IE80882B1 - Synthesis of polycrystalline cubic boron nitride - Google Patents

Synthesis of polycrystalline cubic boron nitride

Info

Publication number
IE80882B1
IE80882B1 IE940108A IE940108A IE80882B1 IE 80882 B1 IE80882 B1 IE 80882B1 IE 940108 A IE940108 A IE 940108A IE 940108 A IE940108 A IE 940108A IE 80882 B1 IE80882 B1 IE 80882B1
Authority
IE
Ireland
Prior art keywords
boron nitride
cbn
nitride
aluminum
recited
Prior art date
Application number
IE940108A
Other versions
IE940108A1 (en
Inventor
Xian Yao
Ghanshyam Rai
Original Assignee
Smith International
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Smith International filed Critical Smith International
Priority to IE940108A priority Critical patent/IE80882B1/en
Publication of IE940108A1 publication Critical patent/IE940108A1/en
Publication of IE80882B1 publication Critical patent/IE80882B1/en

Links

Abstract

A sintered polycrystalline compact of cubic boron nitride is made by first forming a mixture of about 30 to 60 percent by weight cubic boron nitride, up to about 50 percent by weight hexagonal boron nitride, and from about 2 to 7 percent by weight adjuvant materials, or sintering aids, comprising an aluminum containing materials selected from the group consisting of aluminum, aluminum nitride, or aluminum diboride, and up to 50 percent by weight of nitride, carbide, or carbonitride binder material containing a group IVb, Vb, or V1b transition metal. The mixture of cBN crystals, hBN and other materials is compacted into a preform and subjected to heat treatment in a non-oxidizing atmosphere. The preform is placed onto a cemented tungsten-carbide/cobalt substrate and subjected to elevated pressure and tempreature conditions at which cubic boron nitride is thermodynamically stable. The elevated pressure and temperature conditions are maintained for a time sufficient to permit the infiltration of the cobalt into the cBN matrix and sinter the compact. The compact is characterized by substantial intergranular cBN to cBN bonding, and has superior abrasive wear resistance, chemical resistance, impact resistance, thermal conductivity and stability.

Description

SYNTHESIS OF POLYCRYSTALLINE CUBIC BORON NITRIDE Field of the Invention This invention relates to sintered polycrystalline abrasive compacts of cubic boron nitride for use as machining fools, abrasives, wire dies, wear parts, heat sinks, and the like. More particularly, this invention relates to a process of synthesizing polycrystalline cubic boron nitride composites by adding a certain amount of hexagonal boron nitride to cubic boron nitride crystals and utilizing cubic boron nitride crystals as nuclei and hexagonal boron nitride as precipitate and growth materials. The composition also uses a metal nitride, and a metal carbonitride catalyst as well as infiltrated liquid cobalt under high pressure and high temperature sintering conditions which are thermodynamically stable for the cubic boron nitride crystal structure.
Background of the Invention The high pressure forms of boron nitride, known as cubic boron nitride (cBN) and wurzitic boron nitride, are surpassed only by diamond in hardness and have a wide variety of uses as machining tools, abrasives, wire dies, wear parts, heat sinks, and the like.
Wurzite boron nitride, typically formed by shock or explosive techniques, has a hardness equal to cBN and can be substituted or mixed with cBN in most applications. Wurzite boron nitride, however, is thermodynamically unstable relative to cBN under conditions favorable to sintering and will revert to cBN in tbe presence of catalyst-solvents. cBN, in particular, is preferred to diamond in working with ferrous metals because it is chemically more stable than diamond, has a higher temperature threshold for conversion to its hexagonal or graphitic form and is not catalytically degraded by hot ferrous metals, as is diamond. In die applications mentioned above, the primary qualities desired for a polycrystalline compact tool are abrasive wear resistance, -2thennal stability, high thermal conductivity, impact resistance, and a low coefficient of friction in contact with the work piece. While cBN itself possess each of these qualities to a significant degree, whether a polycrystalline compact of cBN as a whole possesses them will depend largely on the characteristics of the other materials that will make up the compact, i.e., binder material, catalysts, substrates, and the like, along with processing parameters such as surface cleanliness, grain size and the like.
Compacts having a lower concentration of cBN and a higher concentration of a nonmetallic adjuvant material have been favored for such applications. Although it is possible to form a sintered compact of cBN with no adjuvant material under conditions of high pressure and temperature, strongly adherent surface oxides of boron act to inhibit significant intergranular bonding and make it difficult, if not impossible, to obtain an adequate compact strength. Various adjuvant materials are thus incorporated, either to enhance intergranular bonding or to surround the grains with a continuous somewhat less brittle matrix, producing a stronger cBN compact. The adjuvant material may also impart other desirable physical characteristics to the compact such as chemical resistance and impact resistance depending on the particular adjuvant material chosen. Additionally, the use of adjuvant materials help to reduce the material cost associated with producing the cBN compact due to the decreased amount of cBN crystals required as a starting material.
The adjuvant materials chosen should possess two general sets of qualities; (1) mechanical and chemical properties as dose to those of cBN as possible, so as not to deteriorate tool performance, and (2) characteristics enabling manufacture of the compact, such as a melting point at readily obtainable temperatures or good plasticity at such temperatures, limited but not excessive chemical reactivity towards cBN, and most preferably, catalytic solvent activity for conversion of hexagonal boron nitride to cBN. This latter characteristic will facilitate crystalline growth and intergranular bonding under conditions of pressure and temperature at which cBN is thermodynamically stable.
The use of adjuvant materials as catalyst-solvents for conversion of hexagonal boron nitride to cBN are disdosed in die prior art. U.S. Patent No. 3,918,219 fo Wentorf, Jr., et al. discloses a method for converting hexagonal boron nitride to cubic boron nitride in the presence of catalyst material. Hexagonal boron nitride (hBN) is the low pressure graphitic powder form of boron nitride. hBN alone, under conditions of elevated temperature and pressure, does not form a sintered cBN compact containing the necessary physical properties to be useful as a machining tool. Instead, hBN forms a weakly intergranular bonded cBN structure having a high degree of interstitial voids that tend to exfoliate. However, hBN can be used as a suitable starting material and -31 will yield a desirable compact if a limited amount is combined with cBN crystals and an adjuvant material.
The use of cBN crystals as a starting material is know in the art. U.S. Patent No. 4,647,546 to Hall, Jr., et al. discloses a process for making a polycrystalline cBN compact by combining cBN with suitable adjuvant materials. cBN is indispensable for imparting the excellent properties of abrasive wear resistance and chipping resistance to the high pressure high temperature sintered compact. Further, cBN crystals act as nucleation sites when combined with hBN and adjuvant materials to facilitate the formation of the polycrystalline cBN structure during sintering.
Aluminum containing materials have certain desirable properties which have led to their use, separately, in prior art compositions. Use of aluminum as an aid in bonding cBN under high pressure, temperature conditions is taught by U. S. Patent No. 3,944,398 to Bell. Bell teaches the use of a material consisting of a boride, nitride, or silicide refractory substance and a solvent of aluminum, lead, tin, magnesium, lithium, or- alloys thereof. The preferred embodiment of Bell employs silicon nitride as the second refractory substance and aluminum as the solvent. Bell teaches that substantially all of the aluminum reacts with die silicon nitride to form aluminum nitride. The.resulting.cBN compact displays good thermal stability, enhanced impact resistance and performs well in aggressive cutting operations of hard ferrous alloys.
However, the large amount of hinder materials used, which are considerablysofterthan cBN, tend to interfere with intergranular cBN to cBN bonding and adversely affect the abrasive wear resistance of die sintered cBN compact.
Another hard material used in combination with cBN is one selected from a carbide, nitride, or carbonitride of a group IVb, Vb, and VIb transition metal of the Periodic Table. U.S. Patent No. 4,334,928 to Hara, et al. discloses cBN compacts made with hard materials selected from carbides, nitrides, carbonitrides, borides, and silicides of the group IVb, Vb, and VIb transition metals. Hara also teaches that a catalyst such as aluminum and/or silicon, may be added to the composition in a small amount. Ihe carbide, nitride, or carbonitride containing hard materials are chosen because of their ability to impart to the cBN compact enhanced chemical and impact resistance. The Hara, et al. patent neither intends nor achieves substantial direct cBN to cBN intergranular bonding, in part due to die low concentration of cBN. Accordingly, die low volume concentration of cBN and lack of substantial intergranular bonding produced a cBN compact having poor wear resistance in abrasive applications.
U.S. Patent No. 4,619,698 to Ueda, et al. discloses very high pressure sintered compacts of cBN containing at least one metal selected from die group consisting of -4cobalt and nickel. The use of cobalt as a binder material has been shown to improve the degree of sintering of the cBN compact.
Although the prior art discloses the advantages of making a cBN compact using a . variety of adjuvant materials, it does not disclose the process of combining these or other 5 adjuvant materials in the appropriate amount to produce an improved sintered polycrystalline cBN compact. Further, the methods described in the prior art are not the most economically advantageous methods for making the cBN compact because of the excessive material cost associated with using a high proportion of cBN crystals as a starting material.
It is therefore highly desirable to provide a method for making a sintered polycrystalline cBN compact, comprising the use of various adjuvant materials that act to facilitate the conversion of hBN to cBN and enhance the strength and degree of intergranular cBN to cBN bonding of the polycrystalline cBN compact and impart to the sintered cBN compact the level of abrasive wear resistance, impact resistance, thermal conductivity and stability needed to perform as a cutting tool. It is also desirable that the method of making the polycrystalline cBN compact be cost effective in terms of starting material costs.
According to the invention there is provided a process for preparing a sintered polycrystalline compact with substantial intercrystalline bonding from high pressure boron nitride which comprises: mixing grains of high pressure boron nitride with low pressure boron nitride, an aluminum containing adjuvant material, and a carbide nitride, or carbonitride containing hard material; subjecting the resulting mixture to elevated temperature in a non-oxidizing environment; placing the mixture onto a cemented tungsten-carbide/cobalt substrate; loading the mixture and substrate into a closed container; subjecting the closed container to elevated temperature and pressure conditions sufficient to melt cobalt from the substrate, and at which conditions the high pressure boron nitride is thermodynamically stable; and maintaining the elevated temperature and pressure conditions for a time sufficient to allow for substantial intercrystalline bonding to thereby sinter the compact. -5Summarv of the Invention There is provided in the practice of this invention, according to a preferred embodiment a method for preparing, at elevated temperature and pressure conditions a sintered polycrystalline compact of cubic boron nitride (cBN) from cBN crystals, hexagonal boron nitride (hBN) and adjuvant materials. cBN crystals having an average particle size less than about 5 micrometers are heat treated in a non-oxidizing atmosphere and combined with hBN particles and adjuvant materials. The hBN has an average particle size of less than about 10 micrometers and comprises in the range of from 30 to 60 percent by weight of the mixture. The other materials comprise; (a) an aluminum containing material selected from the group consisting of aluminum, aluminum nitride, and aluminum diboride, preferably aluminum nitride having an average particle size of less than about 10 micrometers and comprising in the range of from 2 to 7 percent by weight of the mixture, and (b) a carbide, nitride, or carbonitride containing material selected from the group of IVb, Vb, and VIb transition metals, preferably titanium cabonitride having an average particle size of about 2 micrometers and comprising in the range of from 2 to 40 percent by weight of the mixture.
If desired, tungsten carbide (WC) may be added as a hard material up to about 2 percent by weight of the mixture.
The mixture is compacted into a preform and heat treated. The preform is placed onto a cobalt cemented tungsten carbide substrate and loaded into a protective container, which is placed into the working chamber of a suitable high pressure, high temperature apparatus and subjected to elevated pressure conditions in excess of 20 kbar, preferably to between about 50 and 75 kbar, and then to elevated temperature conditions, preferably to between 1200 and 1600°C. These conditions are in the region of cBN crystal stability, and provide melting of the cobalt contained in the cemented tungsten carbide substrate and the conversion of hBN to cBN. Elevated pressure and temperature are maintained for a period of between 5 and 20 minutes to sinter the cBN crystals after which time the temperature and then the pressure are reduced and the compact recovered. -6Detailed Description In the preferred embodiments of the invention, cubic boron nitride (cBN) crystals of a particle size suitable for the intended application of the compact are thoroughly blended with a powder of hexagonal boron nitride (hBN) and adjuvant material.
The preferred adjuvant materials include; (a) an aluminum containing material selected from the group consisting of aluminum, aluminum nitride, aluminum diboride, or mixtures thereof, and (b) a carbide, nitride, or carbonitride containing material of the group IVb, Vb, and VIb transition metals from the periodic table.
In order to ensure enhanced intergranular bonding it is preferred that the particle size of the adjuvant material be approximately equal to that of the cBN crystals. As finer-grained compacts give greater impact resistance, perform suitably in aggressive cutting applications, and give smoother surfaces in finishing applications, a cBN particle size less than about 5 micrometers is preferred. It is preferred that the hBN have a particle size less than about 10 micrometers, that the aluminum containing adjuvant material have a particle size of less than about 10 micrometers, and that the carbide, nitride or carbonitride containing hard material have a particle size less than about 2 micrometers.
The preferred amount of cBN comprising the total mixture of cBN, hBN and adjuvant material is in the range of from 30 to 60 percent by weight. The preferred amount of hBN comprising the total mixture is in the range of up to 50 percent by weight. The preferred ratio of cBN to hBN is about 2:1. A cBN ratio greater than 2:1 produces a mixture that is very difficult to preform due to the inherent hardness of the cBN itself. A cBN ratio less than 2:1 produces a compact having a greater metal phase which greatly decreases die compact’s abrasive wear resistance.
The preferred amount of other material present in the total mixture of cBN, hBN and adjuvant material is in the range of from 5 to 50 percent by weight. The preferred aluminum containing adjuvant material is aluminum nitride (AIN) and may comprise from about 2 to 7 percent by weight of the total mixture. The desired range of AIN contained in the mixture is believed to be stoichiometrically dependant on the amount of hBN. It is believed that hBN is nitrogen deficient and that the AIN provides additional nitrogen as well as removing some boron nitride closer to stoichiometric BN. This facilitates hBN to cBN conversion. A mixture having less than 2 percent by weight AIN may not yield a compact having a high hBN to cBN conversion. A mixture having greater than 7 percent, while having a high hBN to cBN conversion, produces a compact having decreased abrasive wear resistance making die compact a less desirable cutting tool. -7The preferred carbide, nitride, or carbonitride containing hard material of the group IVb, Vb, and VIb transition metals is titanium carbonitride (TiCN) and may comprise from about 2 to 40 percent by weight of the total mixture. TiCN imparts chemical resistance to the cBN compact and a compact having less than 2 percent by weight TiCN does not possess the chemical resistance needed to function as a desirable cutting tool. Because TiCN is relatively softer than cBN, a mixture comprising greater than 40 percent TiCN produces a compact having decreased abrasive wear resistance.
If desired, tungsten carbide (WC) may be added as a hard material up to about 2 percent by weight of the total mixture.
Before combining the cBN crystals with the hBN and adjuvant materials, the cBN crystals are heat treated in a non-oxidizing and preferrably reducing atmosphere at a temperature of about 1000“C for a duration of about 1 to 2 hours. The non.oxidizing atmosphere may either be 104 to 10* Torr vacuum, hydrogen or ammonia. The purpose of the initial heat treatment is to remove any adsorbed water vapor, oxides and other volatile impurities that may interfere with the. intergranular cBN to The cBN crystals are then combined with the powders of the hBN and the adjuvant materials in the preferred weight ratio and thoroughly blended together with tungsten carbide balls and alcohol in a nitrogen charged ball mill. The mixture is then compacted into preforms and heat treated in a non-oxidizing reducing atmosphere at a temperature in the range of from 600 to 1000°C for a duration of about 4 hours. The non-oxidizing atmosphere may either be Iff* to 10* Torr vacuum, hydrogen or ammonia. Preferably, the temperature of heat treatment of the preform is about 1000°C for rapid reaction. If the temperature is less than about 600°C, boron oxide, BsOj, on the surface of hBN may not volatilize. On the other hand, if the temperature is more than about 1000°C, the aluminum nitride begins to vaporize.
Each preform is then placed onto a cobalt cemented tungsten-carbide/cobalt substrate and the preform and substrate are then loaded into a closed contain». Careful selection of container materials will minimize infiltration of undesirable dements into die compact or, alternatively, provide for infiltration of possible desirable elements. While molybdenum, nickel, titanium, zirconium, tungsten, and stainless steel have been found to be suitable, the preferred container material is niobium. The closed niobium container enclosing the substrate and preform to be sintered is surrounded by any well-known plastic pressure transmitting medium. The preferred pressure transmitting medium is a salt such as NaCl, however, hexagonal boron nitride, talc, etc., may also be utilized. -8The container, surrounded by the pressure transmitting medium, is placed within a graphite or metallic heater, surrounded by a pressure transmitting and gasket forming medium such as pyrophyllite, and placed into a chamber of a suitable high pressure, high temperature apparatus. After pressure in excess of about 20 kbar is applied to bring foe mixture into foe region of cBN thermodynamic stability, which is well-known to those skilled in foe art, electrical resistance heating is applied to melt the adjuvant material, convert foe hBN to cBN and sinter foe compact to maximum density. The preferred sintering time at the preferred conditions of at least 50 kbar and at least 1200°C is about 15 minutes.
After sintering is complete, foe electric heating current is slowly removed and the sample is allowed to cool to below 200°C, after which foe applied pressure is removed and the container is removed from the chamber. The compact is then recovered from foe container and readied for use in its final form.
When the charge in foe high pressure high temperature press reaches foe melting point of foe cobalt rich phase in foe cemented tungsten carbide, it melts and the liquid material infiltrates into foe preform of cBN, hBN and adjuvant materials. It is believed that foe aluminum bearing material, specifically aluminum nitride, along with a portion of foe boron nitride dissolves in foe liquid phase. As temperature decreases, boron nitride precipitates in the cubic crystal structure.
While not wishing to be bound by any theory it is theorized that foe excellent catalyst-solvent activity of the aluminum containing adjuvant material is a result of (1) dissolving foe aluminum in foe cobalt rich phase at a temperature significantly lower than the plastic flow point of cBN, providing for. catalytic activation of foe surfaces of foe cBN grains prior to the their complete compaction and enabling complete filing of pores for attainment of maximum density, (2) substantial wetting action for cBN, both as a result of reduction of surface oxides of boron by aluminum and because of foe large difference between foe melting temperature and foe sintering temperature, and (3) significant solubility in the liquid alloy for boron and nitrogen as a result of foe moderate chemical activity of foe diluted aluminum atoms, thereby enabling reversible dissolution of boron nitride and recrystalization as cBN.
The carbide, nitride, or carbonitride containing adjuvant material selected from foe group rvb, Vb, and VIb transition metals is known to have high abrasive wear resistance, heat resistance and chemical resistance characteristics. However, foe abrasive wear resistant qualities of this hard material does not surpass that of cBN alone. Accordingly, the weight percent of carbide, nitride, or carbonitride hard material used in foe mixture reflects a tradeoff between the increased heat resistance and chemical resistance and foe tendency to reduce cBN’s inherent abrasive wear -9resistance. In practice, a mixture comprising less than about 50 percent by weight nitride, carbide, or carbonitride containing material produces a cBN compact having a reasonably high degree of chemical resistance, heat resistance and abrasive wear resistance suitable for finish machining operations.
In using the compact of the invention as a cutting tool, it is enough that the edge of toe tool contains a hard and wear resistance layer comprising cBN and heat-resistant/wear-resistanthard material. Therefore, it is more advantageous to form a composite compact which comprises a polycrystalline cBN hard layer and a cemented carbide substrate integral with foe former, in view of foe cost and foe strength of the tool. The thickness of the hard layer in the complex compact varies according to the operating conditions of the cutting tool as well as the shape thereof, but is generally more than 0.5 millimeters. For a cemented carbide substrate, a tungsten carbide cemented carbide is most preferable since it has a high hardness, heat conductivity and toughness. The thickness of the cemented carbide substrate is generally more than about 2.0 millimeters.
The preferred method of producing this complex compact is as follows. There is previously prepared a substrate alloy of a suitable shape from a cemented metal carbide such astungsten carbide cemented with cobalt. A mixture of the cBN crystals, hBN and adjuvant material for forming a hard layer as an effective cutting edge is put .on,the substrate. The assembly is then hot-pressed by a super-pressure apparatus to sinter the cBN hard layer and at the same time to bond the cBN to the cemented carbide substrate. During foe hot pressing, foe cobalt containing liquid phase of foe cemented carbide substrate infiltrates into foe clearances between cBN particles, thus, forming a bond between foe cBN compact and foe tungsten carbide substrate.
The compact of foe invention has polycrystalline cBN, a second phase which is a carbide, nitride, and carbonitride containing hard material of foe group IVb, Vb, and VIb transition metals, and a third phase mainly composed of cobalt alloy containing residual adjuvant materials such as aluminum, aluminum nitride, and aluminum diboride. The hard materials have a lower rigidity than cBN, and more easily deform under super-pressures to form a densely compacted powder body before the appearance of foe liquid phase. As a result, in the compact of foe invention, there will occur only minimal permeation of foe liquid phase of foe cemented tungsten carbide substrate during hot pressing tinder super-pressures, which permeation may cause foe composition of foe hard layer to vary and foe heat resistance thereof to be lower. Combining cBN, hBN and adjuvant materials as described produces a compact comprising about 25 percent by weight cobalt phase which is highly desirable. -10The following examples demonstrate the practice of preferred embodiments of the invention.
EXAMPLE 1 cBN crystals, having an average particle size of about 3 micrometers, were heat treated in an ammonia atmosphere at 1000°C for 1½ hours. The cBN crystals were then intimately mixed with hBN powder having an average particle size of about 8 micrometers, titanium carbonitride (TiCN) powder having an average particle size of less than about 2 micrometers, aluminum nitride (AIN) powder having an average particle size of about 8 micrometers, and tungsten carbide (WC) powder having an average particle size of less than about 1 micrometer.
The cBN crystals, hBN powder and these three adjuvant materials were combined in the weight ratio of 50:35:8:5:2 and thoroughly mixed with tungsten carbide balls and alcohol in a nitrogen charged mill. The mixture was compacted into preforms having the approximate shape of the sintered cBN compact tool. The preforms were subjected to a preform heat treatment at about IO4 to 10* Torr vacuum and about 1000°C for about 4 hours. Each preform was placed onto a cemented tungsten carbide/cobalt substrate and both were loaded into a closed niobium container.
The closed container was surrounded with a NaCl pressure-transmitting medium, loaded into a pyrophyllite cell and subjected to high pressure at about 75 kbar and high temperature at about 1400°C to 1500°C. After maintaining the temperature for approximately 15 minutes, the load.was allowed to cool, and then the pressure was reduced. A microstructural analysis on the polished surface revealed a complete conversion of hBN to cBN and excellent cBN to cBN intercrystalline bonding. Micro hardness on the polycrystalline cBN layer was measured to be 3000/3200 Kg/mm2 using the Vickers Test Method. -11EXAMPLE2 cBN crystals having an average particle size of about 1.5 micrometers were mixed with hBN, titanium carbonitride, aluminum nitride, and tungsten carbide powders at the weight percent ratios listed in Table 1.
Table 1 * ===== Teat No. Cubic Boron Nitride (cBN) Hexagonal Boron Nitride (hBN) Aluminum Nitride (AIN) Titanium Carbo- nitride ITi(C.N)] Tungaten Carbide (WC) Coating on Substrate Heat Treatment Atmosphere 1 57 O 40 2 1 Nona Vacuum 2 57 O 38.5 3.5 1 TiC Hydrogen 3 57 O 37 5 1 TiC Ammonia 4 34 23 40 2 1 TiC Ammonia 5 34 23 38.5 3.5 1 TiC Vacuum 6 34 23 37 . 5 ’ 1 Nona Hydrogen Tests 1-3 cBN crystals having an average particle size of about 1.5 micrometers were combined with the adjuvant materials at the weight percent ratios listed in Table 1. The mixture was blended in die same manner as described in Example 1 and subjected to a heat treatment at about 1000°C for about 4 hours in a 10r* to 10* Torr vacuum, ammonia, or hydrogen atmosphere as listed in Table 1. The mixture was placed onto a cemented tungsten carbide/cobalt substrate and both were loaded into a high pressure .and high temperature cell as described in Example 1. The sealed load was subjected to high pressure at about 60 kbar and a high temperature at about 1400°C to 1500°C for approximately 15 minutes.
Tests 4-6 cBN crystals, hBN and the adjuvant materials were combined in die weight percent ratios listed in Table 1. The mixture was blended in the same manner as described in Example 1 and subjected to a heat treatment at about 1000°C for about 4 hours in a 104 to IO6 Torr vacuum, ammonia, or hydrogen atmosphere as listed in Table 1. The mixture was then compacted into preforms and subjected to a second heat treatment at identical conditions. After the heat treatment each preform was placed into a cemented tungsten carbide/cobalt substrate and then loaded into a high -12pressure and high temperature cell. The cell was subjected to a high pressure at about 60 kbar and a high temperature at about 1400°C to 1500°C for 15 minutes.
For Tests 1-6, completely bonded structures were observed on the polished surfaces of thus obtained blanks. The Vickers hardness value measured between 2700 to 3000 Kg/mm2.
EXAMPLE 3 cBN crystals having an average diameter of about 1.5 micrometers were mixed with hBN, titanium carbonitride, aluminum nitride, and tungsten carbide in the weight percent ratio shown in Table 2. cBN crystals were combined and blended with hBN and the adjuvant materials in the same manner as described in Example 1. For each test the mixture of cBN, hBN and adjuvant materials was subjected to an initial heat treatment in 104 to 10* Torr vacuum, ammonia, or hydrogen atmosphere at a temperature of about 1000°C for about 4 hours. The mixture was then compacted into preforms and subjected to yet another identical heat treatment process. The preforms were placed onto a cemented tungsten carbide/cobalt substrate and loaded into a high pressure, high temperature cell. The sealed load was surrounded with a NaCl pressuretransmitting medium, loaded into a pyrophyllite cell and then subjected to high pressure at about 60 kbar and a temperature above 1300°C for about 15 minutes.
Table 2 Test No. Cubic Boron Nitride (cBN) Hexagonal Boron Nitride (hBN) Aluminum Nitride (AIN) Titanium Carbo- nitride [Ti(C.N)] Tungsten Carbide (WC) Coating on Substrate Heat Treatment Atmosphere 1 53 39 5 2 1 TiC Hydrogen 2 53 39 3.5 3.5 1 None Ammonia LL 53 39 2 5 1 TiC Vacuum These tests revealed a completely sintered structure of cBN to cBN crystal bonding with an interstitial second ceramic phase. These blanks exhibited Vickers hardness values of about 3000 Kg/mm2.
The resulting compacts have a substantially continuous cBN crystalline matrix possessing advantageous qualities not found simultaneously in the prior art; namely, (1) a high volume cBN concentration with strong intergranular cBN to cBN bonding, resulting in high resistance to binder erosion by abrasive materials, (2) high thermal conductivity, together with (3) high wear resistance under aggressive conditions in -13cutting of ferrous alloys, (4) high thermal stability, (5) low coefficient of friction versus ferrous metals, (6) lack of chemical or metallurgical reaction with the workpiece, and (7) good impact resistance. This method of making foe polycrystalline cBN compact is also economically advantageous because it results in high hBN to cBN conversion. The use of hBN as a starting material reduces foe amount of higher priced cBN crystals needed as foe starting material. a It is possible within foe scope of this invention to practice a wide variety of compositions, adjuvant materials, and temperature and pressure conditions in cycles which will achieve foe same objective as these examples, and foe foregoing examples are designed to be illustrative rather than limiting. For example, while cubic boron nitride is foe preferable high pressure boron nitride phase, foe invention also may be carried out using wurzitic boron nitride or a mixture of cubic and wurzitic boron nitride as a starting material. Additionally, a small amount of tungsten carbide may be used as hard material.
Since many such variations may be made, it is to be understoodthat within foe scope of foe following claims, this invention may be practiced otherwise than specifically described.

Claims (17)

1. CTMMS:
1. A process for preparing a sintered polycrystalline compact with substantial intercrystalline bonding from high pressure boron nitride which comprises: mixing grains of high pressure boron nitride with low pressure boron nitride, 5 an aluminum containing adjuvant material, and a carbide, nitride, or carbonitride containing hard material; subjecting die resulting mixture to elevated temperature in a non-oxidizing environment; placing the mixture onto a cemented tungsten-carbide/cobalt substrate; 10 loading die mixture and substrate into a closed container; subjecting the closed container to elevated temperature and pressure conditions sufficient to melt cobalt from the substrate, and at which conditions the high pressure boron nitride is thermodynamically stable; and maintaining the elevated temperature and pressure conditions for a time IS sufficient to allow for substantial intercrystalline bonding to thereby sinter the compact.
2. The process as recited in claim 1 wherein the high pressure boron nitride is cubic boron nitride. 20
3. The process as recited in either one of claims 1 or 2 wherein the mixture contains in the range of from 30 to 60 percent by weight cubic boron nitride.
4. The process as recited in any one of thepreceding claims wherein the aluminum containing adjuvant material is at least one material selected from the group 25 consisting of aluminum, aluminum nitride, or aluminum diboride.
5. The process as recited in claim 4 wherein the selected aluminum containing adjuvant material is aluminum nitride. 30
6. The process as recited in claim 5 wherein the mixture contains in the range of from 2 to 7 percent by weight aluminum nitride.
7. The process as recited in any one of the preceding claims wherein the carbide, nitride, or carbonitride containing hard material is at least one material 35 selected from die group of carbides, nitrides, and carbonitrides of group IVb, Vb and VIb transition metals from die periodic table. -158. The process as recited in claim 7 wherein the selected carbide, nitride, or carbonitride containing hard material is titanium carbonitride.
8. 9. The process as recited in claim 8 wherein the mixture contains in the range of from 2 to 40 percent by weight titanium carbonitride. *
9. 10. The process as recited in any one of the preceding claims wherein the low pressure boron nitride material is hexagonal boron nitride.
10. 11. The process as recited in claim 10 wherein die weight ratio of high pressure boron nitride to hexagonal boron nitride is approximately 2:1.
11. 12. A process for preparing a sintered polycrystalline cubic boron nitride compact substantially as described.
12. 13. A process for preparing a sintered polycrystalline cubic boron nitride compact comprising the steps of: mixing cubic boron nitride crystals with hexagonal boron nitride, an aluminum containing adjuvant material selected from the group consisting of aluminum, aluminum nitride, and aluminum diboride, and a carbide, nitride, or carbonitride containing hard material of group IVb, Vb and VIb transition metals from the periodic table; compacting the mixture into a preform; subjecting the preform to an elevated temperature; placing the preform onto a cemented tungsten-carbide/cobalt substrate; subjecting the preform and substrate to elevated temperature and pressure conditions sufficient to melt cobalt in the substrate, at which conditions the cubic boron nitride is thermodynamically stable, whereby the cobalt infiltrates the mass of cubic boron nitride crystals causing intercrystalline bonding; and maintaining the elevated conditions for a time sufficient to allow for substantial intercrystalline bonding to thereby sinter the compact.
13. 14. The process as recited in daim 13 wherein foe mixture comprises in foe range of from 2 to 7 percent by weight aluminum containing adjuvant material. v
14. 15. The process as recited in either one of claims 13 or 14 wherein foe r mixture comprises in the range of from 2 to 40 percent by weight nitride, carbide, or carbonitride containing hard material. -1616. The process as recited in any one of the preceding claims wherein the mixture comprises in the range of from 30 to 60 percent by weight cubic boron nitride.
15. 17. The process as recited in any one of the preceding claims wherein the 5 initial elevated temperature treatment is conducted in a vacuum, ammonia, or hydrogen atmosphere at a temperature in the range of from 600 to 1000°C.
16. 18. The process as recited in any on of die preceding claims wherein die weight ratio of cubic boron nitride to hexagonal boron nitride is approximately 2:1.
17. 19. A process substantially as hereinbefore described with reference to Examples 1 to 3.
IE940108A 1994-02-07 1994-02-07 Synthesis of polycrystalline cubic boron nitride IE80882B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
IE940108A IE80882B1 (en) 1994-02-07 1994-02-07 Synthesis of polycrystalline cubic boron nitride

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IE940108A IE80882B1 (en) 1994-02-07 1994-02-07 Synthesis of polycrystalline cubic boron nitride

Publications (2)

Publication Number Publication Date
IE940108A1 IE940108A1 (en) 1995-08-09
IE80882B1 true IE80882B1 (en) 1999-05-05

Family

ID=11040292

Family Applications (1)

Application Number Title Priority Date Filing Date
IE940108A IE80882B1 (en) 1994-02-07 1994-02-07 Synthesis of polycrystalline cubic boron nitride

Country Status (1)

Country Link
IE (1) IE80882B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104941520A (en) * 2006-12-13 2015-09-30 戴蒙得创新股份有限公司 Abrasive compact with improved machinability

Also Published As

Publication number Publication date
IE940108A1 (en) 1995-08-09

Similar Documents

Publication Publication Date Title
US5326380A (en) Synthesis of polycrystalline cubic boron nitride
US5271749A (en) Synthesis of polycrystalline cubic boron nitride
US4647546A (en) Polycrystalline cubic boron nitride compact
JP3091221B2 (en) Polishing compact of cubic boron nitride and its manufacturing method
US4334928A (en) Sintered compact for a machining tool and a method of producing the compact
US4403015A (en) Compound sintered compact for use in a tool and the method for producing the same
KR101190963B1 (en) Method of making a cbn compact
EP0699642A2 (en) Whisker or fiber reinforced polycrystalline cubic boron nitride and diamond
US5368812A (en) Metal carbides and derived composites made by milling to obtain a particular nanostructural composite powder
US4217113A (en) Aluminum oxide-containing metal compositions and cutting tool made therefrom
JP3949181B2 (en) Diamond sintered body using hard alloy as binder and method for producing the same
JPH07188803A (en) Highly tough ceramic/metal composite material and its production
JP2523452B2 (en) High strength cubic boron nitride sintered body
EP0816304B1 (en) Ceramic bonded cubic boron nitride compact
GB2091763A (en) Laminated sintered compositions including boron nitride
IE80882B1 (en) Synthesis of polycrystalline cubic boron nitride
JPS644989B2 (en)
JPH0215515B2 (en)
JPS6137221B2 (en)
JP3481702B2 (en) Cubic boron nitride sintered body using hard alloy as binder and method for producing the same
JP2001179508A (en) Cutting tool
JPS6141873B2 (en)
JP2782524B2 (en) High density phase boron nitride based reaction sintered body and method for producing the same
AU645721B2 (en) Process for manufacturing ceramic-metal composites
AU639803B2 (en) Metal carbides and derived composites

Legal Events

Date Code Title Description
MM4A Patent lapsed