THE MICROSTRUCTURE AND MECHANISM OF FATIGUE CRACK INITIATION OF 2024-T3 AND 2524-T34 ALUMINUM ALLOYS
The micro structure and mechanism of fatigue crack initiation of 2024-T3 and 2524-T34 Al alloys were investigated at the present paper.Four-point bending and tension-tension fatigue tests were conducted on the test alloys along the rolling direction at room temperature and frequency of 15Hz,R=0.1.It was found that the flat grain was elongated along the rolling direction,showing the laminar grain structure.The majority of fatigue cracks of 2524 were initiated at coarse particles,a few of them was formed on sites of material defects or slip bands.The intrusion and extrusion induced by slip band in the Al cladding layer provided principal fatigue crack initiation sites for 2024 Al-cladding aluminum alloys.
Aluminum alloy micro structure fatigue crack fatigue crack initiation
T.Li Q.Y.Wang
College of Civil Engineering and Architecture,South west Univ.of Science and Technology,Mianyang,621 Department of Engineering Mechanics,Sichuan University,Chengdu,610065,China
国际会议
The Third International Conference on Heterogeneous Material Mechanics(第三届国际非均匀材料力学会议)
上海
英文
929-932
2011-05-22(万方平台首次上网日期,不代表论文的发表时间)