US20110168451A1 - Boron Aluminum Magnesium Coating for Earth-Boring Bit - Google Patents
Boron Aluminum Magnesium Coating for Earth-Boring Bit Download PDFInfo
- Publication number
- US20110168451A1 US20110168451A1 US12/986,656 US98665611A US2011168451A1 US 20110168451 A1 US20110168451 A1 US 20110168451A1 US 98665611 A US98665611 A US 98665611A US 2011168451 A1 US2011168451 A1 US 2011168451A1
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- US
- United States
- Prior art keywords
- bearing
- seal
- almgb14
- alloy material
- well tool
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000000576 coating method Methods 0.000 title claims abstract description 17
- 239000011248 coating agent Substances 0.000 title claims abstract description 11
- -1 Boron Aluminum Magnesium Chemical compound 0.000 title description 2
- 229910002111 aluminum magnesium boride Inorganic materials 0.000 claims abstract description 55
- 239000000956 alloy Substances 0.000 claims abstract description 32
- 229910052581 Si3N4 Inorganic materials 0.000 claims abstract description 27
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims abstract description 27
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 14
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 14
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 14
- 239000010936 titanium Substances 0.000 claims abstract description 14
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 14
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 claims abstract description 14
- 210000004907 gland Anatomy 0.000 claims abstract description 10
- 239000000843 powder Substances 0.000 claims abstract description 10
- OFEAOSSMQHGXMM-UHFFFAOYSA-N 12007-10-2 Chemical compound [W].[W]=[B] OFEAOSSMQHGXMM-UHFFFAOYSA-N 0.000 claims abstract description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 7
- 238000005275 alloying Methods 0.000 claims abstract description 7
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 7
- 229910052742 iron Inorganic materials 0.000 claims abstract description 7
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 7
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 6
- 239000000463 material Substances 0.000 claims description 25
- 239000002019 doping agent Substances 0.000 claims description 15
- 239000000835 fiber Substances 0.000 claims description 14
- 230000013011 mating Effects 0.000 claims description 12
- 239000000314 lubricant Substances 0.000 claims description 7
- 229910045601 alloy Inorganic materials 0.000 claims description 5
- 238000005520 cutting process Methods 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 abstract description 14
- 239000002184 metal Substances 0.000 abstract description 14
- 238000004381 surface treatment Methods 0.000 description 22
- 239000002131 composite material Substances 0.000 description 6
- 229910000831 Steel Inorganic materials 0.000 description 4
- 239000000919 ceramic Substances 0.000 description 4
- 238000005553 drilling Methods 0.000 description 4
- 230000003993 interaction Effects 0.000 description 4
- 239000011159 matrix material Substances 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 239000011777 magnesium Substances 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000010408 film Substances 0.000 description 2
- 238000009501 film coating Methods 0.000 description 2
- 229910021480 group 4 element Inorganic materials 0.000 description 2
- 229910021478 group 5 element Inorganic materials 0.000 description 2
- 238000007731 hot pressing Methods 0.000 description 2
- 229910000765 intermetallic Inorganic materials 0.000 description 2
- 238000000608 laser ablation Methods 0.000 description 2
- 238000001755 magnetron sputter deposition Methods 0.000 description 2
- 238000005551 mechanical alloying Methods 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 239000010409 thin film Substances 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 239000003575 carbonaceous material Substances 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 239000013536 elastomeric material Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B10/00—Drill bits
- E21B10/08—Roller bits
- E21B10/22—Roller bits characterised by bearing, lubrication or sealing details
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/58—Raceways; Race rings
- F16C33/62—Selection of substances
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2206/00—Materials with ceramics, cermets, hard carbon or similar non-metallic hard materials as main constituents
- F16C2206/40—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2352/00—Apparatus for drilling
Definitions
- 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.
- 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.
- the seal system may comprise an elastomeric seal that is in sliding engagement with an annular gland journal on the bearing pin.
- journal bearing may be a bearing ring stationarily mounted around the bearing pin rather than the journal surface being the bearing pin itself.
- 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.
- 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).
- nanophase is used to describe materials with phases less than 100 nm.
- 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 whiskers 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.
- BAM alloy materials 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
- 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 .
- 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).
- nanophase is used to describe materials with phases less than 100 nm.
- 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 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 .
- 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.
- 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 .
- 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 .
- 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 .
- 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 .
- 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 .
- 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.
- 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.
- 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.
- the BAM alloy material could be used in bearing systems of earth boring bits other than conventional three-cone bits.
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- Mining & Mineral Resources (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Geology (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Fluid Mechanics (AREA)
- Geochemistry & Mineralogy (AREA)
- Environmental & Geological Engineering (AREA)
- Materials Engineering (AREA)
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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.
Description
- This application claims priority to
provisional application 61/294,675 filed Jan. 13, 2010. - 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.
-
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. -
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. -
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. -
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. -
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. -
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. - Referring to
FIG. 1 , an example of a downhole well tool is illustrated. Abit leg 11 of an earth-boring bit is shown, the bit typically having threebit legs 11. A bearing member or pin 13 extends downward and inward frombit leg 11. Bearing pin 13 has a cylindrical journal surface that terminates in a downward and inward facing thrust shoulder orface 15. The lower portion of the journal surface is the portion of bearing pin 13 that is subject to the highest forces during drilling. Acylindrical nose 17 extends downward and inward fromthrust face 15. - A rotatable member, which in this example comprises a
cone 19, mounts rotatably on bearing pin 13.Cone 19 has acavity 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 orball bearings 23.Ball bearings 23 are located withinmating bearing races 25 formed on bearing pin 13 and incavity 21.Cone 19 has a plurality of cuttingelements 27 that protrude therefrom for disintegrating the earth formation. Aseal 31 is in dynamic, sliding contact with aseal surface 30 on bearing pin 13 adjacent where bearing pin 13 joinsbit 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 withincavity 21 as well as preventing encroachment of drilling fluid from the well bore being drilled. Bearing pin 13 and the shell or body ofcone 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 ofBAM surface treatments 29 to prolong the life of the bearing surfaces between bearing pin 13 andcone 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/orcone cavity 21, or to a coating applied to the steel surfaces of bearing pin 13 and/orcone 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 correspondingBAM treatment 29 could also be on the mating portion ofcavity 21. Or, that portion ofcavity 21 could contain a soft material, such as silver. -
BAM surface treatments 29 may also be located onthrust face 15 and the cylindrical portion ofnose 17. Normally, the flat end ofnose 17 does not engage a surface incone cavity 21, rather all of the thrust is handled bythrust face 15.BAM surface treatments 29 could also be applied as coatings toball bearings 23 andrace 25. EachBAM surface treatment 29 could be in dynamic contact with a steel surface, another surface containing aBAM surface treatment 29, a soft metal or other type of surface. -
FIG. 2 illustrates another example of a BAM surface treatment. Abit leg 33 has abearing pin 35 generally as described above. However in this instance, the journal bearing surface is not formed directly on thebearing pin 35. Instead, abearing ring 37 is press-fitted over or otherwise fixed on bearingpin 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. - In addition, the drill bit in
FIG. 2 may have a BAM surface treatment on seal engaging surface or sealgland 43.Seal surface 43 is located between bearingring 37 and bitleg 33 and is an annular surface that will be engaged by an elastomeric seal, which is not shown inFIG. 2 .Bearing pin 35 inFIG. 2 also has athrust face 39 and anose 41 as illustrated also inFIG. 1 . Thrust face 39 and the cylindrical surface ofnose 41 may have BAM surface treatments, as described in connection withFIG. 1 . - Referring to
FIG. 3 , a somewhatdifferent bit leg 45 and bearingpin 47 are illustrated. In this example, bearingpin 47 has athrust face 49 and anose 51 as described above. Acone 53 slidingly engages and rotates relative to bearingpin 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 inFIGS. 1 and 2 .Cone 53 has cuttingelements 59 and may be retained byball bearings 57 in the same manner as illustrated above. Ametal face seal 61 seals lubricant within the cavity ofcone 53. BAM surface treatments could be applied to a number of places on thebearing pin 47 and incone 53. These areas could include thrustface 49,roller bearings 55,ball bearings 57 and the dynamic sealing surfaces engaged byseal 61. - Referring to
FIG. 4 , a different type of seal assembly is illustrated that could be used in place ofelastomeric seal 31 shown inFIG. 1 . The metal or rigid face seal assembly illustrated inFIG. 4 locates in aseal gland 65 betweenbit leg 63 andcone 67.Cone 67 may have asleeve 69 within its cavity that rotates withcone 67. A metal orrigid seal ring 71 and a metal orrigid 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 endface 73. As is conventional with this type of metal face seal, anelastomeric energizer ring 75 exerts a force onmetal seal ring 71 againstface 73 ofcone sleeve 69.Energizer ring 75 is non-rotating and is deformed betweenseal gland 65 inbit leg 63 andmetal seal ring 71. Abackup ring 77 of elastomeric material may be deformed inseal gland 65 between one side ofenergizer ring 75 and also an end ofmetal seal ring 71. -
FIG. 5 illustrates another embodiment of a seal assembly that could be used in place ofelastomeric seal 31 ofFIG. 1 andmetal face seal 61 ofFIG. 3 . InFIG. 5 ,bit leg 79 has abearing pin 81 extending downward and inward. A floatingsleeve 83 slides over bearingpin 81 and is fixed against rotation relative to bearingpin 81. However,sleeve 83 is free to move slightly relative to the axis of bearingpin 81 because it has an inner diameter slightly larger than the outer diameter of bearingpin 81. Floatingsleeve 83 is also able to cock slightly relative to the axis of bearingpin 81.Cone 85 has a seal groove or recess formed in it. An elastomericdynamic seal 89 is located inrecess 87 and deformed against floatingsleeve 83.Dynamic seal 89 will normally rotate withcone 85 and slide against the exterior cylindrical surface of floatingsleeve 83. Preferably aBAM surface treatment 91 is located on the portion of floatingsleeve 83 that is slidingly engaged bydynamic seal 89. Astatic seal 93 is located in a groove on bearingpin 81 to engage the inner diameter of floatingsleeve 83. -
FIG. 6 illustrates athrust washer 95 that could be employed inFIG. 1 between thethrust face 15 and the mating surface in the cavity ofcone 19. It could also be employed inFIG. 2 between thrust face 39 and a mating surface of the cone that fits on bearingpin 35. It could also be employed inFIG. 3 between thrust face 49 and the mating surface incone 53.Thrust washer 95 is a flat washer having anouter diameter 97 and aninner diameter 99. Theinner 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 containsBAM surface treatments 101 on one or both sides. - 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. - 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.
Claims (21)
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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US12/986,656 US20110168451A1 (en) | 2010-01-13 | 2011-01-07 | Boron Aluminum Magnesium Coating for Earth-Boring Bit |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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US29467510P | 2010-01-13 | 2010-01-13 | |
US12/986,656 US20110168451A1 (en) | 2010-01-13 | 2011-01-07 | Boron Aluminum Magnesium Coating for Earth-Boring Bit |
Publications (1)
Publication Number | Publication Date |
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US20110168451A1 true US20110168451A1 (en) | 2011-07-14 |
Family
ID=44257642
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US12/986,656 Abandoned US20110168451A1 (en) | 2010-01-13 | 2011-01-07 | Boron Aluminum Magnesium Coating for Earth-Boring Bit |
Country Status (4)
Country | Link |
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US (1) | US20110168451A1 (en) |
CN (1) | CN102128009A (en) |
MX (1) | MX2011000472A (en) |
RU (1) | RU2011100714A (en) |
Cited By (9)
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US8689909B2 (en) | 2010-10-29 | 2014-04-08 | Baker Hughes Incorporated | Inserts, polycrystalline diamond compact cutting elements, earth-boring bits comprising same, and methods of forming same |
WO2015116272A1 (en) * | 2013-11-21 | 2015-08-06 | General Electric Company | Bearing having components fabricated from a almgb14 containing ceramic matrix composite |
US20150322741A1 (en) * | 2013-02-07 | 2015-11-12 | Robert P. Badrak | Hard Surfacing Non-Metallic Slip Components for Downhole Tools |
US9695875B2 (en) | 2013-07-17 | 2017-07-04 | Roller Bearing Company Of America, Inc. | Top drive bearing for use in a top drive system, and made of non-vacuum arc remelted steel configured to achieve an extended life cycle at least equivalent to a life factor of three for a vacuum arc remelted steel |
US20190120291A1 (en) * | 2017-10-24 | 2019-04-25 | Hamilton Sundstrand Corporation | Air bearing |
US10364483B1 (en) | 2013-03-01 | 2019-07-30 | The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | High hardness, high elasticity intermetallic compounds for mechanical components |
US10443237B2 (en) | 2017-04-20 | 2019-10-15 | Samuel J. Lanahan | Truncated icosahedra assemblies |
CN111411270A (en) * | 2020-05-21 | 2020-07-14 | 滨州渤海活塞有限公司 | Method for changing morphology of ferrosilicon phase in aluminum alloy |
US10900751B1 (en) * | 2016-11-29 | 2021-01-26 | New Tech Ceramics, Inc | Boron aluminum magnesium and boron carbide compositions and articles incorporating such compositions |
Families Citing this family (1)
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CN111173454A (en) * | 2019-08-30 | 2020-05-19 | 沧州格锐特钻头有限公司 | Combined drill bit with three-blade composite teeth and three-gear teeth |
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- 2011-01-07 US US12/986,656 patent/US20110168451A1/en not_active Abandoned
- 2011-01-12 MX MX2011000472A patent/MX2011000472A/en not_active Application Discontinuation
- 2011-01-13 RU RU2011100714/02A patent/RU2011100714A/en not_active Application Discontinuation
- 2011-01-13 CN CN2011100409062A patent/CN102128009A/en active Pending
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US20030219605A1 (en) * | 2002-02-14 | 2003-11-27 | Iowa State University Research Foundation Inc. | Novel friction and wear-resistant coatings for tools, dies and microelectromechanical systems |
US20090194339A1 (en) * | 2007-07-13 | 2009-08-06 | Baker Hughes Incorporated | Earth boring bit with wear resistant bearing and seal |
US8039096B2 (en) * | 2008-06-30 | 2011-10-18 | Eaton Corporation | Friction- and wear-reducing coating |
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8689909B2 (en) | 2010-10-29 | 2014-04-08 | Baker Hughes Incorporated | Inserts, polycrystalline diamond compact cutting elements, earth-boring bits comprising same, and methods of forming same |
US20150322741A1 (en) * | 2013-02-07 | 2015-11-12 | Robert P. Badrak | Hard Surfacing Non-Metallic Slip Components for Downhole Tools |
US9739105B2 (en) * | 2013-02-07 | 2017-08-22 | Weatherford Technology Holdings, Llc | Hard surfacing non-metallic slip components for downhole tools |
US10364483B1 (en) | 2013-03-01 | 2019-07-30 | The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | High hardness, high elasticity intermetallic compounds for mechanical components |
US9695875B2 (en) | 2013-07-17 | 2017-07-04 | Roller Bearing Company Of America, Inc. | Top drive bearing for use in a top drive system, and made of non-vacuum arc remelted steel configured to achieve an extended life cycle at least equivalent to a life factor of three for a vacuum arc remelted steel |
WO2015116272A1 (en) * | 2013-11-21 | 2015-08-06 | General Electric Company | Bearing having components fabricated from a almgb14 containing ceramic matrix composite |
US9169872B2 (en) | 2013-11-21 | 2015-10-27 | General Electric Company | Bearing having components fabricated from a ceramic matrix composite |
JP2016539290A (en) * | 2013-11-21 | 2016-12-15 | ゼネラル・エレクトリック・カンパニイ | Bearing with components made from ceramic matrix composite |
US10900751B1 (en) * | 2016-11-29 | 2021-01-26 | New Tech Ceramics, Inc | Boron aluminum magnesium and boron carbide compositions and articles incorporating such compositions |
US10443237B2 (en) | 2017-04-20 | 2019-10-15 | Samuel J. Lanahan | Truncated icosahedra assemblies |
US20190120291A1 (en) * | 2017-10-24 | 2019-04-25 | Hamilton Sundstrand Corporation | Air bearing |
CN111411270A (en) * | 2020-05-21 | 2020-07-14 | 滨州渤海活塞有限公司 | Method for changing morphology of ferrosilicon phase in aluminum alloy |
Also Published As
Publication number | Publication date |
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RU2011100714A (en) | 2012-07-20 |
CN102128009A (en) | 2011-07-20 |
MX2011000472A (en) | 2011-07-21 |
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