Effects of precipitates on fatigue crack growth rate of AA 7055 aluminum alloy

被引：0
|
作者：
陈军洲 [1 ]
甄良 [2 ]
杨守杰 [1 ]
戴圣龙 [1 ]
机构：
[1] Beijing Institute of Aeronautical Materials
[2] School of Materials Science and Engineering,Harbin Institute of Technology
来源：
Transactions of Nonferrous Metals Society of China | 2010年 / 20卷 / 12期
关键词：
7055 aluminum alloy; ageing; fatigue crack growth rate; precipitate;
D O I：
暂无
中图分类号：
TG146.21 [];
学科分类号：
080502 ;
摘要：
The effects of precipitates on the fatigue crack growth rate of AA 7055 Al alloy subjected to different ageing treatments were investigated using transmission electron microscope and fatigue crack growth testing.The results show that the T77 treated samples exhibit the lowest crack growth rate,while the crack growth rate of over-aged samples is the highest.In terms of the model based on the reversibility of dislocation motion within the plastic zone close to the crack tip,the improved crack growth resistance is attributed to many precipitates that are coherent with Al matrix in the under-aged and T77 treated samples.When the precipitate is coherent with the Al matrix,the larger the precipitate is,the slower the fatigue crack grows.The effects of grain boundary precipitates and precipitate free zone on the fatigue crack growth resistance are less significant than those of precipitates within grains of the alloy.
引用
收藏
页码：2209 / 2214
页数：6
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