U.S. patent application number 12/986656 was filed with the patent office on 2011-07-14 for boron aluminum magnesium coating for earth-boring bit.
This patent application is currently assigned to Baker Hughes Incorporated. Invention is credited to Aaron J. Dick, Anthony A. DiGiovanni.
Application Number | 20110168451 12/986656 |
Document ID | / |
Family ID | 44257642 |
Filed Date | 2011-07-14 |
United States Patent
Application |
20110168451 |
Kind Code |
A1 |
DiGiovanni; Anthony A. ; et
al. |
July 14, 2011 |
Boron Aluminum Magnesium Coating for Earth-Boring Bit
Abstract
A rotatable cone earth boring bit has a bearing system with at
least on the surfaces being AlMgB14 alloy material. The alloy
material also contains an alloying agent, which may be titanium
boride (TiB2); titanium carbide (TiC) plus iron, nickel and carbon;
silicon nitride (Si3N4) powder; whiskered silicon nitride (Si3N4);
boron carbide (B4C); titanium boride (TiB2); or tungsten boride
(W2B4). The surface containing the AlMgB14 alloy material may be a
journal surface or thrust face on the bearing pin. The surface
containing the AlMgB14 alloy material may also be a seal surface,
either on a metal face seal or a gland on the bearing pin engaged
by an elastomeric ring. The AlMgB14 alloy material may a coating or
it may be a free-standing structural member within the bearing
system.
Inventors: |
DiGiovanni; Anthony A.;
(Houston, TX) ; Dick; Aaron J.; (Houston,
TX) |
Assignee: |
Baker Hughes Incorporated
Houston
TX
|
Family ID: |
44257642 |
Appl. No.: |
12/986656 |
Filed: |
January 7, 2011 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
|
61294675 |
Jan 13, 2010 |
|
|
|
Current U.S.
Class: |
175/372 |
Current CPC
Class: |
E21B 10/22 20130101;
F16C 33/62 20130101; C22C 21/06 20130101; F16C 2352/00 20130101;
F16C 2206/40 20130101 |
Class at
Publication: |
175/372 |
International
Class: |
E21B 10/22 20060101
E21B010/22 |
Claims
1. A downhole well tool having at least one rotatable member, a
bearing system including a bearing member having bearing surfaces
on which the rotatable member rotates and a seal having a seal
surface in sliding engagement with a mating seal surface to retain
lubricant within the bearing system, the improvement comprising: at
least one of the surfaces comprising an AlMgB14 alloy material.
2. The well tool according to claim 1, wherein the alloy material
further comprises a dopant selected from a group consisting of:
titanium boride (TiB2); titanium carbide (TiC) plus iron, nickel
and carbon; silicon nitride (Si3N4) powder; whiskered silicon
nitride (Si3N4); boron carbide (B4C); titanium boride (TiB2); and
tungsten boride (W2B4).
3. The well tool according to claim 2, wherein the dopant creates a
phase within the alloy material that has a grain size less than 100
nanometers.
4. The well tool according to claim 2, wherein the whiskered
silicon nitride comprise fibers having diameters less than 100
nanometers.
5. The well tool according to claim 1, wherein the AlMgB14 alloy
material comprises a coating on said at least one of the
surfaces.
6. The well tool according to claim 1, wherein the AlMgB14 alloy
material comprises a free-standing structure bonded to said at
least one of the surfaces.
7. The well tool according to claim 1, wherein said at least one of
the surfaces is at least one of the bearing surfaces and which
comprises: a cylindrical journal surface on the bearing member.
8. The well tool according to claim 1, wherein said at least one of
the surface is at least one of the bearing surfaces and which
comprises: a fiat circular thrust face on the bearing member.
9. The well tool according to claim 1, wherein said at least one of
the surface is at least one of the bearing surfaces and which
comprises: cylindrical surfaces of roller bearings.
10. The well tool according to claim 1, wherein said at least one
of the surfaces is at least one of the seal surfaces and which
comprises a seal face of a rigid face seal assembly.
11. The well tool according to claim 1, wherein said at least one
of the surface is the mating seal surface and which comprises an
annular seal gland on the bearing member that is slidingly engaged
by an elastomeric seal ring.
12. An earth boring bit, comprising: at least one rotatable cone
with external cutting elements; a bearing system comprising: a
bearing pin having bearing surfaces on which the cone rotates; a
seal having a seal surface in sliding engagement with a mating seal
surface to retain lubricant within the bearing system; at least one
of the surfaces comprising an AlMgB14 alloy material; and the
AlMgB14 bearing material having an alloying agent selected from a
group consisting of: titanium boride (TiB2); titanium carbide (TiC)
plus iron, nickel and carbon; silicon nitride (Si3N4) powder;
whiskered silicon nitride (Si3N4); boron carbide (B4C); titanium
boride (TiB2); and tungsten boride (W2B4).
13. The bit according to claim 12, wherein said at least one of the
surfaces is at least one of the bearing surfaces and which
comprises: an exterior surface of a bearing ring stationarily
mounted on the bearing pin and defining a bearing journal.
14. The bit according to claim 12, wherein said at least one of the
surface is at least one of the bearing surfaces and which
comprises: a flat circular disk stationarily mounted on a thrust
face of the bearing pin.
15. The bit according to claim 12, wherein said at least one of the
surface is at least one of the bearing surfaces and which
comprises: cylindrical surfaces of roller bearings.
16. The bit according to claim 12, wherein said at least one of the
surfaces is at least one of the seal surfaces and which comprises a
rigid seal face of a rigid face seal assembly.
17. The bit according to claim 12, wherein said at least one of the
surface is the mating seal surface and which comprises a sleeve
mounted around the bearing pin and slidingly engaged by an
elastomeric seal ring.
18. The bit according to claim 12, wherein the AlMgB14 alloy
material comprises a coating on said at least one of the
surfaces.
19. The bit according to claim 12, wherein the AlMgB14 alloy
material comprises a free-standing structure bonded to said at
least one of the surfaces.
20. An earth boring bit, comprising: at least one rotatable cone
with external cutting elements, the cone having a cavity with a
bearing surface; a bearing pin having a bearing surfaces on which
the bearing surface of the cone rotates; at least one of the
bearing surfaces comprising an AlMgB14 alloy coating; and the
AlMgB14 bearing coating having an alloying agent selected from a
group consisting of: titanium boride (TiB2); titanium carbide (TiC)
plus iron, nickel and carbon; silicon nitride (Si3N4) powder;
whiskered silicon nitride (Si3N4); boron carbide (B4C); titanium
boride (TiB2); and tungsten boride (W2B4).
21. The bit according to claim 20, wherein: the bearing surface of
the bearing pin comprises an exterior surface of a bearing ring
stationarily mounted on the bearing pin and defining a bearing
journal; and the coating is located on the exterior surface of the
bearing ring.
Description
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application claims priority to provisional application
61/294,675 filed Jan. 13, 2010.
FIELD OF THE INVENTION
[0002] This application relates in general to hard coatings for
improved abrasion resistance with reduced friction on downhole well
tools such as rotary cone earth-boring bits, and in particular to
coatings formed of boron, aluminum and magnesium.
BACKGROUND
[0003] One type of earth boring bit used in oil and gas well
drilling has rotatable cones mounted to bearing pins of a bit body.
The bearing system for the cones may be a journal bearing or a
cylindrical roller bearing. The bearing system also includes thrust
faces between the cone and bearing pin. A seal system seals
lubricant within the bearing system. The seal system might be a
metal-face-seal assembly, wherein an elastomeric member urges a
metal-face seal into sliding engagement with a mating seal.
Alternately, the seal system may comprise an elastomeric seal that
is in sliding engagement with an annular gland journal on the
bearing pin.
[0004] It is known that the journal bearing may be a bearing ring
stationarily mounted around the bearing pin rather than the journal
surface being the bearing pin itself. It is known that seal systems
for earth boring bit bearings may employ a sleeve mounted around
the bearing pin as the seal gland, rather than the seal gland being
directly formed on the bearing pin.
[0005] Increasing the life of a bearing system is a continuing goal
of earth boring bit manufacturers. It is known that various
materials, such as diamond and diamond-like-carbon material, may be
employed as the bearing and seal surfaces of the bearing system to
enhance the life.
[0006] A recent type of lightweight, ultra-hard and wear resistant
ceramics is in the area of complex ternary borides. These materials
comprise aluminum magnesium boride alloyed with a few atomic
percent group IV or group V elements as doping agents. The AlMgB14
intermetallic compound is based on four B12 icosahedral units
positioned within an orthorhombic unit cell containing 64 atoms.
The icosahedra are positioned at (0,0,0), (0,1/2,1/2), (1/2,0,0),
and (1/2,1/2,1/2) while the Al atoms occupy a four-fold position at
(1/4,3/4,1/4), and the Mg atoms occupy a four-fold position at
(0.25,0.359,0). The hardness and wear resistance of this material
are due to a complex interaction within each icosahedron
(intrahedral bonding) combined with interaction between the
icosahedra (intericosahedral bonding). The hexagonal icosahedra are
arranged in distorted, close-packed layers.
[0007] The family of materials comprising AlMgB14 along with its
alloys or doping agents is referred to herein as "BAM" materials.
The alloy materials may include at least the following doping
agents: titanium boride (TiB2); titanium carbide (TiC) plus iron,
nickel and carbon; silicon nitride (Si3N4) as a powder or
whiskered; boron carbide (B4C); titanium boride (TiB2); and
tungsten boride (W2B4). The alloying may be by mechanical alloying
consolidated by vacuum hot pressing or it may be by laser ablation
and/or magnetron sputtering.
[0008] The alloying agents can increase the hardness by as much as
10-20%, depending upon the particular doping agent used. The
dopants create distinct phases within the material that have
nanophase grain sizes down to 100 nm (nanometer). The term
"nanophase" is used to describe materials with phases less than 100
nm. In addition, some of the whiskered materials have fibers with
diameters in the nanometer realm. The "whiskered" material referred
to above is a form of a fiber composite. In brittle materials, it
generally entails including a small volume fraction of fibers of
one compound or phase with or within another non-fibrous larger
constitutive phase. The larger volume fraction phase is sometimes
considered the "matrix" phase. The general purpose of the
inclusions is to divert and deflect the propagation of cracks
through the body and also subsequently to perform negative work
through friction as two fractured surfaces attempt to pull apart
and withdraw embedded and still intact fibers from the matrix. In
ceramic composites, the whiskers (or fibers) can be between microns
and hundreds of microns long and microns in diameter all the way
down to nanometer dimensions in both length and diameter. There are
many factors that determine the optimization of both size and
volume fraction of fibers used in a composite.
[0009] A suggested use for BAM alloy materials is abrasive cutting
tools for industrial purpose. Applicants are not aware of BAM alloy
materials being used or suggested for use in bearing systems.
SUMMARY
[0010] A downhole well tool has at least one rotatable member, a
bearing system including a bearing member having bearing surfaces
on which the rotatable member rotates and a seal having a seal
surface in sliding engagement with a mating seal surface to retain
lubricant within the bearing system. At least one of the surfaces
comprises an AlMgB14 alloy material to enhance the life of the
bearing system.
[0011] The alloy material may include a dopant or alloy agent
consisting of: titanium boride (TiB2); titanium carbide (TiC) plus
iron, nickel and carbon; silicon nitride (Si3N4) powder; whiskered
silicon nitride (Si3N4); boron carbide (B4C); titanium boride
(TiB2); or tungsten boride (W2B4). The dopant creates a phase
within the alloy material that has a grain size less than 100
nanometers. If whiskered silicon nitride is used, it may comprise
fibers having diameters less than 100 nanometers.
[0012] The AlMgB14 alloy material may be a coating on at least one
of the surfaces of the bearing system. Alternately, it may be a
free-standing structure bonded to or forming one of the surfaces of
the bearing system.
[0013] The AlMgB14 alloy material may be located on and form a
cylindrical journal surface on the bearing member. It may be a flat
circular thrust face on the bearing member. The AlMgB14 alloy
material may be on cylindrical surfaces of roller bearings if the
well tool employs roller bearings.
[0014] The AlMgB14 alloy material may be on at least one of the
seal surfaces. For example it may be on a seal face of a rigid face
seal assembly. If an elastomeric seal is employed rather than a
rigid face seal assembly, the AlMgB14 alloy material may be on the
seal gland that is slidingly engaged by the elastomeric seal.
BRIEF DESCRIPTION OF THE DRAWINGS
[0015] FIG. 1 is a partial sectional view of a cone and bit leg of
an earth-boring bit having coatings applied in accordance with this
invention.
[0016] FIG. 2 is a perspective view of a bearing pin of an
earth-boring bit having a bearing sleeve with a surface treatment
applied in accordance with this invention.
[0017] FIG. 3 is a partial sectional view of an earth-boring bit
cone and bearing pin having roller bearings, the roller bearings
and other surfaces having surface treatments in accordance with
this invention.
[0018] FIG. 4 is an enlarged partial sectional view of a metal face
seal employable with an earth-boring bit, the metal face seal
having surface treatments applied in accordance with this
invention.
[0019] FIG. 5 is a sectional view illustrating an elastomeric seal
being employed with a floating insert ring, the insert ring being
employable with any of the embodiments above and having surface
treatments applied in accordance with this invention.
[0020] FIG. 6 is sectional view of a thrust washer that may be
employed with any of the embodiments above, the thrust washer
having surface treatments in accordance with this invention.
DETAILED DESCRIPTION OF THE INVENTION
[0021] Referring to FIG. 1, an example of a downhole well tool is
illustrated. A bit leg 11 of an earth-boring bit is shown, the bit
typically having three bit legs 11. A bearing member or pin 13
extends downward and inward from bit leg 11. Bearing pin 13 has a
cylindrical journal surface that terminates in a downward and
inward facing thrust shoulder or face 15. The lower portion of the
journal surface is the portion of bearing pin 13 that is subject to
the highest forces during drilling. A cylindrical nose 17 extends
downward and inward from thrust face 15.
[0022] A rotatable member, which in this example comprises a cone
19, mounts rotatably on bearing pin 13. Cone 19 has a cavity 21
that conforms to the configuration of bearing pin 13. Cone 19 may
be retained on bearing pin 13 by a plurality of locking elements or
ball bearings 23. Ball bearings 23 are located within mating
bearing races 25 formed on bearing pin 13 and in cavity 21. Cone 19
has a plurality of cutting elements 27 that protrude therefrom for
disintegrating the earth formation. A seal 31 is in dynamic,
sliding contact with a seal surface 30 on bearing pin 13 adjacent
where bearing pin 13 joins bit leg 11. Seal 31 is illustrated as an
elastomeric seal, but it could be a metal face seal assembly.
Cavity 21 is filled with a lubricant, and seal 31 seals the
lubricant within cavity 21 as well as preventing encroachment of
drilling fluid from the well bore being drilled. Bearing pin 13 and
the shell or body of cone 19 are typically formed of steel.
[0023] At least one of the surfaces of the bearing system is an
ultra-hard and wear resistant ceramic material in the area of
complex ternary borides and specifically comprising an AlMgB14
material. These materials comprise aluminum magnesium boride
alloyed with a few atomic percent group IV or group V elements as
doping agents. The AlMgB14 intermetallic compound is based on four
B12 icosahedral units positioned within an orthorhombic unit cell
containing 64 atoms. The icosahedra are positioned at (0,0,0),
(0,1/2,1/2), (1/2,0,0), and (1/2,1/2,1/2) while the Al atoms occupy
a four-fold position at (1/4,3/4,1/4), and the Mg atoms occupy a
four-fold position at (0.25,0.359,0). The hardness and wear
resistance of this material are due to a complex interaction within
each icosahedron (intrahedral bonding) combined with interaction
between the icosahedra (intericosahedral bonding). The hexagonal
icosahedra are arranged in distorted, close-packed layers.
[0024] The family of materials comprising AlMgB14 along with its
alloys or doping agents is referred to herein as "BAM" materials.
The alloy or doping agents may include at least one of the
following: titanium boride (TiB2); titanium carbide (TiC) plus
iron, nickel and carbon; silicon nitride (Si3N4) as a powder or
whiskered; boron carbide (B4C); titanium boride (TiB2); and
tungsten boride (W2B4). Some of the doping agents other than
silicon nitride may be available in a whiskered form. The alloying
may be by mechanical alloying consolidated by vacuum hot pressing
or it may be by laser ablation and/or magnetron sputtering.
[0025] The alloying agents can increase the hardness by as much as
10-20%, depending upon the particular doping agent used. The
dopants create distinct phases within the material that have
nanophase grain sizes down to 100 nm (nanometer). The term
"nanophase" is used to describe materials with phases less than 100
nm. In addition, some of the whiskered materials have fibers with
diameters in the nanometer realm. The "whiskered" material referred
to above is a form of a fiber composite. In brittle materials, it
generally entails including a small volume fraction of fibers of
one compound or phase with or within another non-fibrous larger
constitutive phase. The larger volume fraction phase is sometimes
considered the "matrix" phase. The general purpose of the
inclusions is to divert and deflect the propagation of cracks
through the body and also subsequently to perform negative work
through friction as two fractured surfaces attempt to pull apart
and withdraw embedded and still intact fibers from the matrix. In
ceramic composites, the whiskers (or fibers) can be between microns
and hundreds of microns long and microns in diameter all the way
down to nanometer dimensions in both length and diameter. There are
many factors that determine the optimization of both size and
volume fraction of fibers used in a composite.
[0026] The BAM materials may be formed into a free standing
structural member that is attached to a downhole well tool.
Alternately, the BAM materials may be applied as a thin film
coating.
[0027] Bearing pin 13 and/or cavity 21 may have a number of BAM
surface treatments 29 to prolong the life of the bearing surfaces
between bearing pin 13 and cone 19. The term "BAM surface
treatment" refers to either a solid, free standing member of BAM
materials attached to various parts of bearing pin 13 and/or cone
cavity 21, or to a coating applied to the steel surfaces of bearing
pin 13 and/or cone cavity 21. BAM surface treatment 29 is
illustrated on the cylindrical journal surface of bearing pin 13.
BAM surface treatment 29 could optionally be located on only the
lower or pressure side of bearing pin 13. A corresponding BAM
treatment 29 could also be on the mating portion of cavity 21. Or,
that portion of cavity 21 could contain a soft material, such as
silver.
[0028] BAM surface treatments 29 may also be located on thrust face
15 and the cylindrical portion of nose 17. Normally, the flat end
of nose 17 does not engage a surface in cone cavity 21, rather all
of the thrust is handled by thrust face 15. BAM surface treatments
29 could also be applied as coatings to ball bearings 23 and race
25. Each BAM surface treatment 29 could be in dynamic contact with
a steel surface, another surface containing a BAM surface treatment
29, a soft metal or other type of surface.
[0029] FIG. 2 illustrates another example of a BAM surface
treatment. A bit leg 33 has a bearing pin 35 generally as described
above. However in this instance, the journal bearing surface is not
formed directly on the bearing pin 35. Instead, a bearing ring 37
is press-fitted over or otherwise fixed on bearing pin 35. Bearing
ring 37 may be composed entirely of BAM material or it may be a
steel member that has a BAM surface treatment on at least the lower
side of its exterior cylindrical surface.
[0030] In addition, the drill bit in FIG. 2 may have a BAM surface
treatment on seal engaging surface or seal gland 43. Seal surface
43 is located between bearing ring 37 and bit leg 33 and is an
annular surface that will be engaged by an elastomeric seal, which
is not shown in FIG. 2. Bearing pin 35 in FIG. 2 also has a thrust
face 39 and a nose 41 as illustrated also in FIG. 1. Thrust face 39
and the cylindrical surface of nose 41 may have BAM surface
treatments, as described in connection with FIG. 1.
[0031] Referring to FIG. 3, a somewhat different bit leg 45 and
bearing pin 47 are illustrated. In this example, bearing pin 47 has
a thrust face 49 and a nose 51 as described above. A cone 53
slidingly engages and rotates relative to bearing pin 47; rather
than a cylindrical journal bearing surface, roller bearings 55 are
employed. Roller bearings 55 comprise individual cylindrical
members that are located in the same area where the journal surface
is located in FIGS. 1 and 2. Cone 53 has cutting elements 59 and
may be retained by ball bearings 57 in the same manner as
illustrated above. A metal face seal 61 seals lubricant within the
cavity of cone 53. BAM surface treatments could be applied to a
number of places on the bearing pin 47 and in cone 53. These areas
could include thrust face 49, roller bearings 55, ball bearings 57
and the dynamic sealing surfaces engaged by seal 61.
[0032] Referring to FIG. 4, a different type of seal assembly is
illustrated that could be used in place of elastomeric seal 31
shown in FIG. 1. The metal or rigid face seal assembly illustrated
in FIG. 4 locates in a seal gland 65 between bit leg 63 and cone
67. Cone 67 may have a sleeve 69 within its cavity that rotates
with cone 67. A metal or rigid seal ring 71 and a metal or rigid
cone sleeve 69 have mating end faces 73 that slidingly engage each
other. One or both end rigid faces 73 has a BAM surface treatment,
which may be a coating or a separate member attached to end face
73. As is conventional with this type of metal face seal, an
elastomeric energizer ring 75 exerts a force on metal seal ring 71
against face 73 of cone sleeve 69. Energizer ring 75 is
non-rotating and is deformed between seal gland 65 in bit leg 63
and metal seal ring 71. A backup ring 77 of elastomeric material
may be deformed in seal gland 65 between one side of energizer ring
75 and also an end of metal seal ring 71.
[0033] FIG. 5 illustrates another embodiment of a seal assembly
that could be used in place of elastomeric seal 31 of FIG. 1 and
metal face seal 61 of FIG. 3. In FIG. 5, bit leg 79 has a bearing
pin 81 extending downward and inward. A floating sleeve 83 slides
over bearing pin 81 and is fixed against rotation relative to
bearing pin 81. However, sleeve 83 is free to move slightly
relative to the axis of bearing pin 81 because it has an inner
diameter slightly larger than the outer diameter of bearing pin 81.
Floating sleeve 83 is also able to cock slightly relative to the
axis of bearing pin 81. Cone 85 has a seal groove or recess formed
in it. An elastomeric dynamic seal 89 is located in recess 87 and
deformed against floating sleeve 83. Dynamic seal 89 will normally
rotate with cone 85 and slide against the exterior cylindrical
surface of floating sleeve 83. Preferably a BAM surface treatment
91 is located on the portion of floating sleeve 83 that is
slidingly engaged by dynamic seal 89. A static seal 93 is located
in a groove on bearing pin 81 to engage the inner diameter of
floating sleeve 83.
[0034] FIG. 6 illustrates a thrust washer 95 that could be employed
in FIG. 1 between the thrust face 15 and the mating surface in the
cavity of cone 19. It could also be employed in FIG. 2 between
thrust face 39 and a mating surface of the cone that fits on
bearing pin 35. It could also be employed in FIG. 3 between thrust
face 49 and the mating surface in cone 53. Thrust washer 95 is a
flat washer having an outer diameter 97 and an inner diameter 99.
The inner diameter 99 will slide over the nose of the bearing pin
and could optionally be prevented from rotating relative to the
bearing pin. Thrust washer 95 contains BAM surface treatments 101
on one or both sides.
[0035] As mentioned, the various BAM surface treatments described
in connection with FIGS. 1-6 may be free standing members attached
to the downhole well tool, or they may be coatings. If coatings,
they can be applied in many different ways. They may be applied as
ceramic powders, ceramic coatings, thin film coatings sputtered
from targets, thick film laser formed or ablated powders, thick
film plasma spray powders and other known and similar coating
techniques in the art.
[0036] The BAM alloy material has very good abrasion resistance and
a low coefficient of friction, making it particularly suited for
use in bearing systems of rotating cone earth boring bits.
[0037] While the specification discloses only a few embodiments, it
should be apparent to those skilled in the art that various changes
and modifications may be made. For example, the BAM alloy material
could be used in non-lubricated bearing systems, such as air
drilling bits, as well as bits having lubricated bearing systems.
In addition, the BAM alloy material could be used in bearing
systems of earth boring bits other than conventional three-cone
bits.
* * * * *