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Evaluation of Microstructure and Mechanical Properties of Multi Axial Forged LM2 Aluminum Alloy

机译:多轴锻造LM2铝合金微观结构和力学性能评价

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摘要

Light metal Al alloys are presently used in aerospace and industrial applications. Hence, in the present study choice of material will be LM2 aluminum alloy and processed by multi-axial forging (MAF) technique at ambient temperature for different number of passes with an equivalent strain of 0.18, 0.36 and 0.54. Microstructural analysis was carried out on unprocessed and processed samples with scanning electron microscopy (SEM). As the number of MAF pass increases the average grain size was reduced because of plastic deformation by plane strain condition. Mechanical properties like Vickers hardness (VHN), tensile and compression test were carried out. Ultimate tensile strength (UTS) was increased after each pass of MAF due to strain hardening effect. After 3 MAF passes the compression strength was reached to maximum of 495 MPa as compared to as received sample 315 MPa and hardness, increased to 81 VHN as compared to 55 VHN for the received samples. The fractography analysis was explained using SEM images. As the number of passes increases dimple size reduces as compared to as received samples and which will be revealing the ductile mode of fracture.
机译:目前在航空航天和工业应用中使用轻金属Al合金。因此,在本研究的材料选择中,材料将是LM2铝合金,并通过多轴锻造(MAF)技术在环境温度下处理,以不同数量的通过0.18,0.36和0.54。通过扫描电子显微镜(SEM)在未加工和加工样品上进行微结构分析。由于MAF通过的MAF通过的数量增加,由于平面应变条件的塑性变形,平均粒度降低。采用维氏硬度(VHN),拉伸和压缩试验等机械性能。在MAF由于应变硬化效果导致的每次通过后,增加了极限拉伸强度(UTS)。与接受的样品315MPa和硬度相比,3MAF通过达到最大495MPa的压缩强度,与接受的样品的55 VH相比,增加至81 VH。使用SEM图像解释Fretography分析。随着通过的次数增加,与所接受的样品相比,凹弱的尺寸减少,并且它将揭示裂缝的延性模式。

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