Cu-Ti-C-B SHS复合材料的热物理性质

N. Pugacheva, T. Bykova, E. Senaeva, L. Goruleva
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摘要

本文研究了以铜、钛、碳化硼(B4C)和碳粉为初始混合物,通过自蔓延高温合成(SHS)制备的Cu-Ti-C-B复合材料的热物理性能。复合材料的基体是钛在铜晶格中的过饱和固溶体,在冷却下均匀析出Cu4Ti纳米颗粒。基体显微硬度为450hv0.1。由SHS产生的碳化钛(TiC)和二硼化钛(TiB2)颗粒在复合材料中随机分布。TiC颗粒优势区显微硬度为640 HV 0.1, TiB2颗粒优势区显微硬度为900 HV 0.1。复合材料的平均硬度为60 HRC。差示扫描量热法表明,在750 ~ 1000°С温度范围内存在统一的宽放热效应,其焓为148.6 J/g,与残余钛和碳化硼(B4C)之间的放热反应有关,而在SHS过程中没有发生反应。通过实验确定了密度、热扩散系数、热容、导热系数和线性热膨胀系数对温度的依赖关系。与纯铜相比,强化相颗粒略微降低了复合材料的热性能。结果表明,800℃和860℃退火可降低复合材料基体的残余应力水平。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Thermophysical properties of a Cu–Ti–C–B SHS composite
The paper studies the thermophysical properties of a Cu-Ti-C-B composite produced by self-propagating high-temperature synthesis (SHS) of an initial mixture of copper, titanium, boron carbide (B4C), and carbon powders. The matrix of the composite is a supersaturated solid solution of titanium in a copper lattice with Cu4Ti nanosized particles homogeneously precipitated under cooling. The matrix microhardness is 450 HV 0.1. Particles of titanium carbide (TiC) and titanium diboride (TiB2) resulting from SHS are randomly distributed in the bulk of the composite. The microhardness of the regions with the predominance of TiC particles is 640 HV 0.1, and the microhardness of the regions with the predominance of TiB2 particles is 900 HV 0.1. The average hardness of the composite is 60 HRC. Differential scanning calorimetry demonstrates a unified wide exothermic effect at temperatures ranging from 750 to 1000 °С, with an enthalpy of 148.6 J/g, associated with the exothermic reaction between residual titanium and boron carbide (B4C), which did not react during SHS. The temperature dependences of density, thermal diffusivity, heat capacity, thermal conductivity, and the coefficient of linear thermal expansion are experimentally determined. The particles of the strengthening phases are found to reduce slightly the thermal properties of the composite compared to pure copper. It is shown that annealing at temperatures of 800 and 860°C decreases the level of residual stresses in the composite matrix.
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