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Influence of crack arresting rib on the fracture characteristic of integral wing-spar

机译:裂纹抑制肋对整体翼翼骨折裂缝特征的影响

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Focus on the problem that fracture characteristic of integral structure is worse than composite structure, this paper studied the influence of anti-crack rib design parameters on the fracture characteristic of integral wing-spar through calculating the stress intensity factor and constructing support vector machine agent model. Results indicated that crack arresting rib could enhance the fracture characteristic of integral wing-spar well. When crack extended to crack arresting rib, residual strength of integral wing-spar will enhance for about 36%, crack growth life enhance about 13.5%; the best location of crack arresting rib is at 1/3 the height of wing-spar. Conclusions gained could provide reference for damage tolerance design of integral wing-spar.
机译:专注于整体结构的断裂特性比复合结构更差的问题,本文研究了通过计算应力强度因子和构建支持向量机代理模型来实现抗裂肋设计参数对整体翼静脉裂缝特性的影响。结果表明,裂纹抑制肋可以增强整体翼氏疮的裂缝特性。当裂缝扩展到破裂腐蚀肋骨时,整体翼状翼疮的剩余强度将增强约36%,裂纹增长寿命增强约13.5%;裂缝腐烂肋骨的最佳位置是翼翼的1/3。所获得的结论可以为整体翼翼氏散损的损伤公差设计提供参考。

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