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首页> 外文期刊>Journal of Aerospace Sciences and Technologies >PROGRESSIVE FAILURE ANALYSIS OF COMPOSITE OVERWRAPPED PRESSURE VESSEL
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PROGRESSIVE FAILURE ANALYSIS OF COMPOSITE OVERWRAPPED PRESSURE VESSEL

机译:复合式压力容器的渐进式失效分析

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摘要

Stress and progressive failure analysis (First Ply Failure to Last Ply Failure) of a composite overwrapped pressure vessel (COPY) with an aluminum liner using the finite element method (FEM) in general and commercial finite element analysis (FEA) software ANSYS in particular is presented in this paper. Ply failure prediction is based on failure criteria implemented in ANSYS software. The first-ply failure (FPF) does not necessarily imply the total failure of a laminate. After FPF, the laminate stiffness is reduced consistent with identified ply failure mode. The strength of the composite laminate is evaluated again to see if it could carry additional load. This ply-by-ply analysis progresses, until the ultimate strength is reached. In the present study the methodology is validated using benchmarks and applied to a filament wound fibre reinforced plastic composite pressure vessel with an aluminum liner. Significant results are presented and critically assessed. Directions for further work in this field are identified.
机译:在常规和商业有限元分析(FEA)软件中,使用有限元方法(FEM)对带有铝衬里的复合包覆压力容器(COPY)进行应力和渐进式失效分析(从第一层失效到最后一层失效),尤其是在本文中提出。板层故障预测基于在ANSYS软件中实现的故障标准。第一层故障(FPF)不一定暗示层压板的全部故障。经过FPF后,层压板的刚度降低,与确定的层破坏模式一致。再次评估复合材料层压板的强度,以查看其是否可以承受额外的载荷。逐层分析将继续进行,直到达到极限强度为止。在本研究中,该方法已使用基准进行了验证,并应用于带有铝衬里的缠绕长丝的纤维增强塑料复合压力容器。提出了重大成果并进行了严格评估。确定了该领域进一步工作的方向。

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