首页> 外文期刊>Journal of Solid Mechanics and Materials Engineering >Investigation of Mechanism for Intergranular Fatigue Crack Propagation of Low Carbon Steel JIS S10C in Hydrogen Gas Environment
【24h】

Investigation of Mechanism for Intergranular Fatigue Crack Propagation of Low Carbon Steel JIS S10C in Hydrogen Gas Environment

机译:氢气环境下低碳钢JIS S10C晶间疲劳裂纹扩展机理的研究

获取原文
           

摘要

In order to investigate the mechanism for the intergranular fatigue crack propagation of a low carbon steel in a low pressure hydrogen gas environment, two kinds of examinations were carried out. One examined the effect of the cyclic pre-strain on the crack growth behavior. The other was the in-situ observation of intergranular fatigue crack propagation in a hydrogen gas environment. The main results are as follows. (1) SEM observation of the specimen surface morphology of a plain specimen fatigued in hydrogen gas showed that a gap at the grain boundary was induced by slip behavior, but not in nitrogen gas. (2) A specimen cyclic-prestrained in hydrogen gas showed slight influences on the increase in the crack propagation rate. (3) Mating intergranular facets on the fatigue fracture surfaces showed the matching of a striation-like pattern in the manner anticipated from the damage mechanism of (1). (4) The environment-change test from hydrogen to nitrogen during the fatigue test showed that intergranular facets appeared even in nitrogen. Results (3) and (4) suggests that the damaging process of (1) is valid in an actual fatigue crack. (5) In-situ observation of the crack propagation behavior in hydrogen gas showed that a crack propagated faster along the grain boundary. However, no visible discontinuous crack advances appeared as a large number of load repetitions was required. Phenomena considered to be a damage process (1) appeared ahead of a crack tip. Based on these results, a convincing mechanism for the intergranular fatigue crack propagation process is as follows. Grain boundaries just ahead of a crack tip are damaged due to the large number of hydrogen-enhanced slip repetitions, therefore, the fatigue crack becomes easier to propagate along the grain boundary in hydrogen.
机译:为了研究低碳钢在低压氢气环境下晶间疲劳裂纹扩展的机理,进行了两种检查。一个研究了循环预应变对裂纹扩展行为的影响。另一个是在氢气环境中原位观察晶间疲劳裂纹扩展。主要结果如下。 (1)SEM观察了在氢气中疲劳的普通试样的试样表面形态,结果表明,晶界处的间隙是由滑移行为引起的,而氮气中却没有。 (2)在氢气中循环预应力的试样对裂纹扩展速率的增加影响很小。 (3)疲劳断裂表面上的交配晶间小面以(1)的损伤机理所预期的方式显示出条纹状图案的匹配。 (4)在疲劳试验中从氢到氮的环境变化试验表明,即使在氮中也出现了晶间小面。结果(3)和(4)表明(1)的破坏过程在实际疲劳裂纹中是有效的。 (5)对氢气中裂纹扩展行为的现场观察表明,裂纹沿晶界的扩展速度更快。然而,由于需要大量的载荷重复,因此没有出现可见的不连续裂纹发展。被认为是破坏过程的现象(1)出现在裂纹尖端之前。基于这些结果,用于晶间疲劳裂纹扩展过程的令人信服的机理如下。由于大量的氢增强的滑动重复而损坏了裂纹尖端之前的晶界,因此,疲劳裂纹变得更容易沿氢的晶界传播。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号