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

机译:涂层织物材料安全气囊结构行为数值模拟的系统和方法

摘要

Methods for numerically simulating the structural behavior of an airbag made of a coated textile material are disclosed. A special purpose finite element is constructed to include the membrane element and a pair of dynamically constructed slave elements, providing additional bending resistance of the coated fabric material. In each solution cycle of the time-advanced simulation, the positions of the nodes of the slave elements are updated from the normal vector of the corresponding average node, the fabric thickness, and the coating thickness of the coated fabric material. The average node's normal vector is the average of the element normal vectors of the membrane elements connected to that particular node. The positions of each node are offset along a mean normal vector at a certain distance from either side of the corresponding node of the membrane element. Using the updated node positions, strains and stresses of the slave elements are obtained and then converted to the internal node's forces for additional bending resistance.
机译:公开了用于数值模拟由涂覆的纺织材料制成的安全气囊的结构行为的方法。特殊用途的有限元构造为包括膜元件和一对动态构造的从动元件,从而为涂层织物材料提供了额外的抗弯性。在时间提前模拟的每个求解周期中,从属元素的节点位置会从相应平均节点的法线向量,织物厚度和涂层织物材料的涂层厚度中进行更新。平均节点的法向矢量是连接到该特定节点的膜元件的元件法向矢量的平均值。每个节点的位置都沿着平均法线矢量偏离了膜元件相应节点两侧的一定距离。使用更新后的节点位置,可以获得从属元素的应变和应力,然后将其转换为内部节点的力,以获得附加的抗弯强度。

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