航天用aa2195基复合材料力学性能试验研究

S. M, Dr. K. T. Balaram Padal
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引用次数: 0

摘要

现代铝铜锂(Al-Cu-li)基复合材料由于其轻量化、高强度、高刚度和优异的机械性能,在航空航天应用中有着很大的需求。本文研究了石墨和碳化硼等增强剂对AA2195复合材料力学性能和微观组织的影响。采用中频感应炉(MFIF),以田口L16正交阵列为序,以4个水平分别制备了两种增强剂。显微组织表明,增强材料在复合材料中分布均匀。x射线衍射(XRD)元素分析表明,形成的金属间化合物(IMCs)有助于细化微观结构,进一步提高力学性能。8%碳化硼(B4C)和6%石墨(Gr)制备的复合材料具有较好的抗拉强度、伸长率和硬度,分别为190.74 MPa、0.58和87.2VHN。复合材料在8点制成。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental Investigation on Mechanical Properties of AA2195-based MMCs for Space Applications
The modern Aluminium-Copper-Lithium (Al-Cu-li) based composites have a great demand in aerospace applications due to their lightweight, high strength, high stiffness, and superior mechanical properties. The present study explored the effect of reinforcements like graphite and boron carbide on the mechanical behaviour and microstructure of AA2195 composite The Medium Frequency Induction Furnace (MFIF) was used to fabricate the composites with two factors each at four levels ordered in Taguchi L16 orthogonal array. The microstructures revealed that the reinforcements were distributed uniformly throughout the composite. The elemental investigation observed by X-ray diffraction (XRD) revealed that the formed intermetallic compounds (IMCs) helped in refining the microstructure and further increasing the mechanical properties. The composite fabricated at 8% boron carbide (B4C) and 6% graphite (Gr) exhibited better ultimate tensile strength, % elongation, and hardness as 190.74 MPa, 0.58, and 87.2VHN, respectively. The composite fabricated at 8 .
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来源期刊
Current Materials Science
Current Materials Science Materials Science-Materials Science (all)
CiteScore
0.80
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0.00%
发文量
38
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