检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:徐效东[1] 杨新岐[1] 周光[1] 佟健华[2]
机构地区:[1]天津大学材料科学与工程学院天津市现代连接技术重点实验室,天津300072 [2]中国搅拌摩擦焊中心北京赛福斯特技术有限公司,北京100024
出 处:《航空材料学报》2012年第3期51-56,共6页Journal of Aeronautical Materials
基 金:国家自然科学基金资助项目(50775159)
摘 要:研究了铝合金2024-T4搅拌摩擦焊(FSW)搭接接头的微观组织特征和疲劳性能。结果表明,搭接接头后退侧热力影响区晶粒变形程度较前进侧严重。疲劳试样断裂位置均位于弱连接缺陷向上"拉起"较严重的焊核区后退侧。当应力比为0.1时,铝合金搅拌摩擦焊搭接接头对应于95%存活率的疲劳强度特征值Δσk为18.25MPa,与铝合金熔焊搭接接头的Δσk为13.92MPa相比,增加了31.11%。与此同时,FSW搭接接头疲劳S-N曲线斜率m为5.39,大于熔焊接头所对应的S-N曲线斜率范围3.0~3.5,可见在长寿命区搭接接头的疲劳性能优于熔焊接头。搭接接头的裂纹源位于搭接接头上板底部位置的表面缺陷或者强化相颗粒处,对应于弱连接缺陷处。Microstructures and the fatigue performances of AA6061-T6 friction-stir-welded overlap joints were investigated. It was shown that the grain deformation of TMAZ was more serious in the retreating side than that in the advancing side. All the fatigue fra ture sites of specimens were initiated at the more serious booking defect, in which the up-trend was larger. When R was equal to 0.1 , the fatigue strength △σk of Aluminum alloy FSW overlap joints was 18.25MPa for the 95% survival probability, which meant an increase of 31.11% as compared with the /△σk 13.92MPa of Aluminum alloy fusion overlap welded joints. Besides, it was observed that the slope value m for the S-N curve of the FSW joints was 5.39, which was higher than that of the fusion welded joint set to 3.0- 3.5. So the FSW joint had better fatigue strength than that of the fusion welded joints in the long life region of fatigue performance. Fatigue cracking was initiated at the surface defects or strengthening phase particles locating at the bottom of the upper plate, which were corresponded to the hooking position.
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.173