Development in Mechanical and Fatigue Properties of AA6061/AL2O3 Nanocomposites Under Stirring Temperature (ST)

Raad Mohammed Abed, A. Khenyab, H. J. Alalkawi
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引用次数: 3

Abstract

Aluminum is expected to remain the core material for many critical applications such as aircraft and automobiles. This is due to the high resistance to different environmental conditions, desired and manageable mechanical properties, as well as high fatigue resistance. Aluminum nanocomposites such as AA6061/Al2O3 can be made in many ways using a liquid metallurgy method. The main challenges for this method in the production of nanocomposites are the difficulties of achieving a uniform distribution of reinforcing materials and possible chemical reactions between the reinforcing material and the matrix. For structural applications exclusive to aerospace sectors. The growing cost-effective nanocomposites mass production technology with essential operational and geometric flexibility is a big challenge all the time. Each method of preparing AA6061/Al2O3 nanocomposites can provide different mechanical properties. In the present study, nine nanocomposites were prepared at three stirring temperatures (800, 850, and 900 °C) with the level of Al2O3 addition of 0, 5, 7, and 9 wt %. The results of tensile, hardness and fatigue tests revealed that the composite including 9 wt % Al2O3 with 850 °C stirring temperatures has the best properties. It was also revealed that the 850 °C stirring temperature (ST) with 9 wt % Al2O3 composite provide an increase in tensile strength, VHN and reduction in ductility by 20 %, 16 % and 36.8 % respectively, compared to zero-nano. Also, the fatigue life at the 90 MPa stress level increased by 17.4 % in comparison with 9 wt % nanocomposite at 800 °C (ST). Uniform distributions were observed for all nine microstructure compositions.
搅拌温度下AA6061/AL2O3纳米复合材料力学与疲劳性能的研究进展
预计铝仍将是许多关键应用的核心材料,如飞机和汽车。这是由于高耐不同的环境条件,理想的和可控的机械性能,以及高抗疲劳性。铝纳米复合材料如AA6061/Al2O3可以通过多种方法使用液体冶金方法制备。这种方法在生产纳米复合材料时面临的主要挑战是难以实现增强材料的均匀分布以及增强材料与基体之间可能发生的化学反应。专用于航空航天领域的结构应用。随着纳米复合材料的大规模生产技术的不断发展,其成本效益和几何灵活性一直是一个巨大的挑战。制备AA6061/Al2O3纳米复合材料的不同方法可以提供不同的力学性能。在本研究中,在三种搅拌温度(800、850和900℃)下制备了9种纳米复合材料,Al2O3的添加量分别为0、5、7和9 wt %。拉伸、硬度和疲劳试验结果表明,添加9wt % Al2O3的复合材料在850℃搅拌温度下具有最佳性能。与零纳米相比,850°C搅拌温度(ST)和9wt % Al2O3复合材料的抗拉强度、VHN和塑性分别提高了20%、16%和36.8%。在800℃(ST)温度下,与9wt %纳米复合材料相比,90mpa应力水平下的疲劳寿命提高了17.4%。9种显微组织组成均呈均匀分布。
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