...
首页> 外文期刊>Journal of Materials Processing Technology >Preliminary study on the microstructure and mechanical properties of dissimilar friction stir welds in aircraft aluminium alloys 2024-T351 and 6056-T4
【24h】

Preliminary study on the microstructure and mechanical properties of dissimilar friction stir welds in aircraft aluminium alloys 2024-T351 and 6056-T4

机译:飞机铝合金2024-T351和6056-T4的异种搅拌摩擦焊的组织和力学性能的初步研究

获取原文
获取原文并翻译 | 示例

摘要

Aircraft aluminium alloys generally present low weldability by traditional fusion welding process. The development of the friction stir welding has provided an alternative improved way of satisfactory producing aluminium joints, in. a faster and reliable manner. In the present work dissimilar Al alloys (AA2024-T351 and AA6056-T4) were friction stir welded. Butt joints were obtained by varying process parameters, namely the rotational speed (500-1200 rpm) and the welding speed (150-400 mm/min), while axial force and tool geometry were kept constant. Parameter optimisation, which has been based on the results of macrographic analysis and microhardness testing, indicated that sound joints can be obtained in the parameters range of rotational speed equal to 800 rpm and welding speed of 150 mm/min. Light and scanning electron microscopy in several positions revealed the presence of a lamellar material flow pattern due to the differential flow, suggesting material mechanical mixing within the stirred zone. High level of strain and temperatures usually over 400℃, resulted in a dynamically recrystallised stirred zone with refined grains. Tensile testing (standard flat L-T samples) has shown that strength is up to 90% of the weakest joining partner 6056-T4. Fracture took place in the thermo-mechanically heat affected zone of the alloy 6056-T4, where annealed structure led to decrease in microhardness. This behaviour was confirmed by microflat tensile testing, which indicated the drop in tensile strength and the associated increase of strain, in the regions of microhardness drop. This study has shown that in a dissimilar friction stir weld, the weaker component dictates the performance of the joint, where failure happens in the region of the greatest strength reduction related to annealing phenomena. Microscopic investigation as well as the evaluation of local mechanical properties has suggested that mechanical mixing is the major material flow mechanism in the formation of the stirred zone.
机译:飞机铝合金通常通过传统的熔焊工艺呈现出低焊接性。搅拌摩擦焊的发展提供了一种替代的改进方式,以更快,更可靠的方式令人满意地生产铝接头。在本工作中,摩擦搅拌焊接了不同的铝合金(AA2024-T351和AA6056-T4)。通过改变工艺参数获得对接接头,即旋转速度(500-1200 rpm)和焊接速度(150-400 mm / min),而轴向力和工具几何形状保持恒定。基于宏观分析和显微硬度测试结果的参数优化表明,在转速等于800 rpm和焊接速度为150 mm / min的参数范围内可以获得良好的接头。在不同位置的光学和扫描电子显微镜显示,由于流动不同,存在层状材料流动模式,这表明在搅拌区内材料机械混合。较高的应变水平和温度通常超过400℃,导致动态重结晶的搅拌区具有细化的晶粒。拉伸测试(标准的扁平L-T样品)显示,强度最高是最弱的连接伴侣6056-T4的90%。断裂发生在6056-T4合金的热机械热影响区,在该区退火结构导致显微硬度降低。此行为已通过微平面拉伸测试得到了证实,该测试表明在显微硬度下降的区域中,拉伸强度下降以及相关的应变增加。这项研究表明,在不同的搅拌摩擦焊中,较弱的部件决定了接头的性能,其中在与退火现象有关的强度降低最大的区域发生失效。微观研究以及对局部机械性能的评估表明,机械混合是搅拌区形成过程中的主要材料流动机理。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号