首页> 外文学位 >Simulations of thermoforming and blow-molding manufacturing processes for load-bearing structural components.
【24h】

Simulations of thermoforming and blow-molding manufacturing processes for load-bearing structural components.

机译:承重结构部件的热成型和吹塑成型制造过程的仿真。

获取原文
获取原文并翻译 | 示例

摘要

Thermoforming and blow molding are two related processes that can be characterized as inflating a pre-heated polymeric membrane into a mold. The most important issue of these manufacturing processes is to control the distribution of thickness of final product. Utilizing differential heating in thermoforming and varying the initial thickness distribution of parison in blow molding, it provides a way to control the final thickness distribution of a formed part. However, both control techniques will require some predication of the final product to determine the control parameters that are required at the beginning of these processes. Historically, these control parameters are obtained by trial and error. As a result, the development of new mold designs and the thermal process parameters has been inefficient and expensive.; The purpose of present study is to investigate the final thickness and temperature distributions of a formed part that will be used to optimize the control parameters at the beginning of the manufacturing processes. By plotting the final thickness distribution at final deformed state on the initial configuration, one can obtain the information of final thickness for every material point. This information can be used to determine the control parameters of differential heating by specifying the heating temperature on individual region of the polymeric sheet in thermoforming to obtain the desired material properties at the specified temperature. In blow molding, it can be used to determine the initial thickness distribution of extruded parison.; In the proposed numerical model, first the parison is inflated freely without any contact with the mold cavity along with the convection heat transfer. Then the polymer hits the mold surface and the heat is transferred from the membrane to the mold surface. Finally, all parts of the membrane contact the mold and the membrane is cooled. Using membrane analogy, the behavior of a parison sheet for thermoforming or a tube for blow molding is analyzed by finite element analysis. In addition to deformation analysis for both axisymmetric and three-dimensional cases, a one-dimensional cooling analysis is also considered to account for the heat transfer from membrane to the air or mold.; This analysis is first verified by theoretical solutions. A set of experimental data from previous literature is also applied to show the agreement. It is found that the thinnest part of the final product is always at the material point that has longest travel path from the undeformed configuration to deformed configuration. To obtain more uniform thickness distribution predicted by the program, one can adjust the initial thickness distribution of the membrane by setting the initial thickness of the corresponding finite elements, re-run the program a couple times until the desired final thickness distribution is obtained. Following this analysis, the stresses and strains obtained by the program can be transferred to a standard structure analysis program to perform residual analysis as well as to determine load-bearing capability to accelerate the design cycle.
机译:热成型和吹塑是两个相关的过程,其特征可以是将预热的聚合物膜充气到模具中。这些制造过程中最重要的问题是控制最终产品的厚度分布。利用热成型中的差热并在吹塑中改变型坯的初始厚度分布,它提供了一种控制成型零件的最终厚度分布的方法。但是,两种控制技术都需要对最终产品进行某种预测,以确定在这些过程开始时所需的控制参数。从历史上看,这些控制参数是通过反复试验获得的。结果,新模具设计和热处理工艺参数的开发效率低下且昂贵。本研究的目的是研究成型零件的最终厚度和温度分布,这些厚度和温度分布将用于在制造过程开始时优化控制参数。通过在初始结构上绘制最终变形状态下的最终厚度分布,可以获取每个材料点的最终厚度信息。通过在热成型过程中在聚合物片材的各个区域上指定加热温度,从而在指定温度下获得所需的材料性能,可以将该信息用于确定差异加热的控制参数。在吹塑中,它可用于确定挤压型坯的初始厚度分布。在所提出的数值模型中,首先对型坯进行自由充气,而对流传热则不与型腔接触。然后,聚合物撞击模具表面,热量从膜传递到模具表面。最后,膜的所有部分都与模具接触,然后将膜冷却。使用膜类比,通过有限元分析来分析用于热成型的型坯板或用于吹塑的管的性能。除了轴对称和三维情况的变形分析外,还考虑一维冷却分析来说明从膜到空气或模具的热传递。该分析首先通过理论解得到验证。一组来自先前文献的实验数据也被用于证明一致性。发现最终产品的最薄部分总是在从未变形构型到变形构型的行程路径最长的材料点上。为了获得该程序预测的更均匀的厚度分布,可以通过设置相应有限元的初始厚度来调整膜的初始厚度分布,重新运行该程序几次,直到获得所需的最终厚度分布。经过此分析,可以将程序获得的应力和应变转移到标准结构分析程序中,以执行残差分析以及确定承载能力,从而加快设计周期。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号