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TiB2颗粒增强ZA—8锌合金的显微组织与疲劳裂纹扩展行为的关系
引用本文:华文君,王执锐,张继荣.TiB2颗粒增强ZA—8锌合金的显微组织与疲劳裂纹扩展行为的关系[J].金属学报,1996,32(3):254-260.
作者姓名:华文君  王执锐  张继荣
作者单位:北京航空材料研究所
摘    要:研究了TiB2颗粒增强ZA-8锌合金复合材料和基体材料和疲劳裂纹扩展行为与显微组织,断口的关系,结果表明:所研究复合材料的抗疲劳裂纹扩展能力优于基体材料,尤其在小裂纹阶段,其原因为:增强粒子与裂纹尖端的相互作用降低了裂纹尖端的应力强度;增强粒子与基体良好的界面结合力。

关 键 词:锌合金  疲劳裂纹  扩展  显微组织  硼化钛
收稿时间:1996-03-18
修稿时间:1996-03-18

RELATIONSHIP BETWEEN MICROSTRUCTURE AND FATIGUE CRACK PROPAGATION BEHAVIOUR IN TiB_2 PARTICULATE REINFORCED ZA-8 Zn ALLOY
HUA Wenjun,WANG Zhirui,ZHANG Jirong.RELATIONSHIP BETWEEN MICROSTRUCTURE AND FATIGUE CRACK PROPAGATION BEHAVIOUR IN TiB_2 PARTICULATE REINFORCED ZA-8 Zn ALLOY[J].Acta Metallurgica Sinica,1996,32(3):254-260.
Authors:HUA Wenjun  WANG Zhirui  ZHANG Jirong
Abstract:The relationships between microstructure, fracture surface and propagation behaviour of fatigue crack in TiB2 particulate reinforced ZA-8 Zn alloy and in the corresponding constitute matrix materials were studied. The present results indicate that the resistance to fatigue crack growth of the employed composite is in general superior to that of constitute matrix materials, especially for the short crack behaviour. This is attributed to (1) the interaction between particle and crack tip decreased the stress intensity ahead of the crack tip,(2) owing to the excellent interface strength,(3) the addition of reinforcement caused the change of matrix microstructure and refined the structure and (4) the bridging function of reinforcement. Finally, the mechanism for the difference in fatigue crack growth behaviour of the two materials was discussed. Correspondent HUA Wenjun, Beijing Institute of Aeronautical Materials, Beijing 100095
Keywords:fatigue crack propagation  interface strength  microstructure
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