期刊文献+

MoS2/Ti复合薄膜对Ti811合金高温摩擦磨损性能及微动疲劳行为的影响 被引量:13

Effect of Unbalanced Magnetron Sputtering MoS_2/Ti Composite Films on the Tribological Properties and Fretting Fatigue Behaviors of Ti811 Alloy at Elevated Temperature
下载PDF
导出
摘要 利用非平衡磁控溅射方法在Ti811合金表面制备MoS2/Ti复合薄膜,研究薄膜的成分、膜-基结合强度和显微硬度,以及MoS2/Ti复合薄膜对Ti811合金基材在350℃中的摩擦磨损性能和微动疲劳性能的影响.结果表明:利用非平衡磁控溅射技术可以获得致密度高、晶粒细化、孔隙率低和膜-基结合强度高的MoS2/Ti复合薄膜;MoS2/Ti复合薄膜对Ti811合金表面具有良好的减摩润滑作用,能够显著改善Ti811合金在350℃下的摩擦磨损性能和微动疲劳性能;经喷丸强化处理后再进行非平衡磁控溅射MoS2/Ti复合薄膜,可以使Ti811合金在350℃下的耐微动疲劳性能优于MoS2/Ti薄膜,但不及喷丸强化处理的结果.这是由于非平衡磁控溅射工艺过程降低了喷丸强化层的残余压应力. MoS2/Ti composite films were prepared on Ti811 titanium alloy substrate by unbalanced magnetron sputtering (UBMS) method. The composition, bonding strength and hardness of the films were measured. The effect of the composite films on the tribological properties and fretting fatigue of Ti811 titanium alloy at 350 ℃ were investigated. The results indicate that the MoS2/Zi composite films prepared by UBMS technique had high density, small grain size, low void radio, and high bonding strength. The MoS2/Ti composite films improved the resistance of wear and fretting fatigue of the Ti alloy due to excellent lubricating the titanium alloy after shot peening exhibited better fretting properties of the films at 350 ℃. The UBMS films on fatigue resistance than the UBMS films without shot peening did. The compressive residual stress on the shot peened surface relaxed during preparing the MoS2/Ti composite films process, so they exhibited reduced fretting fatigue resistance.
出处 《摩擦学学报》 EI CAS CSCD 北大核心 2008年第3期219-224,共6页 Tribology
基金 国家自然科学基金资助项目(50671085,50371060) 国家高技术研究发展计划(863计划)资助项目(2007AA03Z521) 西北工业大学第六批青年科技创新基金资助项目(W016219)
关键词 钛合金 非平衡磁控溅射 复合薄膜 摩擦磨损性能 微动疲劳 高温 titanium alloy, unbalanced magnetron sputtering, composite films, friction and wear behavior, fretting fatigue, elevated temperature
  • 相关文献

参考文献17

  • 1James C W, Edgar A S. Progress in structural materials for aerospace systems[J]. Acta Materialia, 2003, 51 : 5 775-5 799.
  • 2Zhou Y G, Zeng W D, Yu H Q. An investigation of a new near-beta forging process for titanium alloys and its application in aviation components [ J ]. Materials Science and Engineering A, 2005, 393 : 204-212.
  • 3Ray A K, Das G, Ranganath V R. Failure of connecting pins of a compressor disc in an aero engine[ J ]. Engineering Failure Analysis, 2004, 11 : 613-617.
  • 4Bhaumik S K, Rangaraju R, Venkataswamy M A. Fatigue fracture of crank shaft of an aircraft engine[ J]. Engineering Failure Analysis, 2002, 9 : 255-263.
  • 5Hutson A L, Niinomi M, Nicholas T, et al. Effect of various surface conditions on fretting fatigue behavior of Ti-6A1-4V[J]. International Journal of Fatigue, 2002, 24( 12): 1 223-1 234.
  • 6Wei R, Shankar M, Jeffrey H. Evaluation of coatings on Ti-6A1-4V substrate under fretting fatigue [ J ]. Surface and Coatings Technolo- gy, 2004, 192(2): 177-188.
  • 7Hyukjae L, Shankar M, Shamachary S. Investigation into effects of re-shot-peening on fretting fatigue behavior of Ti-6A1-4V[ J ]. Materials Science and Engineering A, 2005, 390: 227-232.
  • 8刘道新,何家文.经不同表面改性处理的钛合金的微动疲劳和微动磨损行为对比研究[J].摩擦学学报,2005,25(1):13-17. 被引量:29
  • 9Hyukjae L, Shankar M. Stress relaxation behavior of shot peening Ti-6A1-4V under fretting fatigue at elevated temperature[J]. Materims Science and Engineering, 2004, A366:412-420.
  • 10张晓化,刘道新,高广睿.喷丸强化因素对Ti811合金高温微动疲劳抗力的影响[J].稀有金属材料与工程,2005,34(12):1985-1989. 被引量:10

二级参考文献40

  • 1翁立军,刘维民,孙嘉奕,薛群基.空间摩擦学的机遇和挑战[J].摩擦学学报,2005,25(1):92-95. 被引量:51
  • 2王均安,于德洋,欧阳锦林.二硫化钼溅射膜在潮湿空气中贮存后润滑性能的退化与失效机理[J].摩擦学学报,1994,14(1):25-32. 被引量:49
  • 3赵永庆,刘炳南.合金成分对Ti 811合金棒材性能的影响[J].稀有金属材料与工程,1994,23(3):59-64. 被引量:16
  • 4陈思觉.TC11钛合金的固体银脆试验[J].材料工程,1996,24(3):36-37. 被引量:2
  • 5STOLTZ R E,STULEN R H.Solid metal embrittlement of Ti6A16V2Sn by cadmium,silver and gold[J].Corrosion,1970,26(10):165-169.
  • 6FERNANDES P J L,.JONES D R H.Mechanisms of liquid metal induced embrittlement[J].International Materials Reviews,1997,42(6):251 -261.
  • 7LYNCH S P.Metal induced embrittlement of materials[J].Materials Characterization,1992,28:279-289.
  • 8Rai A K. Development of advanced coatings as palliatives for avoidance of fretting and galling in titanium alloy[R]. ADA387446, 2001.
  • 9Hoeppner D, Dibnazari S A, Moesser M W. Literature review and preliminary studies of fretting and fretting fatigue including special application to aircraft joints[R]. AD-A280310, 1994.
  • 10Fouvry S, Kapsa P, Vincent L. Fretting wear and fretting fatigue: relation through a mapping concept[C]. ASTM STP1367, 2000, 49-64.

共引文献106

同被引文献174

引证文献13

二级引证文献81

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