深圳大学学报(理工版)
深圳大學學報(理工版)
심수대학학보(리공판)
JOURNAL OF SHENZHEN UNIVERISYT SCIENCE & ENGINEERING
2010年
2期
131-136
,共6页
汪洪峰%左敦稳%邵定林%黄铭敏%应峰
汪洪峰%左敦穩%邵定林%黃銘敏%應峰
왕홍봉%좌돈은%소정림%황명민%응봉
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
7022鋁閤金%摩抆學%滑動摩抆%大飛機銲接殘餘應力%航空材料%退火熱處理%摩抆磨損性能%顯微硬度%磨損機理
7022려합금%마찰학%활동마찰%대비궤한접잔여응력%항공재료%퇴화열처리%마찰마손성능%현미경도%마손궤리
7022 aluminum alloy%tribology%sliding friction%welding residual stress of jumbo jet%aircraft materiol%annealing%properties of friction and wear%hardness%abrasionmechanism
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.
對7022鋁閤金的不同溫度退火試樣進行榦滑動摩抆磨損試驗,用掃描電鏡、顯微硬度測試儀和三維形貌儀分析各試樣的磨損機製.結果錶明,退火溫度對材料的顯微硬度和摩抆磨損性能有明顯影響,退火溫度在200℃時,材料顯微硬度和摩抆磨損性能最好,此溫度下材料得到完全再結晶,且晶粒細化;摩抆磨損性能隨著顯微硬度的提高而減小.塑變磨損、磨粒磨損和疲勞磨損為7022鋁閤金的主要磨損機理.
대7022려합금적불동온도퇴화시양진행간활동마찰마손시험,용소묘전경、현미경도측시의화삼유형모의분석각시양적마손궤제.결과표명,퇴화온도대재료적현미경도화마찰마손성능유명현영향,퇴화온도재200℃시,재료현미경도화마찰마손성능최호,차온도하재료득도완전재결정,차정립세화;마찰마손성능수착현미경도적제고이감소.소변마손、마립마손화피로마손위7022려합금적주요마손궤리.
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.