首页 | 本学科首页   官方微博 | 高级检索  
     检索      

LY-12铝合金应变疲劳性能和疲劳位错结构
引用本文:李庆生,蔡其巩,陈宪禧,潘天喜,周兆祥.LY-12铝合金应变疲劳性能和疲劳位错结构[J].航空学报,1982,3(1):86-91.
作者姓名:李庆生  蔡其巩  陈宪禧  潘天喜  周兆祥
作者单位:北京钢铁研究总院 (李庆生,蔡其巩,陈宪禧,潘天喜),红安公司(周兆祥)
摘    要: 系统研究了LY-12铝合金自然时效及240℃人工时效试样的应变疲劳性能和疲劳位错结构。通过疲劳位错组态、位错的滑移特征以及位错同微观组织相互作用的研究,解释了该种实际合金的疲劳性能。

关 键 词:
收稿时间:1981-01-01;

STRAIN FATIGUE PROPERTIES AND FATIGUE DISLOCATION STRUCTURES OF 2024 ALUMINUM ALLOY
Li Qingsheng,Tsai Chikung,Chen Xianxi,Pan Tianxi,Zhou Zhaoxiang.STRAIN FATIGUE PROPERTIES AND FATIGUE DISLOCATION STRUCTURES OF 2024 ALUMINUM ALLOY[J].Acta Aeronautica et Astronautica Sinica,1982,3(1):86-91.
Authors:Li Qingsheng  Tsai Chikung  Chen Xianxi  Pan Tianxi  Zhou Zhaoxiang
Institution:1. Central Iron and Steel Research Institute;2. Hongan Corporation
Abstract:This paper mainly deals with the relation between the strain fatigue properties and the fatigue dislocation structures in 2024 aluminum alloy. Some interesting features of the fatigue dislocation structure in this commercial alloy are observed.The analysis of deformation work density for smooth fatigue specimens shows that the strain fatigue properties of specimens aged at 240℃ are . much better than naturally aged specimens at high strain level.Systematic study of fatigue dislocation structures in this alloy under the transmission electron microscope reveals that wavy slip mode at high strain level and plain slip mode at low strain level are characteristics of the dislocation slip in the naturally aged specimens, in contrast cross slip is much easier in the 240℃ aged specimens at different strain levels. By foil thickness analysis the existence of {112} slip plane in 240℃ aged specimens was confirmed.It is also pointed out that the helical dislocations in the alloy are formed through cutting of moving dislocations with dislocation loops.The conclusion has been drawn that the features of dislocation slip serve as an essential factor which affects the interaction of dislocations with other microstructures and determines the fatigue properties.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号