Patent Application
20110011965
1. Field of the Technology
The present disclosure is directed to rolls used for high pressure comminution of granular materials such as, for example, minerals and ores in high pressure grinding mills. More specifically, the disclosure is directed to articles adapted for use as wear resistant working surfaces of rolls and to methods of making the articles and rolls including the articles.
2. Description of the Background of the Technology
The comminution of granular materials such as, for example, minerals and ores, is often carried out between rolls in a high pressure grinding mill. High pressure grinding mills typically utilize a pair of opposed counter-rotating grinding rolls. The rotation axis of one of the grinding rolls is fixed, and the rotation axis of the second roll is floating. A hydraulic system connected to the floating roll controls the position of the floating roll relative to the fixed roll, providing pressure between the rolls and an adjustable grinding force on material passing between the rolls. The rotational speed of the rolls is also adjustable to optimize the grinding conditions. By controlling the gap between the rolls, the speed of the rolls, and the applied force, the ore or other materials passing between the rolls can be crushed in an efficient manner with relatively low energy input.
During high pressure grinding of granular materials, the material to be ground is fed into the gap between the rolls. The gap is referred to as the “nip”, and also may be referred to as the “roll gap”. The grinding of ore passing into the nip, for example, occurs by a mechanism of inter-particle breakage caused by the very high pressures developed within the material stream as it passes between the counter-rotating rolls. In addition, ore ground in this way exhibits cracks in the ore grains, which is beneficial to downstream processing of the ore.
As can be expected, the grinding operation exerts very high levels of mechanical stress on the grinding rolls of high pressure grinding apparatuses, and the grinding rolls may quickly wear.
One known approach to improve the wear resistance of a roll surface is by welding layers of hard metallic material onto the surface.
Another known approach to improve wear resistance of a grinding roll surface is by providing hard regions that project from the working surface of the roll.
U.S. Pat. Nos. 5,203,513 and 7,497,396 disclose rolls adapted for use in high pressure grinding mills and that include hard projections with gaps therebetween. As with the prior art roll depicted in
U.S. Pat. Nos. 6,086,003 and 5,755,033 also disclose rolls adapted for use in high pressure grinding mills that include hard projections and gaps between the projections. The method described in the '003 and '033 patents to fabricate the grinding rolls involves embedding hard bodies within a mass of metallic powder and consolidating the powder by hot isotactic pressing.
The methods for fabricating wear resistant high pressure rolls described in the above-identified patents are costly and tedious. For example, the use of a welding process to secure hard elements to a roll surface limits the range of materials from which the hard elements can be fabricated. Hot isotactic pressing of a large roll requires the use of expensive equipment, and a grinding roll fabricated by hot isotactic pressing cannot be repaired easily in the field.
Accordingly, there is a need for articles and methods improving the wear resistance of the working surface of grinding rolls. It is desirable that such articles and methods require relatively inexpensive equipment; allow a wide range of materials to be used as the projecting hard elements; permit tailoring of the base material used in the grinding roll; and permit easy repair of the roll surface in the field.
According to one non-limiting aspect of the present disclosure, an article in the form of one of a plate, a sheet, a cylinder, and a portion of a cylinder, the article adapted for use as at least a portion of a wear resistant working surface of a roll, the article comprises a metal matrix composite comprising a plurality of inorganic particles dispersed in a matrix material comprising at least one of a metal and a metal alloy The melting temperature of the inorganic particles is greater than a melting temperature of the matrix material. A plurality of hard elements is interspersed in the metal matrix composite. In a non-limiting embodiment a wear resistance of the metal matrix composite is less than a wear resistance of the hard elements and the metal matrix composite may preferentially wear away when the article is in use, thereby providing or preserving a gap between each of the plurality of hard elements at a working surface of the article.
In a non-limiting embodiment, a method of making an article adapted for use as a wear resistant working surface of a roll includes positioning a plurality of hard elements in predetermined positions on a bottom surface of a mold. Each of the hard elements comprises a first end and an opposed second end. A substantially equidistance exists between the first end and the opposed second end. The opposed second end of each of the hard elements rests on the bottom surface of the mold, so as to partially fill a void space of the mold and defines an unoccupied volume in the mold. Inorganic particles may be added to the mold to at least partially fill the unoccupied volume and provide a remainder space between the inorganic particles and between the inorganic particles and the hard elements. A non-limiting embodiment includes heating the plurality of hard elements and the inorganic particles to an infiltrating temperature. The remainder space may be infiltrated with a matrix material comprising at least one of a molten metal and a molten metal alloy that has a melting temperature that is less than a melting temperature of the inorganic particles. The matrix material disposed in the remainder space is to solidify the matrix material and bind the hard elements and the inorganic particles in the article.
A certain aspect of the disclosure includes a grinding roll for the comminution of granular materials. In a non-limiting embodiment, a grinding roll may comprise a cylindrical core comprising an external surface, and at least one wear resistant article adapted for use as a wear resistant working surface of the grinding roll, which is removably attached to the external surface of the cylindrical core. The article may include a metal matrix composite comprising a plurality of inorganic particles dispersed in a matrix material comprising at least one of a metal and a metal alloy, and a plurality of hard elements interspersed in the metal matrix composite. The wear resistance of the metal matrix composite may be less than a wear resistance of the hard elements, and the metal matrix composite may preferentially wear away when the grinding roll is in use, thereby providing or preserving a gap between each of the plurality of hard elements at a surface of the article.
A method of one of manufacturing or maintaining a grinding roll may include providing a cylindrical core comprising a external surface, and removably attaching an embodiment of a wear resistant article disclosed herein to the external surface of the cylindrical core.
The features and advantages of articles and methods described herein may be better understood by reference to the accompanying drawings in which:
The reader will appreciate the foregoing details, as well as others, upon considering the following detailed description of certain non-limiting embodiments according to the present disclosure.
In the present description of non-limiting embodiments, other than in the operating examples or where otherwise indicated, all numbers expressing quantities or characteristics are to be understood as being modified in all instances by the term “about”. Accordingly, unless indicated to the contrary, any numerical parameters set forth in the following description are approximations that may vary depending on the desired properties one seeks to obtain in the parts and methods according to the present disclosure. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter described in the present description should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques.
Any patent, publication, or other disclosure material, in whole or in part, that is said to be incorporated by reference herein is incorporated herein only to the extent that the incorporated material does not conflict with existing definitions, statements, or other disclosure material set forth in this disclosure. As such, and to the extent necessary, the disclosure as set forth herein supersedes any conflicting material incorporated herein by reference. Any material, or portion thereof, that is said to be incorporated by reference herein, but which conflicts with existing definitions, statements, or other disclosure material set forth herein is only incorporated to the extent that no conflict arises between that incorporated material and the existing disclosure material.
According to an aspect of this disclosure,
Referring to
A plurality of hard elements 24 are interspersed within the article 20. In an embodiment, the wear resistance of the metal matrix composite 21 is less than the wear resistance of the hard elements 24. In such case, as shown in
In certain non-limiting embodiments, each of the hard elements may comprise at least one of a high hardness metal, a high hardness metal alloy, a sintered cemented carbide, and a ceramic material. The terms “high hardness metal” and “high hardness metal alloy” are defined herein as a wear resistant metal or metal alloy, respectively, having a bulk hardness equal to or greater than 40 HRC, as determined by the Rockwell hardness test, and measured according to the Rockwell C scale. In another non-limiting embodiment, the bulk hardness of the high hardness metal or high hardness metal alloy may be equal or greater than 45 HRC, as determined by the Rockwell hardness test. Examples of high hardness metal alloys include, but are not limited to, tool steels. In embodiments wherein the hard elements 24 comprise a ceramic material, the ceramic material is a wear resistant ceramic material and may be selected from, but is not limited to, the group of ceramic material including silicon nitride and aluminum oxide reinforced with silicon carbide whiskers.
In another non-limiting embodiment, one or more of the hard elements 24 may include a sintered cemented carbide. Non-limiting examples of sintered cemented carbides that may be used for the hard elements disclosed herein are cemented carbides comprising particles of at least one carbide of a Group IVB, a Group VB, and a Group VIB metal of the Periodic Table dispersed in a continuous binder comprising at least one of cobalt, a cobalt alloy, nickel, a nickel alloy, iron, and an iron alloy. Those skilled in the art are familiar with grades of cemented carbide powders that, when processed, provide sintered cemented carbides having high strength and wear resistance, and the sintered cemented carbides produced from such grades may be used to form certain non-limiting embodiments of the hard elements 24 disclosed herein. Exemplary grades of cemented carbide powders useful in preparing sintered cemented carbide hard elements 24 that may be used in non-limiting embodiments of wear resistant articles according to the present disclosure include, but are not limited to, Grade AF63 and Grade 231 available from ATI Firth Sterling, Madison, Ala.
In certain non-limiting embodiments according to the present disclosure, the hard elements are positioned and spaced apart in a predetermined pattern. In certain non-limiting embodiments, the pattern of hard elements may be periodic and conform to a regular lattice-type structure, or may be in irregular or aperiodic arrangements, which do not conform to a regular lattice structure. A non-limiting embodiment of a pattern of a periodic arrangement of hard elements that may be used in an article according to the present disclosure is depicted in
For the efficient and economical operation of high pressure grinding mills, for example, the working surface of the rolls must be resistant to wear and abrasion and must efficiently draw the material to be comminuted into the nip. Referring again to
Any of the shape of the hard elements 24, the average distance between adjacent hard elements 24, i.e., the average gap distance, and the average size of the hard elements 24 of the article 20 can be varied to impart different characteristics to the working surface of a grinding roll and thereby influence the comminution process. In addition, the gaps 25 between the hard elements 24 collect fine particles, i.e., ground fines, which provide a protective surface over the matrix material 23. The ground fines collected in the gaps 25 provide an exposed surface that is rougher than the any exposed surface of the hard elements 24, and thereby serve to provide areas of higher friction, which aids in drawing the material to be comminuted (ground) into the nip. If the gaps 25 are too small, the fines will tend not to accumulate in the gaps. If the gaps 25 are too large, a compact cake of the fines will not form in the gaps 25. In the non-limiting embodiment depicted in
In one non-limiting exemplary embodiment of an article 20 according to the present disclosure adapted for use as a wear resistant working surface of a roll, the pattern of the hard elements 24 may be similar to the pattern schematically depicted in
It will be understood that the hard elements 24 may be in a form different from a cylinder and/or have ends that are non-planar, and that the hard elements 24 may not be of a uniform shape. For example, in certain embodiments the hard elements may be in the shape of a cube or a cuboid, wherein the values for the average hard element diameters provided above may be, for example, the average diagonal or average edge length of a face of the cube or cuboid. A person skilled in the art will understand that hard elements 24 having other three-dimensional shapes are within the scope of embodiments disclosed herein, so long as a plurality of gaps 25 are provided between a plurality of the hard elements 24, either initially or, as discussed herein below, through preferential wear of the metal matrix composite when the article is in use.
According to one non-limiting embodiment, the hard elements 24 comprise 25% to 95% of a projected surface area of the surface of the article 20. In other non-limiting embodiments, the hard elements 24 comprise 40% to 90%, or 50% to 80% of the projected surface area. It will be understood, however, that the hard elements may comprise any fraction of the projected surface area of the hard elements suitable for the intended application of the article 20. The term “projected surface area” is defined herein as the two dimensional projection of the total surface area of the metal matrix composite 21 exposed at the working surface 26 of the article 20 and the total surface area of the first ends 27 of the hard elements 24 (discussed below) exposed at the working surface 26.
Referring to
Referring to
In a non-limiting embodiment, the first end 27 and the opposed second end 28 of a hard element 24 are substantially planar and substantially parallel to each other. In one non-limiting embodiment, each of the hard elements 24 comprises a cylindrical shape and the first end 27 and the opposed second end 28 of a hard element 24 are substantially planar and substantially parallel to each other. In yet another non-limiting embodiment, each of the hard elements 24 comprises a cylindrical shape and the first end 27 and the opposed second end 28 of each hard element 24 exhibits a curvature. In still another non-limiting embodiment, each of the hard elements 24 comprises a cylindrical shape and one of the first end 27 and the opposed second end 28 is substantially planar, while the other of the first end 27 and the opposed second end 28 exhibits a curvature.
According to a non-limiting aspect of this disclosure, certain embodiments of the metal matrix composite 21 comprise inorganic particles 22 having an average particle size ranging from 0.5 μm to 250 μm. In other non-limiting embodiments, the inorganic particles 22 may have an average particle size ranging from 2 μm to 200 μm. In the various embodiments, the metal matrix composite 21 binds the hard elements 24 into the article 20.
In certain non-limiting embodiments according to the present disclosure, the inorganic particles 22 of the metal matrix composite 21 may comprise at least one of a metal powder and a metal alloy powder. In certain non-limiting embodiments, the metal or metal alloy powder of the metal matrix composite 21 comprises at least one of tungsten, a tungsten alloy, tantalum, a tantalum alloy, molybdenum, a molybdenum alloy, niobium, a niobium alloy, iron, an iron alloy, titanium, a titanium alloy, nickel, a nickel alloy, cobalt, and a cobalt alloy.
In another non-limiting embodiment according to the present disclosure, the inorganic particles 22 of the metal matrix composite 21 may comprise hard particles. The term “hard particles” is defined herein as inorganic particles exhibiting a hardness of at least 60 HRC, as measured by the Rockwell hardness test using scale C. A non-limiting embodiment of the metal matrix composite 21 includes inorganic particles 22 comprising at least one of a carbide, a boride, an oxide, a nitride, a silicide, a sintered cemented carbide, a synthetic diamond, and a natural diamond. In yet another non-limiting embodiment, the inorganic particles 21 comprise at least one of: a carbide of a metal selected from Groups IVB, VB, and VIB of the Periodic Table of the Elements; tungsten carbide; and cast tungsten carbide.
As noted above, the matrix material 23 of certain non-limiting embodiments comprises at least one of a metal and a metal alloy. In a non-limiting embodiment, the matrix material 23 includes at least one of copper, a copper alloy, aluminum, an aluminum alloy, iron, an iron alloy, nickel, a nickel alloy, cobalt, a cobalt alloy, titanium, a titanium alloy, a bronze alloy, and a brass alloy. In one non-limiting embodiment, the matrix material 23 is a bronze alloy consisting essentially of 78 weight percent copper, 10 weight percent nickel, 6 weight percent manganese, 6 weight percent tin, and incidental impurities. In another non-limiting embodiment, the matrix material consists essentially of 53 weight percent copper, 24 weight percent manganese, 15 weight percent nickel, 8 weight percent zinc, and incidental impurities. In non-limiting embodiments, the matrix material 23 may include up to 10 weight percent of an element that will reduce the melting point of the matrix material, such as, but not limited to at least one of boron, silicon, and chromium.
A non-limiting aspect of the article 20 according to the present disclosure includes providing the article 20 with at least one machinable region 29. In certain non-limiting embodiments, a machinable region 29 may comprise a region of metal or metal alloy joined to the article 20 by the metal matrix composite 21. Non-limiting embodiments of a machinable region 29 may include a metal or a metal alloy comprising at least one of iron, an iron alloy, nickel, a nickel alloy, cobalt, a cobalt alloy, copper, a copper alloy, aluminum, an aluminum alloy, tantalum, and a tantalum alloy. In yet other non-limiting embodiments, a machinable region 29 of the article 20 may include particles of a machinable metal joined together by the matrix material 23 included in the metal matrix composite 21. In certain non-limiting embodiments, the particles of a machinable metal included in the machinable region 29 may include at least one of iron, an iron alloy, nickel, a nickel alloy, cobalt, a cobalt alloy, copper, a copper alloy, aluminum, an aluminum alloy, tantalum, and a tantalum alloy. A machinable region 29 of the article 20 may be adapted for fixturing (i.e., connecting) the article 20 to a peripheral surface of a roll (see
One non-limiting embodiment of a method of making an article adapted for use as a wear resistant working surface of a roll, such as, for example, article 20, is depicted in the flow diagram of
The mold 51 may be machined from graphite or any other suitable chemically inert material that can withstand the processing temperatures of the methods disclosed herein without significantly warping or otherwise degrading. The mold 51 may be adapted to form a part that is in the shape of a plate, a sheet, a cylinder, a portion of a cylinder, or any other shape suitable to form all or a portion of a wear resistant working surface of a roll when fixtured to the roll. A plate mold or a sheet mold, for example, typically includes a mold cavity including a substantially planar bottom surface and four upward extending sidewalls.
A mold cavity of a mold adapted to form a cylindrical part or a part in the shape of a portion of a cylinder according to the present disclosure may include a bottom surface that conforms to the curvature of all or a portion of the cylindrical peripheral surface of a roll. A non-limiting embodiment of a mold 51 that may be used to form an article 20 having a curved surface is schematically depicted in
Although the foregoing embodiment utilizes a mold 51 having curved surfaces in the mold cavity to make a curved article, it will be understood that non-limiting embodiments of an article according to the present disclosure also may be made in flat forms, such as plates or sheets. For example, in certain non-limiting embodiments, the metal matrix composite 21 is ductile, and a wear resistant article 20 in the form of a plate or other flat form may be hot worked or otherwise suitably processed to provide a curvature to the article 20 that matches the curvature of the peripheral surface of a roll to which the article is to be attached.
The bottom surface 50 of a mold 51 used to form a wear resistant part according to the present disclosure may be further machined to accommodate the contours or shapes of the opposed second ends 28 of the hard elements 24 that are disposed in the mold cavity of the mold 51 and form regions of the part made using the mold 51. Also, machining contours or shapes in the mold may aid in positioning the hard elements 24. For example, the bottom surface 50 of a mold 51 may be machined to include contours such as, but not limited to, dimples to accommodate corresponding curved opposed second ends 28 of hard elements 24.
Following is a description of additional details of certain non-limiting embodiments of methods of making wear resistant articles according to the present disclosure, which will be better understood by reference to
In one non-limiting embodiment of a method of making an article 20 according to the present disclosure, comprises positioning 41 in the mold cavity each of the hard elements 24, wherein the hard elements 24 each comprise a first end 27 and an opposed second end 28 and the distance between the ends 27 and 28 of each hard element 24 is the same or approximately the same (i.e., the ends 27 and 28 are substantially equidistant). In certain non-limiting embodiments of a method according to the present disclosure, the opposed second end 28 of each of the hard elements 24 rests on the bottom surface 50 of the mold cavity of the mold 51, so as to partially fill a void space in the mold cavity and thereby define an unoccupied volume 52 in the mold cavity, that is, the volume in the mold cavity that is not occupied by the hard elements 24.
Another aspect of a non-limiting embodiment of a method according to the present disclosure comprises adding 42 inorganic particles 22 to the mold cavity of the mold 30. The addition of inorganic particles 22 at least partially fills the unoccupied volume 52 and provides a remainder space (56 in the blown up section of
In a non-limiting embodiment, the plurality of hard elements 24 and the inorganic particles 22 disposed in the mold cavity of the mold 51 are heated 43 to an infiltrating temperature (defined below). Heating 43 can be achieved by heating the mold 51 containing the plurality of hard elements 24 and the inorganic particles 22 in a convection furnace, a vacuum furnace, or an induction furnace, by another induction heating technique, or by another suitable heating technique known to those having ordinary skill in the art. In certain embodiments, the heating can be conducted in atmospheric air, in an inert gas, or under vacuum.
Following heating 43, the remainder space 56 is infiltrated 44 with a matrix material 23 comprising at least one of a molten metal and a molten metal alloy that has a melting temperature that is less than a melting temperature of the inorganic particles 22. Infiltrating 44 the remainder space 56 is accomplished at the infiltrating temperature mentioned hereinabove. Thus, it will be understood that the infiltrating temperature is a temperature that is at least the melting temperature of the matrix material 23 that is infiltrated into the remainder space 56, but that is less than the melting temperature of the inorganic particles 22. In certain non-limiting embodiments, an infiltration temperature may range from 700° C. (1292° F.) for low melting temperature metals and alloys such as, for example, aluminum and aluminum alloys, to 1300° C. (2372° F.) for higher melting temperature metals and alloys such as, for example, copper, nickel, iron, cobalt, and alloys of any of these metals.
A further step of a non-limiting embodiment of a method according to the present disclosure includes cooling 45 the matrix material 23 disposed in the remainder space 56 to solidify the matrix material 23 and bind the hard elements 24 and the inorganic particles 22 in the article 20.
In certain non-limiting embodiments, positioning 41 the hard elements 24 comprises positioning 41 hard elements 24 that comprise at least one of a high hardness metal, a high hardness metal alloy, a sintered cemented carbide, and a ceramic. In yet another non-limiting embodiment, each of the hard elements 24 comprises a sintered carbide comprising particles of at least one carbide of a Group IVB, a Group VB, or a Group VIB metal of the Periodic Table of the Elements dispersed in a continuous binder comprising at least one of cobalt, a cobalt alloy, nickel, a nickel alloy, iron, and an iron alloy.
Adding 42 the inorganic particles 22 may include but is not limited to adding particles of a metal powder or a metal powder alloy. The metal powder or metal alloy powder may comprise at least one of tungsten, a tungsten alloy, tantalum, a tantalum alloy, molybdenum, a molybdenum alloy, niobium, a niobium alloy, iron, an iron alloy, titanium, a titanium alloy, nickel, a nickel alloy, cobalt, and a cobalt alloy.
In another non-limiting embodiment, adding 42 the inorganic particles 22 may include, but are not limited to, adding hard particles. Hard particles may include, but is not limited to, particles comprising at least one of a carbide of a metal selected from Groups IVB, VB, and VIB of the Periodic Table of the Elements; tungsten carbide, and cast tungsten carbide.
Infiltrating 44 with a matrix material 23 may include infiltrating into the remainder space a metal or metal alloy that has a melting temperature that is less than the melting temperature of the inorganic particles 22. The matrix material 23 may include, but is not limited to, at least one of copper, a copper alloy, aluminum, an aluminum alloy, iron, an iron alloy, nickel, a nickel alloy, cobalt, a cobalt alloy, titanium, a titanium alloy, a bronze alloy, and a brass alloy. In one non-limiting embodiment, the matrix material is a bronze alloy consisting essentially of 78 weight percent copper, 10 weight percent nickel, 6 weight percent manganese, 6 weight percent tin, and incidental impurities. In another non-limiting embodiment, the matrix material 23 consists essentially of 53 weight percent copper, 24 weight percent manganese, 15 weight percent nickel, 8 weight percent zinc, and incidental impurities.
Optionally, one of more machinable materials 29 may be positioned in the mold cavity of the mold 51 at predetermined positions. Positioning one or more machinable materials may include positioning one of more solid pieces comprising at least one of iron, iron alloy, nickel, nickel alloy, cobalt, cobalt alloy, copper, copper alloy, aluminum, aluminum alloy, tantalum, and tantalum alloy. In another non-limiting embodiment, positioning one or more machinable materials 29 comprises positioning a plurality of particles of at least one of a machinable metal and a machinable metal alloy in a region of the mold cavity, thereby creating a second remainder space between the particles of the machinable metal and/or a metal alloy. After heating the mold and the materials in the mold cavity to the infiltrating temperature, the matrix material is infiltrated into the second remainder space and is then cooled to form a solid machinable region of the part 20. The particles of a machinable metal and/or a machinable metal alloy may include, but are not limited to, particles of iron, iron alloy, nickel, nickel alloy, cobalt, cobalt alloy, copper, copper alloy, aluminum, aluminum alloy, tantalum, and tantalum alloy.
Certain embodiments of a method of making an article adapted for use as at least a portion of a wear resistant working surface of a roll include cleaning the article after it is formed. In some embodiments, an excess of material may be machined from the article to form a finished article that is of a desired size and configuration. In other embodiments, a finished article is obtained after the cooling 45 step.
Advantages of the methods for producing the wear resistant articles according to the present disclosure include, but are not limited to, the possibility of using relatively inexpensive equipment to make the articles, the possibility of using a wide range of materials to tailor the characteristics of the articles, and the possibility of incorporating one or more machinable regions on the article to facilitate attachment (fixturing) and detachment of the wear resistant articles from the peripheral surface of a roll.
Referring now to
The wear resistant article 63 may comprise a metal matrix composite 21 including a plurality of inorganic particles 22 dispersed in a matrix material 23. The matrix material 23 may comprise a metal or metal alloy having a melting temperature that is less that the melting temperature of the inorganic particles. A plurality of hard elements 24 may be interspersed in and bonded together by the metal matrix composite 21 of the wear resistant article 63. In an embodiment, the wear resistance of the metal matrix composite 21 is less than a wear resistance of the hard elements 24, and the metal matrix composite 21 preferentially wears away when the grinding roll 60 is in use, thereby providing or preserving gaps 25 between a plurality of the hard elements 24 at a surface 26 of the article 63.
The hard elements 24 of the wear resistant article 63 of the grinding roll 60 may include materials comprising, but not limited to, at least one of a high hardness metal, a high hardness metal alloy, a sintered cemented carbide, and a ceramic. In a non-limiting embodiment, the hard elements comprise a high hardness metal alloy that is a tool steel. In another non-limiting embodiment, each of the plurality of hard elements 24 of the wear resistant article 63 comprises a sintered cemented carbide.
In a non-limiting embodiment, the plurality of hard elements 24 of the wear resistant article 63 secured to grinding roll 60 comprise a first end 27 and a opposed second end 28, wherein the first end 27 and opposed second end 28 are substantially planar and substantially parallel to each other, and wherein for each hard element 24 a distance between the first end 27 and the opposed second end 28 is substantially the same.
The inorganic particles 22 of the wear resistant article 63 of the grinding roll 60, in a non-limiting embodiment, comprise a metal powder or a metal alloy powder, which may be selected from, but is not limited to, at least one of tungsten, a tungsten alloy, tantalum, a tantalum alloy, molybdenum, a molybdenum alloy, niobium, a niobium alloy, iron, an iron alloy, titanium, a titanium alloy, nickel, a nickel alloy, cobalt, and a cobalt alloy. In another non-limiting embodiment, the inorganic particles 22 comprise hard particles, which may include, but are not limited to, at least one of a carbide, a boride, an oxide, a nitride, a silicide, a sintered cemented carbide, a synthetic diamond, and a natural diamond.
A grinding roll 60 may include a wear resistant article 63 comprising a matrix material 23 that includes, but is not limited to at least one of copper, a copper alloy, aluminum, an aluminum alloy, iron, an iron alloy, nickel, a nickel alloy, cobalt, a cobalt alloy, titanium, and a titanium alloy.
In certain non-limiting embodiments, the hard elements 24 of the wear resistant article 63 are spaced in a predetermined pattern in the metal matrix composite 21. In other embodiments, not meant to be limiting, the hard elements 24 of the wear resistant article 63 comprise 25% to 95%, or 40% to 90%, or 50% to 80% of the projected surface area of the surface 26 of the wear resistant article 63.
The wear resistant article 63 may further comprise at least one machinable region 29 bonded to the article 63 by the metal matrix composite 21. The one or more machinable regions 29 may comprise at least one of iron, an iron alloy, nickel, a nickel alloy, cobalt, a cobalt alloy, copper, a copper alloy, aluminum, an aluminum alloy, tantalum, and a tantalum alloy. In a non-limiting embodiment, the machinable areas 29 of the wear resistant article 63 are removably attached to the external peripheral surface 62 of the grinding roll 60 by any means now or hereafter known to a person having skill in the art, including, but not limited to mechanical clamping, brazing, welding, and adhesives (including, but not limited to, epoxies). The provision of one or more machinable regions 29 of the wear resistant article 63, and the possibility of using many means to attach the machinable regions 29 (and thus the article 63) to the external peripheral surface 62 of a grinding roll 60, permits an article according to the present disclosure to be used with cylindrical grinding roll cores made from a variety of materials.
A method of one of manufacturing and maintaining a grinding roll according to the present disclosure comprises providing a cylindrical core 61 comprising an external peripheral surface 62, and attaching embodiments of the article 20 disclosed in
Hard elements comprised of a sintered cemented carbide prepared from Grade 231 cemented carbide powder, available from ATI Firth Sterling, Madison, Ala., were prepared using conventional powder metallurgy techniques, including the steps of powder compaction and high temperature sintering. Grade 231 cemented carbide powder is a mixture of 10 percent by weight of cobalt powder and 90 percent by weight of tungsten carbide powder. Powder compaction was performed at a pressure of 206.8 MPa (15 tons per square inch). Sintering was conducted at 1400° C. (2552° F.) in an over pressure furnace using argon gas at a pressure of 5.52 MPa (800 psi). The sintered cemented carbide prepared with Grade 231 powder typically has a hardness of 87.5 HRA and a density of 14.5 g/cm3. The hard elements had a form of substantially fiat bottomed cylinders. A mold adapted to form articles having the shape of a square plate was machined from graphite. The cylindrical cemented carbide parts were placed on the bottom of a mold cavity of the mold. The unoccupied volume in the mold, i.e., the space between the sintered cemented carbide hard elements within the mold cavity, was filled with a blend of 50 percent by weight of cast tungsten carbide powder and 50 percent by weight of nickel powder. A graphite funnel was placed on top of the mold assembly and bronze pellets were placed in the funnel. The bronze pellets had a composition of 78 weight percent copper, 10 weight percent nickel, 6 weight percent manganese, 6 weight percent tin, and incidental impurities. The entire assembly was disposed for 60 minutes in an air atmosphere in a preheated furnace maintained at a temperature of 1180° C. (2156° F.). The bronze melted and infiltrated the space between the cast tungsten carbide powder, the nickel powder, and the hard elements. The mold was allowed to cool, thereby allowing a metal matrix composite to form comprising the cast tungsten carbide particles in a matrix material comprising bronze and nickel. The cylindrical cemented carbide parts were embedded within the metal matrix composite. The wear resistant article was removed from the mold cavity and was cleaned, and excess material was removed from the article by machining.
A photograph of the article fabricated in Example 1 is presented in
It will be understood that the present description illustrates those aspects of the invention relevant to a clear understanding of the invention. Certain aspects that would be apparent to those of ordinary skill in the art and that, therefore, would not facilitate a better understanding of the invention have not been presented in order to simplify the present description. Although only a limited number of embodiments of the present invention are necessarily described herein, one of ordinary skill in the art will, upon considering the foregoing description, recognize that many modifications and variations of the invention may be employed. All such variations and modifications of the invention are intended to be covered by the foregoing description and the following claims.
