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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
Referring to
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.
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.
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.
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.
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.
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.
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.
In addition, the drill bit in
Referring to
Referring to
As mentioned, the various BAM surface treatments described in connection with
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.
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.
This application claims priority to provisional application 61/294,675 filed Jan. 13, 2010.
Number | Date | Country | |
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61294675 | Jan 2010 | US |