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Assessment of a creep-fatigue crack initiation and crack propagation for a welded cylindrical shell

机译:焊接圆柱壳蠕变疲劳裂纹萌生和裂纹扩展的评估

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摘要

An assessment of the creep-fatigue crack bahaviour for a cylindrical structure with weldments has been carried out by using a structural test and an evaluation with an assessment procedure. The structural specimen with a diameter of 600 mm and thickness of 7 mm is a welded cylindrical shell made of 316L stainless steel (SS) for one half of the cylinder and 304 SS for the other half. Eight artificial defects were machined and the defect behaviours were examined. In the creep-fatigue test, the hold time was 1 h at 600 deg C and the primary nominal stress was 45 MPa. The evaluation results for the creep-fatigue crack initiation and crack propagation were compared with those of the observation images from the structural test. The assessment results for the creep-fatigue crack behaviour by using the French A16 procedure showed that the A16 guide is reasonably conservative but overly conservative for the creep-fatigue crack propagation in the case of a short hold time. It was shown that the crack initiation and propagation were dominated by a creep.
机译:通过使用结构试验和带有评估程序的评估,对带有焊接件的圆柱结构的蠕变疲劳裂纹行为进行了评估。直径为600毫米,厚度为7毫米的结构试样是由圆柱体的一半制成的316L不锈钢(SS),另一半为304 SS制成的焊接圆柱壳。加工了八个人造缺陷并检查了缺陷行为。在蠕变疲劳试验中,在600摄氏度下的保持时间为1小时,主名义应力为45 MPa。将蠕变疲劳裂纹萌生和裂纹扩展的评估结果与结构测试的观察图像进行了比较。通过使用法国A16程序对蠕变疲劳裂纹行为的评估结果表明,在保持时间较短的情况下,A16指南对于蠕变疲劳裂纹扩展是相当保守的,但过于保守。结果表明,裂纹的萌生和扩展以蠕变为主。

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