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Tungsten carbide composite lining material for centrifugal casting and tungsten carbide composite lining layer

机译:离心铸造用碳化钨复合衬里材料及碳化钨复合衬里层

摘要

PURPOSE:To improve the wear resistance, thc corrosion resistance and the strength of the inner surface of a cylinder of an injection molding machine at a low cost. CONSTITUTION:In a tungsten carbide composite lining material for centrifugal casting having the composition consisting of 30-45% tungsten carbide, 35-50% (in total) of nickel and cobalt, =1% molybdenum, =10% chromium, 1-3% boron, =2% manganese, 8-25% iron, =1% carbon, powder of spherical tungsten carbide of 6-12mum in mean grain size are used. The coefficient of thermal expansion of the lining material is smaller than that of the material to be lined by the difference of 3X10-6 deg.C. The coefficient of cubical expansion of tungsten carbide in the lining layer is 25-45%, and the grain spacing is 8-20mum in mean free path. The inexpensive centrifugal casting method forms thc lining excellent in the wear resistance, the corrosion resistance and the strength on the inner surface of a cylinder. The attackability to the counterpart can be reduced by adjusting the shape and grain size of tungsten carbide, and the machinability can also be improved.
机译:目的:以低成本提高耐磨性,耐腐蚀性和注塑机气缸内表面的强度。组成:在一种离心铸造的碳化钨复合衬里材料中,其成分由30-45%的碳化钨,35-50%(总计)的镍和钴组成,<= 1%钼,<= 10%铬,1使用-3%的硼,<= 2%的锰,8-25%的铁,<= 1%的碳,平均粒度为6-12μm的球形碳化钨粉末。衬里材料的热膨胀系数小于要衬里的材料的热膨胀系数,相差3X10 -6℃。内层碳化钨的立方膨胀系数为25-45%,平均自由程中晶粒间距为8-20μm。廉价的离心铸造方法在耐磨性,耐腐蚀性和气缸内表面上的强度方面形成了优异的衬里。通过调整碳化钨的形状和晶粒尺寸,可以降低对对方的侵蚀性,并且还可以改善切削性。

著录项

  • 公开/公告号JP2872571B2

    专利类型

  • 公开/公告日1999-03-17

    原文格式PDF

  • 申请/专利权人 NIPPON SEIKOSHO KK;

    申请/专利号JP19940110199

  • 发明设计人 CHIKARA KENJIRO;

    申请日1994-04-27

  • 分类号B22C3/00;B22D13/10;C22C1/05;C22C29/08;

  • 国家 JP

  • 入库时间 2022-08-22 02:29:30

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