组织对sae9254脱碳弹簧钢过早疲劳失效的影响

Jéssica Cristina Costa de Castro Santana , Silvano Leal dos Santos , Renato Altobelli Antunes , Sydney Ferreira Santos
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引用次数: 0

摘要

疲劳寿命是机械部件制造中使用的合金性能的关键问题,例如汽车工业中使用的Si-Mn弹簧钢。在这些合金中,表面缺陷和微观组织对疲劳寿命有很大影响。本文研究了总脱碳深度和纳米硬度分布对sae9254弹簧钢过早疲劳失效的影响。热处理(850℃奥氏体化和油淬)形成脱碳层。研究了不同脱碳层厚度和控制表面粗糙度的热处理试样,以评价脱碳层深度与疲劳行为的相互作用。经过40万次循环的应力控制疲劳测试和断口分析,可以确定厚度达25 μm的完全脱碳层(铁素体层)没有断裂。在此临界厚度以上,发生过早疲劳断裂。显微组织表征和纳米硬度剖面测量表明,疲劳试验中过早的裂纹形核与全脱碳区和部分脱碳区界面处的突然硬度变化有关。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Influence of the microstructure on the premature fatigue failure of decarburized SAE 9254 spring steel
Fatigue life is a key issue on the performance of alloys employed in mechanical components manufacturing such as Si-Mn spring steels used in the automotive industry. In these alloys, the fatigue life is strongly affected by surface defects and microstructure. In this paper, the effect of total decarburization depth and nanohardness profile on the premature fatigue failure of the SAE 9254 spring steel is reported. Decarburization layer was developed during heat treatment (austenitization at 850 °C and oil quenching). Heat treated specimens with different decarburized layer thickness and controlled surface roughness were investigated to evaluate the interplay between the decarburized layer depth and fatigue behavior. Stress-controlled fatigue tests up to 400,000 cycles and fractographic analysis allowed determining that fully decarburized layers (ferrite layers) with thickness up to 25 μm did not fracture. Above this critical thickness, premature fatigue fracture took place. Microstructural characterization and nanohardness profile measurements indicated that premature crack nucleation during the fatigue tests is associated with an abrupt hardness variation at the interface between total and partial decarburization regions.
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