氢对SUS301奥氏体不锈钢拉伸和疲劳性能的影响

T. Iijima, H. Enoki, J. Yamabe, M. Kimura, B. An
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摘要

对SUS301奥氏体不锈钢进行了SSRT和疲劳寿命试验,研究了氢对其力学性能的影响。SUS301的Ni含量为6.00-8.00质量%,低于JIS奥氏体不锈钢标准SUS304的Ni含量。在SSRT测试的情况下,在实验室空气中,在室温(rt), - 45°C和- 80°C下测试有氢气和没有氢气的样品。在试验温度范围内,充氢试样的0.2%偏置屈服强度(Ys)小于300 MPa。充氢试样的抗拉强度(Ts)和总伸长率(El)显著降低。随着试验温度的降低,含氢试样的断裂面面形占主导地位。因此,氢对SUS301拉伸性能的影响应该是很大的。充氢和不充氢的试样在室温下在实验室空气中疲劳,未充氢的试样在室温下在100mpa氢气气氛中疲劳。充氢试样和在氢气气氛中疲劳的有限寿命区循环次数(Nf)比在空气中短两个数量级。然而,充氢试样的有限疲劳寿命区与充氢试样的有限疲劳寿命区表现出不同的特征。此外,所有疲劳试样的铁素体当量和疲劳断口形貌表明,在空气中充氢试样和在100 MPa氢气中不充氢试样的疲劳断裂机制似乎有所不同。因此,需要进一步调查以消除这一差异。
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Effect of Hydrogen on Tensile and Fatigue Properties of SUS301 Austenitic Stainless Steel
SSRT and fatigue life tests of SUS301 austenitic stainless steel were performed to examine the effect of hydrogen on the mechanical properties. Ni content of SUS301, 6.00–8.00 mass%, is lower than that of SUS304 in JIS standard for austenitic stainless steels. In the case of SSRT tests, specimens with and without hydrogen charging were tested in laboratory air at room temperature (R.T.), −45 °C, and −80 °C. The 0.2% offset yield strength (Ys) of the hydrogen charged specimens was less than 300 MPa in the tested temperature range. The tensile strength (Ts) and total elongation (El) of hydrogen charged specimens decreased remarkably. With decreasing testing temperature, fracture surface facet of the hydrogen charged specimens became dominant. Therefore, the effect of hydrogen on the tensile properties of SUS301 is supposed to be large. Specimens with and without hydrogen charging were fatigued in laboratory air at R.T., and specimens without hydrogen charging were fatigued in 100 MPa hydrogen gas atmosphere at R.T. Number of cycles (Nf) at finite fatigue life region of the hydrogen charged specimens and of the specimens tested in hydrogen gas were two orders shorter than that of the specimens tested in air. However, the finite fatigue life region of the hydrogen charged specimens and the specimens tested in hydrogen gas showed a different profile. Additionally, ferrite equivalents of all fatigue tested specimens and fatigued fracture surface morphology suggested the fatigue fracture mechanism between the hydrogen charged specimens tested in air and the non-charged specimens tested in 100 MPa hydrogen gas seems to be different. Therefore, further investigations are required to clear this difference.
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