极限载荷解在均匀匹配管道环焊缝内埋缺陷工程临界评估中的应用

A. Pépin, T. Tkaczyk, N. O’Dowd, K. Nikbin, S. V. Chettiar
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引用次数: 0

摘要

工程关键评估(ECA)通常用于确定采用低应变安装方法(如S-Lay或J-Lay)或高应变安装方法(如Reel-Lay)部署在海底的刚性管道的环焊缝缺陷的验收标准。ECA通常考虑管道从制造到使用结束的整个负荷历史,包括断裂和疲劳评估。本文主要关注的断裂,当(i)裂纹驱动力(以j积分或裂纹尖端张开位移(CTOD) δ表示)大于材料阻力,或(ii)施加的载荷超过裂纹结构韧带的承载能力,也称为塑性破坏或极限载荷时,认为断裂已经发生。非洲经委会程序的稳健性取决于评估解决办法的准确性。管道环焊缝的大部分缺陷都是预埋的。与表面断裂缺陷不同,在高应变断裂ECA中,嵌入缺陷通常不能直接评估,因为现有的评估方案过于保守。通常采用一种变通方法,如果嵌入深度等于或大于缺陷高度的一半,则表面以下的最大可接受表面破碎缺陷尺寸也被认为是可接受的。否则,必须将嵌入缺陷重新分类为表面破碎缺陷,其高度等于嵌入缺陷高度与嵌入深度之和。为了能够对预埋缺陷进行直接的断裂评估,作者在前期工作中对预埋缺陷短韧带的塑性破坏载荷进行了参数化有限元研究,研究了预埋深度、裂缝高度和裂缝长度对塑性破坏载荷的影响。随后,提出了一种新的极限载荷解,用于均匀匹配管道环焊缝在拉伸和/或弯曲作用下的内埋缺陷断裂评估。结果表明,与文献中其他解相比,该闭式解对裂缝驱动力和韧带塑性破坏荷载的估计更为准确。然而,对于某些几何形状,预测的极限载荷仍然需要显著调整(增加),以正确评估j积分,在联合撕裂和崩溃评估中。这表明,进一步增强解决方案是可能的。本文描述了进行的小规模断裂试验,以确定在改进的中裂纹张力(MMCT)试样中坍塌较小的嵌入缺陷韧带所需的载荷。对试验结果拟合一个封闭解,并与基于有限元的解进行比较,该解也可作为缺陷再分类准则。最后,提出了在载荷或位移控制条件下,对均匀匹配管道环焊缝内埋缺陷进行直接断裂评估的建议。
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Application of Limit Load Solutions for Engineering Critical Assessment of Embedded Flaws in Evenmatch Pipeline Girth Welds
Engineering Critical Assessment (ECA) is commonly undertaken to derive the acceptance criteria for girth weld flaws in rigid pipelines deployed subsea by low-strain installation methods, such as S-Lay or J-Lay, or high-strain installation methods, such as Reel-Lay. The ECA generally considers the whole load history seen by the pipeline from fabrication to the end of service, and involves fracture and fatigue assessments. Fracture, which is the main focus of this paper, is deemed to have initiated when either (i) the crack driving force, expressed in terms of the J-integral or the Crack Tip Opening Displacement (CTOD), δ, is greater than the materials resistance, or (ii) the applied load exceeds the bearing capacity of the ligament of a cracked structure, also referred to as the plastic collapse or limit load. The robustness of the ECA procedure relies on the accuracy of the assessment solutions. Most flaws in pipeline girth welds are embedded. Unlike surface breaking flaws, embedded flaws are typically not directly assessed in a high-strain fracture ECA because the available assessment solutions are too conservative. A work-around approach is often followed, where the maximum acceptable surface breaking flaw sizes are also considered acceptable below the surface if the embedment depth is equal to or greater than half of the flaw height. Otherwise, an embedded flaw must be reclassified as a surface breaking flaw with a height equal to the sum of the embedded flaw height and embedment depth. To enable the direct fracture assessment of embedded flaws, the authors undertook in a previous work a parametric finite-element (FE) study on the effect of the embedment depth, the crack height and the crack length on the plastic collapse load of the shorter ligament of embedded flaws. Subsequently, a new limit load solution was proposed for the fracture assessment of embedded flaws in evenmatch pipeline girth welds subjected to tension and/or bending. This closed-form solution was shown to be significantly more accurate for estimating the crack driving force and the ligament plastic collapse load than other solutions available in the literature. For some geometries, however, the predicted limit load still needs to be significantly adjusted (increased) to correctly evaluate the J-integral, in a combined tearing and collapse assessment. This suggests that further enhancement of the solution is possible. This paper describes small-scale fracture tests which were undertaken to determine the load required to collapse a smaller ligament of embedded flaws in a modified middle crack tension (MMCT) specimen. A closed-form solution, which can also be used as a flaw reclassification criterion, is fitted to the test results and then compared to the FE-based solution. Finally, recommendations are made for the direct fracture assessment of embedded flaws in evenmatch pipeline girth welds subjected to load or displacement-controlled conditions.
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