WO2012089566A1 - A superhard structure and method of making same - Google Patents

A superhard structure and method of making same Download PDF

Info

Publication number
WO2012089566A1
WO2012089566A1 PCT/EP2011/073473 EP2011073473W WO2012089566A1 WO 2012089566 A1 WO2012089566 A1 WO 2012089566A1 EP 2011073473 W EP2011073473 W EP 2011073473W WO 2012089566 A1 WO2012089566 A1 WO 2012089566A1
Authority
WO
WIPO (PCT)
Prior art keywords
region
regions
thermal expansion
polycrystalline
superhard structure
Prior art date
Application number
PCT/EP2011/073473
Other languages
English (en)
French (fr)
Inventor
Moosa Mahomed Adia
Geoffrey John Davies
David Christian BOWES
Original Assignee
Element Six Abrasives S.A.
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Element Six Abrasives S.A. filed Critical Element Six Abrasives S.A.
Priority to US13/997,785 priority Critical patent/US20130344309A1/en
Priority to CA2822828A priority patent/CA2822828A1/en
Priority to CN2011800674776A priority patent/CN103370154A/zh
Priority to EP11808197.5A priority patent/EP2658667A1/en
Priority to JP2013546664A priority patent/JP2014506297A/ja
Publication of WO2012089566A1 publication Critical patent/WO2012089566A1/en
Priority to US15/455,653 priority patent/US20170183761A1/en

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C26/00Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B29/00Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
    • C30B29/02Elements
    • C30B29/04Diamond
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01JCHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J3/00Processes of utilising sub-atmospheric or super-atmospheric pressure to effect chemical or physical change of matter; Apparatus therefor
    • B01J3/06Processes using ultra-high pressure, e.g. for the formation of diamonds; Apparatus therefor, e.g. moulds or dies
    • B01J3/062Processes using ultra-high pressure, e.g. for the formation of diamonds; Apparatus therefor, e.g. moulds or dies characterised by the composition of the materials to be processed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24DTOOLS FOR GRINDING, BUFFING OR SHARPENING
    • B24D18/00Manufacture of grinding tools or other grinding devices, e.g. wheels, not otherwise provided for
    • B24D18/0009Manufacture of grinding tools or other grinding devices, e.g. wheels, not otherwise provided for using moulds or presses
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01BNON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B32/00Carbon; Compounds thereof
    • C01B32/25Diamond
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01BNON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B32/00Carbon; Compounds thereof
    • C01B32/25Diamond
    • C01B32/28After-treatment, e.g. purification, irradiation, separation or recovery
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped 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
    • C04B35/52Shaped 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 carbon, e.g. graphite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped 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
    • C04B35/58Shaped 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
    • C04B35/583Shaped 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
    • C04B35/5831Shaped 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
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B29/00Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
    • C30B29/10Inorganic compounds or compositions
    • C30B29/38Nitrides
    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B10/00Drill bits
    • E21B10/46Drill bits characterised by wear resisting parts, e.g. diamond inserts
    • E21B10/56Button-type inserts
    • E21B10/567Button-type inserts with preformed cutting elements mounted on a distinct support, e.g. polycrystalline inserts
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C26/00Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes
    • C22C2026/007Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes with additional metal compounds being nitrides
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree

Definitions

  • This disclosure relates to a superhard structure comprising a body of polycrystalline material, a method of making a superhard structure, and to a wear element comprising a polycrystalline superhard structure.
  • Polycrystalline diamond (PCD) materials may be made by subjecting a mass of diamond particles of chosen average grain size and size distribution to high pressures and high temperatures while in contact with a pre-existing hard metal substrate. Typical pressures used in this process are in the range of around 4 to 7 GPa but higher pressures up to 10 GPa are also practically accessible. Temperatures employed are above the melting point at such pressures of the transition metal binder of the hard metal substrate. For the common situation where tungsten carbide/cobalt substrates are used, temperatures above 1395°C suffice to melt the metal in the binder, for example cobalt, which infiltrates the mass of diamond particles enabling sintering of the diamond particles to take place.
  • the resultant PCD material may be considered as a continuous network of bonded grains of diamond with an interpenetrating network of binder, for example a cobalt based metal alloy.
  • the so-formed PCD material which forms a PCD table bonded to the substrate is then quenched by dropping the pressure and temperature to room conditions. During the temperature quench, the metal in the binder solidifies and bonds the PCD table to the substrate. At these conditions, the PCD table and substrate may be considered as being in thermoelastic equilibrium with one another.
  • cutting elements or cutters for boring, drilling or mining applications consist of a layer of polycrystalline diamond material (PCD) in the form of a diamond table bonded to a larger substrate or body often made from tungsten carbide/cobalt cemented hard metal.
  • PCD polycrystalline diamond material
  • Such cutters with their attendant carbide substrates are traditionally and commonly made as right cylinders with the polycrystalline diamond layer or table typically ranging in thickness from about 0.5mm to 5.0mm but more often in the range 1 .5mm to 2.5mm.
  • the hard metal substrates are typically from 8mm to 16mm long.
  • the commonly used diameters of the right cylindrical cutters are in the range 8mm to 20mm.
  • PCD constructions such as general domed and pick shaped elements are also used in various applications, for example drilling, mining and road surfacing applications.
  • the PCD material forms an outer layer on such elements with a metal carbide being used as a substrate bonded thereto. Again, the substrate is usually the largest part of such structures.
  • the types of drill bit where such cutters are employed are termed drag bits.
  • this type of drill bit several PCD cutters are arranged in the drill bit body so that a portion of the top peripheral edge of each PCD table bears on the rock formations. Due to the rotation of the bit, the top peripheral edge of each PCD table of each cutter experiences loading and subsequent abrasive wear processes resulting in a progressive removal of a limited amount of the PCD material. The worn area on the PCD table is referred to as the wear scar.
  • the performance of PCD cutters during drilling operations is determined, to a large extent, by the initiation and propagation of cracks in the PCD table. Cracks which propagate towards and intersect the free surface of a cutter may result in spalling of the cutter where a large volume of PCD breaks off from the PCD table. The result of this phenomenon may reduce the useful life of the drill bit and may lead to catastrophic failure of the cutter.
  • a superhard structure comprising:
  • a body of polycrystalline superhard material comprising:
  • the second region being adjacent an exposed surface of the superhard structure, the second region comprising a diamond material or cubic boron nitride, the density of the second region being greater than 3.4x10 3 kilograms per cubic meter when the second region comprises diamond material;
  • the material or materials forming the first and second regions have a difference in coefficient of thermal expansion, the first and second regions being arranged such that the difference between the coefficients of thermal expansion induces compression in the second region adjacent the exposed surface; and wherein the first region or a further region has the highest coefficient of thermal expansion of the polycrystalline body and is separated from a peripheral free surface of the body of polycrystalline superhard material by the second region or one or more further regions formed of a material or materials of a lower coefficient of thermal expansion, wherein the regions comprise a plurality of grains of polycrystalline superhard material.
  • first region or a further region has the highest coefficient of thermal expansion of the polycrystalline body and is separated from a peripheral free surface of the body of polycrystalline superhard material by the second region or one or more further regions formed of a material or materials of a lower coefficient of thermal expansion, wherein the regions comprise a plurality of grains of polycrystalline superhard material.
  • a drill bit or a cutter or a component therefor comprising the superhard structure(s) described herein.
  • Figure 1 is a schematic cross sectional drawing of a planar interface PCD cutter in which the shaded areas depict regions in which cracks preferentially propagate;
  • Figure 2a is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a first embodiment;
  • Figure 2b is a partially sectioned three dimensional representation of the embodiment of Figure 2a with a cutaway section to expose the internal arrangement of various regions;
  • Figure 3 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a second embodiment
  • Figure 4 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a third embodiment
  • Figure 5 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a fourth embodiment
  • Figure 6 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a fifth embodiment
  • Figure 7 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a sixth embodiment
  • Figure 8 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a seventh embodiment
  • Figure 9 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to an eighth embodiment
  • Figure 10 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a ninth embodiment
  • Figure 1 1 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a tenth embodiment
  • Figure 12 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to an eleventh embodiment
  • Figure 13 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to a twelfth embodiment
  • Figures 14 a, b, c are schematic representations of the stress distribution in a conventional planar cutter made from one PCD material only, showing the axial, radial and hoop tensile and compressive stress fields, respectively, together with the position of the tensile and compressive maxima;
  • Figure 15 is a schematic diagram of a half cross-section of a PCD body attached to a substrate, according to an embodiment derived from Figure 7;
  • Figures 16a, b and c are schematic representations showing the stress distribution in a cutter according to an embodiment where the axial, radial and hoop tensile and compressive stress fields, respectively, are shown together with the position of the tensile and compressive maxima;
  • Figure 17 is a three dimensional schematic diagram having a cutaway section of material at the top peripheral edge of a cutter, and adjoined and abutted by the embodiment of Figure 16a.
  • Figure 18 is an optical micrograph, pertaining to example 5, of a half cross- section of a worn cutter corresponding to the schematic diagram of Figure 15 which in turn is according to an embodiment derived from Figure 7.
  • the geometric arrangement of the two types of PCD material can be clearly seen labelled as volumes 1 and 12.
  • the wear scar after laboratory simulated rock drilling is labelled as 17 and the major crack is labelled 18.
  • Figure 19 pertains to Example 6 and shows the arrangement of the different materials for the embodiment of Example 6.
  • Figure 20 is an optical micrograph pertaining to Example 6 of a half cross- section of a warn cutter corresponding to the diagram of Figure 19. The wear scar and the major cracks are indicated.
  • Figure 21 shows the arrangement of the three dissimilar PCD materials of the embodiment of Example 7.
  • Figure 22 is an optical micrograph pertaining to Example 7 of a half cross- section of a warn cutter corresponding to the diagram of Figure 21 . The wear scar and the major cracks are indicated.
  • a "superhard material” is a material having a Vickers hardness of at least about 25GPa.
  • Diamond and cubic boron nitride (cBN) material are examples of superhard materials.”
  • Diamond is the hardest known material with cubic boron nitride (cBN) considered to be second in this regard. Both materials are termed to be superhard materials. Their measured hardnesses are significantly greater than nearly all other materials. Hardness numbers are figures of merit, in that they are highly dependent upon the method employed to measure them. Using Knoop indenter hardness measurement techniques at 298°K, diamond has been measured to have a hardness of 9000 kg/mm 2 and cBN 4500 kg/mm 2 both with 500g loading.
  • PCD materials typically have a hardness falling in the range 4000 to 5000 kg/mm 2 when measured using similar techniques with either Vickers or Knoop indenters.
  • Other hard materials such as boron carbide, silicon carbide, tungsten carbide and titanium carbide have been similarly measured to have hardnesses of 2250, 3980, 2190 and 2190 kg/mm 2 respectively.
  • materials with measured hardnesses greater than around 4000 kg/mm 2 are considered to be superhard materials. Residual stresses locked into a cutter comprising the superhard material after the fabrication process thereof at HPHT conditions are considered to be particularly pertinent to crack initiation and propagation during application of the cutter.
  • polycrystalline material such as a PCD material having increased compression or lowered tension in the path of the cracks may have the effect of channelling or deflecting cracks into the regions of higher tension.
  • Such channelling or deflection preferably directs the cracks away from the free surfaces of the superhard material, for example the PCD material.
  • Another way of inducing compression in a material is by adjoining materials of differing elastic modulus during a high pressure fabrication process. On release of pressure, the material with the higher modulus of elasticity will induce a compression on the material with the lower modulus of elasticity and itself will undergo an increased tension.
  • Cutters containing, for example, a body of PCD material may be fabricated using high temperature combined with high pressure, in which these approaches for inducing compression are utilised. It has been observed that some PCD material types differ significantly in both coefficient of thermal expansion and modulus of elasticity. In these materials, when the coefficient of thermal expansion is low, the elastic modulus is high. Thus when different materials from this group are exploited, the quench from high temperature and high pressure during formation of the material causes opposing stress induction effects. However, the stress change effects brought about by the coefficient of thermal expansion differences dominate.
  • critical regions within which cracks have a preference to initiate and/or propagate are indicated schematically in Figure 1 . These critical regions may differ in position, magnitude and direction of the tensile stress, and may be defined as follows:
  • Region A1 indicates the region of crack initiation during the early stages of cutter wear, whereas region A2 refers to the later stages of wear.
  • Region A1 is associated with a tensile hoop stress and A2 with a tensile axial stress.
  • region B1 and B2 The region towards the top surface of the PCD material into which cracks propagate and cause premature spalling of the cutter, shown as region B1 and B2 in Figure 1 .
  • regions B1 and B2 are associated with the early and later stages of wear, respectively.
  • Regions B1 and B2 are associated with tensile radial and axial stresses.
  • region C The region towards the centre of the PCD material immediately above the carbide substrate into which some of the cracks propagate after the cutter has been worn substantially, shown as region C in Figure 1. Cracks propagating into this region are less likely to be harmful as they do not break out to a free surface of the PCD material. Region C is associated with a small tensile axial stress.
  • Region D in Figure 1 represents the bulk volume of the PCD material outside of these critical regions but wherein there is a significantly lower tendency for cracks to propagate.
  • hoop and radial stresses are generally compressive and axial stresses move from mildly tensile to compressive in a radial direction.
  • the critical regions described above identify the positions in the PCD table where volumes of different PCD materials may be placed in order to alter the residual stress distribution which arises from the general cutter structure and manufacturing process thereof.
  • the desired alteration in the residual stress distribution involves the induction of compression or reduced tension in the critical regions.
  • the critical regions with their attendant tensile stress maxima may be displaced from the free surface of the PCD table to the inside volume of the PCD table where they are less harmful.
  • These alterations to the stress distribution serve to arrest or deflect or direct cracks to less critical regions away from free surfaces and towards the bulk volume of the PCD table and the carbide interface. In turn, the occurrence of cracks propagating to the free surfaces which would previously cause spalling of the PCD table is diminished and this may lead to a desirable increase in cutter life.
  • Figure 2a shows a schematic partial view of the cross section of half of a body of superhard material such as a PCD material attached to a substrate, which indicates adjacent volumes associated with the regions of Figure 1 .
  • These volumes may be made of materials differing in structure and composition and associated properties in order that stress distributions may be modified.
  • Figure 2b is three dimensional representation of the embodiment of Figure 2a with a 60° cutaway section to expose the internal arrangement of the various regions.
  • the first region 1 in these figures comprises mainly region D of Figure 1 and occupies the general centre of the PCD table. It is surrounded by five adjacent and bonded regions 2, 3, 4, 5 and 6.
  • the first volume 1 is separated from the circumferential free surface of the PCD table by the third 3, fourth 4, and fifth 5, regions.
  • the substrate is labelled as 7.
  • the sixth region 6 is positioned between the first central region 1 and the substrate 7, which may be for example a carbide substrate, and is associated or corresponds to region C in Figure 1 .
  • the third region 3, is adjacent to the sixth region 2 and is situated adjacent the substrate 7 and the circumferential free surface of the PCD table. This region is associated with region A2 of Figure 1 .
  • the fourth region 4 is adjacent to the third region 3, and is situated at the circumferential free surface of the PCD table. This region 4 is associated with region A1 of Figure 1 .
  • the fifth region 5, is adjacent to the fourth region 4 and separates the first region 1 , from the top free surface of the PCD table.
  • the fifth region 5, is associated with region B1 of Figure 1 .
  • the second region 2, is adjacent to the fifth region 5, and separates the first region 1 from the remainder of the top free surface of the PCD table.
  • the second region 2 extends across the middle of the top free surface of the PCD table and is associated with region B2 of Figure 1 .
  • Material of the highest coefficient of thermal expansion may be chosen to occupy the first or the sixth regions 1 and 6.
  • the first region 1 may contain the material of highest coefficient of thermal expansion, and the materials chosen for the second to the sixth regions 2 to 6, may all differ from one another in regard to the coefficient of thermal expansion and all be lower in this property than the first region 1 .
  • the material of the fifth region 5, may be lower in coefficient of thermal expansion than those of both fourth and second regions, 4 and 2.
  • the material of the sixth region 6 may be lower in coefficient of thermal expansion than that of the third region 3, and the material of the fourth region 4, may have a coefficient of thermal expansion lower than that of the third region 3.
  • Materials that may be used for forming the various regions include, for example, diamond containing materials such as PCD, and composites with other metals such as copper, tungsten and the like, and composites with ceramics such as silicon carbide, titanium carbide and nitride and the like.
  • non diamond containing materials compatible with cutter structures and fabrication procedures may also be used and may include hard metals such as tungsten carbide/cobalt, titanium carbide/nickel and the like, cermets such as aluminium oxide, nickel combinations and the like, general ceramics and refractory metals.
  • the modulus of elasticity may be used to appropriately alter the stress field in the PCD cutter.
  • the material of the first region 1 may be chosen to have the lowest modulus of elasticity as compared to the materials of the second to sixth regions, 2 to 6.
  • Typical PCD materials often differ in both coefficient of expansion and modulus of elasticity. In the case of PCD material produced under high pressure high temperature conditions for diamond sintering, the stresses induced due to thermal expansion mismatch typically dominate.
  • the first region 1 is of a sufficient proportion of the overall PCD table volume to have a significant influence on the stresses in the surrounding regions.
  • the first region 1 may occupy between around 30 and 95% of the overall PCD table volume.
  • the adjacent boundaries between each of the second, third, fourth, fifth and sixth regions, 3, 4, 5 and 6, may be positioned in order to optimize the desired changes of stress distribution.
  • PCD materials have linear thermal expansion coefficients within the range of 3x10 "6 to 5x10 "6 per degree Centigrade.
  • region 4 is made from a sufficiently wear resistant material for adequate cutting performance such as PCD materials and the like, other hard materials fulfilling the thermal expansion criteria and preferences outlined above may be used in the other regions.
  • PCD materials may be considered as a combination of diamond and transition metals such as cobalt, nickel and the like.
  • the linear thermal expansion coefficient of diamond is very low with a literature value of 0.8+/-0.1x10 "6 per degree Centigrade.
  • Metals such as cobalt have high thermal expansion coefficients, typical of transition metals such as 13x10 "6 per degree Centigrade.
  • the thermal expansion coefficients of typical PCD materials have a strong dependence upon the diamond to metal compositional ratio.
  • a very convenient way of practically producing PCD material variants with differing thermal expansion coefficients is to manufacture PCD materials with significantly different metal contents.
  • the metal content of PCD materials may typically, but not exclusively, fall in the range from 1 to 15 volume percent and materials with possibly as high as 25 volume percent metal may be produced.
  • the PCD material in the first region 1 has a metal content greater than the PCD material in the remaining regions 2 to 6, in order to alter the stress distribution in the PCD layer in the desired manner.
  • the metal content of the fifth region 5 may be less than the fourth and second regions 4 and 2.
  • the metal content of the material of the second region 2 may be less than that of the third region 3, and the metal content of the material of the fourth region 4, may be less than or equal to that of the third region 3.
  • the difference in metal content between the PCD materials of the first region 1 , and the second to sixth regions, 2 to 6, may be at least around 1.5 volume percent. Additionally, the difference in metal content between any of the adjacent materials of the second to the sixth regions 2 to 6, may be, for example, at least around 0.5 volume percent.
  • PCD materials made with large average grain sizes of diamond particles tend to have lower metal contents than those made with smaller average grain sizes. It is therefore practically possible to create PCD materials with differing metal contents with the attendant differing thermal expansion coefficient by means of choice of average grain size of the diamond particles.
  • the average grain size of the material in the first region 1 may, for example, be smaller than the materials of the second to sixth regions 2 to 6.
  • the average grain size of the material in the sixth region 6 may be smaller than that of the materials of all the other regions namely, regions 1 to 5.
  • the average grain size of the material of the first region 1 falls in the range of around 1 to 10 microns and the average grain size of the material of the other regions 2 to 6 is greater than around 10 microns.
  • the differing moduli of elasticity may be used to induce relative stresses.
  • the modulus of elasticity in the material of the first region 1 , or in the material of the sixth region 6, of Figure 2a is greater than that of the materials in each of the other regions.
  • PCD materials typically have modulus of elasticity within the range of around 750 to 1050 GPa.
  • a difference in modulus of elasticity between materials in the first region 1 , or that of the sixth region 6, and the materials of each of the remaining regions may be, for example, at least around 20 GPa.
  • the material of the fourth region 4 is made from a sufficiently wear resistant material for adequate cutting performance, such as PCD materials and the like, other hard materials fulfilling the modulus of elasticity criteria and preferences outlined above may be used.
  • PCD materials may be considered to comprise a combination of diamond and transition metals such as cobalt, nickel and the like.
  • Single crystal diamond is one of the stiffest materials known to man with an extremely high modulus of elasticity.
  • PCD materials contain, as their greatest component, diamond grains which may be synthetic or natural, and which are intergrown together with the interstices filled with the transition metal.
  • a way of modifying the elastic modulus is to change the overall diamond content. The higher the diamond content, the higher the value of the modulus of elasticity.
  • the diamond content of PCD materials may typically but not exclusively fall in the range from 75 to 99 volume percent.
  • the PCD material of the first region 1 may have diamond content more than the PCD materials in the remaining regions.
  • the difference in diamond content between the PCD materials of the first region 1 or the sixth region 6 and that of the remaining regions may, for example, be at least around 0.2 volume percent.
  • the stress at the interface between the chosen different materials in adjacent regions is very high, resulting in a steep and undesirable stress gradient at these interfaces which may, by itself, be sites of localised crack initiation.
  • the diamond content, grain size and metal content may be selected to change gradually from one region to an adjacent region, over a distance of, for example, at least 3 times the largest average grain size of the materials.
  • Figure 3 is a schematic diagram of a PCD cutter where the first and sixth regions 1 and 6, have the same and the highest coefficient of thermal expansion and the second, third, fourth, and fifth regions 2, 3, 4, and 5, have materials with lower and different coefficients of thermal expansion.
  • the material having the highest coefficient of thermal expansion extends to the PCD table-carbide substrate interface but is still separated from the circumferential free surface of the PCD table by material of lower coefficient of thermal expansion.
  • Figure 4 is a schematic diagram of a PCD cutter which also has the first and sixth regions 1 and 6, with the same highest coefficient of thermal expansion but the materials of the second, third, fourth, and fifth regions 2, 3, 4, and 5, have equal lower coefficients of thermal expansion to one another.
  • the PCD table of the cutter may now be considered as being made up of two regions differing in coefficient of thermal expansion, the region of highest coefficient of thermal expansion is situated symmetrically around the central axis at the interface of the PCD table and the substrate and is separated from the free surfaces of the PCD table by a region of lowest coefficient of thermal expansion.
  • Cutters made according to Figures 2, 3 and 4 may result in a significant reduction of axial tensile stress in region A2 of Figure 1 and the movement of both the tensile hoop stress of region A1 and the radial tensile stress of region B1 away from the free surface of the PCD.
  • Embodiments of this nature as shown in Figures 3 and 4 may thus address the crack behaviour during the early and latter stages of wear of a cutter, respectively.
  • FIG. 5 is a schematic diagram showing a cutter where the boundaries between the combined first and sixth regions 1 and 6 and the combined second, third, fourth, and fifth regions 2, 3, 4, and 5, of Figure 4 are expanded to make a new separating volume labelled as the eighth region 8.
  • the combined first and sixth region is now labelled as the ninth region 9, and the combined second, third, fourth, and fifth regions are shown as the tenth region 10.
  • the eighth, ninth and tenth regions 8, 9, 10 may be made from materials with differing coefficients of thermal expansion.
  • the eighth or the ninth region 8, 9 may be made of the material with the highest coefficient of thermal expansion.
  • the material of the ninth region 9 has the highest coefficient of thermal expansion and the eighth and ninth regions 8, 9 differ in this property.
  • the material of the eighth region 8 may have an intermediate coefficient of thermal expansion between that of the ninth and tenth regions 9, 10.
  • Cutters made according to the latter example may have a significant reduction of axial tensile stress in region A2 of Figure 1 and due to this and the movement of the radial tensile stress of region B1 , the hoop stresses in all the regions may be rendered compressive. The elimination of tensile hoop stresses would be a highly favourable outcome.
  • cutter designs may be arrived at with four or five regions whilst still retaining the geometric form of the original interfacial boundaries.
  • cutter designs with multiple volumes still retaining the original interfacial boundary geometric form may be arrived at, as shown in Figure 6.
  • the region containing the material of highest coefficient of thermal expansion having the largest relative volume occupies the centre region of the carbide-PCD interface and there is a progressive reduction in coefficient of thermal expansion in each subsequent adjacent volume extending from the central region of the PCD table to the circumferential edge.
  • the thickness of these regions approaches the dimensional scale of the microstructure of the material and thus a continuous graduation of the structure, composition and properties may result.
  • the PCD table may be largely or completely graduated in this manner, with the central region of the PCD table being located away from the circumferential free surface and occupied by material of the highest coefficient of thermal expansion.
  • the material of the eighth region 8 may, on average, be intermediate in coefficient of thermal expansion between the ninth and tenth regions 9, 10, but arranged to be continuously graduated in structure composition and properties from the material of the ninth region 9 to that of the tenth region 10. This may be advantageous as it may enable any undesirable sharp change in stress from one region to the other to be mitigated.
  • FIG. 1 A block diagram illustrating an exemplary computing environment in accordance with the present disclosure.
  • FIG. 1 A block diagram illustrating an exemplary computing environment in accordance with the present disclosure.
  • FIG. 1 A block diagram illustrating an exemplary computing environment in accordance with the present disclosure.
  • FIG. 1 A block diagram illustrating an exemplary computing environment in accordance with the present disclosure.
  • FIG. 1 A block diagram illustrating an exemplary computing environment in accordance with the present disclosure.
  • Cutters made according to the latter example may however reduce both the radial tensile stress of B1 and the hoop stress of A1 along with importantly moving these two latter critical regions away from the free surface and into the body of the PCD table.
  • Other embodiments may be arrived at from considering Figure 2, for example with the first region 1 comprising the material of highest coefficient of thermal expansion occupying a generally toroidal volume remote from the free surfaces of the PCD table and the carbide interface as shown in Figure 8. Variants associated with permutations of the relative coefficients of thermal expansions of the materials in the second to sixth regions 2 to 6, may be applicable.
  • Figure 9 is a schematic diagram where the second, third, fourth, fifth and sixth regions 2 to 6 of Figure 8 are made of materials having the same coefficient of thermal expansion now labelled 1 1 which surrounds the toroidal first region 1 , made of the material of the highest coefficient of thermal expansion.
  • the region having the material of the highest coefficient of thermal expansion may be sub divided into more than one separate region, all of which may be separated from the circumferential free surface of the PCD table by at least one material of lower coefficient of thermal expansion.
  • These multiple volumes of the same, highest coefficient of thermal expansion may be, for example any three dimensional geometric shape such as toroids, ellipsoids, cylinders, spheres and the like.
  • the total volume of the material of the highest coefficient of thermal expansion may, for example, occupy 30 to 95% of the overall volume of the PCD table.
  • Figure 1 1 is an example with four toroidal volumes distributed in the PCD table. All of the embodiments so far described are axially symmetrical with regard to the common prior art cylindrical geometry cutter and are relatable to the critical regions of crack initiation and propagation as shown in Figure 1 . Generally, circumferential sub division of the volumes containing chosen dissimilar materials with their attendant dissimilar chosen properties, both axially symmetrical and asymmetrical, may be exploited to alter the residual stress distributions and may advantageously affect crack initiation and propagation. By using this approach the residual stress distribution may be altered from being axially symmetrical to axially asymmetrical so that undesired tensile stresses in the general location of the wear scar may be reduced or eliminated.
  • a particular PCD material may, although being particularly good in terms of its wear properties and behaviour in rock cutting, not be an ideal material to have at the periphery of a cutter due to a less than ideal thermal coefficient of expansion and/or elastic modulus in regard to surrounding volumes and so have less than ideal residual stress in its volume.
  • any of the axisymmetric embodiments described and schematically represented by Figures 2 to 12 or any other such variants may be exploited to adjoin and abut a volume of such material such that the residual stress field within that volume's boundaries is favourably altered.
  • "Abut” in this context means a supporting volume of material adjacent to a chosen sector which imposes favourable stress alterations on the said sector.
  • Favourable alterations include reduction of tension, increases of compression and the displacement and movement of tensile stress maxima away from the free surface of the PCD table, particularly where these maxima are then separated from the free surface by compressive stress fields.
  • a segment or sector of such a material with good wear behaviour may be inserted into a peripheral discontinuity created in any of the embodiments described and represented by Figures 2 to 12. This segment or sector will then be used as the site for the rock cutting and the subsequent formation of a wear scar. More than one such segments or sectors may be disposed at the periphery of the PCD table, either symmetrically or asymmetrically arranged, and facilitate multiple re-use of such cutters.
  • PCD cutters based upon the embodiment of Figures 2a, 2b were manufactured.
  • Figure 13 is a diagram of the particular design employed for these cutters.
  • the final PCD table thickness was 2.2 mm, bonded to a tungsten carbide, 13 weight percent cobalt hard metal substrate of 13.8 mm in length.
  • the right cylinder cutters were 16 mm in diameter, 16 mm in overall length and had a planar interface between the PCD table and the carbide substrate.
  • the volumes of differing PCD materials, 1 to 6 were made by using tape casting fabrication techniques known in the art. Green state discs or washers of six different diamond powders were made using a water soluble binder. In each case, the assembly of discs and washers to form the geometry of Figure 13 was contained in a refractory metal cup, which, in turn, was fitted over a cylinder of pre-sintered tungsten carbide/ cobalt hard metal. These assemblies were then vacuum degassed in a furnace at a temperature and time sufficient to remove the binder materials. The assemblies were then subjected to a temperature of about 1450°C at a pressure of about 5.5 GPa in a high pressure apparatus. At these conditions, the cobalt binder of the tungsten carbide hard metal melted and infiltrated the porosity of the diamond power assembly and diamond sintering took place.
  • the material of the first region 1 was made from diamond powder of average particle size of about 6 microns with a multimodal size distribution extending from 2 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 12 volume percent, with a linear coefficient of thermal expansion of 4.5 X 10 "6 /°C and an elastic modulus of 860 GPa. This is the material of highest coefficient of thermal expansion.
  • the material of the second region 2 was made from a diamond powder of average particle size of about 12.5 micron with a multimodal size distribution, extending from 2 microns to 30 micron.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of 10.2 volume percent, with a linear coefficient of thermal expansion of 4.15 x 10 "6 /°C and an elastic modulus of 980 GPa.
  • the material of the third region 3 was made from a diamond powder of average particle size of about 5.7 micron with a multimodal size distribution, extending from 1 micron to 12 micron. This diamond powder is known to form
  • PCD material at the high pressure and temperature conditions used, with a cobalt content of 10 volume percent, with a linear coefficient of thermal expansion of 4.0 x 10 "6 /°C and an elastic modulus of 1005 GPa.
  • the material of the fourth region 4 was made from a diamond powder of average particle size of about 25 microns with a multimodal size distribution, extending from 4 microns to 45 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of 7.7 volume percent, with a linear coefficient of thermal expansion of 3.7 x 10 "6 /°C and an elastic modulus of 1030 GPa.
  • the material of the fifth region 5 was made from a diamond powder of average particle size of about 33.5 microns with a multimodal size distribution, extending from 4 microns to 75 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of 7.0 volume percent, with a linear coefficient of thermal expansion of 3.4 x 10 "6 /°C and an elastic modulus of 1040 GPa. This is the material of lowest coefficient of thermal expansion with the highest diamond content of 93 volume percent.
  • the material of the sixth region 6, was made from a diamond powder of average particle size of about 6.4 microns with a trimodal size distribution, extending from 3 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of 1 1.5 volume percent, with a linear coefficient of thermal expansion of 4.25 x10 "6 /°C and an elastic modulus of 925 GPa.
  • each cutter was brought to final size by grinding and polishing procedures known in the art. A sample of the cutters was cut and cross-sectioned and the dimensions of the volumes of different PCD materials measured and their volumes relative to the overall volume of the PCD table estimated.
  • the material of the first region 1 made up of the material of highest coefficient of thermal expansion, occupied approximately 75% of the overall volume of the PCD table.
  • the material of the sixth region 6, occupied approximately 3 % of the overall PCD table volume, extended radially approximately 4 mm from the central axis and was about 0.25 mm in thickness and separated the material of the first region 1 , from the tungsten carbide, hard metal substrate.
  • the material of the fourth region 4 occupied approximately 5 % of the overall PCD table volume, was adjacent to the material of the third region 3, was situated at the circumferential free surface of the PCD table and separated the material of the first region 1 , from the circumferential free surface of the PCD table.
  • the cutters as manufactured with the resultant measured volume dimensions and expected PCD material properties were modelled using Finite Element Analysis (FEA). This is a numerical stress analysis technique which allows the calculation of the stress distribution over the dimensions of the cutter. For comparative purposes, the stress distribution of a planar cutter with the table made solely of one material corresponding to the material of the fourth region 4, was calculated and used as reference.
  • FEA Finite Element Analysis
  • Figures 14a, b, c are a schematic representation of the stress distribution in such a planar cutter made from one PCD material only.
  • Figure 14a shows the axial tensile and compressive fields together with the position of the tensile and compressive maxima.
  • the dotted lines indicate the boundary between the tensile and compressive fields, the tensile field being hatched.
  • the axial tensile maximum is situated at the circumferential free surface of the PCD table immediately above the interface with the substrate. This axial tensile maximum is associated with the A2 critical region of Figure 1 .
  • Most of the PCD table is in axial tension except for an axial compressive stress field which extends from the substrate interface to the top free surface of the PCD and is separated from the circumferential free surface by an axial tensile field.
  • the compressive maximum is positioned inside the compressive field immediately above the substrate interface.
  • Figure 14b shows the radial tensile and compressive fields together with the position of the tensile and compressive maxima.
  • the single radial tensile field is hatched as shown in the Figure 14b, the radial tensile maximum being situated at the top free surface of the PCD table. This radial maximum is associated with the B1 critical region of Figure 1 .
  • the compressive maximum is situated at the substrate interface as shown.
  • Figure 14c shows the hoop tensile and compressive fields together with the position of the tensile and compressive maxima.
  • Most of the PCD table is in hoop compression apart from a limited volume at the circumferential top corner which is in tension as shown by the hatched area.
  • the hoop tensile maximum is situated at the free surface and is associated with the A1 critical region of Figure 1 .
  • Table 1 gives the comparative FEA results expressed as the magnitude of the components of stress for this example compared the reference planar cutter.
  • the hoop tensile maximum associated with critical region A1 of Figure 1 is reduced by 126% and so now has become a position of lowest compression and has been displaced and moved away from the free surface of the PCD table. It now occupies a position inside the material of region 1 as indicated by H in Figure 13. Moreover, the whole of the volume of the PCD table is now under hoop compression and there is hence an absence of any hoop tensile stress. It is thus seen that the critical regions A2, B1 and A1 have been significantly reduced in tension as compared to the reference planar one material cutter. In the case of critical regions B1 and A1 , they have been moved away from the free surface of the PCD table and are separated from the top free surface by material which is in radial and hoop compression.
  • Example 2 PCD cutters based upon the embodiment of Figure 7 were manufactured.
  • Figure 15 is a diagram of the particular design employed for these cutters.
  • the final PCD table thickness was 2.2 mm, bonded to a tungsten carbide, 13 weight percent cobalt hard metal substrate of 13.8 mm in length.
  • the right cylinder cutters were 16 mm in diameter, 16 mm in overall length and had a planar interface between the PCD table and the carbide substrate.
  • the PCD table is made from only two volumes of different PCD material.
  • the PCD material of highest coefficient of thermal expansion formed a disc, labelled as 1 in Figure 15, which is separated from the substrate interface, the top surface and the circumferential free surface of the PCD table by a surrounding volume of PCD material of lower coefficient of thermal expansion, labelled as 12 in Figure 15.
  • the temperature and pressure conditions employed were about 1470°C and 5.7 GPa, respectively.
  • the first region 1 was made from diamond powder of average particle size of about 12.6 microns with a multimodal size distribution extending from 2 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 9 volume percent, with a linear coefficient of thermal expansion of 4.0x10 "6 /°C and an elastic modulus of 1020 GPa. This is the material of highest coefficient of thermal expansion.
  • the second region 12 which surrounds the first region 1 in Figure 15 was made from diamond powder of average particle size of about 33 microns with a multimodal size distribution extending from 6 microns to 75 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 6.5 volume percent, with a linear coefficient of thermal expansion of 3.4 x 10 "6 /°C and an elastic modulus of 1040 GPa.
  • each cutter was brought to final size by grinding and polishing procedures known in the art. A sample of the cutters was cut and cross-sectioned and the dimensions of the volumes of different PCD materials measured and their volumes relative to the overall volume of the PCD table estimated.
  • the first region 1 made up of the material of highest coefficient of thermal expansion, occupied approximately 67% of the overall volume of the PCD table and that of the surrounding volume about 33%.
  • the first region 1 was separated from the substrate by about 0.25 mm, from the top surface of the table by about 0.4 mm and from the circumferential free surface of the table by about 0.4 mm.
  • the cutters as manufactured with the resultant measured volume dimensions and expected PCD material properties were modelled using Finite Element Analysis (FEA). This technique allows the calculation of the stress distribution over the dimensions of the cutter.
  • FEA Finite Element Analysis
  • Table 2 gives the FEA results expressed as the principle stress maxima and also as the components of the principle stress in the convenient cylindrical coordinates, axial, radial and hoop. Table 2.
  • cutters made according to the embodiment of Figure 7 are likely to have a reduction of axial tensile stress of region A2 in Figure 1 , together with an intensified adjacent axial compression.
  • the tensile radial stress of region B1 was reduced and moved so that it was no longer bounded by the top free surface of the PCD table, and was separated from the top free surface by a zone of radial compression.
  • the tensile hoop stress maximum associated with critical region A1 was not reduced but, in fact increased; it too was moved away from the free surface of the PCD table.
  • This tensile hoop maximum now occupied an immediately adjacent position inside the first region 1 , and was completely surrounded by hoop compression separating it from all the free surfaces of the PCD table and the substrate interface.
  • PCD cutters were made as per Figure 16a which is a specific design based upon the embodiment of Figure 5, where the PCD table is made from three volumes of different PCD material.
  • the PCD material of highest coefficient of thermal expansion, and highest metal content formed a disc, labelled as 13 in Figure 16a, which was situated at the substrate interface centrally and symmetrically arranged around the central axis of the cutter.
  • the volume of material, made from a PCD material of lowest coefficient of thermal expansion and metal content labelled 15 in Figure 16a extended across all the free surface both circumferential and top surface, of the PCD table.
  • the final PCD table thickness was 2.2 mm, bonded to a tungsten carbide, 13% weight cobalt hard metal substrate of 13.8 mm length.
  • the right cylinder cutters were 16 mm in diameter and had a planar interface between the PCD table and the carbide substrate.
  • the PCD material of region 13 of Figure 16a was made from diamond powder of average particle size of about 5.7 microns with a multimodal size distribution extending from 1 micron to 12 micron.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 10 volume percent, with a linear coefficient of thermal expansion of 4.1x10 "6 /°C and an elastic modulus of 1006 GPa. This is the material of highest coefficient of thermal expansion and highest metal content.
  • the outer region 15, in Figure 16a was made from diamond powder of average particle size of about 25 microns with a multimodal size distribution extending from 4 microns to 45 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 7.4 volume percent, with a linear coefficient of thermal expansion of 3.6x10 "6 /°C and an elastic modulus of 1030 GPa.
  • the intermediate region 14, in Figure 16a was made from diamond powder of average particle size of about 12.6 microns with a multimodal size distribution extending from 2 microns to 30 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 8.9 volume percent, with a linear coefficient of thermal expansion of 3.9x10 "6 /°C and an elastic modulus of 1020 GPa
  • each cutter was brought to final size by grinding and polishing procedures known in the art.
  • a sample of the cutters was cut and cross-sectioned and the dimensions of the volumes of different PCD materials measured and their volumes relative to the overall volume of the PCD table estimated.
  • the boundary between the regions 13 and 14 was situated about 1 .0 mm axially away from the substrate interface and about 0.5 mm from the circumferential free surface.
  • the boundary between the regions 15 and 14 is situated about 0.6mm away from the top free surface of the PCD table and about 0.25mm from the circumferential free surface.
  • Region 13 was estimated to be approximately 38% of the overall volume of the PCD table.
  • Regions 14 and 15 were estimated to be approximately 23% and 47% of the overall volume of the PCD table, respectively.
  • the tensile stress is indicated by hatches and the boundaries between tension and compression by dotted lines.
  • the positions of the tensile and compressive maxima are also indicated on the diagrams.
  • the axial tensile maximum for the reference cutter in Figure 14a is associated with the critical region A2 of Figure 1
  • the radial tensile maximum in Figure 14b is associated with the critical region B1 of Figure 1
  • the hoop tensile maximum in Figure 14c is associated with the critical region A1 of Figure 1 .
  • Table 3 gives the comparative FEA results expressed as the stress maxima of the components of the convenient cylindrical coordinates, axial, radial and hoop of the cutter of Example 3 of Figures 16a, b and c relative to the reference planar cutter ( Figures 14 a, b and c).
  • Table 3 clearly shows that the stress in the critical regions A2, B1 and A1 of the cutter of Example 3 has been significantly reduced in tension. Moreover the hoop stress associated with critical region A1 has been rendered significantly compressive, resulting in the whole PCD table being in hoop compression.
  • PCD cutters were made according to Figure 17 whereby a single 60° segment of PCD material was formed at the top peripheral edge of the cutter and was adjoined and abutted by the design of example 3, in the remaining 300° part of the cutter.
  • Figure 17 is a three dimensional schematic representation of this new design, with a cut away section, where a 60° peripheral segment of the outer volume of Figures 16 a,b,c, labelled 15 was replaced by a material labelled as 16 in Figure 17.
  • This PCD material was known to have very good wear behaviour as determined from rock cutting tests. In the 300° remainder of the cutter, abutting the 60° segment, the design of Figure 16 was used. '
  • the final PCD table thickness was 2.2 mm, bonded to a tungsten carbide, 13% weight cobalt hard metal substrate of 13.8 mm length.
  • the right cylinder cutters were 16 mm in diameter and had a planar interface between the PCD table and the carbide substrate.
  • tape casting techniques known in the art were used to form so called green state discs, washers, and sectors of four appropriately chosen diamond powders bonded with water soluble organic binders. By assembling these discs, washers and sectors in a refractory metal container, the geometry of Figure 17 was produced. A cylinder of tungsten carbide, 13% cobalt hard metal cylinder was then inserted into the refractory metal container to form and provide the substrate.
  • the 60° segment material labelled 16 in Figure 17 was made from diamond powder of average particle size of about 13.0 microns with a multimodal size distribution extending from 2 microns to 30 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 8.8 volume percent, with a linear coefficient of thermal expansion of 3.95 x 10 "6 /°C and an elastic modulus of 1025 GPa. This particular material had been demonstrated to have very good low wear characteristics in rock cutting tests.
  • each cutter was brought to final size by grinding and polishing procedures known in the art.
  • a sample of the cutters was cut and cross-sectioned and the dimensions of the volumes of different PCD materials measured and their volumes relative to the overall volume of the PCD table estimated.
  • the boundary between the regions 13 and 14 was situated about 1 .0 mm axially away from the substrate interface and about 0.5 mm from the circumferential free surface.
  • the boundary between the regions 15 and 14 is situated about 0.6mm away from the top free surface of the PCD table and about 0.25mm from the circumferential free surface.
  • the 60° segment extended about 2mm in a radial direction from the circumferential free surface, was of thickness approximately 0.6 mm at the top free surface and approximately 0.25 at the circumferential free surface of the PCD table.
  • Regions 13, 14 and 15 were estimated to be approximately 38%, 23% and 44% of the overall volume of the PCD table respectively.
  • the 60° segment, region 16 was estimated to occupy approximately 3% of the overall volume of the PCD table.
  • the cutters as manufactured with the resultant estimated volumes and dimensions and expected PCD material properties were modelled using Finite Element Analysis (FEA).
  • FEA Finite Element Analysis
  • a planar cutter as in Figures 14a, b, c was considered, with material of the same properties as expected for the 60° segment, 16 in Figure 17.
  • the boundary conditions and type of mesh chosen for the calculation were constant for the reference and the design for the example so that the magnitudes of the stress maxima could be compared.
  • Table 4 gives the comparative FEA results where the stress maxima calculated in the 60° segment were compared to the corresponding stress maxima of the planar reference cutter where the PCD material is the same as material 16 of Figure 17.
  • the axial tensile stress maximum was situated at the circumferential PCD table free surface just above the substrate interface, as in the planar reference cutter and associated with the critical region A2 of Figure 1 , but at the 30° position in regard to the segment circumferential boundary, indicated by A in Figure 17. This axial tensile maximum had been reduced by about 47% as compared to the planar reference cutter.
  • the radial tensile stress maximum in the segment was situated at the top free surface of the PCD table, as in the planar cutter reference and associated with the critical region B1 of Figure 1 , indicated by R in Figure 17. This radial tensile maximum had been reduced by about 66% as compared to the planar reference cutter.
  • the hoop tensile stress maximum in the segment was situated at the top free surface of the PCD table, as in the planar cutter reference and associated with the critical region A1 of Figure 1 , indicated by H in Figure 17. This hoop tensile maximum had been reduced by about 52% as compared to the planar reference cutter.
  • the cutter design of Example 3 used to adjoin and abut a segment of PCD material may induce significant reduction in the tensile stresses in the material of that segment. It was also found that the favourable stress distribution of Example 3 was largely also found in the abutting material of Example 4, with however some increase in tensile stress immediately adjacent to the 60° segment boundary.
  • Example 3 It is expected that the tendency for crack propagation in the material of the segment will thus be reduced as compared to a planar cutter made from the same material, reducing in turn the spalling tendency, so that the good wear properties of the segment material may be exploited in rock cutting applications. Moreover the highly favourable stress distribution in the adjoining and abutting material with the design of Example 3 may also inhibit crack propagation, to inhibit cracks from reaching the PCD table free surfaces as in Example 3. This may also contribute to a reduction in spall occurrence.
  • cutter designs based upon some embodiments with favourable residual stress distributions may be used to adjoin and abut segments of PCD materials and may favourably reduce the tensile stresses in these segments as compared to situations where the segment material is used alone.
  • the interfacial boundary between a PCD table and a carbide substrate attached thereto may be geometrically modified in order to alter the residual stress field in the PCD table.
  • These modified interfaces are termed non planar interfaces and may have an influence on the general stress distributions in locations immediate to the interface.
  • the general character of the critical regions described and indicated in Figure 1 is not materially altered by adopting a non planar interface design but may be used in conjunction with some embodiments.
  • An example is given in Figure 12 which has the first to sixth regions 1 to 6 as shown in Figure 2a and 2b, but with a non-planar interface where the carbide substrate interface is generally convex with respect to the top surface of the PCD table.
  • modification of the geometry of the starting edge may be carried out by including, for example, a chamfer or the like, in order to reduce early chipping events. This practice may be used in conjunction with any or all of the embodiments.
  • treatments which remove in total or in part the metal component of PCD materials to a chosen depth from the free surface may be used to benefit the performance of PCD cutters. Typical depths exploited fall between 50 and 500 microns. The benefit is believed to reside primarily in improvements of thermal stability of the materials in the treated depth.
  • an associated disadvantage of this treatment process is the occurrence of increased tensile stresses in the PCD materials adjacent to the treated layer or layers which may result in undesirable crack propagation.
  • Embodiments may provide a means of mitigating this disadvantage by offsetting the tensile stresses by an already present induced compression brought about by placement of chosen materials. It is therefore possible to use such treatments in conjunction with one or more embodiments.
  • certain heat treatments are able to partially anneal residual stresses and thereby reduce their magnitude.
  • Typical of such treatments is to heat PCD cutters after removal from the high pressure apparatus under a vacuum at temperatures between 550°C and 750°C for time durations of a few hours.
  • Such treatments are able to favourably alter the residual stress distributions but only to a limited degree. Heat treatments of this nature may be applied to the embodiments.
  • Figure 15 is a diagram of the specific design employed for this cutter variant.
  • the PCD material with the highest coefficient of thermal expansion occupied the volume labelled 1 in Figure 15 and the material of relative lower coefficient of thermal expansion occupied the volume labelled 12 in Figure 15.
  • the PCD material occupying volume 1 in Figure 15 was made from diamond powder of average particle size of about 6.4 microns with a multimodal size distribution extending from 2 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 1 1 .5 volume percent, with a linear coefficient of thermal expansion of 4.4x10 "6 /°C and an elastic modulus of 930 GPa.
  • the material in volume 12 of Figure 15 was made from diamond powder of average particle size of about 12.6 microns with a multimodal size distribution extending from 1 .5 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 8.9 volume percent, with a linear coefficient of thermal expansion of 4.0x10 "6 /°C and an elastic modulus of 1020 GPa.
  • the final PCD table thickness was 2.2 mm, bonded to a tungsten carbide, 13 weight percent cobalt hard metal substrate of 13.8 mm in length.
  • the right cylinder cutters were 16 mm in diameter, 16 mm in overall length and had a planar interface between the PCD table and the carbide substrate.
  • the high pressure high temperature sintering conditions of 6.8 GPa and 1450 °C were maintained for 10 minutes.
  • An exemplary cutter was then tested using a laboratory rock drill simulating apparatus. A portion of the top peripheral edge of the cutter made to bear on a rotating granite rock sample such that a continuous groove was made in the rock sample with the dominant rock fracture being brought about by shearing action. The test was continued until the developing wear scar on the cutter just reached the region of the tungsten carbide, PCD table interface. No obvious chipping or spalling had occurred. The worn sample was sectioned radially to intersect the wear scar, the cross section being polished and prepared for microscopic examination.
  • Figure 18 is an optical micrograph at about 20x magnification where it may be clearly seen that the PCD material in the central region as per volume 1 of Figure 15 is approximately 1 .5mm in thickness. This material is separated from the substrate interface by a thickness of about 0.3mm of the lower coefficient of thermal expansion PCD material, as per volume 12 of Figure 15.
  • the PCD material in the central region is separated from the top free surface of the PCD table by a 0.4mm thickness of the lower coefficient of thermal expansion material as per volume 12 of Figure 15.
  • the wear scar, 17, extends as far as the PCD, tungsten carbide substrate interface and the material of volume 1 is just being exposed. It may be seen that the dominant cracks extending from the wear scar are propagating mainly in volume 1 , the central PCD volume of the cutter and are angled sharply away from the direction of the top free surface of the PCD layer and are directed towards the PCD, tungsten carbide substrate interface. Such cracks thus cannot cause spalling whereby large volumes of PCD material are detached from the top free surface of the PCD table. This exhibited guiding of cracks away from the free surface of the PCD table is consistent with the residual stress distribution given in Example 1 for this general embodiment and is a feature of some embodiments.
  • PCD cutters were made to an embodiment derived from Figure 2a whereby the volumes labelled 2, 4 and 5 were made of the same PCD material.
  • Figure 19 shows this consolidated volume labelled 19.
  • the volumes 1 , 3 and 6 of Figure 2a were made of a different PCD material, Figure 19 labelled as 20, with a linear coefficient of thermal expansion and metal content greater than that of the material of volume 19.
  • Volume 20 of Figure 19 was substantially thicker than volume 19 separates volume 19 from the tungsten carbide substrate and extends to the circumferential free surface of the PCD table only at a local position immediately above the PCD table, substrate interface. Volume 19 extends across the top free surface of the PCD table and most of the circumferential free surface of the PCD.
  • the material in volume 19 of Figure 19 was made from diamond powder of average particle size of about 12.6 microns with a multimodal size distribution extending from 1 .5 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 8.9 volume percent, with a linear coefficient of thermal expansion of 4.0x10 "6 /°C and an elastic modulus of 1020 GPa.
  • the PCD material occupying volume 20 in Figure 19 was made from diamond powder of average particle size of about 6.4 microns with a multimodal size distribution extending from 2 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 1 1 .5 volume percent, with a linear coefficient of thermal expansion of 4.4x10 "6 /°C and an elastic modulus of 930 GPa.
  • the dimensions of the PCD table, tungsten carbide substrate and the overall size and shape of the cutters together with the conditions under which the PCD materials were sintered were as per Example 5.
  • Figure 20 is an optical micrograph of a half cross-section of a tested and partially worn cutter, showing the two PCD materials labelled 19 and 20 and the wear scar surface, 21 .
  • the ultimate position of the wear scar is also indicated in Figure 19 labelled 21 .
  • the dominant cracks labelled 22 extend from the wear scar and are guided towards the PCD table, substrate interface, and have thus been deflected away from the free surface of the PCD table, and these cracks cannot therefore lead to spalling behaviour.
  • Cracks labelled 23 tended initially to propagate into the position just inside the boundary of material 20, occupied by both the hoop and radial maximum tensile stresses as indicated by the Finite Element analysis of this embodiment. These cracks initially were being guided in the desired manner away from the top free surface of the PCD table but seem to abruptly change direction when the wear scar extended beyond the boundary between the materials 19 and 20.
  • PCD cutters were made to a design derived from the embodiment of Example 6, whereby a material of intermediate linear coefficient of thermal expansion and metal content occupied a volume shown labelled as 19 in Figure 21 and 22.
  • This volume separates the material of lowest linear coefficient of thermal expansion and metal content extending to the PCD table top free surface, labelled 24 in Figures 21 and 22, and the PCD material of highest linear coefficient of thermal expansion and metal content extending to the PCD table and tungsten carbide, substrate interface, labelled as 20 in Figures 21 and 22.
  • the material in volume 24 of Figure 21 was made from diamond powder of average particle size of about 20 microns with a multimodal size distribution extending from about 4 microns to about 45 microns. This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 7 volume percent, with a linear coefficient of thermal expansion of 3.5x10 "6 /°C and an elastic modulus of 1040 GPa.
  • the material in volume 19 of Figure 21 was made from diamond powder of average particle size of about 12.6 microns with a multimodal size distribution extending from 1 .5 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 8.9 volume percent, with a linear coefficient of thermal expansion of 4.0x10 "6 /°C and an elastic modulus of 1020 GPa.
  • the PCD material occupying volume 20 in Figure 21 was made from diamond powder of average particle size of about 6.4 microns with a multimodal size distribution extending from 2 microns to 16 microns.
  • This diamond powder is known to form PCD material at the high pressure and temperature conditions used, with a cobalt content of about 1 1 .5 volume percent, with a linear coefficient of thermal expansion of 4.4x10 "6 /°C and an elastic modulus of 930 GPa.
  • Figure 22 is an optical micrograph of a part cross-section of a partially worn after laboratory simulated rock drilling test.
  • the wear scar labelled 25 extends from the top free surface of the PCD table to a position on the circumferential free surface close to the PCD table, tungsten carbide substrate interface and has worn through the top layer, material 24, and has partially worn into the material 19.
  • the dominant cracks labelled 26 extend from the lower portion of the wear scar and are directed downwards towards the interface between the PCD table and tungsten carbide substrate. These cracks are unlikely to intersect the top free surface of the PCD table and thus will not contribute to spalling behaviour.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Manufacturing & Machinery (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Mining & Mineral Resources (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Metallurgy (AREA)
  • Inorganic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Fluid Mechanics (AREA)
  • Composite Materials (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Structural Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Earth Drilling (AREA)
  • Cutting Tools, Boring Holders, And Turrets (AREA)
  • Powder Metallurgy (AREA)
  • Drilling Tools (AREA)
PCT/EP2011/073473 2010-12-31 2011-12-20 A superhard structure and method of making same WO2012089566A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US13/997,785 US20130344309A1 (en) 2010-12-31 2011-12-20 Superhard structure and method of making same
CA2822828A CA2822828A1 (en) 2010-12-31 2011-12-20 A superhard structure and method of making same
CN2011800674776A CN103370154A (zh) 2010-12-31 2011-12-20 超硬结构及其制造方法
EP11808197.5A EP2658667A1 (en) 2010-12-31 2011-12-20 A superhard structure and method of making same
JP2013546664A JP2014506297A (ja) 2010-12-31 2011-12-20 超硬質構造体及びその製造方法
US15/455,653 US20170183761A1 (en) 2010-12-31 2017-03-10 Superhard structure and method of making same

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US201061428932P 2010-12-31 2010-12-31
US61/428,932 2010-12-31
GB1022127.3 2010-12-31
GBGB1022127.3A GB201022127D0 (en) 2010-12-31 2010-12-31 A superhard structure and method of making same

Related Child Applications (2)

Application Number Title Priority Date Filing Date
US13/997,785 A-371-Of-International US20130344309A1 (en) 2010-12-31 2011-12-20 Superhard structure and method of making same
US15/455,653 Continuation US20170183761A1 (en) 2010-12-31 2017-03-10 Superhard structure and method of making same

Publications (1)

Publication Number Publication Date
WO2012089566A1 true WO2012089566A1 (en) 2012-07-05

Family

ID=43599131

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2011/073473 WO2012089566A1 (en) 2010-12-31 2011-12-20 A superhard structure and method of making same

Country Status (7)

Country Link
US (2) US20130344309A1 (ja)
EP (1) EP2658667A1 (ja)
JP (1) JP2014506297A (ja)
CN (1) CN103370154A (ja)
CA (1) CA2822828A1 (ja)
GB (2) GB201022127D0 (ja)
WO (1) WO2012089566A1 (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10036208B2 (en) 2012-12-31 2018-07-31 Element Six Abrasives S.A. Cutter element for rock removal applications
US10180034B2 (en) 2012-12-31 2019-01-15 Element Six Abrasives S.A. Cutter element for rock removal applications

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130167979A1 (en) * 2011-12-29 2013-07-04 General Electric Company Method of predicting quench cracking in components formed by high deformation processes
MX2016014105A (es) * 2014-04-28 2017-02-09 Owen Oil Tools Lp Dispositivos y metodos relacionados para activar herramientas de sondeo con un gas presurizado.
CA2975261C (en) * 2015-03-10 2019-07-30 Halliburton Energy Services, Inc. Polycrystalline diamond compacts and methods of manufacture
WO2017105804A1 (en) * 2015-12-14 2017-06-22 Smith International, Inc. Cutting elements formed from combinations of materials and bits incorporating the same
CN106869805B (zh) * 2017-02-24 2018-10-19 深圳先进技术研究院 一种聚晶金刚石复合片及其制备方法
GB2575711B (en) * 2018-05-18 2020-11-25 Element Six Uk Ltd Polycrystalline diamond cutter element and earth boring tool

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4729440A (en) * 1984-04-16 1988-03-08 Smith International, Inc. Transistion layer polycrystalline diamond bearing
WO2004111284A2 (en) 2003-06-12 2004-12-23 Element Six (Pty) Ltd Composite material for drilling applications
US20070187155A1 (en) * 2006-02-09 2007-08-16 Smith International, Inc. Thermally stable ultra-hard polycrystalline materials and compacts
EP2108630A1 (en) * 2007-02-02 2009-10-14 Sumitomo Electric Hardmetal Corp. Diamond sinter

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ZA862903B (en) * 1985-04-29 1987-11-25 Smith International Composite polycrystalline diamond compact
US5011514A (en) * 1988-07-29 1991-04-30 Norton Company Cemented and cemented/sintered superabrasive polycrystalline bodies and methods of manufacture thereof
JP2000054007A (ja) * 1998-07-31 2000-02-22 Sumitomo Electric Ind Ltd ダイヤモンド焼結体及びその製造方法
JP2001187431A (ja) * 1999-12-28 2001-07-10 Sumitomo Electric Ind Ltd 積層構造材料
US6610095B1 (en) * 2000-01-30 2003-08-26 Diamicron, Inc. Prosthetic joint having substrate surface topographical featurers and at least one diamond articulation surface
US20050133277A1 (en) * 2003-08-28 2005-06-23 Diamicron, Inc. Superhard mill cutters and related methods
JP4230492B2 (ja) * 2006-04-11 2009-02-25 Towa株式会社 低密着性材料、樹脂成形型及び防汚性材料
CN104031632A (zh) * 2007-03-12 2014-09-10 圣戈本陶瓷及塑料股份有限公司 高强度陶瓷元件及其制造方法和使用方法

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4729440A (en) * 1984-04-16 1988-03-08 Smith International, Inc. Transistion layer polycrystalline diamond bearing
WO2004111284A2 (en) 2003-06-12 2004-12-23 Element Six (Pty) Ltd Composite material for drilling applications
US20070187155A1 (en) * 2006-02-09 2007-08-16 Smith International, Inc. Thermally stable ultra-hard polycrystalline materials and compacts
EP2108630A1 (en) * 2007-02-02 2009-10-14 Sumitomo Electric Hardmetal Corp. Diamond sinter

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10036208B2 (en) 2012-12-31 2018-07-31 Element Six Abrasives S.A. Cutter element for rock removal applications
US10180034B2 (en) 2012-12-31 2019-01-15 Element Six Abrasives S.A. Cutter element for rock removal applications

Also Published As

Publication number Publication date
GB201022127D0 (en) 2011-02-02
GB2486974A (en) 2012-07-04
CA2822828A1 (en) 2012-07-05
US20170183761A1 (en) 2017-06-29
GB2486974B (en) 2015-08-19
US20130344309A1 (en) 2013-12-26
GB201121921D0 (en) 2012-02-01
JP2014506297A (ja) 2014-03-13
EP2658667A1 (en) 2013-11-06
CN103370154A (zh) 2013-10-23

Similar Documents

Publication Publication Date Title
US20170183761A1 (en) Superhard structure and method of making same
US9352448B2 (en) Superhard structure and method of making same
US11498873B2 (en) Superhard constructions and methods of making same
RU2303688C2 (ru) Композитный материал с плотным слоем абразивного материала
US9297211B2 (en) Polycrystalline diamond construction with controlled gradient metal content
CA2549061C (en) Polycrystalline diamond abrasive elements
EP1750876B1 (en) Cutting tool insert
US10214967B2 (en) Composite polycrystalline diamond body
ZA201101040B (en) Composite cutter substrate to mitigate residual stress
WO2010075168A2 (en) Earth-boring particle - matrix rotary drill bit and method of making the same
WO2014078620A1 (en) Sintering of thick solid carbonate-based pcd for drilling application
US20160230473A1 (en) A rock removal body
US10233697B2 (en) Methods of reducing stress in cutting elements for earth-boring tools and resulting cutting elements
US20120304547A1 (en) Superhard construction
WO2014186050A1 (en) Metal mesh stabilizer between superabrasive and substrate layers
CN107206498B (zh) 具有加速催化剂的完全浸出的过渡层的固体多晶金刚石
EP2961912B1 (en) Cutting elements leached to different depths located in different regions of an earth-boring tool and related methods
WO2022144167A1 (en) A polycrystalline superhard construction and a method of making same

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 11808197

Country of ref document: EP

Kind code of ref document: A1

ENP Entry into the national phase

Ref document number: 2822828

Country of ref document: CA

ENP Entry into the national phase

Ref document number: 2013546664

Country of ref document: JP

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 2011808197

Country of ref document: EP

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2013135704

Country of ref document: RU

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 13997785

Country of ref document: US