变曲率与圆柱构型复合材料薄壁壳体极限承载能力对比试验

Ultimate bearing capacity contrast test of composite thin-walled shells with variable curvature and cylindrical configuration

  • 摘要: 针对复合材料圆柱壳体实现广义等强度设计目标的局限性,提出了变曲率壳体构型以提高其屈曲载荷。基于纤维缠绕工艺设计并制备了复合材料变曲率耐压壳体试验模型,通过静水压力试验与圆柱壳体的极限承载能力进行对比。基于数值计算的方法,分析了复合材料变曲率壳体的渐进损伤过程,探讨了复合材料变曲率壳体的极限承载特性。研究结果表明:复合材料变曲率壳体的极限承载过程存在三阶段性特征,结构的损伤与失效出现在后屈曲阶段;复合材料变曲率壳体的后屈曲承载区间略长于圆柱壳体,说明其极限承载能力优于圆柱壳体;复合材料变曲率壳体的失效模式与圆柱壳体相似,临界屈曲阶段出现后,壳体的应力与位移分布规律出现变化,结构最先在失稳半波的波峰与波谷处出现基体失效,继而出现纤维失效,最后壳体达到极限载荷而发生破坏。

     

    Abstract: A variable curvature shell configuration was proposed to improve the buckling load of composite cylindrical shells due to the limitations of achieving generalized equivalent strength design goals. The composite variable curvature pressure hull test model was designed and prepared based on fiber winding technology. The ultimate bearing capacity of the shell was compared with that of a cylindrical shell through hydrostatic pressure testing. Based on numerical calculation methods, the progressive damage process of composite variable curvature shells was analyzed, and the ultimate bearing mechanism was explored. The research results indicate that the ultimate bearing process of composite variable curvature shells exhibits a three-stage characteristic, with structural damage and failure occurring in the post buckling stage. The post buckling bearing range of the composite variable curvature shell is slightly longer than that of the cylindrical shell, indicating that its ultimate bearing capacity is better than that of the cylindrical shell. The failure mode of composite variable curvature shells is similar to that of cylindrical shells. After the critical buckling stage occurs, the stress and displacement distribution of the shell changes. The structure first experiences matrix failure at the peaks and valleys of the buckling half wave, followed by fiber failure, and finally the shell reaches its ultimate load and fails.

     

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