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退火温度对7022铝合金干摩擦性能的影响
引用本文:汪洪峰,左敦稳,邵定林,黄铭敏,应峰.退火温度对7022铝合金干摩擦性能的影响[J].深圳大学学报(理工版),2010,27(2).
作者姓名:汪洪峰  左敦稳  邵定林  黄铭敏  应峰
作者单位:1. 南京航空航天大学机电学院,南京,210016
2. 南京航空航天大学材料科学与技术学院,南京,210016
基金项目:国家高技术研究发展计划(863计划),江苏省研究生创新计划项目 
摘    要:对7022铝合金的不同温度退火试样进行干滑动摩擦磨损试验,用扫描电镜、显微硬度测试仪和三维形貌仪分析各试样的磨损机制.结果表明,退火温度对材料的显微硬度和摩擦磨损性能有明显影响,退火温度在200℃时,材料显微硬度和摩擦磨损性能最好,此温度下材料得到完全再结晶,且晶粒细化;摩擦磨损性能随着显微硬度的提高而减小.塑变磨损、磨粒磨损和疲劳磨损为7022铝合金的主要磨损机理.

关 键 词:7022铝合金  摩擦学  滑动摩擦  大飞机焊接残余应力  航空材料  退火热处理  摩擦磨损性能  显微硬度  磨损机理

The effect of annealing temperature to the tribological property of 7022 aluminum alloy
WANG Hong-feng,ZUO Dun-wen,SHAO Ding-lin,HUANG Ming-min,YING Feng.The effect of annealing temperature to the tribological property of 7022 aluminum alloy[J].Journal of Shenzhen University(Science &engineering),2010,27(2).
Authors:WANG Hong-feng  ZUO Dun-wen  SHAO Ding-lin  HUANG Ming-min  YING Feng
Affiliation:WANG Hong-feng1,ZUO Dun-wen1,SHAO Ding-lin1,HUANG Ming-min1,and YING Feng21)College of Mechanical & Electrical Engineering Nanjing University of Aeronautics and Astronautics,Nanjing 210016 P.R.China2)College of Material Science & Technology Nanjing University of Aeronautics and Astronautics,Nanjing 210016 P.R.China
Abstract:Wear mechanisms of 7022 aluminum alloy annealed specimens at different temperatures were studied by means of scanning electron microscopy (SEM),micro hardness tester and three-dimensional shape analysis instrument.The results showed that annealing temperature has a significant effect on the sliding friction,on the wear properties and on the microhardness.Annealing temperature at 200 ℃,microhardness and friction and wear properties of 7022 aluminum alloy were the best.The material was fully recrystallized and the grain was refined.In addition,the sliding friction coefficient and the wear volume decrease as the microhardness increasing.Plastic deformation wear,the abrasive wear and the fatigue wear were the main wear mechanisms for 7022 aluminum alloy.
Keywords:7022 aluminum alloy  tribology  sliding friction  welding residual stress of jumbo jet  aircraft materiol  annealing  properties of friction and wear  hardness  abrasionmechanism
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