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Systems and Methods of Numerically Simulating Structural Behaviors of Airbag Made of Coated Fabric Material

机译:数值模拟涂层织物材料安全气囊结构行为的系统和方法

摘要

Methods of numerically simulating structural behaviors of airbag made of coated fabric material are disclosed. A special purpose finite element is configured to include a membrane element and a pair of dynamically configured slave elements, which provides additional bending resistance of the coated fabric material. At each solution cycle of a time-marching simulation, nodal locations of the slave elements are updated from corresponding averaged nodal normal vector, fabric thickness and coating thickness of the coated fabric material. The averaged nodal normal vector of a particular node is an average of element normal vector of those membrane elements connected to that particular node. Respective nodal locations are offset at a distance at either side of the corresponding node of the membrane element along the averaged normal vector. Using updated nodal locations, strains and stresses of the slave elements are obtained and then converted to internal nodal forces for additional bending resistance.
机译:公开了对由涂层织物材料制成的安全气囊的结构行为进行数值模拟的方法。特殊用途的有限元配置为包括膜元件和一对动态配置的从属元件,这对涂覆的织物材料提供了额外的抗弯曲性。在时间行进模拟的每个求解循环中,从属元素的节点位置根据相应的平均节点法向矢量,织物厚度和涂层织物材料的涂层厚度进行更新。特定节点的平均节点法向矢量是连接到该特定节点的那些膜单元的单元法向矢量的平均值。各个节点位置沿着平均法线向量在膜元件的相应节点的任一侧偏移一定距离。使用更新的节点位置,可以获得从属元件的应变和应力,然后将其转换为内部节点力,以获得额外的抗弯性。

著录项

  • 公开/公告号US2014180648A1

    专利类型

  • 公开/公告日2014-06-26

    原文格式PDF

  • 申请/专利权人 LIVERMORE SOFTWARE TECHNOLOGY CORPORATION;

    申请/专利号US201213721194

  • 发明设计人 THOMAS BORRVALL;

    申请日2012-12-20

  • 分类号G06F17/50;

  • 国家 US

  • 入库时间 2022-08-21 16:07:53

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