Microstructural modification, mechanical properties, and wear behaviour of aged Al–Si–Mg/Si3N4 composites for aerospace applications

Q1 Engineering
Chinmay Mundayadan Chandroth , Jithin Vishnu , Bassiouny Saleh , K.R. Ananthakrishnan , Deva Narayan A , Aswin R. Kurup , Sidharth S , Karthik V. Shankar
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引用次数: 0

Abstract

The main objective of the present research is to probe how ageing time influences the morphological, mechanical, and wear behaviour of stir cast Al–Si–Mg alloy, reinforced with 10 wt% Si3N4 particles subsequently heat treated in T6 condition. The findings reveal that the presence of Si3N4 reinforcements, followed by the heat treatment, enhances the mechanical and tribological properties of the composite. The ensuing mechanical properties show significant improvement prior to aging heat treatment (180 °C/4h), reaching a hardness of 120.8 HV (45 % increase) and tensile strength of 275 MPa (50 % increment), respectively compared to as-cast composite. Fractography reveals dimples, transgranular cleavage surfaces, cracks, and micro-ploughing. Among the samples tested, the composite aged for 4 h (180 °C/4h, ASN-4) demonstrates the lowest wear rate. Abrasive and adhesive wear in combination is the primary wear mechanism in these samples. Overall, this research provides insights for research endeavors in manufacturing various components in the aerospace industry.
用于航空航天应用的老化铝硅镁/Si3N4 复合材料的微结构改性、力学性能和磨损行为
本研究的主要目的是探讨时效时间如何影响搅拌铸造Al-Si-Mg合金的形态、力学和磨损行为,并在T6条件下进行热处理,增强10 wt%的Si3N4颗粒。结果表明,Si3N4增强剂的存在和热处理提高了复合材料的力学性能和摩擦学性能。时效热处理(180°C/4h)前,复合材料的力学性能得到显著改善,硬度达到120.8 HV(提高45%),抗拉强度达到275 MPa(提高50%)。断口学显示了韧窝、穿晶解理面、裂纹和微犁耕。在测试样品中,时效4h(180°C/4h, ASN-4)的复合材料磨损率最低。磨料和黏着磨损的结合是这些样品的主要磨损机制。总体而言,本研究为航空航天工业中制造各种部件的研究工作提供了见解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
International Journal of Lightweight Materials and Manufacture
International Journal of Lightweight Materials and Manufacture Engineering-Industrial and Manufacturing Engineering
CiteScore
9.90
自引率
0.00%
发文量
52
审稿时长
48 days
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