期刊文献+

航空轴承表面合成DLC薄膜的结构特征和滚动接触疲劳物理模型 被引量:5

Characteristics and Rolling Contact Fatigue Model of Diamond-like Carbon Films on Aerospace Bearing Surfaces
原文传递
导出
摘要 利用等离子体浸没离子注入与沉积(PIIID)复合强化技术,在AISI440C航空轴承钢表面合成了类金刚石碳(DLC)薄膜。Raman光谱分析揭示出所制备的DLC膜层主要是由金刚石键(sp3)和石墨键(sp2)组成的混合无定形碳膜,且sp3键含量大于10%。原子力显微镜(AFM)形貌表明,DLC膜层表面光滑,结构致密均匀,与基体结合良好。被处理薄膜试样在90%置信区间下的疲劳寿命L10,L50,特征疲劳寿命La和平均寿命较基体分别延长了10.1,4.2,3.5和3.6倍。ANSYS模拟结果显示,最大剪切应力出现在膜基结合处并且靠近膜层内部,最大值达到2150MPa。结合ANSYS模拟结果和扫描电镜(SEM)观察形貌分析发现,膜层内部存在的微观缺陷是滚动接触疲劳裂纹产生的诱因,循环载荷所形成的最大剪切应力和润滑油中污染颗粒的共同作用是疲劳磨坑最终形成的外在动力。建立了循环载荷条件下PIIIDDLC/AISI440C轴承接触疲劳破坏的5阶段物理模型。 Diamond-like carbon (DLC) films are synthesized by the plasma immersion ion implantation and deposition (PIIID) technique on the steel substrate surface of aerospace bearing AISI440C. Raman spectroscopy analysis indicates that the DLC consists of a mixture of amorphous and crystalline phases, with a variable ratio of sp^2/sp^3 carbon bonds in which the sp^3 bonds content is more than 10%. Atomic force microscope (AFM) reveals that the DLC film has extremely smooth surface, very high uniformity, and efficiency of space filling over large areas. The rolling contact fatigue (RCF) life results show that the maximum L10 ,L50 ,La and mean fatigue life L of the treated samples, at 90% confidence level, increase by 10.1, 4.2, 3.5, and 3.6 times respectively. The ANSYS simulation result exhibits that the maximum shear stress is about 2.15 GPa, which is generated in the substrate-film interface inside a certain depth in the film layer. Combined with the scanning electron microscope (SEM) morphology of DLC/AISI440C bearing fatigue pitches, a conclusion can be drawn that the micro-defects in the film interior induce the initiation of rolling contact fatigue pitches, while the action of the maximum shear stress together with the polluted gains in the lubricant oil is the exterior driving force for their final formation. A five phase physical model of PIIID DLC/AISI440C bearing fatigue failure is established under cyclic contact stress conditions.
出处 《航空学报》 EI CAS CSCD 北大核心 2009年第9期1769-1775,共7页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金(50665004) 教育部博士点基金(20060674002)
关键词 等离子体浸没离子注入与沉积 类金刚石碳薄膜 滚动接触疲劳 物理模型 轴承 plasma immersion ion implantation and deposition (PIIID) diamond-like carbon films rolling contact fatigue physical model bearings
  • 相关文献

参考文献21

  • 1Harris T A. Roiling bearing analysis[M]. New York: Wiley Interscienee Press, 2001 : 1-36.
  • 2唐云冰,高德平,罗贵火.航空发动机滚动轴承的载荷分布研究[J].航空学报,2006,27(6):1117-1121. 被引量:31
  • 3Ebert Franz-Josef.An Overview of Performance Characteristics, Experiencesand Trends of Aerospace Engine Bearings Technologies[J].Chinese Journal of Aeronautics,2007,20(4):378-384. 被引量:27
  • 4Ceschini L, Minak G. Fatigue behaviour of low temperature carburised AISI 316L austenitic stainless steel [J]. Surface and Coatings Technology, 2008, 202(9): 1778- 1781.
  • 5Andre A. From plasma immersion ion implantation to deposition: a historical perspective on principles and trends [J]. Surface and Coatings Technology, 2002, 156 (1 -3): 3-12.
  • 6Tong H H, Monterio O R, Macgill R A, et al. Fabrica tion and characteristics of ta C biomaterial coatings on Ti- 6Al-4V using metal plasma immersion ion implantation and deposition [J]. Current Applied Physics, 2001, 1 (2- 3): 197 201.
  • 7Tomita A, Kusuda M, Otsuki S, et al. Enhancement of adhesive strength of DLC film prepared by PBIID on Co-Cr alloy for biomaterial [J]. Thin Solid Films, 2006, 506 507(5) : 59- 64.
  • 8Cheng Y, Zheng Y F. Effect of N2/Ar gas flow ratio on the deposition of TiN/Ti coatings on NiTi shape memory alloy by PIIID [J]. Materials Letters, 2006, 60 (18) : 2243-2246.
  • 9Huang N, Yang P, Leng Y X, et al. Hemocompatibility of titanium oxide films[J]. Biornaterials, 2003, 24(13) : 2177-2180.
  • 10Tang B Y, Liu H X, Wang L P. Fabrication of titanium carbide film on bearing steel by plasma immersion ion implantation and deposition [J]. Surface and Coatings Technology, 2004, 186(1 2): 320 323.

二级参考文献72

共引文献75

同被引文献94

引证文献5

二级引证文献11

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