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Ag/Ni多层膜对钛合金微动磨损和微动疲劳抗力的影响 被引量:18

The Effect of Ag/Ni Multilayer Film on Fretting Wear and Fretting Fatigue Resistance of Titanium Alloy
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摘要 为了有效提高钛合金耐微动磨损和抗微动疲劳性能,且避免银脆隐患,在Ti811钛合金表面利用离子辅助磁控溅射沉积技术制备了不同调制周期的Ag/Ni金属多层膜,测试了多层膜的结构、结合强度、显微硬度和韧性,研究了不同调制周期的Ag/Ni多层膜对钛合金基材微动磨损和微动疲劳抗力的影响,并与纯Ag膜和纯Ni膜进行了对比.结果表明:离子辅助磁控溅射技术可以制备出致密度高、晶粒细致、结合强度高的Ag/Ni多层膜,多层膜的硬度随多层膜调制周期的减小而提高,调制周期小于100 nm时呈现明显的超硬度现象.Ag/Ni多层膜具有良好的减摩润滑作用和抗疲劳性能,能够显著改善Ti811钛合金耐微动磨损和抗微动疲劳性能,改善效果随多层膜调质周期降低而增大. To significantly improve the fretting wear (FW) and fretting fatigue (FF) resistance of titanium alloys and avoid the silver - induced embrittlement damage, the Ag/Ni muhilayer films with different modulation period thickness was prepared on a Ti811 titanium alloy surface by an ion assisted magnetron sputtering deposition (IAD) technique. The structure, bonding strength, micro - hardness and ductility of the multilayer films were measured. The effects of the Ag/Ni multilayer films with different modulation periods on the FW and FF resistance of the titanium alloy substrate were studied, and compared with pure Ag film and Ni film. The results indicated that the IAD technique can prepare Ag/Ni muhilayer films with high density, small grain size, high bonding strength. The micro - hardness of the Ag/Ni multilayer films increased with decreasing the modulation period thickness. The superhardness phenomenon occurred when the modulation period thickness of the muhilayer films was less than 100 nm. The Ag/Ni multilayer films could improve the FW and FF resistance of the Ti811 alloy due to its excellent lubricating and anti -fatigue properties. The FW and FF resistances of the TiS11 alloy increased with decreasing the modulation period thickness of the Ag/Ni muhilayer films.
出处 《摩擦学学报》 EI CAS CSCD 北大核心 2010年第5期498-504,共7页 Tribology
基金 国家自然科学基金项目(50671085 50771070) 国家863高技术研究发展计划项目(2007AA03Z521)的资助
关键词 微动疲劳 微动磨损 多层膜 磁控溅射 钛合金 fretting fatigue, fretting wear, muhilayer film, magnetron sputtering, titanium alloy
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参考文献18

  • 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 ( 3 ) : 255 - 263.
  • 5Hutson A L, Niinomi M, Nicholas T, et al. Effect of various surface conditions on fretting fatigue behavior of Ti - 6Al - 4V [J]. International Journal of Fatigue, 2002, 24(12) :1 223 - 1 234.
  • 6Wei R, Shankar M, Jeffrey H. Evaluation of coatings on Ti - 6Al- 4V substrate under fretting fatigue [ J ]. Surface and Coatings Technology, 2004, 192(2) : 177 -188.
  • 7Jin O, Mall S, Sanders J H, et al. Durability of Cu - Al coating on Ti - 6Al - 4V substrate under fretting fatigue [ J ]. Surface and Coatings Technology, 2006, 201 (10): 1704- 1 710.
  • 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
  • 9刘道新,马宗耀,何家文,黄淑菊.钛合金的银脆、镉脆敏感性及其控制[J].材料工程,1998,26(8):20-23. 被引量:9
  • 10Yang W M C, Tsakalakos T, Hilliard J E. Enhanced elastic modulus in composition - modulated gold - nickel and copper - palldium foils [ J ]. Journal of Applied Physics, 1977,48 : 876 - 879.

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