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    • 1. 发明授权
    • Reduction of stresses in the polycrystalline abrasive layer of a
composite compact with in situ bonded carbide/carbide support
    • 通过原位结合的碳化物/碳化物支撑减少复合材料的多晶磨料层中的应力
    • US5560754A
    • 1996-10-01
    • US489877
    • 1995-06-13
    • David M. JohnsonFrancis R. Corrigan
    • David M. JohnsonFrancis R. Corrigan
    • B24D3/00B01J3/06B22F7/06B24D3/06C04B35/645C04B37/00
    • B24D3/06B01J3/062B22F7/06C04B35/645C04B37/006B01J2203/062B01J2203/0645B01J2203/0655B01J2203/066B01J2203/0685C04B2237/123C04B2237/124C04B2237/125C04B2237/127C04B2237/36
    • The present invention is directed to polycrystalline diamond and cubic boron nitride (CBN) composite compacts and a method of making the same under high temperature/high pressure (HP/HT) processing conditions, and more particularly to HP/HT polycrystalline composite compacts having reduced abrasive layer stresses. The method of the invention involves making a metal carbide supported polycrystalline composite compact under conditions of high pressure and high temperature (HP/HT) in an HP/HT apparatus by the following steps:(a) placing within an enclosure a mass of abrasive particles, a first mass of metal carbide support material adjacent said abrasive particles, and a second mass of metal carbide support material adjacent said first mass with a layer of brazing filler alloy having a liquidus above about 700.degree. C. between said first and second masses;(b) subjecting said enclosure to said HP/HT conditions for a time sufficient to form a composite compact wherein said first carbide support is bonded to said second carbide support; and(c) recovering said composite compact.The resulting composite compact exhibits reduced abrasive table stresses such as result from the HP/HT processing conditions, and especially for composite compacts with thick carbide supports.
    • 本发明涉及多晶金刚石和立方氮化硼(CBN)复合压块及其在高温/高压(HP / HT)加工条件下制备相同的方法,更具体地涉及具有减少的HP / HT多晶复合材料 研磨层应力。 本发明的方法涉及通过以下步骤在HP / HT装置中在高压和高温(HP / HT)条件下制备金属碳化物负载的多晶复合压块(a)在外壳内放置一批磨料颗粒 邻近所述磨料颗粒的第一质量的金属碳化物支撑材料和与所述第一块相邻的第二块金属碳化物支撑材料,所述第一块与所述第一和第二块之间具有高于约700℃的液相线的钎焊填充合金层; (b)使所述外壳经历所述HP / HT条件足够长的时间以形成复合压块,其中所述第一碳化物支撑件结合到所述第二碳化物支撑件; 和(c)回收所述复合压块。 所得到的复合材料压实体表现出减少的磨料台应力,例如由HP / HT加工条件导致的,特别是对于具有厚的碳化物载体的复合材料。
    • 9. 发明授权
    • Polycrystalline cubic boron nitride abrasive and process for preparing
same in the absence of catalyst
    • 多晶立方氮化硼磨料及其制备方法,无催化剂
    • US4289503A
    • 1981-09-15
    • US47656
    • 1979-06-11
    • Francis R. Corrigan
    • Francis R. Corrigan
    • C04B35/583B01J3/06C04B35/5831C09K3/14B24D3/28
    • B01J3/062C04B35/5831C09K3/1418B01J2203/0645B01J2203/066B01J2203/0685
    • Cubic boron nitride has been made from powdered hexagonal boron nitride by a process which comprises vacuum firing of the HBN and conversion by high pressure-high temperature processing at 55-80 kilobars and 1600.degree. C. to the reconversion temperature.The high pressure reaction cell has a special design which prevents the entrance of impurities into the sample. This cell, referring to FIG. 2, comprises, for example, a carbon tube (8) enclosing concentric titanium sleeve (9). Within the cylinder defined by the tube and sleeve are: the HBN sample (4), carbon filler (3), shielding tantalum foil discs (2) and carbon end plugs (10).The vacuum firing is done at pressures of 10.sup.-5 --10.sup.-10 mm Hg, 1400.degree.-1900.degree. C., for 5 minutes--4 hours, and is believed to form a thin, free-boron coating on the HBN particles.The process works on both pyrolytic (turbostratic) and graphitic hexagonal boron nitride.Grinding grits formed by milling cubic boron nitride chunks recovered from the high pressure-high temperature process have resulted in higher grinding ratios than commercially available CBN.
    • 立方氮化硼已经由粉末状六方氮化硼制成,包括通过HBN的真空烧制和通过在55-80千磅和1600℃的高压高温处理转化为再转化温度的方法。 高压反应池具有防止杂质进入样品的特殊设计。 该单元参照图1。 如图2所示,包括例如包围同心钛套筒(9)的碳管(8)。 在由管和套筒限定的圆筒内是:HBN样品(4),碳填料(3),屏蔽钽箔盘(2)和碳端塞(10)。 真空烧制在10-5-10-10mmHg,1400-1900℃的压力下进行5分-4小时,据信在HBN颗粒上形成薄的自由硼涂层。 该方法在热解(涡旋)和石墨六方氮化硼两者中起作用。 通过研磨由高压 - 高温工艺回收的立方氮化硼块形成的研磨砂粒导致比市售CBN更高的研磨比。