Wear-resistant, superabrasive compacts are utilized in a variety of mechanical applications. For example, polycrystalline diamond compacts (“PDCs”) are used in drilling tools (e.g., cutting elements, gage trimmers, etc.), machining equipment, bearing apparatuses, wire-drawing machinery, and in other mechanical systems.
PDCs have found particular utility as superabrasive cutting elements in rotary drill bits, such as roller cone drill bits and fixed cutter drill bits. A PDC cutting element or cutter typically includes a superabrasive diamond layer or table. The diamond table is formed and bonded to a substrate using an ultra-high pressure, ultra-high temperature (“HPHT”) process. The substrate is often brazed or otherwise joined to an attachment member, such as a stud or a cylindrical backing A stud carrying the PDC may be used as a PDC cutting element when mounted to a bit body of a rotary drill bit by press-fitting, brazing, or otherwise securing the stud into a receptacle formed in the bit body. The PDC cutting element may also be brazed directly into a preformed pocket, socket, or other receptacle formed in the rotary drill bit. A rotary drill bit typically includes a number of PDC cutting elements affixed to the bit body.
Conventional PDCs are normally fabricated by placing a cemented-carbide substrate into a container or cartridge with a volume of diamond particles positioned on a surface of the cemented-carbide substrate. A number of such cartridges may be loaded into an HPHT press. The substrates and volume of diamond particles are then processed under HPHT conditions in the presence of a catalyst material that causes the diamond particles to bond to one another to form a matrix of bonded diamond grains defining a diamond table. The catalyst material is often a solvent catalyst, such as cobalt, nickel, iron, or alloys thereof that is used for facilitating the intergrowth of the diamond particles.
In one conventional approach, a constituent of the cemented-carbide substrate, such as cobalt from a cobalt-cemented tungsten carbide substrate, liquefies and sweeps from a region adjacent to the volume of diamond particles into interstitial regions between the diamond particles during the HPHT process. The cobalt acts as a catalyst to facilitate intergrowth between the diamond particles, which results in formation of bonded diamond grains. Often, a solvent catalyst may be mixed with the diamond particles prior to subjecting the diamond particles and substrate to the HPHT process.
The solvent catalyst dissolves carbon from the diamond particles or portions of the diamond particles that graphitize due to the high temperature being used in the HPHT process. The solubility of the stable diamond phase in the solvent catalyst is lower than that of the metastable graphite under HPHT conditions. As a result of this solubility difference, the undersaturated graphite tends to dissolve into solvent catalyst and the supersaturated diamond tends to deposit onto existing diamond particles to form diamond-to-diamond bonds. Accordingly, diamond grains become mutually bonded to form a matrix of polycrystalline diamond with interstitial regions between the bonded diamond grains being occupied by the solvent catalyst.
Despite the availability of a number of different superabrasive materials, manufacturers and users of superabrasive materials continue to seek superabrasive materials that exhibit improved mechanical and/or thermal properties.
Embodiments of the present invention relate to superabrasive materials, superabrasive compacts employing such superabrasive materials, and methods of fabricating such superabrasive materials and compacts. In one embodiment of the present invention, a superabrasive material includes a matrix including a plurality of coarse-sized superabrasive grains, with the coarse-sized superabrasive grains exhibiting a coarse-sized average grain size. The superabrasive material further includes a plurality of superabrasive regions dispersed within the matrix, with each superabrasive region including a plurality of fine-sized superabrasive grains exhibiting a fine-sized average grain size less than the coarse-sized average grain size.
In another embodiment of the present invention, the superabrasive materials may be employed in a superabrasive compact. The superabrasive compact comprises a substrate including a superabrasive table bonded thereto that comprises any of the disclosed embodiments of superabrasive materials.
In yet another embodiment of the present invention, a superabrasive material or a superabrasive compact may formed. A mixture may be sintered to form a superabrasive material. The mixture includes a plurality of coarse-sized superabrasive particles, with the coarse-sized superabrasive particles exhibiting a coarse-sized average particle size. The mixture further includes a plurality of agglomerates dispersed through the plurality of coarse-sized superabrasive particles, with each agglomerate including a plurality of fine-sized superabrasive particles. The fine-sized superabrasive particles exhibit a fine-sized average particle size that is less than the coarse-sized average particle size.
Further embodiments of the present invention relate to applications utilizing the disclosed superabrasive materials in various articles and apparatuses, such as, rotary drill bits, machining equipment, bearing apparatuses, wire-drawing dies, and other articles and apparatuses.
The drawings illustrate several embodiments of the present invention, wherein identical reference numerals refer to identical elements or features in different views or embodiments shown in the drawings.
Embodiments of the present invention relate to superabrasive materials, superabrasive compacts employing such superabrasive materials, and methods of fabricating such superabrasive materials and compacts. The embodiments of superabrasive materials disclosed herein include a plurality of relatively fine-grained superabrasive regions dispersed within a matrix of relatively coarse-grained superabrasive grains to provide a tough and abrasion resistant superabrasive material. The superabrasive regions provide relatively abrasion-resistant regions and the matrix provides a relatively impact-resistant and/or thermally stable region. The embodiments of superabrasive materials disclosed herein may be used in a variety of applications, such as drilling tools (e.g., compacts, cutting elements, gage trimmers, etc.), machining equipment, bearing apparatuses, wire-drawing machinery, and other apparatuses. As used herein, the term “superabrasive” means a material that exhibits a hardness exceeding a hardness of tungsten carbide.
Still referring to
The superabrasive regions 104 provides the superabrasive material 100 with relatively high-abrasion resistant regions, while the matrix comprising the coarse-sized superabrasive grains 102 provides the superabrasive material 100 with a relatively impact-resistant and/or thermally stable region. According to one specific embodiment of the present invention, the matrix may comprise about 40 to about 70 percent by weight of the superabrasive material 100, with the superabrasive regions 104 being the balance.
Still referring to
The coarse-sized superabrasive particles may exhibit a coarse-sized average particle size of about 6 μm to about 30 μm, and the fine-sized superabrasive particles may exhibit a fine-sized average particle size of about 6 μm or less. In some embodiments of the present invention, the coarse-sized average particle size of the coarse-sized superabrasive particles is about five times or more than the fine-sized average particle size of the fine-sized superabrasive particles of the agglomerates. Additionally, in some embodiments, the coarse-sized superabrasive particles may exhibit a bimodal or greater size distribution, while the coarse-sized average particle size is still greater than that of the fine-sized average particle size. However, an average size (i.e., a diameter or other cross-sectional dimension) of the agglomerates may be about 50 μm to about 200 μm. Each agglomerate may exhibit a selected geometry, such as a generally ellipsoid geometry, a generally spherical geometry, a non-spherical geometry, a generally cylindrical geometry, or another selected geometry. Non-spherically-shaped agglomerates may be formed by initially forming the agglomerates to exhibit the non-spherical shape or forming the agglomerates to exhibit a generally spherical geometry and compacting the agglomerates with rollers to form non-spherically-shaped particles. Furthermore, the plurality of agglomerates may comprise a mixture of differently shaped agglomerates, which may improve packing density.
In act 206, the mixture is subjected to an HPHT sintering process in the presence of a sintering aid, such as a metal-solvent catalyst comprising any of the previously mentioned metal-solvent catalysts. The metal-solvent catalyst may be in the form of metal-solvent-catalyst particles that are mixed in with the mixture prior to the HPHT sintering process or the metal-solvent catalyst may be in the form a metal-solvent-catalyst foil or green layer of metal-solvent catalyst placed adjacent to the mixture prior to the HPHT sintering process. Despite the relatively fine-size and relatively high-surface area of the fine-sized superabrasive particles that comprise each agglomerate, the metal-solvent catalyst may still effectively wet the fine-sized superabrasive particles to promote growth and bonding between adjacent fine-sized superabrasive particles and the coarse-sized superabrasive particles. This is currently believed by the inventor to be as a result of the proportion of the agglomerates in the mixture being sufficiently low (e.g., about less than 70 percent by weight) so that the collective surface area of the fine-sized superabrasive particles is sufficiently low.
In order to efficiently sinter the mixture, the mixture may be placed in a pressure transmitting medium, such as a refractory metal can, graphite structure, pyrophyllite and/or other pressure transmitting structure, or another suitable container or supporting element. The pressure transmitting medium, including the mixture, is subjected to an HPHT process using an ultra-high pressure press at a temperature of at least about 1000° Celsius (e.g., about 1100° Celsius to about 2200° Celsius) and a pressure of at least about 40 kilobar (e.g., about 50 kilobar to about 80 kilobar) for a time sufficient to sinter and form the superabrasive material 100 shown in
Referring to
In other embodiments of the present invention, the superabrasive table 304 may be separately formed using an HPHT sintering process and, subsequently, bonded to the interfacial surface 306 of the substrate 302 by brazing, using a separate HPHT bonding process, or any other suitable joining technique, without limitation. In yet another embodiment of the present invention, the substrate may be formed by depositing a binderless carbide (e.g., tungsten carbide) via chemical vapor deposition onto the separately formed superabrasive table.
In any of the embodiments disclosed herein, substantially all or a selected portion metal-solvent catalyst may be removed (e.g., via leaching) from the superabrasive material so-formed. For example, substantially all or a selected portion metal-solvent catalyst may be removed from the superabrasive table 304 so-formed in the superabrasive compact 300.
It is noted that the superabrasive material 100 described with respect to
The superabrasive compacts disclosed herein (e.g., the superabrasive compact 300 shown in
Thus, the embodiments of superabrasive compacts disclosed herein may be used on any apparatus or structure in which at least one conventional PDC is typically used. For example, in one embodiment of the present invention, a rotor and a stator (i.e., a thrust bearing apparatus) may each include a superabrasive compact (e.g., the superabrasive compact 300 shown in
Although the present invention has been disclosed and described by way of some embodiments, it is apparent to those skilled in the art that several modifications to the described embodiments, as well as other embodiments of the present invention are possible without departing from the spirit and scope of the present invention. Additionally, the words “including,” “having,” and variants thereof (e.g., “includes” and “has”) as used herein, including the claims, shall have the same meaning as the word “comprising” and variants thereof (e.g., “comprise” and “comprises”) and mean “including, but not limited to.”
This application is a continuation of application Ser. No. 12/858,032 filed on 17 Aug. 2010, now U.S. Pat. No. 8,151,911, which is a continuation of application Ser. No. 12/070,149 filed on 15 Feb. 2008, now U.S. Pat. No. 7,806,206, the disclosure of each of the foregoing applications is incorporated herein, in its entirety, by reference.
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Number | Date | Country | |
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Parent | 12858032 | Aug 2010 | US |
Child | 13414180 | US | |
Parent | 12070149 | Feb 2008 | US |
Child | 12858032 | US |