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Computational method for in-situ finite element modeling of inflatable membrane structures based on geometrical shape measurement using photogrammetry

机译:基于摄影测量的几何形状测量的充气膜结构现场有限元建模的计算方法

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Inflatable membrane structures with the advantages of light weight, large span, long duration and aesthetical appearance have gained considerable attentions from buildings, super-pressure balloons, airships and deployable antennas. This paper presents a novel computational method for in-situ finite element modeling of inflatable membrane structures based on geometrical shape measurement using photogrammetry for further structural analysis. Firstly, kinematic equations of membrane link structure simplified from the measured inflatable membrane structure are established on force equilibrium between membrane internal and external forces to calculate the tensile forces. Then, computational method for solving zero-stress state is proposed through unloading internal pressure based on equilibrium matrix theory. Finally, true finite element model is established through numerical simulation of reloading internal pressure with considering the zero-stress state as initial model. For verifying purpose, inflated forming and normal working tests of an ethylene-tetrafluoroethylene (ETFE) air-inflated cushion structure were carried out. By comparing geometrical shapes and stress distributions of ETFE cushion between numerical and experimental results, good agreements with 0.72% and 4.76% maximum errors are acquired. These findings strongly confirm the need of in-situ finite element modeling of inflatable membrane structures undergoing long-term service and provide an effective computational method for further structural analysis. (C) 2019 Elsevier Ltd. All rights reserved.
机译:具有重量轻,跨度大,持续时间长和美观的优点的可充气膜结构已经受到建筑物,超压气球,飞艇和可展开天线的相当大的关注。本文提出了一种新的计算方法,用于基于充气摄影结构的几何形状测量的可充气膜结构的现场有限元建模,以进行进一步的结构分析。首先,在膜的内外力之间建立力平衡,从测量的可充气膜结构简化了膜连接结构的运动学方程,以计算拉力。然后,基于平衡矩阵理论,提出了一种通过卸荷来解决内应力零状态的计算方法。最后,以零应力状态为初始模型,通过对内压再加载的数值模拟,建立了真实的有限元模型。为了验证目的,进行了乙烯-四氟乙烯(ETFE)充气垫结构的充气成型和正常工作测试。通过在数值结果和实验结果之间比较ETFE缓冲垫的几何形状和应力分布,可以得出最大误差为0.72%和4.76%的良好一致性。这些发现强烈证实了对长期使用的可充气膜结构进行现场有限元建模的需求,并为进一步的结构分析提供了有效的计算方法。 (C)2019 Elsevier Ltd.保留所有权利。

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