GB2338007A - Preform cutting elements for rotary drill bits - Google Patents

Preform cutting elements for rotary drill bits Download PDF

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Publication number
GB2338007A
GB2338007A GB9911920A GB9911920A GB2338007A GB 2338007 A GB2338007 A GB 2338007A GB 9911920 A GB9911920 A GB 9911920A GB 9911920 A GB9911920 A GB 9911920A GB 2338007 A GB2338007 A GB 2338007A
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United Kingdom
Prior art keywords
substrate
facing table
periphery
preform
element according
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB9911920A
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GB9911920D0 (en
GB2338007B (en
Inventor
Terry Richard Matthias
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ReedHycalog UK Ltd
Original Assignee
Camco International UK Ltd
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Priority claimed from GBGB9811705.4A external-priority patent/GB9811705D0/en
Application filed by Camco International UK Ltd filed Critical Camco International UK Ltd
Priority to GB9911920A priority Critical patent/GB2338007B/en
Publication of GB9911920D0 publication Critical patent/GB9911920D0/en
Publication of GB2338007A publication Critical patent/GB2338007A/en
Application granted granted Critical
Publication of GB2338007B publication Critical patent/GB2338007B/en
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Classifications

    • 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
    • E21B10/54Drill bits characterised by wear resisting parts, e.g. diamond inserts the bit being of the rotary drag type, e.g. fork-type bits
    • E21B10/55Drill bits characterised by wear resisting parts, e.g. diamond inserts the bit being of the rotary drag type, e.g. fork-type bits with preformed cutting elements
    • 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
    • E21B10/5676Button-type inserts with preformed cutting elements mounted on a distinct support, e.g. polycrystalline inserts having a cutting face with different segments, e.g. mosaic-type inserts
    • 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
    • E21B10/573Button-type inserts with preformed cutting elements mounted on a distinct support, e.g. polycrystalline inserts characterised by support details, e.g. the substrate construction or the interface between the substrate and the cutting element
    • 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
    • E21B10/573Button-type inserts with preformed cutting elements mounted on a distinct support, e.g. polycrystalline inserts characterised by support details, e.g. the substrate construction or the interface between the substrate and the cutting element
    • E21B10/5735Interface between the substrate and the cutting element
    • 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
    • E21B10/60Drill bits characterised by conduits or nozzles for drilling fluids
    • E21B10/602Drill bits characterised by conduits or nozzles for drilling fluids the bit being a rotary drag type bit with blades

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Mining & Mineral Resources (AREA)
  • Geology (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Fluid Mechanics (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Chemical & Material Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Drilling Tools (AREA)

Abstract

A preform cutting element, for a rotary drill bit, includes a facing table 120 of super hard material having a front face, a peripheral surface 121, and a rear surface bonded to the front surface of a substrate 119 which is less hard than the super hard material. The peripheral surface of the facing table 121 includes a region where, throughout at least a major part of its thickness it is spaced inwardly from the outer periphery of the substrate. When such a cutting element is mounted on a bit body with the part of the facing table periphery which is engaged by the substrate being located opposite the cutting edge of the element, the part 127 of the substrate which engages the periphery 121 of the facing table acts as a mechanical support to the facing table so as to resist impact and other loads to which the facing table may be subject in use.

Description

2338007 Weform cutting elements for rotary drill bits" The invention
relates to preform cutting elements for rotary drag-type drill bits, of the kind comprising a facing table of superhard material having a front face, a peripheral surface, and a rear surface bonded to the front surface of a substrate which is less hard than the superhard material.
Such preform cutting elements usually have a facing table of polycrystalline diamond, although other superhard materials are available, such as cubic boron nitride. The substrate of less hard material is often formed from cemented tungsten carbide, and the fiLcing table and substrate are bonded together during formation of the element in a high pressure, high tefnpm forming press. This forming process is well known and will not be described in detail.
Each preform cutting element may be mounted on a carrier in the form of a generally cylindrical stud or post received in a pocket in the body of the drill bit. The carrier is often formed from cemented tungsten carbide, the surface of the substrate being brazed to a surface on the carrier, for example by a process known as 'IS bonding". Alternatively, the sj itself may be of sufficient thickness as to provide, in effect, a cylindrical stud which is sufficiently long to be directly received in a pocket in the bit body, without being first brazed to a carrier. The bit body itself may be machined from metal, usually steel, or may be moulded using a powder metallurgy process.
In preform cutting elements of the above type the interface between the superhard table and the substrate may be flat and planar. However, the bond between 2 the superhard facing table and the substrate may be improved by providing a configured non-planar interface between the rear face of the facing table and the front face of the substrate, so as to provide a degree of mechanical interlocking between the facing table and substrate.
In such preform cutting elements it is the usual practice for the facing table to extend over the whole area of the front face of the substrate so that the periphery of the facing table is exposed at the periphery of the preform element.
Such preform cutting elements are subjected to high temperatures and heavy loads when the drill bit on which they are mounted is in use down a borehole. It is found that as a result of such conditions spalling and delamination of the superhard facing table can occur, that is to say the separation and loss of the diamond or other superhard material over part or all of the cutting surface of the table.
It is believed that impact loads on the cutting edge of the facing table can initiate such spalIffig or delamination and such impacts can also cause cracking of the superhard facing table, which tends to be comparatively brittle.
Another disadvantage of existing designs is that when the cutting element is brazed into a pocket in the bit body, the braze alloy cannot wet or bond to the portion of the facing table which is exposed at the periphery of the cutting element. This not only reduces the effective braze area but also means that the bit body provides no effective support for the facing table at its periphery.
The present invention sets out to provide a novel and improved form of cutting element where these disadvantages may be reduced or overcome.
3 According to the invention there is provided a preform cutting element, for a rotary drag-type drill bit, including a facing table of superhard material having a front face, a peripheral surface, and a rear surface bonded to the front face of a substrate which is less hard than the superhard material, the peripheral surface of the facing table including a region where the peripheral surface, throughout at least a major part of its thickness, is spaced inwardly from the outer periphery of the substrate, part of the substrate engaging said inwardly spaced part of the peripheral surface of the facing table.
When such a cutting element is mounted on a bit body with the part of the facing table periphery which is en by the substrate being located opposite the cutting edge of the element, the part of the substrate which engages the periphery of the facing table acts as a mechanical support to the facing table so as to resist impact and other loads to which the facing table may be subject in use, thereby reducing the shear stress which is otherwise whofly borne by the interface between the facing table and substrate.
Furthermore, since the part of the substrate which engages the peripheral surface of the facing table may then he between the facing table and the internal wall of a pocket in which the cutting element is mounted, the braze alloy can be bonded to the substrate material in this region, thereby increasing the area of bond when compared to a conventional cutting element of similar size.
The facing table may across only a part of the front face of the substrate, the whole thickness of said region ofthe peripheral surface of the facing table then being spaced inwardly from the outer periphery of the substrate.
The peripheral surface of the facing table andlor the substrate may be circular, 4 part-circular or of any other suitable shape.
Another region of the peripheral surface of the facing table may be exposed at the periphery of the preform element, so as to define the cutting edge of the element.
Preferably said part of the substrate which engages the peripheral surface of the facing table preferably is exposed, and may have a front surface which is substantially co-planar with the front face of the facing table. The front face of the facing table, and the co-planar front surface of the part of a substrate, may be substantially flat.
The part of the substrate which engages the periphery of the facing table may also overlie part of the front face of the facing table. For example, the front face of the 10 facing table may be formed with a rebate adjacent part of the periphery thereof, said rebate being at least partly filled with material of the substrate. The rebate may have a bottom wall and a side wall, or may comprise a chamfer extending from the periphery of the facing table to a region of the front face thereof inward of the periphery.
In one embodiment of the invention the facing table and substrate may have respective central axes, the axis of the facing table being displaced from the axis of the substrate so that one part of the periphery of the facing table lies at the periphery of the substrate and another part of the periphery of the facing table is spaced inwardly from the periphery of the substrate. The facing table and/or the substrate may be generally circular, although they might also be of any other suitable shapes.
In any of the above arrangements, an exposed part of the front face of the substrate may be formed with a rebate adjacent part of the periphery of the substrate.
The rebate may have a bottom wall and a side wall, or may comprise a chamfer extending from the periphery of the substrate to a region of the substrate inward of the periphery. in the case where the preform element is mounted in a pocket in the bit body, a part of the material of the bit body may engage within said rebate so as to assist in retaining the element in the pocket.
In any of the above arrangements, there may be provided a non-planar interface between at least a part of the rear surface of the facing table and the front surface of the substrate. For example, the ffifing table may be formed with a thickened peripheral wall or rim which projects into a correspondingly shaped groove in the front surface of the substrate. Alternatively or additionally, the rear surface of the facing table and the front surface of the substrate may be formed with any other configuration of inter-engaging projections and recesses.
Also in any of the above arrangements there may be provided a transition layer between the sup material and the less hard material, the transition layer comprising material having one or more properties which is intermediate the corresponding properties of the superhard and less hard materials. In this case the transition layer may be regarded as forming part ofthe affistrate or part of the facing table, depending on the configuration.
The transition layer may extend across the whole of the interface between the superhard material of the facing table and the less hard material of the substrate.
However, in some cases it may be desirable for the transition layer to extend only over one or more specific regions of the interface.
The invention includes within its scope a rotary drag-type drill bit having a bit 6 body formed with at least one pocket in which is received a preform cutting element including a facing table of superhard material having a front face, a peripheral surface, and a rear surface bonded to the front surface of a substrate which is less hard than the superhard material, the peripheral surface of the facing table including a region where 5 the peripheral surface, throughout at least a major part of its thickness, is spaced inwardly from the outer periphery of the substrate, part of the substrate engaging said inwardly spaced part of the peripheral surface of the facing table, the pocket having an inner peripheral surface to which a part of the outer periphery of the preform element is brazed, including the outer periphery of said part of the substrate which engages the peripheral surface of the facing table.
The invention further provides a method of manufacturing a preform cutting element of any of the kinds referred to above, comprising forming an intermediate member having a facing table of superhard material extending across only a part of a substrate of less hard material, and then removing material from the intermediate 15 member to leave a smaller preform element wherein only a part of the periphery of the facing table is exposed at the periphery of the preform element.
For example, the intermediate member may comprising a single facing table spaced inwardly from the periphery of the substrate, at least part of the periphery of the substrate of the intermediate member subsequently being removed, for example by 20 grinding, to expose part of the periphery of the facing table. The facing table may be either concentrically of eccentrically located with respect to the substrate of the intermediate member.
7 Alternatively, the intermediate member may comprise a plurality of facing tables spaced apart on the front surface of the substrate of the intermediate member, each facing table, together with an adjacent larger area of substrate, being subsequently separated from the intermediate member to provide a plurality of preform elements in 5 accordance with the invention. Brief description of the drawings:
Figure 1 is an end view of one form of rotary drill bit according to the invention, Figure 2 is a side elevation of the drill bit of Figure 1, Figure 3 is a diagmmmatic section through a prior art cutting element mounted 10 on a drill bit,
Figure 4 is a similar view of an alternative prior art arrangement,
Figure 5 is a view to Figum 3 of a cutting element in accordance with the present invention, Figure 6 is a front view of the cutting element shown in Figure 5, Figures 7-10 are s views to Figure 5 of alternative embodiments of the invention, Figures 11 - 13 are plan views of intermediate members which may be used to manufacture cutting elements according to the present invention, and Figures 14 and 15 are diagrammatic sections through further types of cutting 20 element in accordance with the invention.
Refendrig to Figures 1 and 2, the drill bit comprises a bit body 10 on which are formed four primary blades 11 and four secondary blades 12. The blades extend 8 generally radially with respect to the bit axis.
The leading edges of the secondary blades are substantially equally spaced with respect to one another, but the leading edge of each secondary blade is closer to its associated preceding primary blade than it is to the following primary blade.
cutters 14 are spaced apart side-by-side along each primary blade 11 and secondary cutters 15 are spaced apart side-by-side along each secondary blade 12. Each secondary cutter 15 is located at the same radial distance from the bit axis as an associated one of the primary cutters on the preceding primary blade.
Each cutter 14, 15 is generally cylindrical and of circular cross-section and comprises a front facing table of polyerystalline diamond bonded to a cylindrical substrate of cemented tungsten carbide. Each cutter is received within a part-cylindrical pocket in its respective blade.
The primary cutters 14 are arranged in a generally spiral configuration over the drill bit so as to form a cutting profile which sweeps across the whole of the bottom of the borehole being drilled.
The three outermost cutters 14 on each primary blade 11 are provided, in known manner, with back-up studs 24 mounted on the same primary blade rearwardly of the primary cutters. The back-up studs may be in the form of cylindrical studs of tungsten carbide embedded with particles of synthetic or natural diamond.
The bit body 10 is formed with a central passage (not shown) which communicates through subsidiary passages with nozzles 18 mounted at the surface of the bit body. In known manner drilling fluid under pressure is delivered to the nozzles 9 18 through the internal passages and flows outwardly through the spaces 19, 20 between adjacent blades for cooling and cleaning the cutters. The spaces 19, 20 lead to junk slots 21 through which the g fluid flows upwardly through the annulus between the drill string and the surrounding fortnation. The junk slots 21 are separated by gauge pads 22 which bear against the side wad of the borehole and are formed with beating or abrasion inserts 23.
The bit body and blades may be machined from metal, usually steel, which may be hardfaced. Alternatively the bit body, or a part thereof, maybe moulded from matrix material using a powder metallurgy process. The methods of manufacturing drill bits of 10 this general type are well known in the art and will not be described in detail.
Figures 3 and 4 are sections through prior art preform cutting elements mounted on a rotary drag-type drill bit.
Referring to Figure 3, the bit body 110 is formed with a part cylindrical pocket 111 in which is brazed a preform cutting element 112, the braze alloy being indicated at 113.
The cutting element co a circular front facing table 114 of polycrystalline diamond bonded to a cylindrical substrate 115 of cemented tungsten carbide. The facing table 114 is co-extensive with the substrate 115 so that the whole of the peripheral edge of the facing table is exposed around the periphery of the cutting element. In this instance the interface 116 between the facing table and substrate is flat.
Since the braze material 113 cannot wet the polyerystalline diamond material of the substrate, as indicated diagrammafically at 117, the whole of the outer surface of the cutting element which engages the inner surface of the pocket 110 is not actually bonded to that inner surface, so that the effective surface area of the bonding is not as great as it could be. Furthermore, the component parallel to the front face of the facing table 114 of any impact load on the cutting edge 118 of the element is borne solely by the shear strength of the bond at the interface 116 between the facing table and the substrate. No effective support to resist this component of the impact load is provided by the comparatively soft braze material 113.
Similar comments apply to the other prior art arrangement shown in Figure 4 where the facing table 114 actually protrudes from the mouth of the pocket 111.
In the arrangement according to the invention shown in Figures 5 and 6 the substrate 119 is again cylindrical but in this case the circular facing table 120 extends across only a part of the front surface of the substrate. At one side of the cutting element the peripheral edge 121 of the facing table is tangential to the outer periphery 122 of the substrate and is therefore partly exposed, as indicated at 123, to form the cutting edge of the element. Around the rest of the facing table 120, however, the peripheral edge 121 of the facing table is engaged by the material of the substrate 119. As may be seen from Figure 5, the front surface 124 of the region of substrate around the facing table is flush and co-planar with the front surface of the facing table 120 itself.
Consequently, most of the outer peripheral surface of the cutting element is provided by the substrate material, and indeed the whole of the outer surface of the element which engages the inner surface of the pocket 125 can be substrate material. Consequently, bonding by the braze alloy 126 occurs over the whole of the internal 11 surface of the pocket.
Furthermore, the body of substrate material 127 which lies between the facing table and the wall of the pocket 125 around most of the periphery of the facing table serves to provide a physical support for the facing table to resist impact loads having a component in a direction parallel to the front surface of the facing table.
In the example of Figures 5 and 6, the rear surface of the facing table is formed with a thickened peripheral rim 128. This not only increases the thickness of the facing table at the cutting edge 123, thus providing greater resistance to wear and impact loads, but the shape of the interface thus provided between the facing table 120 and substrate 10 119 serves to improve the bond between the facing table and substrate.
However, it should be appreciated that the interface between the facing table and substrate shown in Figures 5 and 6 is by way of example only and this interface may be of any desired planar or non-planar configuration.
Another advantage ofthe present invention is that the part of the substrate which is not covered by the diamond facing table can be shaped so as partly to interlock with the material of the bit body to pr some mechanical retention of the cutting element in the socket, in addition to the braze. Two such arrangements are shown in Figures 7 and 8. These are modifications of the ement shown in Figures 5 and 6 and similar parts therefore bear the same reference numerals.
In the arrangement of Figure 7 the portion 127 of the substrate 119 which is bonded to the peripheral edge 121 of the facing table is formed with an angled chamfer 129 which extends from the periphery of the substrate to the front surface and extends 12 around part of the periphery of the substrate. The pocket 125 in the bit body has a corresponding tapered flange 130 which overlies the chamfer 129 and is brazed to it. The flange 130 serves to enhance the retention of the cutting element in the pocket and the arrangement also increases the area of braze between the substrate and the interior wall of the pocket.
In the modified arrangement shown in Figure 8 the rebate around part of the periphery of the substrate 119 has a bottom wall 131 and a side wall 132 so that the rebate is generally rectangular in section. A correspondingly shaped flange 133 formed on the bit body is brazed within the rebate.
In the arrangements of Figures 5-8 the thickened peripheral rim 128 which projects from the rear ffice of the diamond facing table projects rearwardly by a distance which is substantially equal to the thickness of the facing table. However, the rim, or any other form of protuberance on the rear surface of the facing table, may project into the substrate to any lesser or greater extent. For example, the rim or other protuberance may project from the rear face of the facing table by a distance which is up to two or three times the thickness of the facing table, and arrangements are also possible where the protuberance projects rearwardly an even greater distance from this. There is indicated in Figure 5, by way of example, an alternative arrangement (shown in dotted lines at 128A) where the peripheral rim projects rearwardly from the facing table by a distance which is about three times the thickness of the rest of the facing table and where the rim extends through more than half the overall depth of the preform element. It will be appreciated that, as wefl as providing mechanical interlock between the substrate and 13 facing table, the peripheral rim provides an increased thickness of diamond at the cutting edge of the element and thus increases the resistance of the element to wear and impact damage in that region. It may therefore be advantageous to increase the depth of the protuberance in this region, for example as indicated at 128A, to improve the 'wear and impact resistance. lle main part of the facing table 120, from which the peripheral rim 128 projects, may also be of any desired thickness.
Since the facing table does not extend across the whole area of the substrate, it becomes possible to so shape the facing table that a part of the substrate can overlie part of the facing table thereby mechanically assisting the retention of the facing table on the substrate and thereby finther reducing the risk of delamination. Such arrangements are shown in Figures 9 and 10. In the arrangement of Figure 9 the front face of the facing table 134 is chamfered, as indicated at 135, in a region opposite the cutting edge 136 of the facing table. The chwder may be a straight chamfer extending across a chord of the circular facing table, or the chamfer may be curved, extending around part of the periphery of the facing table.
Due to the presence of the chamfer a part 13 7 of the substrate 119 overlies the portion of the facing table 134 where the chamfer is formed, and thus helps retain the facing table on the substrate.
In the alternative arrangement shown in Figure 10, the facing table 138 is formed with a stepped rebate 139 in the region opposite the cutting edge and a portion 140 of the substrate 119 fills the rebate and thus assists in retaining the facing table on the substrate. As before, the rebate 139 may be straight, extending across a chord of the 14 facing table, or may extend around part of the periphery of the facing table.
In all of the arrangements described above and shown in the drawings, any form of protuberance, or number of protuberances, may be integrally formed on the rear face of the facing table and may project from the rear face of the facing table by any desired distance, for example as described above in relation to Figure 5.
Figures 11- 13 illustrate various methods by which preform elements according to the present invention may be manufactured.
Referring to Figure 11, a circular intermediate me 141 is formed comprising a substrate 142 of cemented tungsten carbide in the centre of which is formed a concentric circular facing table 143 of smaller diameter. This intermediate member is manufactured by the normal processes by which preform elements are manufactured.
Thus, the substrate 142 may be preformed with a central circular recess into which particulate diamond material is packed, the assembly then being submitted to extreme temperature and pressure in a press to bond the diamond particles together and to the substrate.
In order to produce from this intermediate member a preform element in accordance with the invention, part of the substrate is removed along the dotted line 144 of Figure 11 so as to expose a part of the periphery of the facing table 143, as indicated at 145, The facing table 143 then extends across only part of the preform element. The region 145 forms the cutting edge of the element and the facing table 143 is supported by the portion of substrate which is opposite the cutting edge portion 145.
In the modified arrangement shown in Figure 12 the circular facing table 146 is eccentric in relation to the substrate 147 and in this case a constant thickness peripheral layer of the substrate is then removed, as indicated by the dotted line 148 so as to expose a portion 149 of the facing table 146 to form the cutting edge of the element.
In either of the arrangements of Figures 11 and 12 the removal of the substrate material to expose part of the periphery of the facing table may be effected by electrical discharge machining (EDA4), by gd by a combination of these methods, or by any other suitable process.
In the arrangement of]Fqpze 13 a large intermediate element 150 is formed with three inlaid circular facing table regions 15 1. Circular elements, each incorporating one of the facing tables 151, are then cut from the intermediate member as indicated by the dotted lines 152. In each case the facing table 151 lies adjacent the periphery of the resulting element.
Instead of methods of the kind shown in Figures 11- 13, utilising an intermediate member, preform elements according to the invention may also simply be made by the normal methods used to manufacture prior art preform elements. That is to say a substrate of the required configuration is preformed with a recess corresponding to the shape of the required facing table. 11e recess is then packed with diamond particles and submitted to the conventional beating and pressing process to produce the element.
Once a preform element has been formed in the press it is nonnally necessary to grind the periphery of the element to provide a smooth surface and eliminate any irregularities which might lead to stress concentrations, with a consequent risk of cracks being initiated. Also, such grinding may be partly eftected to size the element accurately.
16 In prior art elements where the peripheral edge of the facing table is exposed around the whole periphery of the element, such grinding necessitates removal of polycrystalline diamond around the whole periphery of the element, and this may be a costly and time consuming process due to the extreme hardness of the diamond. An additional advantage of preform elements according to the present invention is that diamond may form only a small part of the peripheral surface of the element, thus facilitating the grinding process.
In all of the arrangements according to the invention described with reference to Figures 5-13, the superhard facing table extends across only a part of the front face of the substrate, so that the whole thickness of one region of the peripheral surface of the flicing table is spaced inwardly from the outer periphery of the substrate. However, this is not essential, and the invention also includes arrangements where the peripheral of the superhard facing table is spaced inwardly from the outer periphery of the substrate through only a part of the thickness of the facing table. Arrangements of this kind are shown in Figures 14 and 15.
In the arrangement of Figure 14 one region of the facing table 154 of the cutting element is bevelled, as indicated at 153, so that the front face 155 of the facing table extends across the whole area of the front of the cutting element. Rearwardly of the front surface 155, however, the peripheral surface of the facing table is increasingly spaced from the peripheral surface 15 6 of the substrate 15 7 as a result of the provision of the bevel 153. A ridge 158 of superhard material extends into the gap left by the bevel 153 so as to form the outer periphery of the cutting element outwardly of the 17 bevelled edge of the facing table 154. The ridge 158 of the substrate thus serves, as in the arrangements according to the invention previously described, to provide mechanical support for the facing table 154 against impact on the opposite cutting edge 159 and also provides a region of substrate around part of the periphery of the facing table which can be brazed to the wall of the in which the cutting element is received, as previously described.
Figure 15 shows another form of cutting element which provides a similar efflect.
In this case a part of the peripheral surface of the facing table 160 is stepped or rebated, as indicated at 161, so as to provide a thin portion 162 of the facing table which extends across the whole area of the frontof the cutting element, and a region behind the thin portion 162 where the peripheral of the facing table 160 is spaced inwardly from the outer periphery 163 of the substrate. This arrangement again provides a ridge 164 of the subs Mich engages put of the peripheral surface of the facing table 160 and provides mechanical support for the facing table and a brazing surface at the peripheral surface of the cutting element.
As previously mentiowd, in any of the arrangements according to the invention there may be provide a on layer between the superhard material of the facing table and the less hard material of the substrate, the transition layer comprising material having one or more properties, such as coefficient of thermal expansion, which is intermediate the corresponding properties of the superhard and less hard materials. The transition layer may extend across the whole of the interface between the facing table and substrate or may extend across only one or more regions of the interface. For example, in the 18 arrangements of Figures 5-8 of the drawings, the transition layer may extend only across all or part of the interface between the central region of the facing table and the substrate, inwardly of the thickened peripheral rim on the facing table. Alternatively, the transition layer or layers may be provided only at the interface between the peripheral rim and the substrate.
In the examples of the invention described above, and shown in the drawings, the peripheral surface of each facing table and substrate is referred to as circular, or nearcircular, since this is a common shape for preform cutting elements. However, it must be stressed that the invention is not limited to circular or part-circular arrangements but is applicable to elements having a flicing table andlor substrate of virtually any peripheral shape, including both regular and irregular shapes. Indeed, in some circumstances making the facing table andlor the substrate of non-circular shape may enable better advantage to be taken of the benefits provided by the invention.

Claims (34)

19 CLAIMS
1. A preform cutting element, for a rotary drag-type drill bit, including a facing table of superhard material having a front face, a peripheral surface, and a rear surface bonded to the front face of a substrate which is less hard than the superhard material, the peripheral surface of the facing table including a region where the peripheral surface, throughout at least a major part of its thickness, is spaced inwardly from the outer periphery of the substrate, part of the substrate engaging said inwardly spaced part of the peripheral surface of the facing table.
2. A preform element according to Claim 1, wherein the facing table extends across only a part of the front face of the substrate, and the whole thickness of said region of the peripheral surface of the facing table periphery of the substrate.
is spaced inwardly from the outer
3. A preform element according to Claim 1 or Claim 2, wherein the peripheral surface of the facing table is at least partly circular.
4. A preform element according to any of Claims 1 to 3, wherein the peripheral surface of the substrate is at least partly circular.
5. A preform element according to any of the preceding claims, wherein another region of the peripheral surface of the facing table is exposed at the periphery of the preform element so as to define the cutting edge of the element.
6. A preform element according to any of the preceding claims, wherein said part of the substrate which engages the peripheral surface of the facing table has a front surface which is exposed.
7. A preform element according to any of the preceding claims, wherein said part of the substrate which engages the peripheral surface of the facing table has a front surface which is exposed and is substantially coplanar with the front face of the facing table.
8. A preform element according to Claim 7, wherein the front face of the flicing table, and the co-planar front surface of the part of a substrate, are substantially flat.
9. A preform element according to any of the preceding claims, wherein the part of the substrate which engages the periphery of the facing table also overfies part of the front face of the facing table.
10. A preform element according to Claim 9, wherein the front face of the facing table is formed with a rebate adjacent part of the periphery thereof, said rebate being at least partly filled with material of the substrate.
11. A preform element according to Claim 10, wherein said rebate has a bottom wall and a side wall.
12. A preform element according to Claim 10, wherein said rebate comprises a chamfer extending from the periphery of the facing table to a region of the front face thereof inward of the periphery.
13. A preform element according to any of the preceding claims, wherein the facing table and substrate have respective central axes, the axis of the facing table being displaced from the axis of the substrate so that one part of the periphery of the facing table lies at the periphery of the substrate and another part of the periphery of the facing 21 table is spaced inwardly from the periphery of the substrate.
14. A preform element according to Claim 13, wherein the facing table and the substrate are generally circular.
15. A preform element according to any of the preceding claims, wherein there is provided a non-plan-a interface between at least part of the rear surface of the facing table and the front surface of the substrate.
16. A preform element according to Claim 15, wherein the facing table is formed with at least one protuberance which projects into a correspondingly shaped groove in the substrate.
17. A preform element according to Claim 16, wherein the protuberance comprises a thickened peripheril rim formed on the rear surface of the facing table and extending into a correspondingly shaped recess in the substrate.
18. A preform element according to Claim 16 or Claim 17, wherein the protuberance projects from the rear face of the facing table by a distance which is substantially equal to the thickness of the facing table.
19. A preform element according to Claim 16 or Claim 17, wherein the protuberance projects from the rear face of the facing table by a distance which is no greater than twice the thickness of the rest of the facing table.
20. A preform element according to Claim 16 or Claim 17, wherein the protuberance projects from the rear face of the facing table by a distance which is no greater than three times the thickness of the rest of the facing table.
21. A preform element according to any of the preceding Claims 16-20, 22 wherein the maximum thickness of the facing table, including the protuberance, is greater than half the overall thickness of the preform element.
22. A preform element according to any of the preceding claims, wherein there is provided a transition layer between the superhard material and the less hard material, the transition layer comprising material having at least one property which is intermediate the corresponding properties of the superhard and less hard materials.
23. A preform element according to Claim 22, wherein said transition layer extends across only a part of the interface between the superhard material and the less hard material.
24. A prefonn element according to Claim 23, wherein there are provided a plurality of transition layers extending across different parts of the interface between the superhard material and the less material.
25. A rotary drag-type drill bit having a bit body formed with at least one pocket in which is received a preform cutting element including a facing table of superhard material having a front face, a peripheral surface, and a rear surface bonded to the front surface of a substrate which is less hard than the superhard material, the peripheral surface of the facing table including a region where the peripheral surface, throughout at least a major part of its thickness, is spaced inwardly from the outer periphery of the substrate, part of the substrate engaging said inwardly spaced part of the peripheral surface of the facing table, the pocket having an inner peripheral surface to which a part of the outer periphery of the preform element is brazed, including the outer periphery of said part of the substrate which engages the peripheral surface of the 23 facing table.
26. A drill bit according to Claim 25, wherein a part of the material of the bit body overfies part of the substrate so as to assist in retaining the element in the pocket.
27. A drill bit according to Claim 26, wherein a part of the front face of the substrate of the cutting element is formed with a rebate adjacent part of the periphery of the substrate, and wherein a part of the material of the bit body engages within said rebate.
28. A drill bit according to Claim 27, wherein said rebate has a bottom wall and a side wall.
29. A drill bit according to Claim 28, wherein said rebate comprises a chamfer extending from the periphery of the substrate to a region of the front surface thereof inward of the periphery.
30. A method of manufacturing a preform cutting element, comprising forming an intermediate member having a facing table of superhard material extending across only a part of a substrate of less hard material, and then removing material from the intermediate member to leave a smaller preform element wherein only a part of the periphery of the facing table is exposed at the periphery of the preform element.
31. A method according to Claim 30, wherein the intermediate member comprises a single facing table spaced inwardly from the periphery of the substrate, at least part of the periphery of the substrate of the intermediate member subsequently being removed to expose part of the periphery of the facing table.
32. A method according to Claim 30, wherein the intermediate member 24 comprises a plurality of facing tables spaced apart on the front surface of the substrate of the intermediate member, each facing table, together with an adjacent larger area of substrate, being subsequently separated from the intermediate member to provide a plurality of preform elements.
33. A preform cutting element substantially as hereinbefore described with reference to any of Figures 5-10, 14 or 15 of the accompanying drawings.
34. A method of manufacturing a preform cutting element substantially as hereinbefore described with reference to any of Figures 11 - 13 of the accompanying drawings.
GB9911920A 1998-06-02 1999-05-24 Rotary drill bits Expired - Lifetime GB2338007B (en)

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GBGB9811705.4A GB9811705D0 (en) 1998-06-02 1998-06-02 Preform cutting elements for rotary drill bits
GB9911920A GB2338007B (en) 1998-06-02 1999-05-24 Rotary drill bits

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GB2338007A true GB2338007A (en) 1999-12-08
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GB2396636A (en) * 2002-12-23 2004-06-30 Smith International An earth boring bit and method of forming a bit

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US5435403A (en) * 1993-12-09 1995-07-25 Baker Hughes Incorporated Cutting elements with enhanced stiffness and arrangements thereof on earth boring drill bits
EP0687797A1 (en) * 1994-06-18 1995-12-20 Camco Drilling Group Limited Improvements in or relating to elements faced with superhard material
EP0692607A2 (en) * 1994-06-16 1996-01-17 De Beers Industrial Diamond Division (Proprietary) Limited Tool component with abrasive compact
US5605198A (en) * 1993-12-09 1997-02-25 Baker Hughes Incorporated Stress related placement of engineered superabrasive cutting elements on rotary drag bits

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GB2334269B (en) * 1998-02-13 2002-04-17 Camco Internat Improvements in or relating to elements faced with superhard material

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US5435403A (en) * 1993-12-09 1995-07-25 Baker Hughes Incorporated Cutting elements with enhanced stiffness and arrangements thereof on earth boring drill bits
US5605198A (en) * 1993-12-09 1997-02-25 Baker Hughes Incorporated Stress related placement of engineered superabrasive cutting elements on rotary drag bits
EP0692607A2 (en) * 1994-06-16 1996-01-17 De Beers Industrial Diamond Division (Proprietary) Limited Tool component with abrasive compact
EP0687797A1 (en) * 1994-06-18 1995-12-20 Camco Drilling Group Limited Improvements in or relating to elements faced with superhard material

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Publication number Priority date Publication date Assignee Title
GB2396636A (en) * 2002-12-23 2004-06-30 Smith International An earth boring bit and method of forming a bit
GB2396636B (en) * 2002-12-23 2006-06-07 Smith International An earth-boring bit and a method for forming a bit
US7469757B2 (en) 2002-12-23 2008-12-30 Smith International, Inc. Drill bit with diamond impregnated cutter element

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GB9911920D0 (en) 1999-07-21
GB2338007B (en) 2003-01-22

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Expiry date: 20190523