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首页> 外文期刊>International journal of structural integrity >Finite element modeling of mandrel speed in cold expansion process
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Finite element modeling of mandrel speed in cold expansion process

机译:冷胀过程中心轴速度的有限元模拟

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摘要

Purpose - The bodies of aircraft structures have a lot of fastener holes and under different situations these holes bear external forces, which cause a tensile stress on the surface that leads to the failure of materials. Cold expansion process is one of the widely-used methods to improve the fatigue behavior of materials used in aerospace industry, and such improvement is due to the compressive residual stress around cold expanded hole. The induced residual stress distribution around cold expanded hole is affected by several parameters such as, diametrical interfaces, surface finish of fastener holes, temperature, mandrel speed, i.e. the speed of inserting mandrel into the hole, and so on. In previous studies, most of effective parameters were investigated, whereas, the effect of mandrel speed on the residual stress distribution has not been considered. The present study, seeks to simulate cold expansion process on aluminum alloy 2A12TA using ABAQUS finite element (FE) package and to consider the effect of different mandrel speeds on residual stress distribution around cold expanded hole. It aims to verify the results of FE simulation by experimental data. Design/methodology/approach - There are two kinds of data in this paper; experimental and FE results. The experimental results for cold expansion process have been extracted from the literature and ABAQUS finite element package was employed in order to simulate the above-mentioned process. Moreover, FE results were validated by the experiments. Findings - The results presented here show the influence of mandrel speed on residual stress distribution around cold expanded hole using a new analytical-numerical method. The results gained by FE simulation show relative differences between the diagrams of residual stress distribution corresponding different mandrel speeds. It is shown in the paper; the residual stress around cold expanded hole rises by the increase of mandrel speed and consequently the improvement of fatigue life will be achieved. Originality/value - The present study is part of Abbas Hosseini's MSc. dissertation, an original research work.
机译:目的-飞机结构的主体上有许多紧固件孔,在不同情况下,这些孔承受外力,这会在表面上产生拉应力,从而导致材料失效。冷膨胀工艺是改善航空航天业材料疲劳性能的一种广泛使用的方法,这种改进是由于冷膨胀孔周围的压缩残余应力所致。冷膨胀孔周围引起的残余应力分布受几个参数的影响,例如直径界面,紧固件孔的表面光洁度,温度,心轴速度(即,将心轴插入孔中的速度等)。在以前的研究中,大多数有效参数已得到研究,而心轴速度对残余应力分布的影响尚未考虑。本研究旨在使用ABAQUS有限元(FE)封装模拟铝合金2A12TA的冷膨胀过程,并考虑不同心轴速度对冷膨胀孔周围残余应力分布的影响。它旨在通过实验数据验证有限元模拟的结果。设计/方法/方法-本文有两种数据:实验和有限元结果。从文献中提取了冷膨胀过程的实验结果,并使用ABAQUS有限元程序包模拟了上述过程。此外,有限元结果得到了实验的验证。发现-使用新的解析数值方法,此处显示的结果显示了心轴速度对冷扩孔周围残余应力分布的影响。有限元模拟得到的结果表明,对应于不同心轴速度的残余应力分布图之间存在相对差异。如论文所示。随着心轴速度的增加,冷扩孔周围的残余应力增加,从而达到疲劳寿命的改善。原创性/价值-本研究是Abbas Hosseini的MSc的一部分。论文,原创研究工作。

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