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首页> 外文期刊>Journal of the European Ceramic Society >Multifunctional hetero-modulus composites in the B_4C-BN-TiC-SiC-C system
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Multifunctional hetero-modulus composites in the B_4C-BN-TiC-SiC-C system

机译:B_4C-BN-TiC-SiC-C系统中的多功能异模量复合材料

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Experiments have been carried out to develop multifunctional composites with improved properties and structure for use in air turbines, ballistic armor, cutting tools and atomic reactors. For optimization of the sintering process, microstructure improvement and increased plasticity we used MgO, Y_2O_3 additives. The composites contained carbon fiber (S-242 L_(av) = 370 ìm, d= 13 ìm) the carbide stoichiometric composition was maintained. Sintering was by hot pressing (25 MPa) in vacuum in the interval of 1800-1900 °C with dwell time 5-7 min. Structural analysis proved the homogeneous structure of the composite. The properties satisfy ISO standards. In summary, H_v = 24GPa, compressive strength=2300 MPa, HRA = 94, bending strength = 500-600 MPa.
机译:已经进行了实验,以开发具有改进的性能和结构的多功能复合材料,用于航空涡轮机,弹道装甲,切削工具和原子反应堆。为了优化烧结工艺,改善微观结构和增加塑性,我们使用了MgO,Y_2O_3添加剂。复合材料包含碳纤维(S-242 L_(av)= 370ìm,d = 13ìm),保持了碳化物化学计量组成。通过在真空中以1800-1900°C的间隔热压(25 MPa)进行烧结,保压时间为5-7分钟。结构分析证明了复合材料的均匀结构。性能满足ISO标准。总之,H_v = 24GPa,抗压强度= 2300MPa,HRA = 94,抗弯强度= 500-600MPa。

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