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Deflation behavior and related safety assessment of an air-supported membrane structure

机译:空气支撑膜结构的放气行为及相关安全性评估

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As a large span structure that might serve many occupants, the deflation behavior of an air-supported membrane structure under emergency deflation is of critical importance for safety assessment on occupants' evacuation but has received few studies. This paper presents experimental field tests and numerical simulations on deflation behaviors of a real-life air-supported membrane structure. A numerical model is employed in deflation simulation which considers tension-only membrane based on the vector form intrinsic finite element method for membrane motion analysis and pressure change due to air loss in deflation according to the classic thermodynamics. The correctness and the applicability of the model are verified by good correlation of prediction in response of pressure, displacement, and wrinkling formation and development of the structure with those measured and observed in deflation tests. The study shows that the structure in emergency deflation will lose its high pressure quickly first, and then sustain deflating under low residual pressure for a long time. The model is further used in parametrical analysis on factors that affect deflation progress and a complete deflation simulation to predict the whole collapse process, which is accordingly characterized by two typical phases, the tender deflation stage and the severe deflation stage. In tender stage the structure holds a relatively plump form, while in the severe stage the structure bears low decreasing residual pressure, membrane losses most tension stress so that many elements wrinkle and the structure experiences instability. Due to wrinkling, the residual pressure is found to approximately balance with its vertical loads. As a result, the feasible method proposed based on the residual pressure in deflation is very simple and reliable to predict the deflation duration and evaluate maximum escape area for deflation assessment of the studied structure.
机译:作为可能服务于许多乘员的大跨度结构,在紧急放气下的空气支撑膜结构的放气行为对于乘员撤离的安全性评估至关重要,但很少进行研究。本文介绍了真实的空气支撑膜结构的放气行为的实验现场测试和数值模拟。放气模拟中采用了一个数值模型,该模型基于矢量形式的固有有限元方法考虑了仅张拉的膜,从而根据经典的热力学对膜进行运动分析和因放气中的空气损失而引起的压力变化。该模型的正确性和适用性通过压力,位移,皱纹的形成和发展与在放气试验中测量和观察到的响应的良好预测相关性得到验证。研究表明,紧急放气结构首先会迅速失去高压,然后在低残余压力下持续长时间放气。该模型进一步用于影响通缩进度的因素的参数分析中,并通过完整的通缩模拟来预测整个坍塌过程,因此,该过程的特征在于两个典型阶段,即柔和的通缩阶段和严重的通缩阶段。在柔嫩阶段,结构保持相对丰满的形式,而在严重阶段,结构承受较低的残余压力,膜损失最大的张应力,因此许多元素起皱并且结构经历不稳定。由于起皱,发现残余压力与其垂直载荷大致平衡。因此,基于放气中残余压力提出的可行方法非常简单可靠,可以预测放气持续时间并评估最大逸出面积,以便对研究结构进行放气评估。

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