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Fatigue life estimation of explosive cladded transition joints with the use of the spectral method for the case of a random sea state

机译:随机海况情况下基于谱法的熔覆过渡接头疲劳寿命估算

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摘要

The problem with fatigue lifetime estimation of explosive cladded transition joints under random loading conditions has been described. The paper presents the fatigue test results performed for the random state of tension-compression under a generated spectrum according to the Pierson-Moskowitz model. The obtained spectrum has a non-Gaussian characteristic. The tested material consists out of a transition joint clad with four layers of aluminium alloy A5083, A1050, Titanium Grade 1 and steel Grade D. The material has been tested for the existence of residual stresses after the welding process with the hole drilling method. The welding process has been also simulated with ANSYS and the residual stresses have been generated for the Goldak volumetric distribution. The obtained values of residual stresses comprise to the values of real tests performed for the hole drilling method. The information about the residual stress values have been taken into account in the process of fatigue lifetime estimation in the form of non-zero mean stresses compensation inside the clad. The fatigue life has been calculated with the use of the frequency domain method. The Goodman mean stress compensation model has been used in the process of residual stress compensation. The non-gaussianity has been compensated with the use of the Bracessi formula. The obtained fatigue life assessment results have been compared with stand test results. The calculated results are within the scatter area of 3, but individual scatter values have been calculated for calculated series.
机译:已经描述了在随机载荷条件下估算熔覆过渡接头疲劳寿命的问题。本文介绍了根据Pierson-Moskowitz模型在生成的频谱下对随机压缩状态的拉伸进行疲劳测试的结果。所获得的光谱具有非高斯特性。被测材料由过渡接头包覆而成,该过渡层包覆有四层铝合金A5083,A1050,钛1级和钢D级。该材料已通过钻孔方法测试了焊接工艺后是否存在残余应力。还使用ANSYS对焊接过程进行了模拟,并为Goldak体积分布生成了残余应力。所获得的残余应力值包括针对钻孔方法进行的实际测试的值。在疲劳寿命估算过程中已经考虑了有关残余应力值的信息,其形式为包层内部的非零平均应力补偿。疲劳寿命已使用频域方法进行了计算。 Goodman平均应力补偿模型已用于残余应力补偿过程中。非高斯性已通过使用Bracessi公式进行了补偿。将获得的疲劳寿命评估结果与标准测试结果进行比较。计算结果在散布区域3内,但已为计算的序列计算了各个散布值。

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