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Effect of specimen geometries on the C* versus da/dt master curve for type 316L stainless steel

机译:样品几何形状对316L型不锈钢的C *与da / dt主曲线的影响

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摘要

This work deals with engineering components made of stainless steels working at high temperature and subjected to creep-fatigue loading history. The defect assessment procedures generally use the crack growth properties curve da/dt versus C* parameter for estimating the creep-crack growth. The ASTM E 1457-98 [ASTM E 1457-98. Standard test method for measurement of creep crack growth rates in metals, 1998] procedure proposes the rule to establish such a master curve. In particular, it is stipulated that this rule only applies for CT specimens. Previously [Laiarinandrasana L, Kabiri R, Dru-bay B. In: Gupta A, editor. Proceedings of the 16th international conference on structural mechanics in reactor technology, Washington, USA, 2001], some practical methodology to produce this crack growth curve on CT specimens has been described by introducing the way to determine the upper and lower limits of relevant experimental points and by adopting the ASTM E 1457-98 method to estimate the creep component of the load line displacement rate (d delta/dt_(behavior))- This latter is the interesting part of the total displacement rate recorded during the test. This paper focuses on the application of the procedure proposed in [Laiarinandrasana L, Kabiri R, Drubay B. In: Gupta A, editor. Proceedings of the 16th international conference on structural mechanics in reactor technology, Washington, USA, 2001] on specimen geometries other than CT, such as circumferentially cracked round bar (CCRB) and double edged notched in tension (DENT) specimens. The da/dt versus C curves issued from all of these specimens are compared. Discussion about the effect of geometry on these curves is carried out. Additionally, some finite element analyses have been performed in order to simulate the creep crack growth using the node release technique. These simulations allow to verify the validity of the proposed expressions of C* and consequently the master curve of the 316L(N) stainless steel.
机译:这项工作涉及由不锈钢制成的工程部件,这些部件在高温下工作并承受蠕变疲劳载荷的历史。缺陷评估程序通常使用裂纹扩展特性曲线da / dt对C *参数来估计蠕变裂纹扩展。 ASTM E 1457-98 [ASTM E 1457-98。用于测量金属中蠕变裂纹增长率的标准测试方法,[1998]程序提出了建立这种主曲线的规则。特别规定,该规则仅适用于CT标本。以前[Laiarinandrasana L,Kabiri R,Dru-bayB。在:Gupta A,编辑中。第16届国际反应堆技术结构力学会议论文集(美国华盛顿,2001年)中,通过介绍确定相关实验点的上限和下限的方法,描述了一些在CT样品上生成此裂纹扩展曲线的实用方法并通过采用ASTM E 1457-98方法来估算负载线位移率的蠕变分量(d delta / dt_(behavior))。后者是测试期间记录的总位移率的有趣部分。本文着重于[Laiarinandrasana L,Kabiri R,Drubay B.在:Gupta A,编辑中提出的程序的应用。 [第16届国际反应堆技术结构力学国际会议论文集,美国华盛顿,2001年],涉及CT以外的其他几何样品,例如圆周裂纹圆棒(CCRB)和拉伸双刃缺口(DENT)样品。比较所有这些样品的da / dt与C曲线。讨论了几何形状对这些曲线的影响。此外,已经进行了一些有限元分析,以便使用节点释放技术来模拟蠕变裂纹的增长。这些模拟可以验证所提出的C *表达式的有效性,从而验证316L(N)不锈钢的主曲线的有效性。

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