WO2001041974A9 - Process for making an abrasive sintered product - Google Patents
Process for making an abrasive sintered productInfo
- Publication number
- WO2001041974A9 WO2001041974A9 PCT/US2000/042418 US0042418W WO0141974A9 WO 2001041974 A9 WO2001041974 A9 WO 2001041974A9 US 0042418 W US0042418 W US 0042418W WO 0141974 A9 WO0141974 A9 WO 0141974A9
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- region
- regions
- abrasive
- extracted
- border
- Prior art date
Links
- 238000005296 abrasive Methods 0.000 title claims abstract description 90
- 238000000034 method Methods 0.000 title description 8
- 239000002245 particle Substances 0.000 claims abstract description 72
- 238000005245 sintering Methods 0.000 claims abstract description 16
- 239000011159 matrix material Substances 0.000 claims abstract description 11
- 238000005520 cutting process Methods 0.000 claims description 36
- 239000000463 material Substances 0.000 claims description 23
- 239000000853 adhesive Substances 0.000 description 7
- 230000001070 adhesive Effects 0.000 description 7
- 239000003082 abrasive agent Substances 0.000 description 6
- 239000000969 carrier Substances 0.000 description 6
- 239000011248 coating agent Substances 0.000 description 5
- 238000000576 coating method Methods 0.000 description 5
- 238000000605 extraction Methods 0.000 description 5
- 238000003754 machining Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 238000005219 brazing Methods 0.000 description 4
- 238000000227 grinding Methods 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- 239000010432 diamond Substances 0.000 description 3
- 238000010894 electron beam technology Methods 0.000 description 3
- 238000011068 load Methods 0.000 description 3
- 239000010949 copper Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 230000000875 corresponding Effects 0.000 description 2
- 239000007791 liquid phase Substances 0.000 description 2
- 230000000737 periodic Effects 0.000 description 2
- 229910052582 BN Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N N#B Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 230000000903 blocking Effects 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000004070 electrodeposition Methods 0.000 description 1
- 230000003628 erosive Effects 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 230000001264 neutralization Effects 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000001590 oxidative Effects 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 230000002093 peripheral Effects 0.000 description 1
- 238000005240 physical vapour deposition Methods 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000001681 protective Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 239000007790 solid phase Substances 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Definitions
- This invention relates to a process for making an abrasive sintered product and more particularly, to a process for extracting a useful abrasive product from a sintered unitary structure having at least one first region containing a plurality of abrasive particles embedded therein and at least one second region containing substantially less or no abrasive particles adjacent the first region.
- the abrasive product can then be readily extracted from the structure by cutting or otherwise fracturing the structure through the second region or along the borderlines between the two regions.
- U.S. Patent Nos. 4,925,457; 5,092,910; and 5,791 ,330 teach cutting abrasive products out of structure of a sintered retaining matrix containing a plurality of abrasive particles.
- the structure can contain a mesh-type material as shown in the '457 and '910 patents or no mesh-type material as shown in the '330 patent.
- the particles are distributed throughout the structure so that if a product is to be cut out of the larger structure, it is necessary to cut through the abrasive containing material which is not only difficult and time consuming, but can lead to inaccurate results and premature cutting tool wear.
- U.S. Patent No. 5,980,678 shows sintered abrasive materials having a pattern of first regions containing a plurality of abrasive particles and a second region adjacent to and surrounding the first region and fully integrated therewith containing no abrasive particles.
- the purpose is to form a patterned abrasive material having abrasive particles in some parts and no particles in others, but there is no suggestion to cut up the material to provide abrasive products of just the first regions or of the first regions with some of the second regions integrated therewith.
- 5,620,489 also shows sintered abrasive material having a fist region containing a plurality of abrasive particles and a second region along one side thereof containing no particles fully integrated therewith.
- a purpose for the second region is to provide a "foot" to the first region containing no abrasive particles enabling the material to be more readily attached to a cutting tool.
- the reference discloses that such material can be cut up into pieces of the required shape and mounted on a suitable carrier. However, to provide such pieces it would be necessary to cut through not only the second region, but also the first region containing the abrasive particles.
- a new and improved method for making an abrasive product comprising forming a structure of a sinterable retaining matrix having at least one first region containing a plurality of abrasive particles embedded therein and at least one second region containing substantially less or no abrasive particles adjacent said first region, at least one of said regions substantially surrounding the other of said regions, sintering said structure to form a unitary structure wherein said first and second regions are integrated along a border between said regions, and extracting at least said first region from said unitary structure to form an abrasive product.
- FIG. 1 is a plan view of a unitary structure of flat configuration illustrating shapes of cutting segments to be cut from the structure.
- FIGS. 2A, 2B, and 2C show various cutting segments extracted from the structure of FIG. 1 and mounted on the working edge of a cutting tool.
- FIGS. 3A, 3B, and 3C show similar cutting segments of an alternative shape.
- FIGS. 4A, 4B, and 4C show similar cutting segments of yet another alternative shape.
- FIG. 5 is a fragmentary side elevational view showing a cutting tool having the cutting segments of FIGS. 2-4 mounted thereon.
- FIG. 6 is a structure similar to FIG. 1 , but of contoured configuration.
- FIG. 7A shows a cutting element of annular configuration.
- FIG. 7B illustrates a method for making a structure from which the cutting element of FIG. 7A can be formed
- FIG. 7C illustrates the structure formed in FIG. 7B
- FIG. 8 is a structure similar to FIG. 1 showing a plurality of cutting segments of the same shape and size;
- FIG. 9 is a view similar to FIG. 8 showing a plurality of cutting segments of different shapes and sizes.
- the structure from which the abrasive products are extracted may, for example, be of flat or undulating configuration such as a corrugated sheet of material and may be an essentially one or two dimensional plate or 3-dimensional block.
- the types of abrasive particles in the two regions can be different in composition, size, and shape.
- the second region comprises little or no abrasive particles to aid in the extraction of the products from the structure and the abrasive particles are diamonds.
- the abrasive particles may be randomly or non-randomly distributed in one or the other or both of the regions or in selected areas of the regions.
- at least the first regions contain predominately non-randomly distributed abrasive particles.
- a distribution, e.g., a non-random one, of the abrasive particles in the first regions of the structure reference by way of example is made to one or more of the following U.S.
- any hard particles capable of performing an abrasive function can be used in this invention.
- suitable abrasive particles see for instance U.S. Patent No. 5,791 ,330.
- these hard particles include carbons, e.g., diamonds (i.e., natural synthetic and polycrystalline diamonds); nitrides (i.e., cubic boron nitride); carbides, and borides.
- at least some of the hard particles can be in the form of agglomerates of the individual hard particles.
- the hard particles can also be in at least one coating layer.
- the coating can be made by at least one of the electrodeposition methods or chemical or physical vapor deposition methods and can comprise carbide forming elements, e.g., boron and silicon and/or elements of IVA, VA, VIA groups of The Periodic Table of The Elements, e.g., chromium, titanium, molybdenum, tungsten.
- the sinterable retaining matrix of the structure comprises at least one element of Group IV A, VA, VI A, VII A, VIII A, IB, MB, IIIB, IVB, and VB of the Periodic Table.
- Matrix materials in the first and second regions can differ from each other at least by the elements included and/or their concentrations and/or the porosity of the sintered material.
- the content of copper, if present, in the first region could exceed the content of copper in the second region. This is especially helpful in extracting abrasive products from the structure by cutting through the second regions where there is a lower concentration of the abrasive particles than the first region with a laser.
- the structure having first regions containing abrasive particles has been sintered, preferably under pressure and/or load and can include the step of infiltration before and/or during and/or after sintering.
- the sinterable matrix material can consist of or in addition include fusible and/or brazable materials that when molten can infiltrate into non-molten sinterable material.
- "sinterable matrix material" is intended to include, but is not limited to fusible and brazable materials as discussed, for example, in the above-mentioned U.S. Patent No. 5,380,390.
- sintering includes, but is not limited to, sintering at atmospheric or room pressure, at negative (vacuum) pressure or at positive pressure, including also placing the material under pressure and/or load. Sintering can occur in the presence of a protective and/or reduction, and/or oxidizing, and/or neutral atmosphere, in a solid and/or liquid phase and/or in the partial presence of the liquid phase; and in a mold or tray, in a furnace or in a sinter press. Examples of suitable sinterable matrix materials and more detailed methods for sintering can be found in the above-recited U.S. patents.
- the first regions of the structure are surrounded by and separated from each other by the second regions and the step of extracting abrasive products from the structure preferably comprises cutting the structure through the second regions either along the borders between the regions or through the second regions at a distance spaced from the borders.
- a part of the second regions form a part of the first regions extracted from the structure.
- the extracted products can have a portion on at least one side thereof, derived from the second region that contains no abrasive material, to provide a "foot" and/or a peripheral area for the products that enables them to be readily fixed to the working edge or a carrier or a surface of an abrasive machining tool.
- One method for providing a structure having areas containing abrasive particles and areas containing essentially no abrasive particles comprises blocking designated regions when making the structure by the use of a mask as disclosed in U.S. Patent Nos. 5,380,390; 5,817,204; and 5,980,678.
- the structure may be prepared by filling materials with a lower concentration of or no abrasive particles into one section of an assembly or a compacting or sinter mold or a sinter tray and materials having higher concentrations of particles in other sections and then sintering the materials to form a unitary structure containing both first and second regions.
- Another method comprises providing a plurality of blocks of sinterable matrix material containing differing amounts of abrasive material, assembling the blocks in abutting relationship to form an assembly and then sintering the assembly, preferably under pressure and/or load, to form a unitary structure containing regions that contain particles (i.e., first regions) and regions that do not (i.e., second regions) as taught in copending application Serial
- the bodies may be extracted from the structure by means of, for example, electrical erosion, laser, electron beam, gas-arc, water-jet breakage with or without a utilization of the mechanical breakage or fracturing before, during, or after application of said means or any combination thereof.
- the extracting may be along the border or junction lines between the regions or at least partially through or predominately through the second regions.
- the extracting method is by cutting with a laser or water-jet that goes exclusively through the second regions of the structure.
- abrasive products can be "scooped" out of the structure.
- the extracted product comprises the first region of the structure and a portion of the second region.
- the extracted products containing abrasive particles can then function as abrasive members, elements, inserts, caps, linings, straps or segments (i.e., cutting and/or grinding segments) and be fixed (either one or more) to the working surface or carrier of a machining tool.
- the bodies comprise a portion of the second or service region of the structure from which the product is extracted which portion can be readily fixed to the tool carrier.
- Methods for fixing include soldering, brazing, sintering, welding, mechanical fixing, gluing or any combination thereof.
- Brazing and welding include but are not limited to electron beam processing such as laser welding or laser assisted brazing. Also discharge welding methods or machinery, e.g., of a type recently developed by Robosintris Sri of Piacenza, Italy, can be used.
- the products connected to the tool carrier by a portion from the second region of the structure are subjected to a further dressing process which may include abrasive, water-jet, or laser treatment or any combination thereof.
- At least one of a plurality of extracted products containing abrasive particles are fixed to the carrier or core of a machining tool through foot portions containing no abrasive particles.
- Such tools may include tools providing abrasive cutting, drilling, grinding, dressing and polishing functions such as circular segment blades, reciprocating segment blades, wire beads and blades, dressers, drill bits, face grinding tools, and the like. Preferred embodiments of the invention will now be illustrated with reference to the drawings.
- FIG. 1 is an example of a structure 1 in the form of a flat plate having first regions 2 of various shapes containing abrasive particles and second regions 3 substantially surrounding the first regions containing no abrasive particles.
- This plate can be made, for example, by the process disclosed in U.S. Patent No. 5,817,204, the contents of which are incorporated herein by reference, by providing a preform of sinterable matrix material, such as a soft, easily deformable and flexible preform of U.S. Patent No. 5,620,489, the contents of which are also incorporated herein by reference, coating one surface of the preform with an adhesive and then placing a mask over the adhesive coated side of the preform having openings corresponding to the various shapes of the desired cutting segments. Abrasive particles are then applied over the top of the mask, the particles adhering to the adhesive coating in the openings of the mask.
- the abrasive particles can be randomly distributed in the openings of if desired can be distributed in a non-random pattern by means of, for example, a mesh material on top of the preform or on top of the mask. Following application of the abrasive particles the hard particles not adhering to the adhesive coating and the mask are removed. If a mesh material is used between the preform and the mask, it can also be removed or, alternatively, it can be left to form a part of the sintered plate and the cutting segments cut therefrom.
- Pressure is then applied to the preform to urge the abrasive particles into the preform and preform is then heated under pressure to sinter the preform and form the structure 1 having first regions 2 of various shapes corresponding to the openings in the mask containing abrasive particles and second regions 3 substantially surrounding the first regions containing no abrasive particles.
- the particles and mesh if present can be urged into the preform before the preform is sintered under pressure or simultaneously with the sintering of the preform.
- these segments can be extracted from the plate by cutting in the second region along the borderline between the regions along the sides of the segments that will form their cutting surface and at a distance spaced from the side or sides that will be secured to a cutting tool to provide the foot portion 31 .
- These segments can then be fixed in a regular and spaced manner to the core 25 of a machining tool as shown in FIG. 5 by securing the foot of the segments to the core.
- the cutting segments can be cut from a sheet of abrasive material 59 having corrugations 60 with regions containing abrasive particles and regions containing no particles as in FIG. 1.
- FIG. 7A illustrates an alternative embodiment of the invention showing a cutting segment 100 having an abrasive particle containing region 101 and a non-abrasive particle containing region or foot 102.
- the segment can be prepared by providing a structure of a first sinterable material 101 ' containing abrasive particles and of annular shape and a core of a second sinterable material 102 ' containing no particles that is substantially surrounded by the first material.
- the structure is then sintered providing a diffusion between material 101 and 102, for example in sinter press 103 under pressure as shown in FIG. 7B to form a unitary structure 104 as shown in FIG. 7C having a particle containing region 101 " fully integrated along its inner border with no particle containing region 102".
- Structure 104 is then cut along the line 105 to provide the cutting segment 100 of FIG. 7A.
- the regions 2 of a variety of shapes and dimensions can be arbitrarily distributed within the structure 1.
- the structure 1 may comprise one or a plurality of substantially the same or different regions 2.
- FIG. 8 illustrates a structure 201 having first regions 202 each containing abrasive particles of substantially the same rectangular shape and dimension distributed within the structure in a non-random manner and a second region 203 substantially surrounding the first regions containing no abrasive particles.
- FIG. 9 that more than one plurality of regions 202 (different by shapes and dimensions such as regions 204 and 205) could be distributed within the structure 201 , for example, for the sake of increasing utilization of the structure by maximizing the number of regions to be extracted from it.
- the sequence of the extraction e.g, cutting, can be arbitrary or be pre-programmed, optimized according to the desired algorithm.
- Abrasive parts e.g., segments in the form of regions 202 (with or without a portion of region 203 attached) can be extracted from the structure one by one or in groups. Further, the parts, e.g, can be extracted completely , i.e, fully separated from the structure or only partially therefrom. A partial extraction provides some integrity between a non-completely extracted abrasive part and the structure. It means that while extracting an abrasive part partially, at least one little bridge or tab, preferably in a region 202, is left to connect the partially extracted abrasive part to the structure 201.
- Such partial extraction allows greater ease in transporting and moving the structure 201 with non-completely extracted abrasive parts within and outside the extraction machine (i.e., laser, water jet) and other equipment without having to deal with a plurality of loose, individual extracted abrasive parts.
- Partially extracted abrasive parts can then be completely extracted from the structure simply by breaking the bridge or tab.
- the bridge or tab could be broken by a mechanical fracturing or breaking, e.g., hammering, compression air blow-up, vibration, etc.
Abstract
A method for making an abrasive product comprising forming a structure (1) of a sinterable retaining matrix having at least one first region (2) containing a plurality of abrasive particles embedded therein and at least one second region (3) containing substantially less or no abrasive particles adjacent the first region (1), at least one of the regions substantially surrounding the other of the regions, sintering the structure to form a unitary structure, wherein the first and second regions are integrated along a border between the regions, and extracting at least the first region from the unitary structure to form an abrasive product.
Description
PROCESS FOR MAKING AN ABRASIVE SINTERED PRODUCT
BACKGROUND OF THE INVENTION
This invention relates to a process for making an abrasive sintered product and more particularly, to a process for extracting a useful abrasive product from a sintered unitary structure having at least one first region containing a plurality of abrasive particles embedded therein and at least one second region containing substantially less or no abrasive particles adjacent the first region. The abrasive product can then be readily extracted from the structure by cutting or otherwise fracturing the structure through the second region or along the borderlines between the two regions.
U.S. Patent Nos. 4,925,457; 5,092,910; and 5,791 ,330 teach cutting abrasive products out of structure of a sintered retaining matrix containing a plurality of abrasive particles. The structure can contain a mesh-type material as shown in the '457 and '910 patents or no mesh-type material as shown in the '330 patent. However, in these structures the particles are distributed throughout the structure so that if a product is to be cut out of the larger structure, it is necessary to cut through the abrasive containing material which is not only difficult and time consuming, but can lead to inaccurate results and premature cutting tool wear.
U.S. Patent No. 5,980,678 shows sintered abrasive materials having a pattern of first regions containing a plurality of abrasive particles and a second region adjacent to and surrounding the first region and fully integrated therewith containing no abrasive particles. The purpose is to form a patterned
abrasive material having abrasive particles in some parts and no particles in others, but there is no suggestion to cut up the material to provide abrasive products of just the first regions or of the first regions with some of the second regions integrated therewith. U.S. Patent No. 5,620,489 also shows sintered abrasive material having a fist region containing a plurality of abrasive particles and a second region along one side thereof containing no particles fully integrated therewith. A purpose for the second region is to provide a "foot" to the first region containing no abrasive particles enabling the material to be more readily attached to a cutting tool. The reference discloses that such material can be cut up into pieces of the required shape and mounted on a suitable carrier. However, to provide such pieces it would be necessary to cut through not only the second region, but also the first region containing the abrasive particles.
SUMMARY OF THE INVENTION In accordance with the invention, a new and improved method is provided for making an abrasive product comprising forming a structure of a sinterable retaining matrix having at least one first region containing a plurality of abrasive particles embedded therein and at least one second region containing substantially less or no abrasive particles adjacent said first region, at least one of said regions substantially surrounding the other of said regions, sintering said structure to form a unitary structure wherein said first and second regions are integrated along a border between said regions, and extracting at least said first region from said unitary structure to form an abrasive product.
BRIEF DESCRIPTION OF THE DRAWINGS
The detailed features and advantages of the invention will now be explained in connection with the accompanying drawings in which:
FIG. 1 is a plan view of a unitary structure of flat configuration illustrating shapes of cutting segments to be cut from the structure.
FIGS. 2A, 2B, and 2C show various cutting segments extracted from the structure of FIG. 1 and mounted on the working edge of a cutting tool.
FIGS. 3A, 3B, and 3C show similar cutting segments of an alternative shape. FIGS. 4A, 4B, and 4C show similar cutting segments of yet another alternative shape.
FIG. 5 is a fragmentary side elevational view showing a cutting tool having the cutting segments of FIGS. 2-4 mounted thereon.
FIG. 6 is a structure similar to FIG. 1 , but of contoured configuration. FIG. 7A shows a cutting element of annular configuration.
FIG. 7B illustrates a method for making a structure from which the cutting element of FIG. 7A can be formed;
FIG. 7C illustrates the structure formed in FIG. 7B;
FIG. 8 is a structure similar to FIG. 1 showing a plurality of cutting segments of the same shape and size; and
FIG. 9 is a view similar to FIG. 8 showing a plurality of cutting segments of different shapes and sizes.
DETAILED DESCRIPTION OF THE INVENTION
The structure from which the abrasive products are extracted may, for example, be of flat or undulating configuration such as a corrugated sheet of material and may be an essentially one or two dimensional plate or 3-dimensional block.
The types of abrasive particles in the two regions can be different in composition, size, and shape. In a preferred embodiment the second region comprises little or no abrasive particles to aid in the extraction of the products from the structure and the abrasive particles are diamonds. The abrasive particles may be randomly or non-randomly distributed in one or the other or both of the regions or in selected areas of the regions. In a particularly preferred embodiment, at least the first regions contain predominately non-randomly distributed abrasive particles. For providing a distribution, e.g., a non-random one, of the abrasive particles in the first regions of the structure, reference by way of example is made to one or more of the following U.S. Patents No.: 4,925,457; 5,049,165; 5,092,910; 5,190,568; 5,203,880; 5,380,390; 5,620,489; 5,791 ,330; 5,817,204; and 5,980,678, all of which are incorporated therein by reference.
Any hard particles capable of performing an abrasive function can be used in this invention. For a list of suitable abrasive particles, see for instance U.S. Patent No. 5,791 ,330. For example, these hard particles include carbons, e.g., diamonds (i.e., natural synthetic and polycrystalline diamonds); nitrides (i.e., cubic boron nitride); carbides, and borides. Moreover, at least
some of the hard particles can be in the form of agglomerates of the individual hard particles.
The hard particles can also be in at least one coating layer. The coating can be made by at least one of the electrodeposition methods or chemical or physical vapor deposition methods and can comprise carbide forming elements, e.g., boron and silicon and/or elements of IVA, VA, VIA groups of The Periodic Table of The Elements, e.g., chromium, titanium, molybdenum, tungsten.
The sinterable retaining matrix of the structure comprises at least one element of Group IV A, VA, VI A, VII A, VIII A, IB, MB, IIIB, IVB, and VB of the Periodic Table. Matrix materials in the first and second regions can differ from each other at least by the elements included and/or their concentrations and/or the porosity of the sintered material. For example, preferably the content of copper, if present, in the first region could exceed the content of copper in the second region. This is especially helpful in extracting abrasive products from the structure by cutting through the second regions where there is a lower concentration of the abrasive particles than the first region with a laser.
In a particularly preferred embodiment, the structure having first regions containing abrasive particles has been sintered, preferably under pressure and/or load and can include the step of infiltration before and/or during and/or after sintering. In addition, the sinterable matrix material can consist of or in addition include fusible and/or brazable materials that when molten can infiltrate into non-molten sinterable material. Thus "sinterable
matrix material" is intended to include, but is not limited to fusible and brazable materials as discussed, for example, in the above-mentioned U.S. Patent No. 5,380,390. It is to be noted that sintering includes, but is not limited to, sintering at atmospheric or room pressure, at negative (vacuum) pressure or at positive pressure, including also placing the material under pressure and/or load. Sintering can occur in the presence of a protective and/or reduction, and/or oxidizing, and/or neutral atmosphere, in a solid and/or liquid phase and/or in the partial presence of the liquid phase; and in a mold or tray, in a furnace or in a sinter press. Examples of suitable sinterable matrix materials and more detailed methods for sintering can be found in the above-recited U.S. patents.
In one embodiment, the first regions of the structure are surrounded by and separated from each other by the second regions and the step of extracting abrasive products from the structure preferably comprises cutting the structure through the second regions either along the borders between the regions or through the second regions at a distance spaced from the borders. In a preferred embodiment, a part of the second regions form a part of the first regions extracted from the structure. For example, if the first regions contain abrasive particles and the second regions essentially no abrasive particles, the extracted products can have a portion on at least one side thereof, derived from the second region that contains no abrasive material, to provide a "foot" and/or a peripheral area for the products that enables them to be readily fixed to the working edge or a carrier or a surface of an abrasive machining tool.
One method for providing a structure having areas containing abrasive particles and areas containing essentially no abrasive particles, comprises blocking designated regions when making the structure by the use of a mask as disclosed in U.S. Patent Nos. 5,380,390; 5,817,204; and 5,980,678. Alternatively, the structure may be prepared by filling materials with a lower concentration of or no abrasive particles into one section of an assembly or a compacting or sinter mold or a sinter tray and materials having higher concentrations of particles in other sections and then sintering the materials to form a unitary structure containing both first and second regions. Another method comprises providing a plurality of blocks of sinterable matrix material containing differing amounts of abrasive material, assembling the blocks in abutting relationship to form an assembly and then sintering the assembly, preferably under pressure and/or load, to form a unitary structure containing regions that contain particles (i.e., first regions) and regions that do not (i.e., second regions) as taught in copending application Serial
No. 09/444,840 filed November 22, 1999 entitled Method for Making a Sintered Article and Products Produced Thereby, the contents of which is incorporated herein by reference.
The bodies may be extracted from the structure by means of, for example, electrical erosion, laser, electron beam, gas-arc, water-jet breakage with or without a utilization of the mechanical breakage or fracturing before, during, or after application of said means or any combination thereof. The extracting may be along the border or junction lines between the regions or at least partially through or predominately through the second regions.
Preferably, the extracting method is by cutting with a laser or water-jet that goes exclusively through the second regions of the structure. Alternatively, abrasive products can be "scooped" out of the structure. Preferably, as noted above, the extracted product comprises the first region of the structure and a portion of the second region.
More specific methods for extracting bodies can be found in the above-mentioned U.S. Patent Nos. 5,620,489; 5,791 ,330; and 5,980,678 as well as the copending application Serial No. 09/444,840 of the inventor filed November 22, 1999. The products extracted from the structure may be further processed into any desired shape or look. These include compacting, heating, cooling, sintering, coning, forging, extruding, brazing, infiltrating, impregnating, cleaning, painting, coating, plating, adhering, etching, and machining which may include deburring, laser, electron beam, flame jet, water-jet cutting, milling and grinding or any combination thereof.
The extracted products containing abrasive particles can then function as abrasive members, elements, inserts, caps, linings, straps or segments (i.e., cutting and/or grinding segments) and be fixed (either one or more) to the working surface or carrier of a machining tool. In a particularly preferred embodiment of the invention, the bodies comprise a portion of the second or service region of the structure from which the product is extracted which portion can be readily fixed to the tool carrier. Methods for fixing include soldering, brazing, sintering, welding, mechanical fixing, gluing or any combination thereof. Brazing and welding include but are not limited to
electron beam processing such as laser welding or laser assisted brazing. Also discharge welding methods or machinery, e.g., of a type recently developed by Robosintris Sri of Piacenza, Italy, can be used.
In a preferred embodiment, the products connected to the tool carrier by a portion from the second region of the structure are subjected to a further dressing process which may include abrasive, water-jet, or laser treatment or any combination thereof.
In a particularly preferred embodiment, at least one of a plurality of extracted products containing abrasive particles are fixed to the carrier or core of a machining tool through foot portions containing no abrasive particles. Such tools may include tools providing abrasive cutting, drilling, grinding, dressing and polishing functions such as circular segment blades, reciprocating segment blades, wire beads and blades, dressers, drill bits, face grinding tools, and the like. Preferred embodiments of the invention will now be illustrated with reference to the drawings.
FIG. 1 is an example of a structure 1 in the form of a flat plate having first regions 2 of various shapes containing abrasive particles and second regions 3 substantially surrounding the first regions containing no abrasive particles. This plate can be made, for example, by the process disclosed in U.S. Patent No. 5,817,204, the contents of which are incorporated herein by reference, by providing a preform of sinterable matrix material, such as a soft, easily deformable and flexible preform of U.S. Patent No. 5,620,489, the contents of which are also incorporated herein by reference, coating one
surface of the preform with an adhesive and then placing a mask over the adhesive coated side of the preform having openings corresponding to the various shapes of the desired cutting segments. Abrasive particles are then applied over the top of the mask, the particles adhering to the adhesive coating in the openings of the mask.
The abrasive particles can be randomly distributed in the openings of if desired can be distributed in a non-random pattern by means of, for example, a mesh material on top of the preform or on top of the mask. Following application of the abrasive particles the hard particles not adhering to the adhesive coating and the mask are removed. If a mesh material is used between the preform and the mask, it can also be removed or, alternatively, it can be left to form a part of the sintered plate and the cutting segments cut therefrom.
Pressure is then applied to the preform to urge the abrasive particles into the preform and preform is then heated under pressure to sinter the preform and form the structure 1 having first regions 2 of various shapes corresponding to the openings in the mask containing abrasive particles and second regions 3 substantially surrounding the first regions containing no abrasive particles. The particles and mesh if present can be urged into the preform before the preform is sintered under pressure or simultaneously with the sintering of the preform.
While use of an adhesive for the purpose of temporarily retaining the abrasive particles in a non-random pattern prior to and in the process of sintering is preferred, as taught in U.S. Patents No. 4,925,457; 5,049,165;
5,092,910; 5,190,568; and 5,203,880, it is still possible to obtain a non-random pattern without the use of an adhesive. Thus the present invention is not limited to use of adhesives in the process of making the sintered plate. This enables various shaped cutting segments 26, 28, and 29 to be easily extracted from the plate, each having an abrasive particle containing portion 30 and a "foot" portion 31 devoid of particles as shown in FIGS 2-4. As discussed above, these segments can be extracted from the plate by cutting in the second region along the borderline between the regions along the sides of the segments that will form their cutting surface and at a distance spaced from the side or sides that will be secured to a cutting tool to provide the foot portion 31 . These segments can then be fixed in a regular and spaced manner to the core 25 of a machining tool as shown in FIG. 5 by securing the foot of the segments to the core. These cutting segments are described in greater detail in U.S. Patent No. 5,791 ,330, the contents of which are incorporated herein by reference.
Alternatively, the cutting segments can be cut from a sheet of abrasive material 59 having corrugations 60 with regions containing abrasive particles and regions containing no particles as in FIG. 1. FIG. 7A illustrates an alternative embodiment of the invention showing a cutting segment 100 having an abrasive particle containing region 101 and a non-abrasive particle containing region or foot 102. The segment can be prepared by providing a structure of a first sinterable material 101 ' containing abrasive particles and of annular shape and a core of a second sinterable
material 102 ' containing no particles that is substantially surrounded by the first material. The structure is then sintered providing a diffusion between material 101 and 102, for example in sinter press 103 under pressure as shown in FIG. 7B to form a unitary structure 104 as shown in FIG. 7C having a particle containing region 101 " fully integrated along its inner border with no particle containing region 102". Structure 104 is then cut along the line 105 to provide the cutting segment 100 of FIG. 7A.
As shown in FIG. 1 , the regions 2 of a variety of shapes and dimensions can be arbitrarily distributed within the structure 1. However, the structure 1 may comprise one or a plurality of substantially the same or different regions 2. For example, FIG. 8 illustrates a structure 201 having first regions 202 each containing abrasive particles of substantially the same rectangular shape and dimension distributed within the structure in a non-random manner and a second region 203 substantially surrounding the first regions containing no abrasive particles. It should be understood, however, as shown in FIG. 9 that more than one plurality of regions 202 (different by shapes and dimensions such as regions 204 and 205) could be distributed within the structure 201 , for example, for the sake of increasing utilization of the structure by maximizing the number of regions to be extracted from it. Further, the sequence of the extraction, e.g, cutting, can be arbitrary or be pre-programmed, optimized according to the desired algorithm.
Abrasive parts, e.g., segments in the form of regions 202 (with or without a portion of region 203 attached) can be extracted from the structure one by one or in groups. Further, the parts, e.g, can be extracted completely ,
i.e, fully separated from the structure or only partially therefrom. A partial extraction provides some integrity between a non-completely extracted abrasive part and the structure. It means that while extracting an abrasive part partially, at least one little bridge or tab, preferably in a region 202, is left to connect the partially extracted abrasive part to the structure 201. Such partial extraction allows greater ease in transporting and moving the structure 201 with non-completely extracted abrasive parts within and outside the extraction machine (i.e., laser, water jet) and other equipment without having to deal with a plurality of loose, individual extracted abrasive parts. Partially extracted abrasive parts can then be completely extracted from the structure simply by breaking the bridge or tab. For example, the bridge or tab could be broken by a mechanical fracturing or breaking, e.g., hammering, compression air blow-up, vibration, etc.
Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. It is intended that the specification and specific embodiments be considered as exemplary only, with the true scope and spirit of the invention being indicated by the following claims.
Claims
1. A method for making an abrasive product comprising forming a structure of a sinterable retaining matrix having at least one first region containing a plurality of abrasive particles embedded therein and at least one second region containing substantially less or no abrasive particles adjacent said first region, at least one of said regions substantially surrounding the other of said regions, sintering said structure to form a unitary structure, wherein said first and second regions are integrated along a border between said regions, and at least partially extracting at least said first region from said unitary structure to form an abrasive product.
2. The method of claim 1 , wherein the abrasive product is extracted from the unitary structure by cutting through said second region along the border immediately adjacent said first region to provide an abrasive product comprising essentially said first region.
3. The method of claim 1 , wherein the abrasive product is extracted from the unitary structure by cutting through said second region at a distance from said border to provide an abrasive product comprising said first region and a portion of the second region along the border between said regions.
4. The method of claim 1 , wherein the second region substantially surrounds said first region.
5. The method of claim 4, wherein the product is extracted from the unitary structure by cutting through said second region partially along the border immediately adjacent said first region and partially at a distance from said border to provide an abrasive product comprising said first region and a portion of said second region along only a portion of the border between said regions.
6. The method of claim 4, wherein the structure is in the form of a flat plate.
7. The method of claim 4, wherein the structure is in the form of a corrugated sheet.
8. The method of claim 1 , wherein the first region substantially surrounds the second region.
9. The method of claim 8, wherein the product is extracted from the structure by cutting through said second region at a distance from said border to provide an abrasive product comprising said first region and a portion of said second region along the border between said regions.
10. The method of claim 9, wherein said first region is annular and the portion of said second region forms an annular core inside of said first region.
1 1 . The method of claim 1 , wherein the plurality of abrasive particles are embedded in the first region in a non-random pattern.
12. The method of claim 1 , wherein the plurality of particles are distributed in the first region in a random pattern.
13. The method of claim 1 , wherein the second region contains no abrasive particles.
14. The method of claim 1 , containing a plurality of said first regions, each surrounded by said second region.
15. The method of claim 1 , wherein the plurality of abrasive particles are embedded in the first region before sintering.
16. The method of claim 1 , wherein the plurality of abrasive particles are embedded in the first region during sintering.
17. The method of claim 11 , wherein the plurality of abrasive particles are embedded in a non-random pattern in the first region by means of a mesh material.
18. The method of claim 17, wherein the mesh material is incorporated in said first region and forms a part of said abrasive product.
19. The method of any one of claims 2, 3, or 5, wherein the second region is cut with a laser or water-jet.
20. The method of claim 14, wherein the plurality of said first regions are of the same size and shape.
21. The method of claim 14, wherein the plurality of said first regions are of at least two different sizes and shapes.
22. The method of claim 14, wherein the plurality of said first regions are extracted from the unitary structure individually.
23. The method of claim 14, wherein the plurality of said first regions are extracted from the unitary structure simultaneously.
24. The method of claim 14, wherein the plurality of said first regions are extracted completely from the structure.
25. The method of claim 14, wherein the plurality of said first regions are only partially extracted from the structure to leave a small, frangible bridge connecting the first regions to the second region.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU39715/01A AU3971501A (en) | 1999-12-03 | 2000-12-01 | Process for making an abrasive sintered product |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16868099P | 1999-12-03 | 1999-12-03 | |
US60/168,680 | 1999-12-03 |
Publications (3)
Publication Number | Publication Date |
---|---|
WO2001041974A2 WO2001041974A2 (en) | 2001-06-14 |
WO2001041974A3 WO2001041974A3 (en) | 2002-01-03 |
WO2001041974A9 true WO2001041974A9 (en) | 2002-04-25 |
Family
ID=22612491
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2000/042418 WO2001041974A2 (en) | 1999-12-03 | 2000-12-01 | Process for making an abrasive sintered product |
Country Status (2)
Country | Link |
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AU (1) | AU3971501A (en) |
WO (1) | WO2001041974A2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10151802B4 (en) * | 2001-10-19 | 2006-05-04 | Cedima Diamantwerkzeug- Und Maschinenhandelsgesellschaft Mbh | Method for producing an abrasive element for drill bits of hollow drills |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4554117A (en) * | 1982-09-30 | 1985-11-19 | Ford Motor Company | Method of forming dense ceramic bodies |
ZA963789B (en) * | 1995-05-22 | 1997-01-27 | Sandvik Ab | Metal cutting inserts having superhard abrasive boedies and methods of making same |
US6196911B1 (en) * | 1997-12-04 | 2001-03-06 | 3M Innovative Properties Company | Tools with abrasive segments |
-
2000
- 2000-12-01 WO PCT/US2000/042418 patent/WO2001041974A2/en active Application Filing
- 2000-12-01 AU AU39715/01A patent/AU3971501A/en not_active Abandoned
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