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2397合金高周疲劳性能及裂纹萌生扩展行为
引用本文:范雪松,郑子樵,张龙,胡芳,龚铸.2397合金高周疲劳性能及裂纹萌生扩展行为[J].稀有金属材料与工程,2017,46(5):1327-1333.
作者姓名:范雪松  郑子樵  张龙  胡芳  龚铸
作者单位:中南大学 有色金属材料科学与工程教育部重点实验室,中南大学 有色金属材料科学与工程教育部重点实验室,中南大学 有色金属材料科学与工程教育部重点实验室,中南大学 有色金属材料科学与工程教育部重点实验室,中南大学 有色金属材料科学与工程教育部重点实验室
基金项目:国家重点基础研究发展计划(“973”计划)(2012CB619503);
摘    要:研究了2397-T87铝锂合金的高周疲劳性能及裂纹萌生扩展行为。结果表明:在应力比R=0.1时,2397-T87铝锂合金L方向、LT方向和ST方向光滑试样(K_t=1.0)的疲劳寿命极限分别约为192,243和151 MPa;缺口试样(K_t=3.0)的疲劳寿命极限分别约为72,78和70 MPa。其疲劳裂纹主要萌生于试样表面,以及氧化物、夹杂等脱落形成的空洞,Al(CuFeMn)第二相杂质粒子。驻留滑移带(PSB)和晶粒取向对其疲劳裂纹早期扩展有重要影响。

关 键 词:2397合金  高周疲劳性能  裂纹萌生  裂纹扩展
收稿时间:2015/3/5 0:00:00
修稿时间:2015/4/13 0:00:00

High-cycle fatigue properties and crack initiation and propagation behavior of 2397 alloy
fan xue song,zheng zi qiao,zhang long,hu fang and gong zhu.High-cycle fatigue properties and crack initiation and propagation behavior of 2397 alloy[J].Rare Metal Materials and Engineering,2017,46(5):1327-1333.
Authors:fan xue song  zheng zi qiao  zhang long  hu fang and gong zhu
Affiliation:School of Materials Science and Engineering,Central South University,School of Materials Science and Engineering,Central South University,School of Materials Science and Engineering,Central South University,School of Materials Science and Engineering,Central South University,School of Materials Science and Engineering,Central South University
Abstract:The high-cycle fatigue properties and crack initiation and propagation behavior of 2397-T87 Al-Li alloy were investigated. The results show that when the stress ratio R is 0.1, the fatigue limit of smooth specimens of 2397-T87 Al-Li alloy in the L orientation, LT orientation and ST orientation are about 192 MPa, 243 MPa and 151 MPa respectively. The fatigue limit of notch specimens in the L orientation, LT orientation and ST orientation are about 72 MPa, 78 MPa and 70 MPa respectively. Fatigue crack initiation of this alloy mainly occurred on the sample surface, with initiation from the defects caused by the oxides and inclusions, the Al(CuMnFe) secondary phases. Persistent slip bands (PSB) and grain orientation have important influence on fatigue crack propagation at early stage.
Keywords:2397 alloy  high-cycle fatigue properties  crack initiation  crack propagation
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