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首页> 外文期刊>Journal of marine science and technology >A study of fatigue crack propagation at a web stiffener on a longitudinal stiffener
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A study of fatigue crack propagation at a web stiffener on a longitudinal stiffener

机译:纵向加劲肋上腹板加劲肋疲劳裂纹扩展的研究

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Predicting fatigue crack growth after its detection during in-service inspection is necessary to prevent a loss of serviceability, such as the oil and/or water tightness of critical compartments. This paper focuses on the most typical fatigue cracks that start at the weld joint between a flat bar stiffener on a transverse web frame and the flange of a longitudinal stiffener on a bottom plate or inner bottom plate. An experiment is carried out to observe the fatigue crack propagation for two kinds of flat bars at the abovementioned connection. The experimental results, especially the surface crack growth on the flange (which dominates during the total fatigue life of the longitudinal stiffener), are compared with crack growth curves predicted using a few existing formulas. Based on the comparative study, a formula that shows the best agreement with the experiment results is selected. Weld toe magnification factors for the web stiffener are computed from the crack propagation rates measured in the experiment, and two equations for the magnification factors versus crack depth are developed for two types of web stiffeners. The selected existing formula and the proposed equations are applied to two connections at the inner bottom and side longitudinal bulkhead of an LNG carrier. The equivalentrnstress approach based on a long-term distribution is employed to avoid the complexity involved in dealing with the actual stress history. Using this prediction, the remaining service life until an oil or water leakage occurs at a tank boundary can be estimated when a fatigue crack at the connection is detected.
机译:在使用中检查过程中检测到疲劳裂纹后,必须预测疲劳裂纹的增长,以防止诸如关键隔室的油密性和/或水密性之类的维修性损失。本文着眼于最典型的疲劳裂纹,该疲劳裂纹始于横向腹板框架上的扁平加强筋与底板或内部底板上的纵向加强筋的法兰之间的焊接缝。进行实验以观察上述连接处两种扁钢的疲劳裂纹扩展。实验结果,特别是法兰表面的裂纹扩展(在纵向加劲肋的总疲劳寿命中起主要作用),与使用一些现有公式预测的裂纹扩展曲线进行了比较。在比较研究的基础上,选择了与实验结果最吻合的公式。从实验中测得的裂纹扩展速率计算出腹板加劲肋的焊趾放大倍数,并针对两种类型的腹板加劲肋建立了两个放大系数与裂纹深度的关系式。所选的现有公式和建议的公式将应用于LNG船的底部内部和侧面纵向舱壁的两个连接处。采用基于长期分布的等效应力方法来避免处理实际应力历史所涉及的复杂性。使用此预测,当检测到连接处的疲劳裂纹时,可以估算出在油箱边界处发生油或水泄漏之前的剩余使用寿命。

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