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Automated Construction and Insertion of Layer-by Layer Finite Element Sub-Models of Damaged Composites

机译:损坏复合材料的逐层有限元子模型的自动构建和插入

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Finite element models of composite structures are generally shell-based and modeledat the laminate level. More detailed layer-by-layer lamina-level models aresometimes needed for representing joints or for modeling defect growth processes.We describe a method and toolkit for automating the creation and insertion of layerby-layer finite element sub-models of composite laminate. We focus in particularon representing damage captured from nondestructive evaluation (NDE) measurements.The method is based on scripting existing simulation and solid modeling tools(ABAQUS and ACIS). It works even on complicated, curved CAD models. The submodellocation is identified by the intersection of a cylinder with the structure. Wethen execute a series of instructions to generate a new shell with the submodel regionremoved, generate the layer-by-layer submodel, and bond together the layersand models with desired boundary conditions and defects. The instructions representthe steps of lamination and bonding for creating the composite. The output of themethod includes CAD models of the new shell and each lamina within the submodel,and a Python script for ABAQUS that will load the CAD models, bond them together,and apply the specified boundary conditions.
机译:复合结构的有限元模型通常基于壳并进行建模 在层压板级别。更详细的逐层层级模型是 有时需要用来表示关节或为缺陷生长过程建模。 我们描述了一种用于自动创建和插入layerby-的方法和工具包。 复合材料层的层有限元子模型。我们特别关注 代表从无损评估(NDE)测量中捕获的损害。 该方法基于脚本编写现有的仿真和实体建模工具 (ABAQUS和ACIS)。它甚至适用于复杂的弯曲CAD模型。子模型 位置通过圆柱体与结构的交点确定。我们 然后执行一系列指令以生成带有子模型区域的新外壳 删除,生成逐层子模型,并将各层绑定在一起 以及具有所需边界条件和缺陷的模型。指示代表 层压和粘合步骤以创建复合材料。输出 方法包括新壳体的CAD模型和子模型中的每个层, 以及用于ABAQUS的Python脚本,该脚本将加载CAD模型,将它们绑定在一起, 并应用指定的边界条件。

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