基于热弹塑性有限元法的三维初始缺陷加筋板极限强度分析与试验研究

EXPERIMENTAL STUDY AND ULTIMATE STRENGTH ANALYSIS OF STIFFENED PANELS WITH 3D INITIAL IMPERFECTIONS BASED ON THERMAL ELASTO-PLASTIC FEM

  • 摘要: 焊接诱导的初始缺陷是影响结构极限强度的关键因素。目前极限强度分析时普遍对其作简化处理或不予考虑,导致结果存在显著不确定性。基于热弹塑性有限元法,数值模拟某船用加筋板角焊缝的焊接过程,准确评估其焊后三维初始变形与残余应力作为初始缺陷引入极限强度分析模型,设计并开展相关试验验证方法的准确性。在此基础上,系统对比屈曲模态法、经验公式法和热弹塑性有限元法三种初始缺陷评估方法的特点及在极限强度分析中的差异,并分析缺陷形式、受力状态对含缺陷加筋板极限强度的影响机理。研究表明:初始缺陷评估方式是影响加筋板极限强度分析结果的重要因素;热弹塑性有限元法能准确、合理地反映结构的初始缺陷,与试验结果吻合良好,但需仔细考虑焊接边界条件。对于该文的研究模型,相较于初始变形,残余应力对极限强度影响更大,但二者耦合作用未产生明显更不利的影响;不同受力状态下,横向残余应力的分布变化是影响极限强度和应力-应变曲线的关键因素。

     

    Abstract: Welding-induced initial imperfections significantly influence the ultimate strength of hull structures. Conventional ultimate strength analyses often simplify or neglect these imperfections, introducing a considerable uncertainty. One thermal elastic-plastic finite element method is employed to simulate fillet welding in stiffened panels, and to obtain the three-dimensional welding distortion and residual stress as initial imperfections for the ultimate strength analysis. And experiments are conducted for a validation. Various imperfection evaluation methods (including the buckling mode method, empirical formulas and thermal elastic-plastic finite element method) are compared for their characteristics and impact on ultimate strength analyses. The effects of imperfection types and of loading conditions on the defective stiffened panel’s ultimate strength are also investigated. Research results show that the imperfection evaluation methods considerably influence ultimate strength analyses. The thermal elastic-plastic finite element method accurately captures welding-induced imperfections, showing a good agreement with experimental results. The welding boundary conditions require a careful consideration. For the model studied, the residual stress exhibits a more pronounced effect on ultimate strength than that of initial distortion, but their coupling effect does not have a more adverse impact. Under varying loading conditions, changes in the transverse residual stress distribution are crucial to ultimate strength and to stress-strain curves.

     

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