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Reinforcement by polyurethane to stiffness of air-supported fabric formwork for concrete shell construction 被引量:2
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作者 GUO Xiao qian sheng-shen +1 位作者 QING qiang GONG Jing-hai 《Journal of Central South University》 SCIE EI CAS CSCD 2019年第9期2569-2577,共9页
By spraying concrete on inner surface,air-supported fabric structures can be used as formwork to construct reinforced concrete shell structures.The fabric formwork has the finished form of concrete structure.Large dev... By spraying concrete on inner surface,air-supported fabric structures can be used as formwork to construct reinforced concrete shell structures.The fabric formwork has the finished form of concrete structure.Large deviation from the desired shape of concrete shells still remains as central problem due to dead weight of concrete and less stiffness of fabric formwork.Polyurethane can be used not only as a bonding layer between fabrics and concrete but also as an additional stiffening layer.However,there is little research on mechanical behaviors of the polyurethane shell structure.This paper presents experimental studies on an inflated fabric model with and without polyurethane,including relief pressure tests,vertical loading tests and horizontal loading tests.Experimental results show that the additional polyurethane layer can significantly enhance the stiffness of the fabric formwork.Compared with the experiment,a numerical model using shell layered finite elements has a good prediction.The reinforcement by polyurethane to improve stiffness of air-supported fabric formwork is expected to be considered in the design and construction of the concrete shell,especially dealing with the advance of shape-control. 展开更多
关键词 fabric formwork POLYURETHANE STIFFNESS thin-shell structure loading experiment shell layered finite element
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一种膜结构裁剪分析的优化方法 被引量:1
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作者 钱圣申 杨燕 龚景海 《空间结构》 CSCD 北大核心 2019年第3期60-66,共7页
裁剪分析是膜结构设计中的关键步骤,它决定了结构实际使用时的形状和应力分布.然而由于难以模拟膜结构由裁剪膜片拼接、张拉直至成型的过程,缺少求解膜结构实际平衡形态的方法,现有的裁剪分析方法无法确保得到的裁剪形状是最优的.本文... 裁剪分析是膜结构设计中的关键步骤,它决定了结构实际使用时的形状和应力分布.然而由于难以模拟膜结构由裁剪膜片拼接、张拉直至成型的过程,缺少求解膜结构实际平衡形态的方法,现有的裁剪分析方法无法确保得到的裁剪形状是最优的.本文定义了一个膜结构成型过程中的'中间形态',利用该形态将膜结构从初始形态张拉到平衡形态的过程划分为两个变形阶段,从而实现了由裁剪膜片拼接、张拉后膜结构实际平衡形态的求解.利用中间形态的特性,提出了一种力学方法来优化膜结构的裁剪分析,确保了膜结构在实际成型后的形状误差和应力误差最小.选取了一个中国帽模型作为算例,生成了最优化裁剪膜片,分析了结构在中间形态时的应力分布及其实际平衡形态,并与采用了相同模型的其他裁剪分析结果进行了对比. 展开更多
关键词 膜结构 裁剪分析 最优化 成型模拟 平衡形态
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