US20090057033A1 - High energy cutting elements and bits incorporating the same - Google Patents
High energy cutting elements and bits incorporating the same Download PDFInfo
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- US20090057033A1 US20090057033A1 US12/264,172 US26417208A US2009057033A1 US 20090057033 A1 US20090057033 A1 US 20090057033A1 US 26417208 A US26417208 A US 26417208A US 2009057033 A1 US2009057033 A1 US 2009057033A1
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- 239000000463 material Substances 0.000 claims abstract description 65
- 238000005553 drilling Methods 0.000 claims abstract description 20
- GJNGXPDXRVXSEH-UHFFFAOYSA-N 4-chlorobenzonitrile Chemical compound ClC1=CC=C(C#N)C=C1 GJNGXPDXRVXSEH-UHFFFAOYSA-N 0.000 claims abstract 22
- 239000000758 substrate Substances 0.000 claims description 22
- 230000015572 biosynthetic process Effects 0.000 claims description 13
- 230000002093 peripheral effect Effects 0.000 claims 1
- 239000010410 layer Substances 0.000 description 55
- 238000005755 formation reaction Methods 0.000 description 11
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 239000013078 crystal Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- 229910052582 BN Inorganic materials 0.000 description 3
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 239000010941 cobalt Substances 0.000 description 3
- 229910017052 cobalt Inorganic materials 0.000 description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 3
- 229910003460 diamond Inorganic materials 0.000 description 3
- 239000010432 diamond Substances 0.000 description 3
- 238000005087 graphitization Methods 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 2
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000010008 shearing Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 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 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- 229910018125 Al-Si Inorganic materials 0.000 description 1
- 229910000951 Aluminide Inorganic materials 0.000 description 1
- 229910018520 Al—Si Inorganic materials 0.000 description 1
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001347 Stellite Inorganic materials 0.000 description 1
- 229910033181 TiB2 Inorganic materials 0.000 description 1
- -1 TiCN Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- AHICWQREWHDHHF-UHFFFAOYSA-N chromium;cobalt;iron;manganese;methane;molybdenum;nickel;silicon;tungsten Chemical compound C.[Si].[Cr].[Mn].[Fe].[Co].[Ni].[Mo].[W] AHICWQREWHDHHF-UHFFFAOYSA-N 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 229910001026 inconel Inorganic materials 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 239000008207 working material Substances 0.000 description 1
Images
Classifications
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- 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
- E21B10/46—Drill bits characterised by wear resisting parts, e.g. diamond inserts
- E21B10/56—Button-type inserts
- E21B10/567—Button-type inserts with preformed cutting elements mounted on a distinct support, e.g. polycrystalline inserts
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/58—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides
- C04B35/583—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on boron nitride
- C04B35/5831—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on boron nitride based on cubic boron nitrides or Wurtzitic boron nitrides, including crystal structure transformation of powder
-
- 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
- E21B10/46—Drill bits characterised by wear resisting parts, e.g. diamond inserts
- E21B10/56—Button-type inserts
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3804—Borides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3804—Borides
- C04B2235/3813—Refractory metal borides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3817—Carbides
- C04B2235/3839—Refractory metal carbides
- C04B2235/3843—Titanium carbides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
- C04B2235/3856—Carbonitrides, e.g. titanium carbonitride, zirconium carbonitride
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
- C04B2235/3865—Aluminium nitrides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
- C04B2235/3886—Refractory metal nitrides, e.g. vanadium nitride, tungsten nitride
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/74—Physical characteristics
- C04B2235/78—Grain sizes and shapes, product microstructures, e.g. acicular grains, equiaxed grains, platelet-structures
- C04B2235/786—Micrometer sized grains, i.e. from 1 to 100 micron
Definitions
- This invention relates to cutting elements and more specifically to high energy shear cutting elements having a cutting layer comprising polycrystalline cubic boron nitride (PCBN) and to bits incorporating the same and more specifically to turbine driven bits incorporating the same.
- PCBN polycrystalline cubic boron nitride
- PCD polycrystalline diamond
- the catalyst found in PCD material is sometimes fully leached so as to enhance the thermal stability of the PCD material.
- the PCD can withstand temperatures up to 1000° C. in air.
- graphitization of the PCD does increase with temperatures above 1000° C. Consequently, shear cutting elements having a PCD cutting layer cannot be used to cut earth formation when the cutting layer temperature will exceed 650° C. or 1000° C., depending on whether the PCD layer is leached.
- Turbine bits Cutting layer temperatures of cutting elements on bits driven by high speed turbines or motors (hereinafter “turbine bits”) exceed 1000° C. These bits are operated at greater than 300 RPM, to cut formations having a strength greater than 10,000 psi. Turbines driving turbine bits typically operate at RPM levels of 1,000 RPM or greater and the turbine bits rotate at levels of about 300 RPM or greater.
- PCBN has been disclosed for use in cutting elements for drilling of formations.
- no PCBN materials is used as a cutting layer in earth-boring conditions due to its relatively poor strength and toughness when compared to PCD.
- a bit for drilling earth formations having a shear cutting element mounted thereon.
- the shear cutting element includes a substrate and a cutting layer over the substrate.
- the cutting layer includes a PCBN portion for contacting a formation during drilling.
- the bit is operable at rotational speeds exposing the PCBN portion to temperatures of at least 1000° C.
- the entire cutting layer is made of PCBN.
- the PCBN in an exemplary embodiment has a strength of 100 ksi and in another exemplary embodiment has a strength in the range of 100 to 200 ksi.
- another ultra hard material is provided adjacent to the PCBN portion.
- the ultra hard material in one exemplary embodiment is PCD.
- the ultra hard material may form a layer interposed between the PCBN portion and the substrate.
- the PCD layer may be partly of wholly leached.
- the PCBN material may be a single layer of material or may be formed from multiple layers of PCBN material having the same or different characteristics.
- the PCBN protects the PCD from high temperatures.
- the PCBN material ensures that the operating temperature of the PCD is maintained at or below 650° C.
- the operating temperature of the PCD is maintained at or below 1000° C.
- the PCBN has a thermal gradient ranging from about 200 to 2000° C./mm.
- the bit is driven by a turbine operating at least at 1000 RPM. In another exemplary embodiment, the bit rotates at a rotational speed of at least 300 RPM and in a further exemplary embodiment the bit rotates in the range of 400 to 1400 RPM. In yet a further exemplary embodiment, during drilling the weight on the bit is in the range of 10,000 lbs. to 45,000 lbs. In another exemplary embodiment, during drilling the weight on the bit is in the range of 15,000 lbs. to 45,000 lbs. In yet another exemplary embodiment, during drilling the weight on the bit is in the range of 10,000 lbs. to 15,000 lbs.
- the bit may be any type of bit incorporating shear cutting elements, as for example a drag bit or a roller cone bit.
- FIG. 1 is a perspective view of a drag bit incorporating exemplary cutting elements of the present invention.
- FIG. 2 is a partial cut out view of a rotary cone bit incorporating exemplary cutting elements of the present invention.
- FIGS. 3-9 are cross-sectional views of exemplary embodiment cutting elements of the present invention.
- shear cutting elements which include a cutting layer including polycrystalline cubic boron nitride (“PCBN”) for use with turbine bits for drilling earth formations with a shearing action where the temperature at the cutting layer of the cutting element exceeds 1000° C. during drilling.
- PCBN polycrystalline cubic boron nitride
- turbine driven bits incorporating such cutting elements are provided.
- PCBN is a suitable material for a cutting layer in a shear cutting element used in a turbine bit.
- PCBN provides for thermal stability at high temperature and is able to withstand the loads provided during drilling with turbine bits.
- turbine bits although operating at higher RPMs, tend to have lower vibrations and impact loads. Consequently, applicant believes that the PCBN material will withstand the operating environment during drilling.
- PCBN is a suitable material for use in a cutting layer of shear cutting element on a turbine bit.
- the exemplary shear cutting elements for use with turbine bits include PCBN in their cutting layer for making contact with the earth formations during drilling.
- the PCBN material is capable of operating at temperatures is excess of about 1000° C.
- These cutting elements are high-energy cutting elements in that they may be used with turbine bits for high speed high temperature drilling. Turbines drive the turbine bits at RPMs at greater than 300 RPM. Some turbine bits operate in the range of 400 to 1400 RPM. Turbine bits may be used to cut formations having strength of greater than 10,000 psi.
- the exemplary high-energy cutting elements may be used on many types of bits where the cutting elements cut via a shearing action.
- these cutting elements may be used as cutting elements 2 in a drag bit 4 or may be used as gage cutters 6 in a rotary cone bit 8 , as for example shown in FIGS. 1 and 2 , respectively.
- the exemplary cutting elements are formed using known sintering methods whereby CBN powder is sintered onto a substrate such as a tungsten carbide substrate forming a PCBN layer bonded to the substrate.
- the substrate may form the body of the cutting element.
- the substrate with bonded PCBN form a compact which may then be bonded to a body of the cutting element.
- the PCBN cutting layer may be formed separately and then bonded to the body of the cutting element.
- Exemplary PCBN materials that may be used to form the cutting layers of these high-energy cutting elements may be PCBN materials having a strength greater than 100 ksi and in an exemplary embodiment in the range of about 100 to 200 ksi.
- PCBN materials are known in the art.
- An exemplary PCBN material may formed by coarse grain cubic boron nitride (“CBN”) crystals mixed with about 10% to about 20% fine CBN crystals in the range of 0-2 microns, which are synthesized with a catalyst material such as Al, Al—Si, TiCN, cobalt aluminide or mixtures thereof during the sintering process.
- Exemplary coarse grain CBN crystals have a size in the range of 2-10 microns.
- the PCBN material has CBN having an average grain size in the range of 10-20 microns and has a density greater than 93%.
- the PCBN material has an average grain size less than 5 microns.
- PCBN materials that are suitable, include PCBN materials which have been developed for turning applications of ferrous and non-ferrous materials where the working material temperatures exceed 1000° C. and in many instances exceed 1100° C.
- Exemplary materials include materials used in the finish turning of steel and other high temperature metals such Stellite, Inconel etc.
- Other PCBN materials may also be used which have been developed for use in high-speed applications where heat is an issue. In one exemplary embodiment, such materials include in the range of 45% to 80% CBN by volume. Further exemplary embodiment PCBN materials that may be used are described in U.S. Pat. No. 6,331,497, the contents of which are fully incorporated herein by reference.
- PCBN materials may include CBN having a crystal size in the range of from about 10 to 17 microns and including in the range of from 2 to 15% by weight of a material selected from the group of refractory compounds consisting of titanium diboride, aluminum diboride, titanium carbide, titanium nitride, titanium carbonitride, and titanium aluminum carbonitride.
- the carbonitride system encompasses a range of compositions from titanium nitride to titanium carbide.
- the carbonitride has a carbon to nitrogen proportion in the range of from 20 atomic percent carbon and 70 atomic percent nitrogen to 70 atomic percent carbon and 30 atomic percent nitrogen.
- the mixture of CBN and refractory compound is infiltrated with aluminum and/or silicon, preferably a eutectic composition of silicon and aluminum.
- a PCBN layer 10 is bonded to a substrate 12 forming a cutting element 14 , as for example shown in FIG. 3 .
- the PCBN layer 10 makes up the entire cutting layer.
- the PCBN cutting layer is engineered to have a thermal gradient in the range of 2000 to 2000° C./mm.
- the cutting layer is designed such that the temperature drops from about 200° C. to 2000° C. per millimeter away from the working surface 24 as for example shown in FIG. 4 .
- Exemplary cutting layers may contain greater than 90% by weight PCBN or may be formed from mixtures of PCBN and other ceramic materials.
- any of the aforementioned PCBN cutting layers may be formed from two or more PCBN layers 26 each having the same or different thermal gradients, and/or the same or different thicknesses as for example, shown in FIG. 5 .
- the cutting layer may be a composite of PCD and PCBN.
- the cutting layer may be engineered to have better strength and toughness when compared to a PCBN material by itself.
- a PCBN layer 16 may be bonded to a PCD 18 layer as for example shown in FIG. 6 .
- a PCBN layer 20 may cover the entire PCD layer 22 , as for example shown in FIG. 7 where the PCBN layer encapsulates the PCD layer.
- the composite cutting layer incorporating a PCD material as well as a PCBN material may be formed in accordance with the principles described in U.S. Pat. Nos. 4,403,015; 5,510,193; and 5,603,070, the contents of which are fully incorporated herein by reference.
- the PCBN outer layer serves to protect the PCD material from the operating temperatures in excess of 1000° C.
- the temperature to which the PCD material is exposed to can be controlled by controlling the thickness and/or the thermal gradient of the PCBN layer.
- the PCBN layer serves to keep the temperature of the PCD material below 650° C., or below 1000° C. if the PCD material is leached. In this regard, the PCD material is not subject to graphitization due to high temperature exposure.
- any of the aforementioned PCBN materials may be used to form a cutting layer having a layer 28 surrounding another ultra hard material layer 30 , such as a PCD ultra hard material layer 30 , as for example shown in FIG. 8 .
- the cutting edge 32 that will be exposed to the highest temperatures during drilling is made of PCBN.
- the PCBN material may extend around the entire periphery of the cutting element, as for example shown in FIG. 8 .
- the PCBN material may form only the portion of the cutting layer defining an edge 34 that will make contact with the earth formation during drilling, as for example shown in FIG. 9 .
- the remaining portion 36 of the cutting layer may be made from another material such as another PCBN material or another PCD material, as for example shown in FIG. 9 .
- the PCBN portion to make contact with the earth formations may extend along the entire thickness of the cutting layer 38 as shown in FIG. 8 or may extend along a portion of the thickness of the cutting layer 38 as shown in FIG. 9 .
- the PCBN material serves to protect the other ultra hard material in the cutting layer from the high operational temperatures.
- the cutting elements may be engineered for the task at hand by providing the appropriate PCBN materials proximate the cutting edge of the cutting element which is subjected to high temperatures, as for example, temperatures in excess of 1000° C. during drilling.
- high temperatures as for example, temperatures in excess of 1000° C. during drilling.
- an engineered cutting layer material is formed that is capable of withstanding the high operating temperatures and have sufficient strength and toughness for the drilling at task.
- the exemplary embodiment cutting elements mounted on turbine-driven bits would be able to operate in cutting environments where the weight on the bit will be at least 10,000 lbs. and in one exemplary embodiment, will be in the range of 10,000 lbs. to 45,000 lbs. In another exemplary embodiment, the weight on the bit will be in the range of 10,000 lbs. to 15,000 lbs. In a further exemplary embodiment, the weight on the bit will be in the range of 15,000 lbs. to 45,000 lbs.
- substrate means any body onto which an exemplary cutting layer is bonded to.
- a substrate may be the body of a cutting element or a transition layer bonded to the body of a cutting element.
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Abstract
High energy cutting elements and bits incorporating the same are provided. The cutting elements have at least a portion of their cutting layers which will be exposed to high temperatures during drilling formed from a PCBN material capable of operating at temperatures of at least 1000° C.
Description
- This application is a continuation application of U.S. application Ser. No. 11/449,523 filed on Jun. 7, 2006 which claims priority and is based upon U.S. Provisional Application No. 60/705,518 filed on Aug. 3, 2005, the contents of which are fully incorporated herein by reference.
- This invention relates to cutting elements and more specifically to high energy shear cutting elements having a cutting layer comprising polycrystalline cubic boron nitride (PCBN) and to bits incorporating the same and more specifically to turbine driven bits incorporating the same.
- Shear cutting elements used in earth-boring bits have a tungsten carbide substrate body over which is bonded a polycrystalline diamond (“PCD”) material cutting layer which is used to do the cutting. PCD materials, however, have many limitations. For example, the thermal stability of PCD deteriorates due to graphitization at temperatures above 650° C. This is typically caused by the air and the presence of cobalt around the diamond crystals. Similarly, cracking tends to develop at temperatures above 650° C. due to thermal mismatch between the diamond crystals and cobalt forming the PCD material layer.
- In an effort to get PCD to operate at higher temperatures, the catalyst found in PCD material is sometimes fully leached so as to enhance the thermal stability of the PCD material. In such case, the PCD can withstand temperatures up to 1000° C. in air. However, graphitization of the PCD does increase with temperatures above 1000° C. Consequently, shear cutting elements having a PCD cutting layer cannot be used to cut earth formation when the cutting layer temperature will exceed 650° C. or 1000° C., depending on whether the PCD layer is leached.
- Cutting layer temperatures of cutting elements on bits driven by high speed turbines or motors (hereinafter “turbine bits”) exceed 1000° C. These bits are operated at greater than 300 RPM, to cut formations having a strength greater than 10,000 psi. Turbines driving turbine bits typically operate at RPM levels of 1,000 RPM or greater and the turbine bits rotate at levels of about 300 RPM or greater.
- PCBN has been disclosed for use in cutting elements for drilling of formations. However, to date no PCBN materials is used as a cutting layer in earth-boring conditions due to its relatively poor strength and toughness when compared to PCD.
- Cutting elements for drilling earth formations at high temperature and high speeds as well as bits incorporating such cutting elements are provided. In one exemplary embodiment, a bit for drilling earth formations is provided having a shear cutting element mounted thereon. The shear cutting element includes a substrate and a cutting layer over the substrate. The cutting layer includes a PCBN portion for contacting a formation during drilling. The bit is operable at rotational speeds exposing the PCBN portion to temperatures of at least 1000° C. In one exemplary embodiment, the entire cutting layer is made of PCBN. The PCBN in an exemplary embodiment has a strength of 100 ksi and in another exemplary embodiment has a strength in the range of 100 to 200 ksi. In a further exemplary embodiment, another ultra hard material is provided adjacent to the PCBN portion. The ultra hard material in one exemplary embodiment is PCD. The ultra hard material may form a layer interposed between the PCBN portion and the substrate. The PCD layer may be partly of wholly leached. In another exemplary embodiment, the PCBN material may be a single layer of material or may be formed from multiple layers of PCBN material having the same or different characteristics.
- In yet a further exemplary embodiment where PCD is used along with PCBN to form the cutting element cutting layer, the PCBN protects the PCD from high temperatures. For example in cases where the PCD is not leached, the PCBN material ensures that the operating temperature of the PCD is maintained at or below 650° C. In cases where the PCD is fully leached, the operating temperature of the PCD is maintained at or below 1000° C. In another exemplary embodiment, the PCBN has a thermal gradient ranging from about 200 to 2000° C./mm.
- In one exemplary embodiment, the bit is driven by a turbine operating at least at 1000 RPM. In another exemplary embodiment, the bit rotates at a rotational speed of at least 300 RPM and in a further exemplary embodiment the bit rotates in the range of 400 to 1400 RPM. In yet a further exemplary embodiment, during drilling the weight on the bit is in the range of 10,000 lbs. to 45,000 lbs. In another exemplary embodiment, during drilling the weight on the bit is in the range of 15,000 lbs. to 45,000 lbs. In yet another exemplary embodiment, during drilling the weight on the bit is in the range of 10,000 lbs. to 15,000 lbs. The bit may be any type of bit incorporating shear cutting elements, as for example a drag bit or a roller cone bit.
-
FIG. 1 is a perspective view of a drag bit incorporating exemplary cutting elements of the present invention. -
FIG. 2 is a partial cut out view of a rotary cone bit incorporating exemplary cutting elements of the present invention. -
FIGS. 3-9 are cross-sectional views of exemplary embodiment cutting elements of the present invention. - In an exemplary embodiment, shear cutting elements are provided which include a cutting layer including polycrystalline cubic boron nitride (“PCBN”) for use with turbine bits for drilling earth formations with a shearing action where the temperature at the cutting layer of the cutting element exceeds 1000° C. during drilling. In other exemplary embodiments, turbine driven bits incorporating such cutting elements are provided.
- Although PCBN materials have not been suitable for use with cutting elements mounted on earth boring bits, applicant believes that PCBN is a suitable material for a cutting layer in a shear cutting element used in a turbine bit. PCBN provides for thermal stability at high temperature and is able to withstand the loads provided during drilling with turbine bits. Applicant has discovered that turbine bits, although operating at higher RPMs, tend to have lower vibrations and impact loads. Consequently, applicant believes that the PCBN material will withstand the operating environment during drilling. Thus, applicant believes that PCBN is a suitable material for use in a cutting layer of shear cutting element on a turbine bit.
- The exemplary shear cutting elements for use with turbine bits include PCBN in their cutting layer for making contact with the earth formations during drilling. The PCBN material is capable of operating at temperatures is excess of about 1000° C. These cutting elements are high-energy cutting elements in that they may be used with turbine bits for high speed high temperature drilling. Turbines drive the turbine bits at RPMs at greater than 300 RPM. Some turbine bits operate in the range of 400 to 1400 RPM. Turbine bits may be used to cut formations having strength of greater than 10,000 psi.
- The exemplary high-energy cutting elements may be used on many types of bits where the cutting elements cut via a shearing action. For example, these cutting elements may be used as
cutting elements 2 in a drag bit 4 or may be used asgage cutters 6 in arotary cone bit 8, as for example shown inFIGS. 1 and 2 , respectively. - The exemplary cutting elements are formed using known sintering methods whereby CBN powder is sintered onto a substrate such as a tungsten carbide substrate forming a PCBN layer bonded to the substrate. The substrate may form the body of the cutting element. In other exemplary embodiments, the substrate with bonded PCBN form a compact which may then be bonded to a body of the cutting element. In other exemplary embodiments, the PCBN cutting layer may be formed separately and then bonded to the body of the cutting element.
- Exemplary PCBN materials that may be used to form the cutting layers of these high-energy cutting elements may be PCBN materials having a strength greater than 100 ksi and in an exemplary embodiment in the range of about 100 to 200 ksi. Such PCBN materials are known in the art. An exemplary PCBN material may formed by coarse grain cubic boron nitride (“CBN”) crystals mixed with about 10% to about 20% fine CBN crystals in the range of 0-2 microns, which are synthesized with a catalyst material such as Al, Al—Si, TiCN, cobalt aluminide or mixtures thereof during the sintering process. Exemplary coarse grain CBN crystals have a size in the range of 2-10 microns. In another exemplary embodiment, the PCBN material has CBN having an average grain size in the range of 10-20 microns and has a density greater than 93%. In another exemplary embodiment, the PCBN material has an average grain size less than 5 microns.
- Other PCBN materials that are suitable, include PCBN materials which have been developed for turning applications of ferrous and non-ferrous materials where the working material temperatures exceed 1000° C. and in many instances exceed 1100° C. Exemplary materials include materials used in the finish turning of steel and other high temperature metals such Stellite, Inconel etc. Other PCBN materials may also be used which have been developed for use in high-speed applications where heat is an issue. In one exemplary embodiment, such materials include in the range of 45% to 80% CBN by volume. Further exemplary embodiment PCBN materials that may be used are described in U.S. Pat. No. 6,331,497, the contents of which are fully incorporated herein by reference. Other exemplary PCBN materials may include CBN having a crystal size in the range of from about 10 to 17 microns and including in the range of from 2 to 15% by weight of a material selected from the group of refractory compounds consisting of titanium diboride, aluminum diboride, titanium carbide, titanium nitride, titanium carbonitride, and titanium aluminum carbonitride. The carbonitride system encompasses a range of compositions from titanium nitride to titanium carbide. Preferably, the carbonitride has a carbon to nitrogen proportion in the range of from 20 atomic percent carbon and 70 atomic percent nitrogen to 70 atomic percent carbon and 30 atomic percent nitrogen. The mixture of CBN and refractory compound is infiltrated with aluminum and/or silicon, preferably a eutectic composition of silicon and aluminum.
- In one exemplary embodiment, a
PCBN layer 10 is bonded to asubstrate 12 forming a cuttingelement 14, as for example shown inFIG. 3 . In this exemplary embodiment, thePCBN layer 10 makes up the entire cutting layer. - In another exemplary embodiment, the PCBN cutting layer is engineered to have a thermal gradient in the range of 2000 to 2000° C./mm. In other words, the cutting layer is designed such that the temperature drops from about 200° C. to 2000° C. per millimeter away from the working
surface 24 as for example shown inFIG. 4 . Exemplary cutting layers may contain greater than 90% by weight PCBN or may be formed from mixtures of PCBN and other ceramic materials. In alternate exemplary embodiments, any of the aforementioned PCBN cutting layers may be formed from two or more PCBN layers 26 each having the same or different thermal gradients, and/or the same or different thicknesses as for example, shown inFIG. 5 . - In another exemplary embodiment, the cutting layer may be a composite of PCD and PCBN. In this regard, the cutting layer may be engineered to have better strength and toughness when compared to a PCBN material by itself. For example a
PCBN layer 16 may be bonded to a PCD 18 layer as for example shown inFIG. 6 . In an alternate exemplary embodiment, aPCBN layer 20 may cover theentire PCD layer 22, as for example shown inFIG. 7 where the PCBN layer encapsulates the PCD layer. The composite cutting layer incorporating a PCD material as well as a PCBN material may be formed in accordance with the principles described in U.S. Pat. Nos. 4,403,015; 5,510,193; and 5,603,070, the contents of which are fully incorporated herein by reference. - With these exemplary embodiment cutting elements, the PCBN outer layer serves to protect the PCD material from the operating temperatures in excess of 1000° C. In an exemplary embodiment, by using a PCBN material over the PCD material which has a thermal gradient in the range of about 2000 to about 2000° C., the temperature to which the PCD material is exposed to can be controlled by controlling the thickness and/or the thermal gradient of the PCBN layer. In an exemplary embodiment, the PCBN layer serves to keep the temperature of the PCD material below 650° C., or below 1000° C. if the PCD material is leached. In this regard, the PCD material is not subject to graphitization due to high temperature exposure.
- In another embodiment, any of the aforementioned PCBN materials may be used to form a cutting layer having a
layer 28 surrounding another ultrahard material layer 30, such as a PCD ultrahard material layer 30, as for example shown inFIG. 8 . In this regard thecutting edge 32 that will be exposed to the highest temperatures during drilling is made of PCBN. The PCBN material may extend around the entire periphery of the cutting element, as for example shown inFIG. 8 . In other exemplary embodiments, the PCBN material may form only the portion of the cutting layer defining anedge 34 that will make contact with the earth formation during drilling, as for example shown inFIG. 9 . The remainingportion 36 of the cutting layer may be made from another material such as another PCBN material or another PCD material, as for example shown inFIG. 9 . The PCBN portion to make contact with the earth formations may extend along the entire thickness of thecutting layer 38 as shown inFIG. 8 or may extend along a portion of the thickness of thecutting layer 38 as shown inFIG. 9 . Again, the PCBN material serves to protect the other ultra hard material in the cutting layer from the high operational temperatures. - Thus, as can be seen, with the present invention, the cutting elements may be engineered for the task at hand by providing the appropriate PCBN materials proximate the cutting edge of the cutting element which is subjected to high temperatures, as for example, temperatures in excess of 1000° C. during drilling. For example by using a combination of PCBN with PCD to form the cutting layer of the exemplary cutting elements an engineered cutting layer material is formed that is capable of withstanding the high operating temperatures and have sufficient strength and toughness for the drilling at task.
- Applicant believes that the exemplary embodiment cutting elements mounted on turbine-driven bits would be able to operate in cutting environments where the weight on the bit will be at least 10,000 lbs. and in one exemplary embodiment, will be in the range of 10,000 lbs. to 45,000 lbs. In another exemplary embodiment, the weight on the bit will be in the range of 10,000 lbs. to 15,000 lbs. In a further exemplary embodiment, the weight on the bit will be in the range of 15,000 lbs. to 45,000 lbs.
- It should be noted that the term “substrate” as used herein means any body onto which an exemplary cutting layer is bonded to. For example a substrate may be the body of a cutting element or a transition layer bonded to the body of a cutting element.
- Although the present invention has been described and illustrated to respect to exemplary embodiments, it is to be understood that it is not to be so limited, since changes and modifications may be made therein which are within the full intended scope of this invention as hereinafter claimed.
Claims (21)
1. A shear cutting element comprising:
a substrate;
a cutting layer over the substrate comprising at least a portion comprising PCBN for contacting a formation during drilling, wherein said at least a portion comprising PCBN has a thermal gradient in the range from about 200 to 2000° C./mm.
2. The cutting element as recited in claim 1 wherein said entire cutting layer is a PCBN cutting layer.
3. The cutting element as recited in claim 2 wherein the cutting element further comprises a PCD layer interposed between the PCBN layer and the substrate.
4. The cutting element as recited in claim 3 wherein the PCD layer is completely encapsulated by the PCBN layer and the substrate.
5. The cutting element as recited in claim 1 wherein the cutting layer further comprises another portion comprising an ultra hard material adjacent to the at least a portion comprising PCBN.
6. The cutting element as recited in claim 5 wherein the ultra hard material is PCD.
7. The cutting element as recited in claim 1 wherein said cutting layer comprises a plurality of portions comprising PCBN.
8. The cutting element as recited in claim 1 wherein said cutting layer is formed from a plurality of PCBN layers bonded together.
9. A bit as recited in claim 8 wherein said at least a portion comprising PCBN is part of one of said plurality of layers.
10. The cutting element as recited in claim 1 wherein said at least a portion comprising PCBN has a strength of at least 100 ksi.
11. The cutting element as recited in claim 1 wherein said at least a portion comprising PCBN has a strength in the range of 100 ksi to 200 ksi.
12. The cutting element as recited in claim 1 wherein the cutting layer comprises an ultra hard material portion, wherein said at least a portion comprising PCBN forms a cutting edge of the cutting layer.
13. The cutting element as recited in claim 12 wherein the cutting layer comprises a periphery, wherein said at least a portion comprising PCBN extends only along a portion of said periphery.
14. The cutting element as recited in claim 12 wherein said at least a portion comprising PCBN forms a peripheral portion of the cutting layer surrounding said ultra hard material portion.
15. The cutting element as recited in claim 14 wherein said at least a portion comprising PCBN extends to the substrate.
16. The cutting element as recited in claim 12 wherein said at least a portion comprising PCBN is spaced apart from the substrate.
17. The cutting element as recited in claim 16 wherein said ultra hard material portion is sandwiched between the substrate and said at least a portion comprising PCBN.
18. The cutting element as recited in claim 12 wherein said at least a portion comprising PCBN extends to the substrate.
19. The cutting element as recited in claim 1 wherein said at least a portion comprising PCBN comprises greater than 90% by PCBN.
20. A shear cutting element comprising:
a substrate;
a cutting layer over the substrate comprising at least a portion comprising a thermally stable ultra hard material for contacting a formation during drilling, wherein said at least a portion has a thermal gradient in the range from about 200 to 2000° C./mm.
21. The cutting element as recited in claim 20 wherein said thermally stable ultra hard material comprises PCBN.
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US20120037430A1 (en) * | 2009-02-27 | 2012-02-16 | Clint Guy Smallman | Polycrystalline diamond |
US20120037429A1 (en) * | 2009-02-11 | 2012-02-16 | Geoffrey John Davies | Polycrystalline diamond |
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US7451838B2 (en) * | 2005-08-03 | 2008-11-18 | Smith International, Inc. | High energy cutting elements and bits incorporating the same |
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Also Published As
Publication number | Publication date |
---|---|
GB2428712B (en) | 2011-02-16 |
GB0612464D0 (en) | 2006-08-02 |
CA2551939A1 (en) | 2007-02-03 |
US7451838B2 (en) | 2008-11-18 |
US20070029116A1 (en) | 2007-02-08 |
CA2551939C (en) | 2013-02-19 |
GB2428712A (en) | 2007-02-07 |
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