Milling and grinding machines are commonly used in various applications and industries, such as mining, asphalt and pavement removal and installation, and others. Such machines may remove material at desired locations. In some applications, material may be removed to facilitate repair or reconditioning of a surface. One example includes removing a portion or a layer of a paved road surface to facilitate repaving. In some instances, the removed material also may be valuable. For example, removed asphalt may be reprocessed and reused. Similarly, in mining operations, removed material may include valuable or useful constituents.
Conventional machines include cutting tools that may cut or grind target material. Typically, such cutting tools are mounted on a rotating drum assembly and engage (e.g., cut and/or grind) the target material as the drum assembly rotates. Failure of the cutting tools may, in turn, lead to the failure of the drum assembly and/or interruptions in operation thereof.
Therefore, manufacturers and users of cutting tools continue to seek improved cutting tools to extend the useful life of drum assemblies and/or reduce or eliminate interruptions in operation thereof.
Embodiments of the invention are directed to cutting tool assemblies, cutting tool mounting assemblies, material-removing machines that include cutting tool assemblies and/or cutting tool mounting assemblies, and methods of use and operation thereof. In some embodiments, the various assemblies described herein may be used in material-removing machines that may remove target material, such as a portion or a layer of a pavement. For example, a material-removing machine may include a rotary drum, and the cutting tool assemblies and/or the cutting tool mounting assembly may be mounted to or on the rotary drum. Furthermore, as the material-removing machine rotates the cutting tool assemblies together with the rotary drum, the cutting tool assemblies may engage and cut, grind, or otherwise fail the target material, which may be subsequently removed (e.g., by rotary drum assembly of the material-removing machine).
An embodiment includes a cutting tool assembly configured for attachment to a base body on a rotatable assembly of a material-removal machine. The cutting tool assembly includes a support block that includes an elongated mounting shank sized and configured to be secured within the base body. The cutting tool assembly also includes a bolster body fixedly secured to the support block and a cutting element secured to and positioned at least partially within the bolster body. The cutting element has a superhard working surface that includes a superhard material. Moreover the bolster body is sized and configured to protect at least a portion of the cutting element from at least one of erosion or wear during operation of the cutting tool assembly.
At least one embodiment includes a cutting tool mounting assembly. The cutting tool mounting assembly includes a base body sized and configured to be mounted to a rotary drum of a material-removal machine and a cutting tool assembly mounted to the base body. The base body includes a tool recess, and the cutting tool assembly includes a support block that includes an elongated mounting shank positioned in the tool recess of the base body. Moreover, the cutting tool assembly includes a bolster body fixedly secured to the support block and a cutting element secured to and positioned at least partially within the bolster body. The cutting element has a superhard working surface that includes a superhard material, and the bolster body is sized and configured to protect at least a portion of the cutting element from at least one of erosion or wear during operation of the cutting tool assembly.
Embodiments also include a rotary drum assembly. The rotary drum assembly includes a drum body that includes an outer surface and one or more cutting tool mounting assemblies mounted to the drum body. Each of the cutting tool mounting assemblies includes a base body mounted to the outer surface of the drum body and a cutting tool assembly mounted to the base body. The base body includes a tool recess, and the cutting tool assembly includes a support block that includes an elongated mounting shank positioned in the tool recess of the base body. Moreover, the cutting tool assembly includes a bolster body fixedly secured to the support block, and a cutting element secured to and positioned at least partially within the bolster body. The cutting element has a superhard working surface that includes a superhard material, and the bolster body is sized and configured to protect at least a portion of the cutting element from at least one of erosion or wear during operation of the cutting tool assembly.
Features from any of the disclosed embodiments may be used in combination with one another, without limitation. In addition, other features and advantages of the present disclosure will become apparent to those of ordinary skill in the art through consideration of the following detailed description and the accompanying drawings.
The drawings illustrate several embodiments, wherein identical reference numerals refer to identical or similar elements or features in different views or embodiments shown in the drawings.
Embodiments of the invention are directed to cutting tool assemblies, cutting tool mounting assemblies, material-removing machines that include cutting tool assemblies and/or cutting tool mounting assemblies, and methods of use and operation thereof. In some embodiments, the various assemblies described herein may be used in material-removing machines that may remove target material, such as a portion or a layer of a pavement. For example, a material-removing machine may include a rotary drum, and the cutting tool assemblies and/or the cutting tool mounting assembly may be mounted to or on the rotary drum. Furthermore, as the material-removing machine rotates the cutting tool assemblies together with the rotary drum, the cutting tool assemblies may engage and cut, grind, or otherwise fail the target material, which may be subsequently removed (e.g., by rotary drum assembly of the material-removing machine).
In an embodiment, the cutting tool assemblies may include one or more superhard working surfaces that may engage the target material. As used herein, “superhard material” includes materials exhibiting a hardness that is at least equal to the hardness of tungsten carbide (i.e., a portion of or the entire working surface may have a hardness that exceeds the hardness of tungsten carbide). In any of the embodiments disclosed herein, the cutting tool assemblies and the cutting elements may include one or more superhard materials, such as polycrystalline diamond, polycrystalline cubic boron nitride, silicon carbide, tungsten carbide, or any combination of the foregoing superhard materials. For example, a cutting element may include a substrate and a superhard material bonded to the substrate, as described in further detail below. The superhard material may form or define the working surface.
The cutting tool assemblies may include a support block. For example, the support block may be sized and configured to be removably secured to and/or within a base body of cutting tool mounting assembly, and the base body may be secured to a rotatable assembly (e.g., a rotary drum body of a rotary drum). In an embodiment, the support block may include an elongated mounting shank that may be at least partially positioned in a recess of base body and may be secured therein, thereby securing the cutting tool assembly to the base of the cutting tool mounting assembly. Moreover, a bolster body may be bonded to or integrated with the elongated mounting shank of the support block. The bolster body and the elongated mounting shank may be configured such that securing the elongated mounting shank in and/or to the base body to position and orient the bolster body at a predetermined angle relative to a radial line extending from a center of rotation of the rotary drum (e.g., when the base body is mounted to the rotary drum). For example, the bolster body may have a streamlined geometry to help reduce drag during cutting operations and, consequently, improve cutting efficiency.
In an embodiment, the working surface may be formed on or secured to the bolster body (e.g., the working surface may be formed on a cutting element that is secured to the bolster body). Generally, the bolster body may have any number of suitable shapes. In some embodiments, the bolster body may be shaped, sized, or otherwise configured in a manner that may reduce wear thereof during operation. Moreover, in one or more embodiments, the bolster body may be configured to protect or shield at least a portion of the cutting element, such as from erosion and/or wear, (e.g., in a manner that extends the useful life of the cutting element and/or extends useful life of the bond or attachment between the cutting element and the bolster body).
As described below in more detail, the cutting element 120 may include a superhard working surface 121. In the illustrated embodiment, the superhard working surface 121 is generally planar. However, the superhard working surface 121 may have any suitable shape and configuration, which may vary from one embodiment to another (e.g., the superhard working surface 121 may be generally domed, generally pointed, or semi-spherical and/or may have a perimeter that may be circular, semi-circular, elliptical, square, or wedge-shaped). The superhard working surface 121 may be sized and configured to engage, cut, scrape, or otherwise cause the target material to fail. For example, the superhard working surface 121 may include a cutting edge that may define at least a portion of the perimeter of the superhard working surface 121. In an embodiment, the superhard working surface 121 may include the cutting edge that may facilitate entry or penetration of the cutting element 120 into the target material and subsequent failing and/or removal thereof.
In some embodiments, the superhard working surface 121 may include a chamfered periphery. In other words, a chamfer may extend from and about at least a portion of the superhard working surface 121 to a peripheral surface of the cutting element 120. As such, the chamfer may form two or more cutting edges (e.g., a cutting edge formed at the interface between the superhard working surface 121 and the chamfer and another cutting edge formed at the interface between the chamfer and the peripheral surface of the cutting element 120).
In some embodiments, the superhard working surface 121 may include superhard material. As used herein, “superhard material” includes a material exhibiting a hardness that is at least equal to the hardness of tungsten carbide (e.g., a portion or the entire working surface may have a hardness that exceeds the hardness of tungsten carbide). In any of the embodiments disclosed herein, the cutting assemblies and the cutting elements may include one or more superhard materials, such as polycrystalline diamond, polycrystalline cubic boron nitride, silicon carbide, tungsten carbide, or any combination of the foregoing superhard materials. For example, a cutting element may include a substrate and a superhard material bonded to the substrate, as described in further detail below.
In some embodiments, the superhard working surface 121 may be formed or defined by a superhard table that may be attached to a substrate. In an embodiment, the substrate may be attached to the bolster body 140. For example, the cutting element 120 (e.g., the substrate thereof) may be recessed in the bolster body 140, such that the bolster body 140 protects or shields the cutting element 120 from wear and/or erosion. Alternatively, the superhard table may be attached directly to the bolster body 140 (e.g., the bolster body 140 may include cemented carbide, and the superhard table that defines the superhard working surface 121 may be bonded directly to the bolster body). That is, the bolster body 140 may form the substrate (e.g., the bolster body 140 may include suitable material for bonding the superhard table thereto, such as tungsten carbide).
In an embodiment, the superhard table may comprise polycrystalline diamond and the substrate may comprise cobalt-cemented tungsten carbide. Furthermore, in any of the embodiments disclosed herein, the polycrystalline diamond table may be leached to at least partially remove or substantially completely remove a metal-solvent catalyst (e.g., cobalt, iron, nickel, or alloys thereof) that was used to initially sinter precursor diamond particles to form the polycrystalline diamond. In another embodiment, an infiltrant used to re-infiltrate a preformed leached polycrystalline diamond table may be leached or may otherwise have a metallic infiltrant removed to a selected depth from a working surface. Moreover, in any of the embodiments disclosed herein, the polycrystalline diamond may be un-leached and include a metal-solvent catalyst (e.g., cobalt, iron, nickel, or alloys thereof) that was used to initially sinter the precursor diamond particles that form the polycrystalline diamond and/or an infiltrant used to re-infiltrate a preformed leached polycrystalline diamond table. Examples of methods for fabricating the superhard tables and superhard materials and/or structures from which the superhard tables and elements may be made are disclosed in U.S. Pat. Nos. 7,866,418; 7,998,573; 8,034,136; and 8,236,074; the disclosure of each of the foregoing patents is incorporated herein, in its entirety, by this reference.
The diamond particles that may be used to fabricate the superhard table in a high-pressure/high-temperature process (“HPHT)” may exhibit a larger size and at least one relatively smaller size. As used herein, the phrases “relatively larger” and “relatively smaller” refer to particle sizes (by any suitable method) that differ by at least a factor of two (e.g., 30 μm and 15 μm). According to various embodiments, the diamond particles may include a portion exhibiting a relatively larger size (e.g., 70 μm, 60 μm, 50 μm, 40 μm, 30 μm, 20 μm, 16 μm, 15 μm, 12 μm, 10 μm, 8 μm) and another portion exhibiting at least one relatively smaller size (e.g., 15 μm, 12 μm, 10 μm, 8 μm, 6 μm, 5 μm, 4 μm, 3 μm, 2 μm, 1 μm, 0.5 μm, less than 0.5 μm, 0.1 μm, less than 0.1 μm). In an embodiment, the diamond particles may include a portion exhibiting a relatively larger size between about 10 μm and about 40 μm and another portion exhibiting a relatively smaller size between about 1 μm and 4 μm. In another embodiment, the diamond particles may include a portion exhibiting the relatively larger size between about 15 μm and about 50 μm and another portion exhibiting the relatively smaller size between about 5 μm and about 15 μm. In another embodiment, the relatively larger size diamond particles may have a ratio to the relatively smaller size diamond particles of at least 1.5. In some embodiments, the diamond particles may comprise three or more different sizes (e.g., one relatively larger size and two or more relatively smaller sizes), without limitation. The resulting polycrystalline diamond formed from HPHT sintering the aforementioned diamond particles may also exhibit the same or similar diamond grain size distributions and/or sizes as the aforementioned diamond particle distributions and particle sizes. Additionally, in any of the embodiments disclosed herein, the superhard cutting elements may be free-standing (e.g., substrateless) and/or formed from a polycrystalline diamond body that is at least partially or fully leached to remove a metal-solvent catalyst initially used to sinter the polycrystalline diamond body.
As noted above, the superhard table may be bonded to the substrate. For example, the superhard table comprising polycrystalline diamond may be at least partially leached and bonded to the substrate with an infiltrant exhibiting a selected viscosity, as described in U.S. patent application Ser. No. 13/275,372, entitled “Polycrystalline Diamond Compacts, Related Products, And Methods Of Manufacture,” the entire disclosure of which is incorporated herein by this reference. In an embodiment, an at least partially leached polycrystalline diamond table may be fabricated by subjecting a plurality of diamond particles (e.g., diamond particles having an average particle size between 0.5 μm to about 150 μm) to an HPHT sintering process in the presence of a catalyst, such as cobalt, nickel, iron, or an alloy of any of the preceding metals to facilitate intergrowth between the diamond particles and form a polycrystalline diamond table comprising bonded diamond grains defining interstitial regions having the catalyst disposed within at least a portion of the interstitial regions. The as-sintered polycrystalline diamond table may be leached by immersion in or exposure to an acid or subjected to another suitable process to remove at least a portion of the catalyst from the interstitial regions of the polycrystalline diamond table, as described above. The at least partially leached polycrystalline diamond table includes a plurality of interstitial regions that were previously occupied by a catalyst and form a network of at least partially interconnected pores. In an embodiment, the sintered diamond grains of the at least partially leached polycrystalline diamond table may exhibit an average grain size of about 20 μm or less. Subsequent to leaching the polycrystalline diamond table, the at least partially leached polycrystalline diamond table may be bonded to a substrate in an HPHT process via an infiltrant with a selected viscosity. For example, an infiltrant may be selected that exhibits a viscosity that is less than a viscosity typically exhibited by a cobalt cementing constituent of typical cobalt-cemented tungsten carbide substrates (e.g., 8% cobalt-cemented tungsten carbide to 13% cobalt-cemented tungsten carbide).
Additionally or alternatively, the superhard table may be a polycrystalline diamond table that has a thermally-stable region, having at least one low-carbon-solubility material disposed interstitially between bonded diamond grains thereof, as further described in U.S. patent application Ser. No. 13/027,954, entitled “Polycrystalline Diamond Compact Including A Polycrystalline Diamond Table With A Thermally-Stable Region Having At Least One Low-Carbon-Solubility Material And Applications Therefor,” the entire disclosure of which is incorporated herein by this reference. The low-carbon-solubility material may exhibit a melting temperature of about 1300° C. or less and a bulk modulus at 20° C. of less than about 150 GPa. The low-carbon-solubility, in combination with the high diamond-to-diamond bond density of the diamond grains, may enable the low-carbon-solubility material to be extruded between the diamond grains and out of the polycrystalline diamond table before causing the polycrystalline diamond table to fail during operations.
In some embodiments, the polycrystalline diamond, which may form the superhard table, may include bonded-together diamond grains having aluminum carbide disposed interstitially between the bonded-together diamond grains, as further described in U.S. patent application Ser. No. 13/100,388, entitled “Polycrystalline Diamond Compact Including A Polycrystalline Diamond Table Containing Aluminum Carbide Therein And Applications Therefor,” the entire disclosure of which is incorporated herein by this reference.
In some embodiments, one or more portions and/or surfaces of the support block 110 may be configured to be pressed or forced to at least partially contact corresponding portions and/or surfaces of the base body. For example, pressing one or more surfaces of the support block 110 against corresponding one or more surfaces of the base body may prevent or limit movement of the support block 110 in one or more directions or orientations relative to the base body (e.g., during operation of the cutting tool assembly 100). In the illustrated embodiment, the elongated mounting shank 130 includes an angled surface 131 that may at least partially contact a corresponding angled surface and the base body. In particular, for example, the surface 131 may form an obtuse angle with a vertical axis 10 of the cutting tool assembly 100. For example, the vertical axis 10 may be generally parallel to a vertical portion of the elongated mounting shank 130 (e.g., parallel to peripheral surfaces 135, 136 of the elongated mounting shank 130).
Furthermore, the support block 110 may include multiple angled surfaces that may be oriented at various angles relative to the vertical axis 10. For example, the surface 131 may extend between angled surfaces 132, 133, which may be positioned along each side of surface 131 (e.g., the surfaces 132 and/or 133 may be at a different angle relative to the vertical axis than surface 131). In an embodiment, the surface 131 may be generally planar. Similarly, the surfaces 132 and/or 133 may be generally planar. As shown in the illustrated embodiment, the surfaces 131, 132, 133 may be arranged along a generally arcuate path, such as along an imaginary arcuate path 20 (e.g., the surfaces 131, 132, 133 may be generally tangent to the arcuate path 20). For example, as described below in more detail, when the elongated mounting shank 130 is positioned in the base body, and the surfaces 131, 132, 133 may abut or press against corresponding surfaces of the base body, the surfaces 131, 132, 133 may prevent or limit movement of the cutting tool assembly 100 relative to the base body (e.g., in directions generally outward from the surfaces 131, 132, 133) and may prevent or limit pivoting or twisting of the cutting tool assembly 100 relative to the base body (e.g., about the vertical axis 10).
Generally, the vertical portion of the elongated mounting shank 130 may have any suitable peripheral shape that may be defined by one or more peripheral surfaces and may vary from one embodiment to the next. In the illustrated embodiment, the peripheral surfaces defining the vertical portion of the elongated mounting shank 130 may include one or more planar surfaces, such as surfaces 135 and 136 (e.g., surface 135 may be oriented at approximately 90° angle relative to surface 136, and surfaces 135, 136 may be generally parallel to the vertical axis 10). For example, planar surfaces defining the vertical portion of the elongated mounting shank 130 may correspond to and/or abut or at least partially contact corresponding surfaces of the base body in a manner that prevents or limits rotation or pivoting of the cutting tool assembly 100 about the vertical axis 10.
As described above, the bolster body 140 may be secured (e.g., by welding, brazing, soldering, laser fusing, press-fitting, mechanically attaching, combinations of the foregoing, etc.) to the support block 110 (e.g., to the elongated mounting shank 130). In some embodiments, the bolster body 140 may be oriented at a non-parallel and/or non-perpendicular angle relative to the elongated mounting shank 130. For example, the bolster body 140 and the elongated mounting shank 130 may form or define an obtuse angle therebetween.
In some embodiments, the bolster body 140 may be bonded to the elongated mounting shank 130 (e.g., the bolster body 140 may be bonded to the elongated mounting shank 130 by brazing, welding, press-fitting, mechanically attaching, combinations of the foregoing, etc.). Alternatively, the elongated mounting shank 130 and bolster body 140 may be integral or integrated together (e.g., the bolster body 140 and elongated mounting shank 130 may be formed or fabricated from a single piece of material). In some embodiments, the bolster body 140 and elongated mounting shank 130 may include different materials from each other. For example, the bolster body 140 may include a material that is stronger (e.g., exhibiting a higher yield strength) and/or more abrasion resistant than the material of the elongated mounting shank 130). In at least one embodiment, the bolster body 140 may include a material such as carbide and/or cemented carbide (e.g., the bolster body 140 may include any number of carbide materials and/or cementing alloys, which may be similar to or the same as the carbides described herein in connection with the substrate of the cutting element 120) and the elongated mounting shank 130 may include steel, and the bolster body 140 may be brazed to the elongated mounting shank 130. Additionally or alternatively, the bolster body 140 may include any suitable steel (e.g., carbon steel, stainless steel, or tool steel), which may be heat treated to a suitable hardness. For example, a steel bolster body 140 may be welded to the elongated mounting shank 130.
The support block 110 may include an upper portion 150, and the bolster body 140 may be secured to or integrated with the upper portion 150 and may extend outward therefrom. In some embodiments, the upper portion 150 may have a greater peripheral size (e.g., may be wider and/or longer) that the elongated mounting shank 130. For example, the upper portion 150 may include one or more shoulder portions or shoulders, such as shoulders 151, 152 that extend beyond the elongated mounting shank 130 (e.g., one or more surfaces of the shoulders 151, 152 may extend beyond one or more surfaces of the elongated mounting shank 130 and may optionally extend generally perpendicularly therefrom). For example, the shoulders 151 and/or 152 may at least partially contact one or more corresponding portions or surfaces of the base block (e.g., the shoulders 151 and/or 152 may vertically position the cutting tool assembly 100 relative to the base block). Under some operating conditions, as the cutting element 120 engages and/or enters the target material, the cutting tool assembly 100 may experience one or more forces thereon, which may urge movement of the cutting tool assembly 100 relative to the base body.
In some embodiments, however, the cutting tool assembly 100 may be fixedly secured (e.g., by metallurgical attachment, such as brazing, soldering, welding, etc., by mechanical attachment (e.g., bolts and/or clamps), such as by press-fitting, fastening, etc., or combinations of the foregoing, etc.) to the base body in a manner that limits or prevents movement that may otherwise result during operation of the cutting tool assembly 100. For example, the shoulders 151 and/or 152 may at least partially counteract or oppose the forces experience by the cutting tool assembly 100 during operation (e.g., as the shoulders 151 and/or 152 press against corresponding portions and/or surfaces of the base body). Additionally or alternatively, as mentioned above, the shape and/or size of the elongated mounting shank 130 (e.g., the shape and/or size of the vertical portion of the elongated mounting shank 130, the surfaces 131, 132, 133 of the elongated mounting shank 130, etc.) may prevent or limit movement of the cutting tool assembly 100 relative to the base body (e.g., from the forces experienced by the cutting tool assembly 100 during operation).
In some embodiments, the elongated mounting shank 130 may be secured to and/or positioned at least partially within the corresponding recess in the base body by one or more fasteners. For example, the elongated mounting shank 130 may include one or more locations that may accept or facilitate one or more corresponding fasteners that may secure or fasten the cutting tool assembly 100 to the base body. In the illustrated embodiment, the elongated mounting shank 130 includes fastener recesses 160. In particular, for example, the recesses 160 may include at least one surface against which a fastener may press or contact, thereby positioning the elongated mounting shank 130 at least partially into the recess in the base body. In an embodiment, the recesses 160 may include corresponding surfaces 161 (e.g., the surfaces 161 may be generally perpendicular to the surface 131). In any event, contact between a leading face of a fastener and one or more surfaces 161 of the recesses 160 may retain the elongated mounting shank 130 in the base body, thereby securing the cutting tool assembly at least partially within and/or to the base body in a manner that prevents or limits movement of the cutting tool assembly 100 relative to the base body during operation.
As described below in more detail, the bolster body 140 may be generally shaped to reduce drag as the cutting tool assembly 100, together with the bolster body 140, advances into the target material. In an embodiment, the bolster body 140 may be shaped such that the failed material may move away from the cutting element 120. For example, the bolster body 140 may have a generally tapered shape (e.g., a generally conical shape or frusto-conical shape). Moreover, the elongated mounting shank 130 may include a transition region 170, which may provide or form a transition between the bolster body 140 and the upper portion 150. For example, the transition region may extend between the bolster body 140 and an upper surface of the upper portion 150.
In some embodiments, the transition region 170 may be shaped, sized, and otherwise configured to guide or direct the flow or movement of the failed material past the bolster body 140 and along or over the upper portion 150 of the support block 110. For example, the transition region 170 may be generally tapered, such that the smaller portion of the taper is near the bolster body 140 and the larger portion of the taper is near the upper portion 150. In at least one embodiment, at least a portion of the upper portion 150 may be shaped to deflect or channel the failed material away from the support block 110 during operation. As shown in
In an embodiment, the support block 110 may be generally solid or monolithic. Alternatively, the support block 110 may include one or more cutouts or recesses, such as in a back side thereof (e.g., in a side facing away from the direction of movement or cut of the cutting tool assembly 100 during operation). For example, the recess(es) may facilitate or allow channeling movement or flow of failed material away from the cutting tool assembly 100.
As mentioned above, the bolster body 140 may be incorporated with or bonded to the support block 110.
In an embodiment, the support block 110a may include a recess 111a for locating the bolster body 140a relative to the support block 110a. In some embodiments, the recess 111a may have a generally circular perimeter (e.g., the recess 111a may be cylindrical). Alternatively, the perimeter of recess 111a may have at least partially non-circular shape, which may facilitate orienting the bolster body 140a relative to the support block 110a. In any event, in at least one embodiment, the bolster body 140a may be positioned in the recess 111a and may be bonded (e.g., brazed, welded, etc.) to at least a portion of a wall defining the recess 111a and/or to the support block 110a.
As described above, the bolster body may be generally shaped to reduce or minimize or limit drag during operation of the cutting tool assembly, as the cutting tool assembly moves through the target material. In some embodiments, the bolster body may include one or more drag-reduction features that may reduce drag of the bolster body (e.g., as compared with a bolster body without such features), which may extend the useful life of the cutting tool assembly.
In an embodiment, the bolster body 140b may include notches 141b that may extend from a forward facing portion of the bolster body 140b (e.g., portion facing generally in the same direction as the superhard working surface 121 of the cutting element 120) and to the backward facing portion of the bolster body 140b (e.g., portion facing away from the superhard working surface 121 of the cutting element 120). As described above, during operation, as the bolster body 140b of the cutting tool assembly 100b enters the target material, the cutting element 120 may fail the target material. For example, at least some of failed material may flow or move away from the superhard working surface 121 of the cutting element 120 and through one or more notches 141b. In some embodiments, the notches 141b may facilitate movement of the failed material away from the superhard working surface 121, thereby extending useful life thereof. Furthermore, for example, the bolster body 140b that includes the notches 141b may be generate less drag through the target material and thereby may require less energy during operation thereof (as compared with a bolster body that does not include the notches).
In some embodiments, the bolster body may have a generally narrow profile, which may facilitate reduced drag as the cutting tool assembly moves through the target material (as compared with a cutting tool that includes a relatively wider bolster body).
In an embodiment, the bolster body 140c may be generally narrow to reduce drag thereof in the target material (e.g., as compared with wider bolster bodies). More specifically, for example, the cutting element 120 may be mounted to the bolster body 140c, and the bolster body 140c may have a first dimension, such as width 30c, that may be similar to or the same as a dimensions of the cutting element 120, such as the width or diameter of the cutting element 120 (e.g., as measure along an imaginary line that is generally perpendicular to the direction of cut during operation of the cutting tool assembly 100c). For example, the width 30c of the bolster body 140c may be smaller than a length 35c thereof. In an embodiment, the width 30c of the bolster body 140c may be less than 2 times the diameter of the cutting element 120 or less than 3× the diameter of the cutting element 120 (e.g., the width 30c may be a multiple of the diameter of the cutting element 120, which may be in one or more of the following ranges: about 1.01-1.1 times the diameter of the cutting element 120; about 1.09-1.3 times the diameter of the cutting element 120; about 1.1-1.5 times the diameter of the cutting element 120; or about 1.4-1.9 times the diameter of the cutting element 120). Hence, in an embodiment, the width 30c of the bolster body 140c may be suitably narrow (e.g., relative to the support block 110), such as to reduce resistance or contact between the bolster body 140c and the target material engaged by the cutting tool assembly 100c.
Furthermore, in some embodiments, the bolster body 140c may include one or more generally planar surfaces, such as surfaces 142c, 143c. In an embodiments, the width 30c of the bolster body 140c may be defined by generally planar surfaces, such as the surface 142c and a surface opposite thereto, which may be similar to or the same as the surface 142c. In at least one embodiment, the leading face of the bolster body 140c (e.g., a face of the bolster body 140c that generally faces in the direction of cut or movement of the cutting tool assembly 100c during operation) and/or the trailing face thereof (e.g., a face of the bolster body 140c that generally faces away from the direction of cut or movement of the cutting tool assembly 100c during operation) may be defined by one or more generally planar surfaces. For example, the trailing face of the bolster body 140c may be at least partially defined by the surface 143c.
Any of the cutting tool assemblies described herein may include any number of cutting elements, which may vary from one embodiment to the next.
In an embodiment, the cutting elements 120a may be positioned near each other and/or may abut each other. For example, the cutting elements 120a may be aligned generally along a width 30d of the bolster body 140d. Alternatively or additionally, the cutting elements 120a may be positioned near each other and at a predetermined height (e.g., as measured downward from an uppermost portion of the bolster body 140d.
As described above, the bolster body 140d may include one or more notches that (for example) may facilitate movement or flow of failed material away from superhard working surfaces 121a of the cutting elements 120a. In some embodiments, the bolster body 140d may include a notch 141d that may extend between the cutting elements 120a. For example, at least some of the failed material may move away from the superhard working surface 121a of the cutting elements 120a and into the notch 141d of the bolster body 140d, which may extend useful life of the cutting elements 120a.
In an embodiment, the cutting tool assembly 100e may include two cutting elements 120a and one cutting element 120 (e.g., the cutting element 120 may be positioned at least partially between the cutting elements 120a). For example, the corresponding ones of the cutting elements 120a may and the cutting element 120 may be positioned at different apexes of an imaginary triangle (e.g., the imaginary triangle may be an equilateral triangle with the base thereof oriented generally parallel to a width 30e of the bolster body 140e). In some embodiments, the cutting element 120 may be positioned at or near an upper apex and near an uppermost portion of the bolster body 140, and the cutting elements 120a may be positioned at or near lower apexes of the imaginary triangle and along a base thereof.
The bolster body 140e may be generally sized, shaped, and otherwise configured to accommodate the cutting elements 120, 120a at suitable positions or locations. For example, the bolster body 140e may have an upper portion 145e supporting the cutting elements 120, 120a, such that the upper portion 145e is at least in part defined by rounded surfaces 142e, 143e, 144e, which may generally follow the contour of corresponding ones of the cutting elements 120a, 120. In some embodiments, a bolster body 140e may have a reduced drag through the target material (e.g., as compared with the bolster body that includes more material between the outer surface thereof and the cutting elements 120a and/or 120).
As described above, the bolster body may have any number of suitable shapes and/or sizes and may be integrated with the support block.
The support block 110f may include an elongated mounting shank 130f at least portion of which may be inserted into and/or secured to a base body (e.g., the elongated mounting shank 130f may include at least one recess 160f that may accept a portion of a fastener that may contact and/or restrict movement of the elongated mounting shank 130f, thereby securing the elongated mounting shank 130f in a recess of the base body). As described above, the support block 110f may include a upper portion 150f that may be attached to or integrated with the elongated mounting shank 130f (e.g., the upper portion 150f may facilitate positioning and/or securing of the support block 110f relative to the base body). Moreover, the bolster body 140f may extend from and/or may be integrated with the upper portion 150f.
In an embodiment, the bolster body 140f may have a generally cylindrical shape and a rounded upper portion 145f (e.g., a cutting element 120 may be attached to the bolster body 140f at or near the upper portion 145f thereof). In an embodiment, the cutting tool assembly 100s may include a transition region 155f (e.g., bend, notch, fillet, or chamfer) between the bolster body 140f and the upper portion 150f. For example, the transition region 155f may facilitate flow or movement failed material away from a leading portion of the cutting tool assembly 100f (e.g., away from a portion of the cutting tool assembly 100f that faces toward the cutting direction of the cutting tool assembly 100f during operation).
As mentioned above, the bolster body may be bonded to the support block of the cutting tool assembly.
In some embodiments, the bolster body 140g may be bonded to the support block 110g along an angled or interface surface 111g. For example, the interface surface 111g may position and/or orient the bolster body 140g relative to the support block 110g at a predetermined position and orientation. In an embodiment, the support block 110g may include an opening or recess 112g. For example, the recess 112g may facilitate securing the bolster body 140g to the support block 110g with a fastener.
Also, as mentioned above, the particular shape and/or size of cutting element(s) included in the cutting tool assembly may vary from one environment to the next. In the illustrated embodiment, the cutting tool assembly 100g includes a generally convex cutting element 120b (e.g., at least partially domed, pointed, ovoid, conical, or rounded). In particular, the cutting element 120b may include a generally convex superhard working surface 121b, which may be defined by a superhard table 122b bonded to a substrate 123b. Moreover, the cutting element 120b may be bonded to and may extend beyond the bolster body 140g in a manner that facilitates engagement of the superhard working surface 121b with the target material during operation of the cutting tool assembly 100g.
Alternatively or additionally, a bolster body may be mechanically secured to support block (e.g., with fastener(s), press-fitting, fitted at a locking angle, etc.).
In the illustrated embodiment, the support block 110h includes a recess 112h, and the bolster body 140h includes a shank 141h that may fit into the recess 112h and may be secured therein, thereby securing the bolster body 140h to the support block 110h. For example, the recess 112h may have a tapered configuration, and the shank 141h may have a generally corresponding or complementary taper, which may secure or lock the shank 141h in the recess 112h (e.g., the taper of the recess 112h and 114h may have a locking angle and/or may be a machine taper, such as Morse taper). Under some operating conditions, the bolster body 140h may be detached and/or removed from the support block 110h (e.g., for servicing and/or replacement). For example, the recess 112h may extend through the support block 110h, such that the shank 141h may be accessed from a back side of the support block 110h (e.g., access from the backside of the support block 110h may facilitate forcing the shank 141h out of the recess 112h). Moreover, in an embodiment, the shank 141h may be integrated with the bolster body 140h. In an embodiment, the shank 141h may be attached or secured to the bolster body 140h (e.g., the shank may be welded, brazed, soldered, or otherwise metallurgically attached to the bolster body 140h and/or may be fastened to the bolster body 140h).
The particular configuration of the cutting element may vary from one embodiment to the next.
In at least one embodiment, the cutting tool assembly 100k may be fastened to the base body. For example, a portion of a support block 110k may include one or more features that may accommodate a tool for fastening the support block to the base body (e.g., a wrench, etc.). In an embodiment, a lower portion 111k of the support block 110k may be configured to accept a wrench (e.g., the lower portion 111k of the support block 110k may have one or more flats, may have a generally hexagonal or square shape, etc.).
In at least one embodiment the cutting element 120c may be bonded to a bolster body 140k of the cutting tool assembly 100k. In some embodiments, a substrate 123c of the cutting element 120c may be at least partially exposed out of and/or extend beyond the bolster body 140k of the cutting tool assembly 100k. As shown in
Alternatively, as shown in
Moreover, the base body 300 may include a recess that may accommodate a fastener (e.g., similar to or the same as recess 320a and fastener 400 (
As described above, in at least one embodiment, the support block 110 may include the recess that facilitate channeling the flow or movement of failed material away from the cutting tool assembly 100. In some embodiments, The recess 340 may extend between the recess of the support block 110 and an outer or peripheral surface of the base body 300. For example, the failed material may enter the recess in the support block 110, move or flow into the recess 340 in the base body 300, and further move out of the recess 340 and away from the cutting tool mounting assembly. Moreover, in some embodiments, the base body 300 may include a slanted surface 350 that may partially defined the periphery of the base body 300, and which may generally extend from one or more peripheral surfaces of upper portion 150 of the support block 110. For example, the failed material may move along one or more portions of the peripheral surfaces of the upper portion 150, onto the slanted surface 350 of the base body 300, and away from the cutting tool mounting assembly 200.
Generally, the base body 300 may be mounted and/or secured to a rotary drum in any number of suitable ways. In an embodiment, the base body 300 may include a curved surface (e.g., similar to or the same as curved surface 330a of base body 300a (
As shown in
Moreover, as mentioned above, the cutting tool assembly may include multiple cutting elements. In some embodiments, one, some, or all of the cutting elements may have a positive or negative rake angle and/or a positive or a negative clearance angle. Moreover, the rake angles of two, some, or all the multiple cutting elements may be the same as one another or different from one another. In an embodiment, some of the cutting elements may have a positive rake angle, while other cutting elements may have a negative rake angle. Generally, rake angle may be any suitable angle (e.g., the rake angle may be any angle from −20 degrees to 20 degrees). However, the clearance angle will generally be positive (e.g., from 1 degree to 20 degrees; from 15 degrees to 25 degrees; from 25 degrees to 40 degrees, etc.).
In an embodiment, as shown in
The cutting tool assembly and its elements and components (e.g., the support block and/or the bolster body of the cutting tool assembly) may have any number of suitable shapes and may include one or more features for a fastening tool (e.g., for a wrench). As shown in
In some embodiments, at least a portion of the support block 110n may be generally cylindrical (e.g., the elongated mounting shank 130n may be generally cylindrical). In an embodiment, the elongated mounting shank 130n may include one or more recesses, which may accommodate securing the cutting tool assembly 100n to a base body (e.g., as described below in more detail). For example, the support block 110n may include a recess 160n that may accommodate a ring (e.g., a snap ring), a pin, or another expandable mechanical fastener or any other mechanical fastener that may secure the cutting tool assembly 100n to the base body.
Alternatively or additionally, the cutting tool assembly 100n may be secured to the base body with one or more fasteners.
In some embodiments, the cutting tool assembly 100n may be secured to the base body 300n with a fastener 400n. For example, the fastener 400n may secure the elongated mounting shank 130n of the cutting tool assembly 100n in the tool recess 310n of the base body 300n. As mentioned above, in an embodiment, the cutting tool mounting assembly 200n may include one or more fasteners (e.g., snap rings, pins, etc.) or other mechanical fasteners that may secure the cutting tool assembly 100n to and/or within the base body 300n. Furthermore, the cutting tool assembly 100n may be welded, brazed, or otherwise bonded and/or secured to the base body 300n. While in some embodiments the cutting tool assemblies described herein may be secured to a base body that is secured to the rotary drum of a material-removal machine, in one or more additional or alternative embodiment, any of the cutting tool assemblies described herein may be directly secured to the rotary drum of the material-removal machine.
As discussed above, the cutting tool assembly 100p may include a cutting element 120p that may have a generally planar, superhard working surface 121p. As the cutting tool assembly 100p advances in and/or fails material 50, the working surface 121p may have a suitable positive or negative rake angle or orientation, such as to facilitate clearing or moving the failed material away from the cutting element 120 and/or from the cutting tool assembly 100p. For example, rake angle 40p (illustrated as a negative rake angle) may be measured between an imaginary line 43p, which extends in a plane that is coplanar with the working surface 121p, and an imaginary line 41p, which extends from a center point 44p of rotation of the cutting tool assembly 100p to a point of intersection between the imaginary line 41p and a projected cut line 45p. The projected cut line 45p may be generally circular and may be defined by a path of a point or portion of the working surface 121 that is farthest from the center point 44p, as that farthest point moves about the center point 44p. In one or more embodiments, the magnitude of the rake angle 40p (negative or positive) may be in one or more of the following ranges: from about 5 degrees to about 15 degrees; from about 15 degrees to about 25 degrees, from about 25 degrees to about 40 degrees. Moreover, the rake angle 40p may be greater than about 40 degrees or less than about 5 degrees.
In some embodiments, the cutting element 120 may be positioned and/or oriented such as to form a clearance angle 60p between a lowest portion of the outer or peripheral surface (e.g., farthest away from center point 44p) and the projected cut line 45p. Note that while the projected cut line 45p may be generally circular, the circumference of the projected cut line 45p may be such that at the locations near the cutting element 120p (e.g., at a distance from the cutting element 120p that is equal to the 1×, 2×, 3×, etc., the size of the cutting element 120p) the projected cut line 45p may be approximated by a linear segment. In one or more embodiments, the clearance angle 60p may be in one or more of the following ranges, from about 5 degrees to about 15 degrees, from about 15 degrees to about 25 degrees, from about 25 degrees to about 40 degrees. Moreover, the clearance angle 60p may be greater than about 40 degrees or less than about 5 degrees.
In some embodiments, a portion of the working surface 121q may be generally conical. For example, the conical portion of the working surface 121q may form a clearance angle 60q with projected cut line 45q. In one or more embodiments, the clearance angle 60q may be in one or more of the following ranges, from about 5 degrees to about 15 degrees, from about 15 degrees to about 25 degrees, from about 25 degrees to about 40 degrees. Moreover, the clearance angle 60q may be greater than about 40 degrees or less than about 5 degrees.
Also, in at least one embodiment, the cutting tool assembly 100q may be angled relative to the material 50 and/or relative to the projected cut line 45q. For example, the cutting tool assembly 100q may be oriented such that an imaginary line extending through the center of the cutting element 120q is non-perpendicular relative to the projected cut line 45q and/or relative to an imaginary line that is substantially tangent to the projected cut line 45q. As mentioned above, the circumference of the imaginary cut line 45q may be sufficiently great, such that a segment of the projected cut line 45q, which is near the cutting element 120q, may be approximated as a linear segment.
In an embodiment, the rotary drum assembly 500 includes a drum body 510 that may have an outer surface 520, which may have a substantially cylindrical shape. It should be appreciated that the shape of the outer surface 520 may vary from one embodiment to the next. For example, the outer surface 520 may have oval or other non-cylindrical shapes. As described above, the base body 300 may be mounted on the outer surface 520 of the drum body 510 (e.g., the base body 300 may be welded to the drum body 510). In addition, the drum body 510 may be solid, hollow, or tubular (e.g., the drum body 510 may have a cored-out inner cavity or space). In any event, the drum body 510 may have sufficient strength and rigidity to secure the cutting tool mounting assemblies cutting tool mounting assembly 200 and to remove material, as may be suitable for a particular application.
Similarly, a cutting exterior of the rotary drum assembly 500, which may be formed or defined by the cutting tool mounting assemblies cutting tool mounting assembly 200, may have an approximate cylindrical shape. More specifically, superhard working surfaces of the cutting tool assemblies cutting tool assembly 100 (e.g., working surfaces of the cutting element 120 of the cutting tool assembly 100), collectively, may form an approximately cylindrical cutting exterior. It may be appreciated that the particular shape of the cutting exterior formed by the cutting tool assemblies cutting tool assembly 100 depend on the shape of the superhard working surfaces and on the orientation of the cutting tool assemblies cutting tool assembly 100 relative to the drum body 510, among other things.
Moreover, the cutting tool assemblies cutting tool assembly 100 have any number of suitable patterns and/or configurations on the drum body 510, which may vary from one embodiment to the next. For example, cutting tool assemblies cutting tool assembly 100 may form helical rows about the drum body 510, and such rows may wrap about the circumference of the drum body 510. In any event, the cutting exterior of the rotary drum assembly 500 may rotate about the center axis of the drum body 510 to cut, grind, or otherwise fail the target material by engaging the target material with the cutting tool assemblies cutting tool assembly 100.
Additionally, the helical arrangement may facilitate movement of the failed material between the cutting tool mounting assemblies cutting tool mounting assembly 200 and removal thereof from a worksite. Also, the rotary drum assembly 500 may include one or more paddles 530 (e.g., as shown in
In some instances, the rotation of the drum assembly 500 and movement of the material-removing machine 600 may produce conventional cutting motion, where cutting tool assemblies engage the target material in the same direction as the direction of the movement of the material-removal machine 600 (i.e., as shown in
In an embodiment, movement of the material-removal machine 600 together with the rotation of the drum assembly 500 may remove a portion of a pavement 20, thereby producing a cut surface 21. Removed pavement may be subsequently recycled. Additionally or alternatively, the material-removal machine 600 may remove material in any number of suitable applications, including above ground and underground mining.
It should be noted that any of the cutting tool assemblies and cutting tool mounting assemblies disclosed herein may be employed on other types of material removal systems besides the drum assembly 500 and the material-removal machine 600. For example, any of the cutting tool assemblies and cutting tool mounting assemblies disclosed herein may be employed on a long-wall material removal system or any material-removal system disclosed in U.S. Patent Application Nos. 62/030,525, the disclosure of which is incorporated herein, in its entirety, by this reference.
While various aspects and embodiments have been disclosed herein, other aspects and embodiments are contemplated. The various aspects and embodiments disclosed herein are for purposes of illustration and are not intended to be limiting. Additionally, the words “including,” “having,” and variants thereof (e.g., “includes” and “has”) as used herein, including the claims, shall be open ended and have the same meaning as the word “comprising” and variants thereof (e.g., “comprise” and “comprises”).
This application claims priority to U.S. Provisional Patent Application No. 62/232,732 filed 25 Sep. 2015, the disclosure of which is incorporated herein, in its entirety, by this reference.
Number | Name | Date | Kind |
---|---|---|---|
2665893 | Ball | Jan 1954 | A |
3342532 | Krekeler | Sep 1967 | A |
3544166 | Proctor | Dec 1970 | A |
3671075 | Bland et al. | Jun 1972 | A |
3695726 | Krekeler | Oct 1972 | A |
3751114 | Davis | Aug 1973 | A |
3785021 | Norgren et al. | Jan 1974 | A |
3841708 | Kniff | Oct 1974 | A |
D238243 | Polivka | Dec 1975 | S |
3958832 | Sigott et al. | May 1976 | A |
4006936 | Crabiel | Feb 1977 | A |
4083644 | Friedline et al. | Apr 1978 | A |
4140189 | Garner | Feb 1979 | A |
4193638 | Heckenhauer | Mar 1980 | A |
4200159 | Jurgens et al. | Apr 1980 | A |
4299424 | LeBegue et al. | Nov 1981 | A |
4303136 | Ball | Dec 1981 | A |
4335921 | Swisher et al. | Jun 1982 | A |
4337980 | Krekeler | Jul 1982 | A |
4340325 | Gowanlock et al. | Jul 1982 | A |
D270059 | Wilkins | Aug 1983 | S |
D271497 | Green | Nov 1983 | S |
4484644 | Cook et al. | Nov 1984 | A |
4580930 | Zinner et al. | Apr 1986 | A |
4605343 | Hibbs, Jr. et al. | Aug 1986 | A |
4655508 | Tomlinson | Apr 1987 | A |
4678237 | Collin | Jul 1987 | A |
4679858 | Tank | Jul 1987 | A |
D296107 | Andersson | Jun 1988 | S |
4765687 | Parrott | Aug 1988 | A |
4784023 | Dennis et al. | Nov 1988 | A |
4787466 | Tomlinson et al. | Nov 1988 | A |
4836178 | Tomlinson | Jun 1989 | A |
4850649 | Beach et al. | Jul 1989 | A |
4880278 | Tomlinson | Nov 1989 | A |
4902073 | Tomlinson et al. | Feb 1990 | A |
D307279 | Vincent | Apr 1990 | S |
4913125 | Bunting | Apr 1990 | A |
D311747 | Mihic | Oct 1990 | S |
5007685 | Beach et al. | Apr 1991 | A |
5060739 | Griffin et al. | Oct 1991 | A |
5090491 | Tibbitts et al. | Feb 1992 | A |
5318351 | Walker | Jun 1994 | A |
5378050 | Kammerer | Jan 1995 | A |
5417475 | Graham et al. | May 1995 | A |
5431239 | Tibbitts et al. | Jul 1995 | A |
5605382 | Massa et al. | Feb 1997 | A |
5649604 | Fuller et al. | Jul 1997 | A |
5690393 | Massa et al. | Nov 1997 | A |
5881830 | Cooley | Mar 1999 | A |
5906245 | Tibbitts et al. | May 1999 | A |
6089123 | Chow et al. | Jul 2000 | A |
6213931 | Twardowski et al. | Apr 2001 | B1 |
6283844 | Tank | Sep 2001 | B1 |
6485104 | Keller et al. | Nov 2002 | B1 |
6779850 | Schibeci et al. | Aug 2004 | B1 |
7108212 | Latham | Sep 2006 | B2 |
D558802 | Nicholas | Jan 2008 | S |
D616003 | Ueda et al. | May 2010 | S |
7866418 | Bertagnolli et al. | Jan 2011 | B2 |
7998573 | Qian et al. | Aug 2011 | B2 |
8034136 | Sani | Oct 2011 | B2 |
8047260 | Uno et al. | Nov 2011 | B2 |
8079785 | Nicholas | Dec 2011 | B2 |
8236074 | Bertagnolli et al. | Aug 2012 | B1 |
D666640 | Cox et al. | Sep 2012 | S |
8567533 | Myers et al. | Oct 2013 | B2 |
8672415 | Neilson et al. | May 2014 | B2 |
8727044 | Qian et al. | May 2014 | B2 |
8789894 | Claesson et al. | Jul 2014 | B2 |
9017438 | Miess et al. | Apr 2015 | B1 |
9027675 | Jones et al. | May 2015 | B1 |
9028008 | Bookhamner et al. | May 2015 | B1 |
9238893 | Latham et al. | Jan 2016 | B2 |
9272392 | Mukhopadhyay et al. | Mar 2016 | B2 |
9272814 | Carver et al. | Mar 2016 | B2 |
9303511 | George et al. | Apr 2016 | B2 |
9382794 | Latham et al. | Jul 2016 | B2 |
9434091 | Burton et al. | Sep 2016 | B2 |
9487847 | Mukhopadhyay et al. | Nov 2016 | B2 |
9593577 | Ries et al. | Mar 2017 | B2 |
D809031 | Burton | Jan 2018 | S |
10018041 | Wachsmann et al. | Jul 2018 | B2 |
10323514 | Burton et al. | Jun 2019 | B2 |
10408057 | Myers et al. | Sep 2019 | B1 |
20010040053 | Beuershausen et al. | Nov 2001 | A1 |
20020153175 | Ojanen et al. | Oct 2002 | A1 |
20030234569 | Dawood et al. | Dec 2003 | A1 |
20050082898 | Keller et al. | Apr 2005 | A1 |
20060033379 | Frear et al. | Feb 2006 | A1 |
20060087169 | Hesse et al. | Apr 2006 | A1 |
20070090679 | Ojanen et al. | Apr 2007 | A1 |
20080030065 | Frear et al. | Feb 2008 | A1 |
20080035383 | Hall | Feb 2008 | A1 |
20080036280 | Hall et al. | Feb 2008 | A1 |
20080202819 | Fader | Aug 2008 | A1 |
20080250724 | Hall et al. | Oct 2008 | A1 |
20080309146 | Hall et al. | Dec 2008 | A1 |
20100052406 | Beach et al. | Mar 2010 | A1 |
20100194176 | Lucek et al. | Aug 2010 | A1 |
20100244545 | Hall et al. | Sep 2010 | A1 |
20100326741 | Patel | Dec 2010 | A1 |
20110132667 | Smallman et al. | Jun 2011 | A1 |
20110148178 | Lehnert | Jun 2011 | A1 |
20110233987 | Maushart et al. | Sep 2011 | A1 |
20110266070 | Scott et al. | Nov 2011 | A1 |
20120043138 | Myers et al. | Feb 2012 | A1 |
20120138370 | Mukhopadhyay | Jun 2012 | A1 |
20120160573 | Myers et al. | Jun 2012 | A1 |
20120175939 | O'Neill et al. | Jul 2012 | A1 |
20120274123 | Ball | Nov 2012 | A1 |
20120279786 | Cox | Nov 2012 | A1 |
20130052481 | Konyashin | Feb 2013 | A1 |
20130092451 | Mukhopadhyay | Apr 2013 | A1 |
20130092452 | Mukhopadhyay et al. | Apr 2013 | A1 |
20130322975 | Tan et al. | Dec 2013 | A1 |
20140110991 | Sollami | Apr 2014 | A1 |
20140175853 | Warren | Jun 2014 | A1 |
20140225418 | Lachmann et al. | Aug 2014 | A1 |
20140240634 | Matsuzaki | Aug 2014 | A1 |
20140339879 | Burton et al. | Nov 2014 | A1 |
20140339883 | Burton et al. | Nov 2014 | A1 |
20150035342 | Jonker | Feb 2015 | A1 |
20150114727 | Heuser | Apr 2015 | A1 |
20150176408 | Latham | Jun 2015 | A1 |
20150176409 | Latham | Jun 2015 | A1 |
20150240635 | Lachmann et al. | Aug 2015 | A1 |
20150314483 | Miess et al. | Nov 2015 | A1 |
20160102550 | Swope et al. | Apr 2016 | A1 |
20160273356 | Ojanen et al. | Sep 2016 | A1 |
20160332269 | Prezlock et al. | Nov 2016 | A1 |
Number | Date | Country |
---|---|---|
2013101370 | Nov 2013 | AU |
102108866 | Jun 2011 | CN |
202073564 | Dec 2011 | CN |
203081445 | Jul 2013 | CN |
1481278 | Jul 1977 | GB |
2170843 | Aug 1986 | GB |
2177144 | Jan 1987 | GB |
2193740 | Feb 1988 | GB |
WO 2010083015 | Jul 2010 | WO |
WO 2012130870 | Oct 2012 | WO |
WO 2016071001 | May 2016 | WO |
Entry |
---|
Advisory Action received for U.S. Appl. No. 14/266,437 dated Mar. 24, 2017. |
Non-Final Office Action for U.S. Appl. No. 14/266,437 dated Apr. 21, 2017. |
Non-Final Office Action received for U.S. Appl. No. 14/275,574 dated Apr. 7, 2017. |
Non-Final Office Action for U.S. Appl. No. 29/555,279 dated Mar. 24, 2017. |
Notice of Allowance received for U.S. Appl. No. 29/555,269 dated Apr. 6, 2017. |
Notice of Allowance received for U.S. Appl. No. 29/555,281 dated Apr. 12, 2017. |
Supplemental Notice of Allowance for U.S. Appl. No. 29/555,269 dated Apr. 28, 2017. |
Notice of Allowance for U.S. Appl. No. 29/540,584 dated May 8, 2017. |
Notice of Allowance for U.S. Appl. No. 29/540,597 dated May 8, 2017. |
Supplemental Notice of Allowance for U.S. Appl. No. 29/540,597 dated Jun. 1, 2017. |
U.S. Appl. No. 12/961,787, filed Dec. 7, 2010, Mukhopadhyay et al. |
U.S. Appl. No. 13/027,954, filed Feb. 15, 2011, Miess et al. |
U.S. Appl. No. 13/070,636, filed Mar. 24, 2011, Qian et al. |
U.S. Appl. No. 13/100,388, filed May 4, 2011, Jones et al. |
U.S. Appl. No. 13/275,372, filed Oct. 18, 2011, Mukhopadhyay et al. |
U.S. Appl. No. 13/648,913, filed Oct. 10, 2012, Mukhopadhyay et al. |
U.S. Appl. No. 13/765,027, filed Feb. 12, 2013, Carver, et al. |
U.S. Appl. No. 13/795,027, filed Mar. 12, 2013, Mukhopadhyay et al. |
U.S. Appl. No. 61/824,022, filed May 16, 2013, Burton et al. |
U.S. Appl. No. 61/824,007, filed May 16, 2013, Burton et al. |
U.S. Appl. No. 14/266,437, filed Apr. 30, 2014, Miess et al. |
U.S. Appl. No. 14/273,360, filed May 8, 2014, Burton et al. |
U.S. Appl. No. 14/275,574, filed May 12, 2014, Burton et al. |
U.S. Appl. No. 62/030,525, filed Jul. 29, 2014, Myers et al. |
U.S. Appl. No. 14/811,699, filed Jul. 28, 2015, Myers et al. |
U.S. Appl. No. 62/232,732, filed Sep. 25, 2015, Weaver et al. |
U.S. Appl. No. 29/540,584, filed Sep. 25, 2015, Weaver. |
U.S. Appl. No. 29/540,597, filed Sep. 25, 2015, Weaver. |
U.S. Appl. No. 29/555,269, filed Feb. 19, 2016, Burton. |
U.S. Appl. No. 29/555,279, filed Feb. 19, 2016, Burton. |
U.S. Appl. No. 29/555,281, filed Feb. 19, 2016, Burton. |
International Search Report and Written Opinion from International Application No. PCT/US2014/037708 dated Oct. 30, 2014. |
International Search Report and Written Opinion from International Application No. PCT/US2014/037381 dated Oct. 30, 2014. |
International Search Report and Written Opinion for International Application No. PCT/US2015/027830 dated Jul. 14, 2015. |
Roepke et al.; “Drag Bit Cutting Characteristics Using Sintered Diamond Inserts” Report of Investigations 8802; Bureau of Mines Report of Investigations/ 1983; (1983) 35 pages. |
U.S. Appl. No. 14/273,360, Jun. 12, 2015, Restriction Requirement. |
U.S. Appl. No. 14/273,360, Oct. 22, 2015, Office Action. |
U.S. Appl. No. 14/273,360, Mar. 7, 2016, Office Action. |
U.S. Appl. No. 14/273,360, May 18, 2016, Notice of Allowance. |
U.S. Appl. No. 14/273,360, Aug. 10, 2016, Supplemental Notice of Allowance. |
Final Office Action for U.S. Appl. No. 14/266,437 dated Dec. 12, 2016. |
Final Office Action for U.S. Appl. No. 14/275,574 dated Nov. 29, 2016. |
Issue Notification for U.S. Appl. No. 14/273,360 dated Aug. 17, 2016. |
Non-Final Office Action for U. S. Appl. No. 14/266,437 dated Jun. 9, 2016. |
U.S. Appl. No. 13/070,636, filed Mar. 24, 2011. |
U.S. Appl. No. 15/238,486, filed Aug. 16, 2016. |
U.S. Appl. No. 61/824,022, filed May 16, 2013. |
Non-Final Office Action for U.S. Appl. No. 14/275,574 dated Apr. 6, 2016. |
Advisory Action received for U.S. Appl. No. 14/275,574 dated Mar. 9, 2017. |
Final Office Action for U.S. Appl. No. 14/266,437 dated Nov. 15, 2017. |
Final Office Action for U.S. Appl. No. 15/238,486 dated Feb. 26, 2018. |
Issue Notification for U.S. Appl. No. 29/540,584 dated Sep. 14, 2017. |
Issue Notification for U.S. Appl. No. 29/540,597 dated Sep. 6, 2017. |
Issue Notification for U.S. Appl. No. 29/555,279 dated Jan. 10, 2018. |
Non-Final Office Action for U.S. Appl. No. 14/266,437 dated Mar. 28, 2018. |
Non-Final Office Action for U.S. Appl. No. 14/811,699 dated Nov. 29, 2017. |
Non-Final Office Action for U.S. Appl. No. 15/238,486 dated Aug. 17, 2017. |
Notice of Allowance for U.S. Appl. No. 14/275,574 dated Jan. 24, 2018. |
Notice of Allowance for U.S. Appl. No. 14/275,574 dated Sep. 26, 2017. |
Notice of Allowance for U.S. Appl. No. 29/555,279 dated Aug. 31, 2017. |
Notice of Allowance for U.S. Appl. No. 29/555,281 dated Jan. 4, 2018. |
Supplemental Notice of Allowability for U.S. Appl. No. 29/555,279 dated Jan. 2, 2018. |
Supplemental Notice of Allowance for U.S. Appl. No. 29/540,584 dated Sep. 7, 2017. |
Supplemental Notice of Allowance for U.S. Appl. No. 29/540,597 dated Aug. 25, 2017. |
Supplemental Notice of Allowance for U.S. Appl. No. 29/555,281 dated Feb. 9, 2018. |
Supplemental Notice of Allowance for U.S. Appl. No. 29/555,281 dated Jun. 12, 2017. |
Final Office Action for U.S. Appl. No. 14/266,437 dated Sep. 18, 2018. |
Final Office Action for U.S. Appl. No. 14/811,699 dated Jul. 10, 2018. |
Issue Notification for U.S. Appl. No. 29/555,281 dated Aug. 29, 2018. |
Notice of Allowance for U.S. Appl. No. 14/275,574 dated Jun. 15, 2018. |
Notice of Allowance for U.S. Appl. No. 14/275,574 dated Oct. 11, 2018. |
Notice of Allowance for U.S. Appl. No. 15/238,486 dated Oct. 10, 2018. |
Notice of Allowance for U.S. Appl. No. 15/238,486 dated Jun. 20, 2018. |
Notice of Allowance for U.S. Appl. No. 29/555,281 dated May 16, 2018. |
Supplemental Notice of Allowance for U.S. Appl. No. 15/238,486 dated Jun. 27, 2018. |
Supplemental Notice of Allowance for U.S. Appl. No. 29/555,281 dated Jun. 4, 2018. |
U.S. Appl. No. 14/275,574, filed May 12, 2014. |
Advisory Action for U.S. Appl. No. 14/811,699 dated Oct. 22, 2018. |
Non-Final Office Action for U.S. Appl. No. 14/266,437 dated Jan. 8, 2019. |
Non-Final Office Action for U.S. Appl. No. 14/811,699 dated Jan. 4, 2019. |
Supplemental Notice of Allowability for U.S. Appl. No. 14/275,574 dated Oct. 31, 2018. |
Notice of Allowance for U.S. Appl. No. 15/238,486 dated Jan. 28, 2019. |
Notice of Allowance for U.S. Appl. No. 14/275,574 dated Feb. 12, 2019. |
Issue Notification for U.S. Appl. No. 14/275,574 dated May 29, 2019. |
Issue Notification for U.S. Appl. No. 15/238,486 dated May 22, 2019. |
Non-Final Office Action for U.S. Appl. No. 16/406,673 dated Jun. 27, 2019. |
Notice of Allowance for U.S. Appl. No. 14/266,437 dated May 2, 2019. |
Notice of Allowance for U.S. Appl. No. 14/811,699 dated May 1, 2019. |
Notice of Allowance for U.S. Appl. No. 29/660,512 dated Apr. 25, 2019. |
Supplemental Notice of Allowance for U.S. Appl. No. 14/275,574 dated May 21, 2019. |
U.S. Appl. No. 16/406,673, filed May 8, 2019. |
U.S. Appl. No. 16/527,620, filed Jul. 31, 2019. |
Issue Notification for U.S. Appl. No. 14/266,437 dated Aug. 28, 2019. |
Issue Notification for U.S. Appl. No. 14/811,699 dated Aug. 21, 2019. |
Issue Notification for U.S. Appl. No. 29/660,512 dated Aug. 28, 2019. |
Non-Final Office Action for U.S. Appl. No. 16/526,387, dated Oct. 4, 2019. |
Non-Final Office Action for U.S. Appl. No. 16/527,620, dated Oct. 2, 2019. |
Supplemental Notice of Allowability for U.S. Appl. No. 14/266,437 dated Aug. 19, 2019. |
Advisory Action for U.S. Appl. No. 16/406,673 dated Mar. 6, 2020. |
Final Office Action for U.S. Appl. No. 16/527,620 dated Mar. 12, 2020. |
Number | Date | Country | |
---|---|---|---|
62232732 | Sep 2015 | US |