Temperature Dependence of Fatigue Crack Growth in Low-Carbon Steel Under Gaseous Hydrogen

O. Takakuwa, Yuhei Ogawa, S. Okazaki, H. Matsunaga, S. Matsuoka
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引用次数: 2

Abstract

In order to elucidate the temperature dependence of hydrogen-assisted fatigue crack growth (HAFCG), the fatigue crack growth (FCG) test was performed on low-carbon steel JIS-SM490B according to ASTM E647 using compact tension (CT) specimen under 0.7 MPa (≈ 0.1 ksi) hydrogen-gas at room temperature (RT: 298 K (≈ 77 °F)) and 423 K (≈ 302 °F) at stress intensity factor range of ΔK = 30 MPa m1/2 (≈ 27 ksi in1/2). Electron backscatter diffraction (EBSD) observation was performed on the mid-thick section of CT specimen in order to investigate change in plasticity around the crack wake in gaseous hydrogen environment and how it changes due to temperature elevation. The obtained results showed the higher temperature, the lower intense of HAFCG as reported in our previous article. Plasticity around the crack wake became less in gaseous hydrogen environment, especially tested at 298 K. The propensity of the results obtained at higher temperature (423 K) can be separated into two cases: (i) intense plasticity occurs like tested in air, (ii) crack propagates straighter accompanying less plasticity like tested in gaseous hydrogen environment at 298 K. This implies macroscopic FCG rate is determined by combination of microscopic FCG rate in the case (i) and case (ii).
低碳钢在气态氢作用下疲劳裂纹扩展的温度依赖性
为了阐明氢辅助疲劳裂纹扩展(HAFCG)的温度依赖性,根据ASTM E647标准,在0.7 MPa(≈0.1 ksi)室温下(RT: 298 K(≈77°F))和423 K(≈302°F)下,在应力强度因子ΔK = 30 MPa m1/2(≈27 ksi In /2)范围内对低碳钢JIS-SM490B进行了疲劳裂纹扩展(FCG)试验。通过电子背散射衍射(EBSD)对CT试样中厚切片进行观察,探讨了气氢环境下裂纹尾迹周围的塑性变化及其随温度升高的变化规律。得到的结果表明,温度越高,HAFCG的强度越低。在气氢环境下,裂纹尾迹周围的塑性变弱,特别是在298 K时。在较高温度(423 K)下获得的结果倾向可以分为两种情况:(i)像在空气中测试一样出现强烈的塑性;(ii)裂纹扩展更直,同时塑性更小,像在气态氢环境中测试的298 K。这意味着宏观的FCG速率是由案例(i)和案例(ii)的微观FCG速率组合决定的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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