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Fatigue crack non-propagation assisted by nitrogen-enhanced dislocation planarity in austenitic stainless steels

机译:奥氏体不锈钢中氮增强位错平面度辅助的疲劳裂纹扩展

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Rotating bending fatigue tests were conducted to assess the fatigue crack propagation behavior of the Fe-25Cr-1N and Fe-18Cr-14Ni austenitic steels in terms of the microstructure, crack propagation paths, and non-propagating fatigue crack characteristics. The Fe-25Cr-1N steel exhibited a non-propagating fatigue crack at the fatigue limit (310 MPa), but this did not occur in the Fe-18Cr-14Ni steel at the fatigue limit (110 MPa). The non-propagating fatigue crack observed in the Fe-25Cr-1N steel was produced by roughness-induced crack closure. This phenomenon was caused by the enhanced planar dislocation and high dislocation pile-up stress resulting from the suppression of cross-slip, which inhibited the dislocation emission from the crack tip. The Fe-25Cr-1N steel exhibited a lower fatigue crack growth rate than the Fe-18Cr-14Ni steel because of the enhanced dislocation planarity produced by the Cr-N interaction. The Cr-N interaction affected the fatigue crack growth behavior as follows. The short crack region exhibited a planar glide dislocation pattern, but multiple slip systems were activated as the crack lengthened. As the dislocation pattern remained planar on each slip plane, the crack propagation occurred along the {1 1 1}_γ slip planes, even in the long crack. Moreover, the dislocation pile-up at the grain boundaries caused grain boundary subcracks, which can induce crack toughening through mechanisms such as stress redistribution. These positive effects contributed to the lower fatigue crack growth rate in the Fe-25Cr-1N steel than the Fe-18Cr-14Ni steel.
机译:进行了旋转弯曲疲劳试验,以从微观组织,裂纹扩展路径和非扩展疲劳裂纹特征方面评估Fe-25Cr-1N和Fe-18Cr-14Ni奥氏体钢的疲劳裂纹扩展行为。 Fe-25Cr-1N钢在疲劳极限(310 MPa)处表现出非传播性疲劳裂纹,但在疲劳极限(110 MPa)的Fe-18Cr-14Ni钢中未出现这种裂纹。 Fe-25Cr-1N钢中观察到的非传播性疲劳裂纹是由粗糙度引起的裂纹闭合产生的。这种现象是由于横向滑动的抑制导致平面位错的增强和位错堆积应力的增加所致,从而抑制了裂纹尖端的位错散发。 Fe-25Cr-1N钢的疲劳裂纹扩展速度比Fe-18Cr-14Ni钢低,这是由于Cr-N相互作用产生的位错平面度增加。 Cr-N相互作用对疲劳裂纹扩展行为的影响如下。短裂纹区域表现出平面滑移位错模式,但是随着裂纹的延长,多个滑动系统被激活。由于位错模式在每个滑移面上都保持平面,即使在长裂纹中,裂纹也沿{1 1 1}_γ滑移传播。此外,在晶界处的位错堆积引起晶界亚裂纹,这可以通过应力再分布等机制引起裂纹增韧。这些积极的作用使Fe-25Cr-1N钢的疲劳裂纹扩展率比Fe-18Cr-14Ni钢低。

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