期刊文献+

表面氮化对活塞环摩擦磨损参数的影响分析 被引量:2

Analysis of Surface Nitriding Affecting the Ring Wear and Friction Parameters of Piston Ring
下载PDF
导出
摘要 用摩擦磨损试验机对铸铁活塞环在氮化前后与高硼铜铸铁缸套配合分别进行了半小时和一小时摩擦磨损试验,测量了氮化前后的活塞环表面摩擦系数和磨损量、磨损率,并对磨痕进行了分析。结果表明:未氮化活塞环摩擦系数大于氮化环,摩擦系数变化稳定性比氮化活塞环差,未氮化环磨损量较氮化环增大了约39.6%(半小时)及51.0%(一小时),未氮化环磨损率的一小时试验比半小时试验平均升高6.7%,氮化环磨损率降低了13.7%,与未氮化环配合的缸套磨损量较与氮化环配合的缸套的磨损量和磨损率与活塞环比较规律一致,表面磨痕显示未氮化环磨损剧烈,由此氮化处理提高活塞环-缸套摩擦副的稳定性,且耐磨性得到提高。 Testing nitride piston ring and non-nitride piston ring with high boron copper cast iron cylinder with friction and wear testing machine in a half hour and one hour,it measured these two different piston rings' surface friction coefficient,wear volume,wear rate and analyzed the wear scar.The results show that non-nitride piston ring's friction coefficient is bigger than nitride piston ring’s friction coefficient,but no nitride piston ring’s friction coefficient is not very stable.The amount of non-nitride piston ring wear increased by about 39.6% higher than the nitride piston ring(half hour)and 51.0%(one hour),and non-nitride piston ring's wear rate of the one hour test increased by about 6.7% than the half-hour test while the nitride piston ring's wear rate decreased by about 13.7%.The situation of the cylinders which are rubbing with these two different piston rings is same as the situation of piston rings.Surface grinding marks that nitride piston ring wear more Serious.So,nitrogen treatment can improve the stability of the pair of piston ring-cylinder liner friction,and wear resistance is improved.
出处 《机械设计与制造》 北大核心 2013年第8期178-181,共4页 Machinery Design & Manufacture
关键词 活塞环 摩擦磨损 氮化 Piston Ring Friction and Wear Nitride
  • 相关文献

参考文献6

二级参考文献59

  • 1张德坤,葛世荣.钢丝的微动磨损及其对疲劳断裂行为的影响研究[J].摩擦学学报,2004,24(4):355-359. 被引量:24
  • 2桂长林,刘焜.内燃机活塞环-缸套摩擦功耗的设计计算方法之研究[J].摩擦学学报,1994,14(4):328-336. 被引量:10
  • 3胡俊宏,金映丽,丁津原.硫烯在可降解基础油中的摩擦学特性的研究[J].机械设计与制造,2006(5):97-99. 被引量:1
  • 4葛世荣.矿井提升机可靠性技术[M].徐州:中国矿业大学出版社,1994..
  • 5Zhou Z R, Fayeulle S, Vincent L. Cracking behavior of various ',duminium 'alloys during fretting wear [ J ]. Wear, 1992, 189: 51 -57.
  • 6Z R Zhou, M Fiset, A Cardou, et al. Effect of lubricant in electrical conductor fretting fatigue [ J ]. Wear, 1995, 189:51 - 57.
  • 7M Shima, H Suetake, I R McColl, et al. On the behaviour of an oil lubricated fretting contact[ J]. Wear, 1997, 210:304 - 310.
  • 8J Xu, Z R Zhou, C H Zhang, et al. An investigation of fretting wear behaviors of bonded solid lubricant coatings[ J]. Journal of Materials Processing Technology, 2007, 182:146 - 151.
  • 9M H Zhu, Z B Cai, X Z Lin, et al. Fretting wear behaviors of micro -arc oxidation coating sealed by grease[ J ]. Wear, 2007, 267 : 299 - 307.
  • 10Yoshiro lwai, Weiya Hou, Tomomi Honda, et al. Wear behaviour of high tensile strength aluminium alloys under dry and lubricated conditions [ J ]. Wear, 1996, 196 : 46 - 53.

共引文献64

同被引文献16

  • 1仲志全,李华宇,尹琪.发动机运行工况对机油耗影响的试验研究[J].内燃机工程,2004,25(5):69-71. 被引量:16
  • 2飞机设计手册总编委会.飞机设计手册:起飞着陆系统设计[M].北京:航空工业出版社,2002:271-280.
  • 3郑庆林.摩擦学原理[M].北京:高等教育出版社,1994.
  • 4HB6176-88 飞机油-气缓冲器起落架设计[S].
  • 5Norman S-Currey.Air Craft Landing Gear Design:Principles and Practiees[M].USA:AIAA Education Series,1988(49).
  • 6Wei Xiao-Hui,Liu Cheng-Long,Song Xiao-Chen.Drop dynamic analysis of half-axle flexible aircraft landing gear[J].Journal of Vibro engineering,2014,16(1):290-298.
  • 7Khodd amzadeh A,Liu R,Wu XJ.Novel polyte trafluoro-ethylene(PTFE)composites with newly developed tribaloy alloy additive for sliding bearings[J].Wear,2008,266(7/8):646-657.
  • 8GJB67.1A-2008,军用飞机结构强度规范第1部分:总则[S].
  • 9GJB67.4A-2008,军用飞机结构强度规范第4部分:地面载荷[S].
  • 10刘丽兰,刘宏昭,吴子英,王忠民.机械系统中摩擦模型的研究进展[J].力学进展,2008,38(2):201-213. 被引量:165

引证文献2

二级引证文献2

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