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Forming limit of local loading forming of Ti-alloy large-scale rib-web components considering defects in the transitional region

机译:考虑过渡区缺陷的钛合金大型肋腹板局部加载成形的成形极限

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The forming quality in the transitional region largely determines the formability of local loading forming of the large-scale rib-web component. Thus, it is very critical to determine the forming limit considering defects in the transitional region during local loading forming. In this paper, the stepwise searching method based on Kriging metamodels of defect indexes is adopted to determine the above forming limit. First, the finite element (FE) simulation of the transitional region during local loading forming and the evaluation indexes for folding and cavum defects are introduced. Then, the Kriging metamodels of defect indexes are developed based on quantities of FE simulation results under various geometry parameters. During Kriging metamodeling, in order to guarantee the accuracy of the metamodel in the global design space and interesting region simultaneously, the space-filling maximin Latin hypercube designs (maximin LHDs) and sequential sampling approach are employed to design sample points. After metamodeling, extra random samples designed within the whole space are simulated to validate the developed Kriging metamodels. At last, the method of determining the forming limit considering defects in the transitional region is presented and applied to two specific transitional region models. It is realized through stepwise searching based on Kriging metamodels of defect indexes. The application results show that the proposed method is an effective and reliable method to determine the forming limit considering defects in the transitional region. It would provide an important guideline in the processing design of local loading forming of titanium alloy large-scale rib-web components.
机译:过渡区域的成形质量在很大程度上决定了大型肋腹板部件局部载荷成形的可成形性。因此,在局部载荷成形期间考虑过渡区域中的缺陷来确定成形极限是非常关键的。本文采用基于缺陷指标的克里格元模型的逐步搜索方法来确定上述成形极限。首先,介绍了局部载荷成形过程中过渡区域的有限元模拟,以及折叠和凹痕缺陷的评估指标。然后,基于各种几何参数下有限元仿真结果的数量,建立缺陷指标的Kriging元模型。在Kriging元模型化过程中,为了同时确保全局设计空间和感兴趣区域中元模型的准确性,采用空间填充的maximin Latin超立方体设计(maximin LHD)和顺序采样方法来设计采样点。在进行元建模之后,将对整个空间中设计的额外随机样本进行仿真,以验证已开发的Kriging元模型。最后提出了一种考虑过渡区域缺陷的成形极限确定方法,并将其应用于两个特定的过渡区域模型。它是通过基于缺陷索引的Kriging元模型逐步搜索来实现的。应用结果表明,该方法是一种考虑过渡区域缺陷确定成形极限的有效而可靠的方法。这将为钛合金大型肋腹板零件局部载荷成形的加工设计提供重要指导。

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