期刊文献+

等离子氮化保温时间对S45C钢疲劳性能的影响 被引量:3

Time Duration Effect of Plasma Nitriding on Fatigue Behavior of S45C Steel
下载PDF
导出
摘要 温度500℃,气压400 Pa,N2与H2比例为40%∶60%的混合气体中,采用3组不同的处理时间(8、20、48 h)分别对S45C钢试件表面进行等离子氮化,全面探讨不同保温时间下氮化层及渗透层的微观组织、硬度、氮化层组成、残余应力,分析这些参数对S45C疲劳性能和断裂特征的影响。结果表明,3组工艺分别在S45C钢表面获得6、8、12μm深的氮化层。表面硬度由初始230 HV均提高到620 HV以上。表面残余压应力均提高到约-120 MPa。氮化物为单一γ-Fe4N相。渗氮层深度随保温时间增长而大幅增加,氮元素富集及α-Fe向γ-Fe4N相转变诱导的残余压应力在渗氮层内的扩展,使得等离子氮化保温48 h后S45C钢的疲劳强度提升为未处理试样的约3倍。根据村上公式计算"鱼眼"裂纹应力强度因子,可得其近似为3.6 MPa·m1/2。内部裂纹主要由渗透层内夹杂处萌生,夹杂成分为氧化钙、氧化铝和硫锰化合物等。 A group of S45C medium carbon steel specimen was nitrided by plasma nitriding using a mixture of 40% N2 -60% H2. The processes were carried out at 500 ℃ for three different time durations of 8,20 and 48 hours. The effect of case depth on fatigue perfohn- ance of S45C was investigated. The thickness of compound layer for these three time durations were 6 μm,8 μm, 12 μm,respectively. Plasma nitriding treatment enhanced the surface hardness and the surface compressive residual stress. The compound layer was com- posed of the γ - Fe4N phase. Rotating bending fatigue test s.howed that plasma nitriding treatment increased the fatigue strength of S45C by 190% with respect to the untreated specimen because of the increase of the case depth and the expansion of compressive residual stress in the case depth. The stress intensity factor calculated from the facet area was independent of the number of cycles to failure and was found as at 3.6 MPa m1/2. These fish-eye cracks were originated from inclusions in the case depth, and were calcium oxide, alumi- num oxide and manganese sulfide.
出处 《四川大学学报(工程科学版)》 EI CAS CSCD 北大核心 2014年第2期192-197,共6页 Journal of Sichuan University (Engineering Science Edition)
基金 国家自然科学青年基金资助项目(11202108) 教育部创新团队资助项目(IRT1027) 江苏省高校自然科学研究面上项目(13KJB130002)
关键词 等离子氮化 疲劳 X射线衍射 应力强度因子 plasma nitriding fatigue X-ray diffraction stress intensity factor
  • 相关文献

参考文献1

二级参考文献2

  • 1吴志学,第6届全国疲劳学术会议论文集.下,1993年
  • 2吴志学,第5届全国疲劳学术会议论文集.1,1991年

共引文献4

同被引文献32

  • 1张纪奎,郦正能.钛合金结构疲劳全寿命计算方法研究[J].机械强度,2010,32(3):455-460. 被引量:5
  • 2丁传富,刘建中,吴学仁.TC4钛合金和7475铝合金的长裂纹和小裂纹扩展特性的研究[J].航空材料学报,2005,25(6):11-17. 被引量:17
  • 3张庆玲,李兴无.TA15钛合金两类组织对疲劳性能和断裂韧度的影响[J].材料工程,2007,35(7):3-5. 被引量:16
  • 4朱旻昊,徐进,周仲荣.抗微动损伤的表面工程设计[J].中国表面工程,2007,20(6):5-10. 被引量:9
  • 5Bathias C. There is no infinite fatigue life in metallic materials[J]. Fatigue and Fracture of Engineering Materials and Structures, 1999,22(7): 559-565.
  • 6Murakarni Y,Nomoto T,Ueda T. Factors influencing the mechanism of superlong fatigue failure in steels [J]. Fatigue and Fracture of Engineering Materials and Structures, 1999,22 (7): 581-590.
  • 7Wang Q Y,Berard J Y,Bathias C,et al. Gigacycle fatigue of ferrous alloys [J]. Fatigue and Fracture of Engineering Materials and Structures, 1999,22(8): 667-672.
  • 8Cao X J,Murakami R,Wang Q Y. Fatigue properties of Ti-6A1-4V subjected to 0.9% physiological saline solution [J]. International Journal of Modem Physics B,2010,24 (15-16): 2518-2523.
  • 9Zettl B,Mayer H,Stanzl-Tschegg SE. Fatigue properties of AI-1Mg-0.6Si foam at low and ultrasonic frequencies [J]. International Jottrnal of Fatigue,2001,23 : 565-573.
  • 10Sakai T. Review and prospects for current studies on very high cycle fatigue of metallic materials for machine structural use[C] //Allison JE,Jones JW,Larsen JM,Ritchie RO. Fourth international conference on very high cycle fatigue. The Minerals,Metals and Materials Society,Warrendale ,PA,2007: 3-12.

引证文献3

二级引证文献9

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部