马氏体时效钢高温疲劳强化机理

N. Kawagoishi, Yuzo Nakamura, K. Kariya, K. Morino, T. Nagano, K. Yamane
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引用次数: 0

摘要

为了研究18%Ni马氏体时效钢在高温下的疲劳性能,对普通和钻孔试样进行了室温和空气中673K的旋转弯曲疲劳试验。单龄试件在753K下进行欠时效处理,双龄试件在673K下对单龄试件进行二次时效处理。在673K温度下,单时效平原试样的疲劳强度高于室温,但在高温下,静强度呈相反的下降趋势。另一方面,单时效钻孔试样在两种温度下表现出几乎相同的疲劳强度。在673K疲劳单时效的平原试样中,在RT下测得的硬度随时间增加,在673K静时效时也出现了这种情况。这种硬度的增加被认为是由于过量Mo溶质原子的存在而导致的沉淀硬化。另一方面,裂纹观察表明,在673K温度下,平原试样的裂纹萌生速度明显慢于室温,而裂纹扩展速度在这两个温度之间以及平原试样与钻孔试样之间没有显著差异。在673K温度下,普通试样裂纹萌生的明显延迟是由于其表面氧化所致。在高温下,双时效导致疲劳强度大幅度提高,但在673K时,疲劳强度略有提高。综上所述,在673K温度下,平原试样的疲劳强度提高的主要原因是氧化抑制了裂纹萌生,而在该温度下硬度的提高起了次要作用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Strengthening mechanism in fatigue of maraging steel at elevated temperature
In order to investigate fatigue properties of 18%Ni maraging steel at elevated temperature, rotating bending fatigue tests were conducted for plain and drilled specimens at room temperature (RT) and 673K in air. The specimens involved single-aged ones under an under-aging condition at 753K and double-aged ones in which the second aging was performed at 673K to the single-aged ones. Fatigue strength of the single-aged plain specimens was higher at 673K than at RT, though the static strength was inversely decreased at the elevated temperature. On the other hand, the single-aged drilled specimens exhibited nearly the same fatigue strength at both temperatures. It was found that hardness measured at RT increased with time in the single-aged plain specimens fatigued at 673K, which also appeared in the static aging at 673K. This hardness increase was considered to be attributed to precipitation hardening which might occur due to the existence of excess Mo solute atoms. On the other hand, crack observations revealed that crack initiation in the plain specimens was retarded markedly at 673K in comparison with that at RT, whereas crack propagation rate did not differ significantly between these temperatures and between the plain and drilled specimens. The marked delay of crack initiation in the plain specimens at 673K arose from the oxidation of their surfaces. It was also observed that the double-aging led to a large increase in fatigue strength at RT, but resulted in a slight increase at 673K. Based on these results, it was shown that the main reason of the increase in fatigue strength at 673K in the plain specimens was the suppression of crack initiation due to oxidation, while the increase in hardness observed at this temperature played a minor role.
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