循环载荷下激光选区熔化TC4合金小裂纹萌生与扩展行为OA
Small crack initiation and propagation behavior of selective laser melting TC4 alloy under cyclic loading
基于扫描电镜原位疲劳测试技术,开展激光选区熔化(selective laser melting,SLM)TC4合金的小裂纹行为研究,通过聚焦离子束技术模拟增材制造过程中的初始缺陷,观察循环载荷下由缺陷诱发的合金小裂纹萌生与扩展行为.结果表明:循环载荷下,小裂纹极易在表面缺陷处萌生,裂纹萌生寿命较短,SLM TC4合金的疲劳寿命主要消耗在小裂纹扩展阶段.受微观结构影响,裂纹更容易沿着α/β界面扩展,由于α板条取样随机,小裂纹在扩展初期路径发生多次偏折,在晶粒内存在沿α片层与穿过α片层扩展的混合模式,裂纹扩展速率分散性大;当裂纹进入稳定扩展阶段后,裂纹尖端塑性滑移显著,微观结构的影响减弱,扩展路径趋于平直.与长裂纹扩展数据的对比分析表明,SLMTC4合金具有显著的"小裂纹效应".
Based on the in-situ fatigue test technique of scanning electron microscope(SEM),the small crack behavior of selective laser melting(SLM)TC4 alloy is studied.The focused ion beam(FIB)technique is used to manufacture the simulative initial defects in the process of additive manufacturing,and the initiation and propagation behavior of small cracks induced by defects are observed under cyclic loading.The results show that under cyclic loading,small cracks are easy to initiate at the surface defect,and the crack fatigue initiation life is short.The fatigue life of SLM TC4 alloys is mainly consumed in the small crack propagation stage.Affected by the microstructure,the small cracks are more likely to propagate along the α/β interface.Due to the random orientation of α laths,the path of small cracks is deflected several times in the initial propagation stage,exhibiting a mixed mode of propagation along α lamellae and through α lamellae within grains,resulting in significant scatter in crack growth rates.At the stable crack propagation stage,the plastic slips of the crack tip are obvious,the influence of microstructure is reduced,and the propagation path tends to straighten.Comparative analysis with long crack growth data indicates that SLM TC4 alloy exhibits a significant"small crack effect".
武亮亮;许瑞达;焦泽辉;于慧臣
中国航发北京航空材料研究院,北京 100095||中国航空发动机集团材料检测与评价重点实验室,北京 100095||航空材料检测与评价北京市重点实验室,北京 100095中国航发北京航空材料研究院,北京 100095||中国航空发动机集团材料检测与评价重点实验室,北京 100095||航空材料检测与评价北京市重点实验室,北京 100095中国航发北京航空材料研究院,北京 100095||中国航空发动机集团材料检测与评价重点实验室,北京 100095||航空材料检测与评价北京市重点实验室,北京 100095中国航发北京航空材料研究院,北京 100095||中国航空发动机集团材料检测与评价重点实验室,北京 100095||航空材料检测与评价北京市重点实验室,北京 100095
矿业与冶金
激光选区熔化TC4合金小裂纹效应裂纹萌生与扩展
selective laser meltingTC4 alloysmall crack effectcrack initiation and propagation
《材料工程》 2026 (4)
258-268,11
中国航发科技创新平台项目(CXPT-2023-035)财政部稳定支持基础研究计划基金项目(KZ0C190727)
评论