
materials may be made and/or selected based at least in part on
conditions in an environment in which the material or materials are
to be used. As an example, an elastomeric material or elastomeric
materials may be made and/or selected based at least in part on one
or more operational conditions of equipment in an environment. As
an example, an elastomeric material or elastomeric materials may be
made and/or selected based at least in part on conditions in an
environment in which the material or materials are to be used
and/or one or more operational conditions of equipment in an
environment.
[0129] FIG. 16 shows an example of a method 1600 that includes a
formation block 1610 for forming an elastomeric component that
includes carbon-based nanoplatelets in an elastomeric matrix; a
fitting block 1620 for fitting the elastomeric component about a
perimeter surface of a tool that includes a longitudinal axis; and
a tripping block 1630 for tripping the tool into a bore in a
geologic formation. In such an example, the carbon-based
nanoplatelets can include one or more types of chemically modified
carbon-based nanoplatelets. As an example, the method 1600 may
include a compression block 1640 for compressing the elastomeric
component to expand an outer perimeter of the elastomeric component
(e.g., to form a seal with respect to a wall in the geologic
environment such as an earthen wall, a casing wall, etc.). As an
example, the method 1600 can include fitting an elastomeric
component about an inner perimeter surface or an outer perimeter
surface of a tool (e.g., a component of a tool). In such examples,
compression may compress the elastomeric component to decrease its
inner perimeter or to increase its outer perimeter,
respectively.
[0130] FIG. 17 shows an example of a geologic environment 1700 and
a system 1710 positioned with respect to the geologic environment
1700. As shown, the geologic environment 1700 may include at least
one bore 1702, which may include casing 1704 and well head
equipment 1706 (e.g., blowout protector, etc.), which may include a
sealable fitting 1708 that may form a seal about a cable 1720. In
the example of FIG. 17, the system 1710 may include a reel 1712 for
deploying equipment 1725 via the cable 1720. As an example, the
equipment 1725 may be a tool (e.g., a downhole tool). As an
example, the system 1710 may include a structure 1740 that may
carry a mechanism such as a gooseneck 1745 that may function to
transition the cable 1720 from the reel 1712 to a downward
direction for positioning in the bore 1702.
[0131] As shown in the example of FIG. 17, a unit 1760 may include
circuitry that may be electrically coupled to the equipment 1725.
As an example, the cable 1720 may include or carry one or more
wires and/or other communication equipment (e.g., fiber optics,
rely circuitry, wireless circuitry, etc.) that may be operatively
coupled to the equipment 1725. As an example, the unit 1760 may
process information transmitted by one or more sensors, for
example, as operatively coupled to or as part of the equipment
1725. As an example, the unit 1760 may include one or more
controllers for controlling, for example, operation of one or more
components of the system 1710 (e.g., the reel 1712, etc.). As an
example, the unit 1760 may include circuitry to control
depth/distance of deployment of the equipment 1725.
[0132] As an example, the system 1710 may include one or more
stuffing boxes, one or more lubricator, one or more blow-out
protectors, etc. As an example, the system 1710 can include one or
more downhole pieces of equipment such as, for example, one or more
downhole valve units 1770, one or more control line associated with
one or more units, one or more packer assemblies 1780, etc. As an
example, one or more pieces of equipment, tools, etc. in the system
1710 may include an elastomeric material that includes carbon-based
(carbon ring-based) nanoparticles such as, for example,
nanoplatelets.
[0133] As an example, the system 1710 may be utilized to trip
equipment in to and out of the bore 1702. As an example, a system
may be or include a rig. As an example, the system 1710, a rig,
etc., may be utilized to move and position one or more types of
tools in a bore. As an example, a method can include tripping in
and/or tripping out equipment with respect to a bore.
[0134] As an example, the system 1710 may include one or more
stuffing boxes, one or more lubricator, one or more blow-out
protectors, etc. As an example, the system 1710 can include one or
more downhole pieces of equipment such as, for example, one or more
downhole valve units, one or more control line associated with one
or more units, one or more packer assemblies, etc.
[0135] As an example, a bore tool can include a component that
includes a longitudinal axis and a perimeter surface disposed at
one or more radii from the longitudinal axis; and an elastomeric
component disposed about the perimeter surface where the
elastomeric component includes an elastomeric material that
includes carbon-based nanoplatelets. In such an example, the bore
tool can be or include a bore packer assembly. As an example, such
a bore packer assembly can include a force applicator that is
actuatable to apply force to the elastomeric component to at least
in part increase a perimeter of the elastomeric component.
[0136] As an example, a bore tool can include slips. As an example,
a bore tool can be or include a blowout protector (BOP).
[0137] As an example, a bore tool can include two elastomeric
components where an axial gap exists between the two elastomeric
components and where at least one of the two elastomeric components
includes carbon-based nanoplatelets.
[0138] As an example, a bore tool can include two elastomeric
components that contact each other where at least one of the two
elastomeric components includes carbon-based nanoplatelets.
[0139] As an example, where a bore tool includes a plurality of
elastomeric components, one elastomeric component can include a
first elastomeric material composition and another of the
elastomeric components can include a second elastomeric material
composition that differs from the first elastomeric material
composition. As an example, two elastomeric components of a bore
tool can include a first Young's modulus of one elastomeric
component where another of the elastomeric components includes a
second Young's modulus that differs from the first Young's
modulus.
[0140] As an example, an elastomeric material that includes
carbon-based nanoplatelets can include the carbon-based
nanoplatelets at less than approximately 10 percent by weight.
[0141] As an example, an elastomeric material can include a
fluoroelastomer and carbon-based nanoplatelets. As an example, an
elastomeric material can include a nitrile butadiene rubber (e.g.,
NBR type of elastomer) and carbon-based nanoplatelets. As an
example, an elastomeric material can include an
ethylene-propylene-diene-monomer rubber (EPDM rubber or EPDM type
of elastomer).
[0142] As an example, a bore tool can include three elastomeric
components where the three elastomeric components include two end
elastomeric components and an intermediate elastomeric component.
In such an example, one or more of the elastomeric components can
include carbon-based nanoplatelets. In such an example, the two end
elastomeric components can include a Young's modulus that differs
from a Young's modulus of the intermediate elastomeric
component.
[0143] As an example, a bore tool can include an elastomeric
component, disposed about a perimeter surface, that does not
include carbon-based nanoplatelets and an elastomeric component
that does include carbon-based nanoplatelets.
[0144] As an example, carbon-based nanoplatelets of an elastomeric
component can include an average maximum platelet dimension less
than approximately 50 microns and an average platelet thickness
dimension less than approximation 10 nanometers and/or, for
example, carbon-based nanoplatelets include an average maximum
platelet dimension less than approximately 25 microns and an
average platelet thickness dimension less than approximation 5
nanometers.
[0145] As an example, a method can include forming an elastomeric
component that includes carbon-based nanoplatelets in an
elastomeric matrix; fitting the elastomeric component about a
perimeter surface of a tool that includes a longitudinal axis; and
tripping the tool into a bore in a geologic formation. In such an
example, the carbon-based nanoplatelets can include chemically
modified carbon-based nanoplatelets. As an example, a method can
include compressing an elastomeric component to expand an outer
perimeter of the elastomeric component where the elastomeric
component includes carbon-based nanoplatelets.
[0146] As an example, a bore packer assembly can include a first
end elastomeric element; an intermediate elastomeric element; and a
second end elastomeric element where at least one of the
elastomeric elements includes carbon-based nanoparticles. In such
an example, the composition of the end elastomeric elements can
differ from the composition of the intermediate elastomeric
element.
[0147] As an example, one or more methods described herein may
include associated computer-readable storage media (CRM) blocks.
Such blocks can include instructions suitable for execution by one
or more processors (or cores) to instruct a computing device or
system to perform one or more actions.
[0148] According to an embodiment, one or more computer-readable
media may include computer-executable instructions to instruct a
computing system to output information for controlling a process.
For example, such instructions may provide for output to sensing
process, an injection process, drilling process, an extraction
process, an application process, an extrusion process, a curing
process, a tape forming process, a pumping process, a heating
process, etc.
[0149] FIG. 18 shows components of a computing system 1800 and a
networked system 1810. The system 1800 includes one or more
processors 1802, memory and/or storage components 1804, one or more
input and/or output devices 1806 and a bus 1808. According to an
embodiment, instructions may be stored in one or more
computer-readable media (e.g., memory/storage components 1804).
Such instructions may be read by one or more processors (e.g., the
processor(s) 1802) via a communication bus (e.g., the bus 1808),
which may be wired or wireless. The one or more processors may
execute such instructions to implement (wholly or in part) one or
more attributes (e.g., as part of a method). A user may view output
from and interact with a process via an I/O device (e.g., the
device 1806). According to an embodiment, a computer-readable
medium may be a storage component such as a physical memory storage
device, for example, a chip, a chip on a package, a memory card,
etc.
[0150] According to an embodiment, components may be distributed,
such as in the network system 1810. The network system 1810
includes components 1822-1, 1822-2, 1822-3, . . . 1822-N. For
example, the components 1822-1 may include the processor(s) 1802
while the component(s) 1822-3 may include memory accessible by the
processor(s) 1802. Further, the component(s) 1802-2 may include an
I/O device for display and optionally interaction with a method.
The network may be or include the Internet, an intranet, a cellular
network, a satellite network, etc.
[0151] Although only a few examples have been described in detail
above, those skilled in the art will readily appreciate that many
modifications are possible in the examples. Accordingly, all such
modifications are intended to be included within the scope of this
disclosure as defined in the following claims. In the claims,
means-plus-function clauses are intended to cover the structures
described herein as performing the recited function and not only
structural equivalents, but also equivalent structures. Thus,
although a nail and a screw may not be structural equivalents in
that a nail employs a cylindrical surface to secure wooden parts
together, whereas a screw employs a helical surface, in the
environment of fastening wooden parts, a nail and a screw may be
equivalent structures. It is the express intention of the applicant
not to invoke 35 U.S.C. .sctn. 112, paragraph 6 for any limitations
of any of the claims herein, except for those in which the claim
expressly uses the words "means for" together with an associated
function.
* * * * *