摘要
研究加热过程中TiB2/6351Al及其基体合金喷丸形变层组织结构的变化,利用X射线衍射线形分析方法计算不同加热温度和时间下的晶块尺寸和显微畸变。结果表明:喷丸使表层晶粒细化,织构消失并且在加热后不再出现;加热过程中,复合材料晶块长大速度低于基体材料,且复合材料显微畸变更易释放;喷丸过程中增强体周围产生的高密度位错使储存能提高,从而促进再结晶,但晶块的进一步长大因增强体的钉扎作用而受到阻碍;复合材料的热稳定性高于基体合金。
The microstructures of 6351A1 and TiB2/6351A1 during heating process were investigated by X-ray diffractometry. Domain size and microstrain were calculated by modified Warren-Averbach method and Voigt method. The results show that the textures of both specimens are randomized by shot peening and do not appear again after any heat treatments. Domains grow during heat treatments, and the growth of domains in composite is slower than that of monolithic 6351A1 alloy. The microstrain of composite is easier to release than that of the alloy. Higher density dislocation around reinforcements improves stored energy and promotes recrystallization while further domain growth is retarded, The thermostability of composite is higher than that of alloy.
出处
《中国有色金属学报》
EI
CAS
CSCD
北大核心
2008年第8期1402-1406,共5页
The Chinese Journal of Nonferrous Metals
基金
白玉兰科技人才基金资助项目(2007B071)
关键词
复合材料
晶块尺寸
显微畸变
线形分析
喷丸
连续加热
composite
domain size
microstrain
line profile analysis
shot peening
continuous heating
