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超高体积分数SiCP/Al复合材料颗粒级配设计与性能优化

Particle size distribution design and performance optimization of ultra-high volume fraction SiCP/Al composites

  • 摘要: 以航空航天精密仪器为典型应用场景,以超高模量、低膨胀系数为研发目标,设计超高体积分数SiCP/Al复合材料的颗粒级配方案并优化其性能。采用双颗粒级配方法,通过机械混粉工艺将不同粒径的碳化硅(SiC)颗粒与6061铝合金基体混合,系统探讨了颗粒级配中粗颗粒粒径对不同体积分数碳化硅复合材料力学性能和线膨胀系数的影响。结果表明:随着SiC颗粒体积分数的增加,所有配方复合材料的线膨胀系数均单调下降,当体积分数为70%时,增大粗SiC粒径会进一步降低材料的线膨胀系数。当粗颗粒粒径大于100 µm时,70%体积分数的复合材料弯曲强度有所下降,但弯曲模量、微屈服强度等力学性能均优于65%体积分数的复合材料,具有理想的综合性能。当粗颗粒粒径小于100 µm时(73 µm),由于粗颗粒间距过窄,引起细颗粒团聚,相对密度下降,70%体积分数的复合材料的力学性能不及67%体积分数样品。最终确定的最佳配方为123 µm与11 µm碳化硅颗粒质量比为3:1,体积分数为70%,其对应的复合材料弯曲强度为379.61 MPa,弯曲模量为264.34 GPa,线膨胀系数为7.10×10‒6 K‒1

     

    Abstract: Taking aerospace precision instruments as the typical application scenario, with ultra-high modulus and low expansion coefficient as the research and development goals, the particle size distribution design for ultra-high volume fraction SiCP/Al composite materials was designed and the performance was optimized. The influence of coarse particle size in particle gradation on the mechanical properties and linear expansion coefficient of the composites with different volume fraction silicon carbide (SiC) was systematically investigated by double-particle gradation method and mechanical powder mixing process. The results show that with the increase of SiC particle volume fraction, the linear expansion coefficient for all the composites monotonically decreases. When the volume fraction is 70%, increasing the coarse SiC particle size can further reduce the linear expansion coefficient. When the coarse particle size is greater than 100 µm, the flexural strength of the SiCP/Al composites with 70% volume fraction decreases somewhat, but the flexural modulus and micro-yield strength are superior to those of the composites with 65% volume fraction, demonstrating the ideal comprehensive performance. When the coarse particle size is less than 100 µm (73 µm), due to the overly narrow spacing between coarse particles, the fine particles agglomerate, and the relative density decreases, the mechanical properties of the composites with 70% volume fraction are inferior to those of the samples with 67% volume fraction. In the final determined optimal formula, the mass ratio of 123 µm to 11 µm silicon carbide particles is 3:1, and the volume fraction is 70%, the corresponding flexural strength of the composites is 379.61 MPa, the flexural modulus is 264.34 GPa, and the coefficient of linear expansion is 7.10×10‒6 K‒1.

     

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