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首页> 外文期刊>Journal of Materials Research and Technology >Effect of phase in surface layers on rotating-bending fatigue strength of SCM415 steel after austenitic nitriding
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Effect of phase in surface layers on rotating-bending fatigue strength of SCM415 steel after austenitic nitriding

机译:表面层在奥氏体氮化后SCM415钢旋转弯曲疲劳强度的影响

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The rotating bending fatigue strength of JIS-SCM415 steels after austenitic nitriding was evaluated to find the surface phase that gave the highest strength. Nitriding was performed at 903?K under conditions of KN?=?0.15, 0.25 and 0.35 atm-1/2. In addition, specimens which were tempered at 523?K for 7.2?ks after nitridings with KN?=?0.15 and 0.25 atm-1/2were prepared. A specimen prepared by nitrocarburizing at 853?K was also evaluated as a comparison. Specimens nitrided at 903?K at KN?=?0.15?atm-1/2showed the highest fatigue limit because the 10?μm thick surface layer was a dual phase of austenite and martensite that might have a fine microstructure which inhibited initial crack generation and growth. Specimens nitrided at 903?K at KN?=?0.35?atm-1/2showed the second highest fatigue limit because the ε compound layer that was 20?μm thick had a high compressive residual stress. Specimens nitrides at 903?K at KN?=?0.25?atm-1/2showed the third highest fatigue limit because of the formation of a 6?μm thick compound layer which was a dual phase of ε and γ’ that had few voids and a high toughness (low hardness) in addition to its compressive residual stress. Tempered specimens showed a lower fatigue limit than that of non-tempered specimens. This was because the surface layer became brittle in tempered specimens. Specimens other than the tempered specimen in KN?=?0.25?atm-1/2showed a fatigue strength higher than that of a sample nitrocarburized at 853?K.
机译:评估了奥氏体氮化后JIS-SCM415钢的旋转弯曲疲劳强度,以找到给出最高强度的表面阶段。在kn的条件下在903℃下进行氮化α= 0.15,0.25和0.35atm-1/2。另外,用KNα=β= 0.15和0.25atm-1/2,在523Ω·k下以523Ω·k温度为7.2 ks的标本。通过在853℃下通过氮碳化制备的样品也被评价为比较。在kn的903Ωk处氮化标本=?0.15?ATM-1/2表示最高疲劳极限,因为10?μm厚的表面层是奥氏体和马氏体的双相,可能具有精细的微观结构,抑制初始裂纹的微观结构生长。标本氮化为903Ω·k的kn?= 0.35?ATM-1/2表示第二最高疲劳极限,因为ε化合物层为20≤μm厚度具有高压缩残余应力。在kn的903Ωk处的标本氮气α= 0.25?ATM-1/2表示第三次最高疲劳极限,因为形成6Ωμm厚的化合物层,其是ε和γ'的双相和除了压缩残余应力之外,高韧性(低硬度)。钢化标本显示出比非回火标本的疲劳极限较低。这是因为表面层在钢化样本中变得脆弱。在kn的升温样本之外的标本?= 0.25?ATM-1/2表示高于853Ω·k的样品氮碳排出的疲劳强度。

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