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Research of large scale mechanical structure crack growth method based on finite element parametric submodel

机译:基于有限元参数子模型的大规模机械结构裂纹生长方法研究

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摘要

With the development of mechanical structure in large scale, the dimension difference between whole structure and part damage-crack can be widely further. In order to get a precise analytic result of crack structure the grid of crack structure finite element model should be meshed very dense so that the calculation scale is very large and calculation efficiency is lower even the calculation cannot be completed. To solve this mull scale problem of crack structure, presently the submodel method is used, but in the method crack growth trajectory need to be supposition and the crack model also need to be built by man-made, which is not satisfied with need of mix-mode crack growth especially for continuously reconstructing of crack model. In this paper the parametric submodel will be put forward. The method describes crack coarse model and submodel data by parameter way, including meshing, load, boundary condition etc. In the method dynamic relationship of analytical results between coarse model and submodel is built, so that crack stress intensity factor and growth angle can be automatically calculated for every crack tip. According to the dynamic modification of crack coarse model and submodel, the crack growth trajectory simulation can be calculated through iterative steps instead of the traditional supposition growth trajectory and crack propagation life calculation can also be finished. The method gets the accuracy crack growth trajectory and improves analytical efficiency. At last the case of the crack growth trajectory and life analysis in gantry crane verifies the validity of this method.
机译:随着机械结构大规模的发展,整个结构与部件损伤裂缝之间的尺寸差异可以广泛进一步。为了获得裂缝结构的精确分析结果,裂缝结构的电网应啮合非常致密,使得计算比例非常大,并且计算效率均匀降低,即使计算也无法完成。为了解决这种裂缝结构的MULL比例问题,目前使用子模型方法,但在方法中,裂纹增长轨迹需要假设,并且裂缝模型也需要由人造建造,这对COME不满意 - 模特裂纹增长,尤其是裂缝模型的连续重建。在本文中,将提出参数化子模型。该方法通过参数方式描述裂缝粗略模型和子模型数据,包括啮合,负载,边界条件等。在构建粗模型和子模型之间的分析结果的方法动态关系,使裂纹应力强度因子和生长角可以自动计算每个裂缝尖端。根据裂纹粗模型和子模型的动态修改,可以通过迭代步骤来计算裂缝生长轨迹模拟,而不是传统假设生长轨迹,并且还可以完成裂纹传播寿命计算。该方法获得精度裂纹增长轨迹并提高分析效率。最后,龙门起重机裂纹生长轨迹和寿命分析验证了这种方法的有效性。

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