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Evaluation of the creep-fatigue damage mechanism of Type 316L and Type 316LN stainless steel

机译:316L和316LN型不锈钢的蠕变疲劳损伤机理评估

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Low-cycle fatigue tests with continuous cycling and creep-fatigue tests with 10 min hold times at tensile maximum strain were conducted at 600 ℃ in air for Type 316L and Type 316LN stainless steels containing nitrogen contents of 0.04% and 0.10%. The creep-fatigue life was less than the fatigue life for both alloys. The fatigue and creep-fatigue life and saturation stress were increased with the addition of nitrogen. The fracture mode was transgranular for fatigue and intergranular for creep-fatigue regardless of the nitrogen content. The dislocation structure was cellular for Type 316L and planar for Type 316LN after fatigue and creep-fatigue tests. Carbides were precipitated at grain boundaries after creep-fatigue tests and nitrogen decreased the precipitation. Creep-fatigue life was well predicted by a model based on cavity nucleation and growth at grain boundaries. The increase of creep-fatigue life with the addition of nitrogen was due to the decrease of precipitation and stress relaxation by the change in dislocation structure.
机译:对于含氮量分别为0.04%和0.10%的316L和316LN型不锈钢,在600℃的空气中于600℃进行了具有连续循环的低循环疲劳试验和在最大拉伸应力下保持时间为10分钟的蠕变疲劳试验。两种合金的蠕变疲劳寿命均小于疲劳寿命。氮的添加增加了疲劳寿命,蠕变疲劳寿命和饱和应力。不论氮含量如何,断裂模式均为疲劳的晶界和蠕变疲劳的晶界。经疲劳和蠕变疲劳测试后,位错结构对于316L型是多孔的,而对于316LN型则是平面的。蠕变疲劳试验后,碳化物在晶界析出,氮减少了析出。通过基于腔核和晶粒边界生长的模型可以很好地预测蠕变疲劳寿命。氮的添加增加了蠕变疲劳寿命,这是由于位错结构的变化导致了沉淀的减少和应力松弛的缘故。

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