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2A12铝合金疲劳裂纹的成核与扩展机理 |
卞贵学1, 陈跃良2, 张勇2, 赵晨1 |
1.海军航空工程学院研究生管理大队 烟台 264001
2.海军航空工程学院青岛校区 青岛 266041 |
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Microstructural Mechanism Fatigue Crack Nucleation and Propagation of 2A12 Aluminum Alloy |
BIAN Guixue1, CHEN Yueliang2, ZHANG Yong2, ZHAO Chen1 |
1.Graduate Students Team of Naval Aeronautical Engineering University, Yantai 264001
2.Qingdao Branch of Naval Aeronautical Engineering University, Qingdao 266041 |
引用本文:
卞贵学 陈跃良 张勇 赵晨. 2A12铝合金疲劳裂纹的成核与扩展机理[J]. 材料研究学报, 2012, 26(5): 521-526.
BIAN Guixue CHEN Yueliang ZHANG Yong ZHAO Chen.
Microstructural Mechanism Fatigue Crack Nucleation and Propagation of 2A12 Aluminum Alloy[J]. Chinese Journal of Materials Research, 2012, 26(5): 521-526.
1 M.Liao, G.Renaud, Probabilistic modeling of short crack growth in airframe aluminum alloys, Aircraft, 45, 1105(2008)2 Lynn Eugene Oswald, Effects microstructure on high–cycle fatigue of an Al–Zn–Mg–Cu alloy(AL–7055), MS Degree (Pittsburgh, University of Pittsburgh, 2003) p.3 Ali Merati, Graeme Eastaugh, Determination of fatigue related discontinuity state of 7000 series of aerospace aluminum alloys, Engineering Failure Analysis, 14, 673(2007)4 Ali Merati, A study of nucleation and fatigue behavior of an aerospace aluminum alloy 2024–T3, International Journal of Fatigue, 27, 33(2005)5 Min Liao, Probabilistic modeling of fatigue related microstructural parameters in aluminum alloys, Engineering Failure Mechanics, 76, 668(2009)6 LI Tang, WANG Qingyuan, The microstructure and fatigue initiation of an AA2524–T34 aluminum alloy, Journal of Southwest University of Science and Technology, 24(3), 23(2009)(李 棠, 王清远, AA2524--T34铝合金的微观结构与疲劳裂纹萌生机制, 西南科技大学学报, 24(3), 23(2009))7 WANG Xishu, TANG Bin, TAO Sha, In–situ observation technology and application of fatigue crack initiation and propagation for cast magnesium alloys, Materials for Mechanical Engineering, 30(2), 1(2006)(王习术, 汤 彬, 陶 沙, 铸造镁铝合金的微观破坏机理原位观测技术与应用, 机械工程材料, 30(2), 1(2006))8 BIAN Guixue, CHEN Yueliang, YU Dazhao, Study on initial discontinuity state of LY12 aluminium alloy, Structure & Environment Engineering, 34(5), 58(2007)(卞贵学, 陈跃良, 郁大照, LY12 铝合金初始不连续状态研究, 强度与环境, 34(5), 58(2007))9 BIAN Guixue, CHEN Yueliang, ZHANG Danfeng, Study on fatigue life of pre–corroded aluminium alloy based on IDS, Acta Aeronau Tica et Astronautica Sinica, 29(6), 1526(2008)(卞贵学, 陈跃良, 张丹峰, 基于IDS 的铝合金预腐蚀疲劳寿命研究, 航空学报, 29(6), 1526(2008))10 ZHONG Qunpeng, ZHAO Zihua, ZHANG Zheng, Development of “fractography” and research of fracture micromechanism, Journal of Mechanical Strength, 27(3), 358(2005)(钟群鹏, 赵子华, 张 峥, 断口学的发展及微观断裂机理研究, 机械强度, 27(3), 358(2005))11 ZHONG Qunpeng, ZHAO ZiHua, Fractography (Beijing, High Education Press, 2006) p.6(钟群鹏, 赵子华, 断口学 (北京, 高等教育出版社, 2006) p.6)12 Derek Hull, translated by LI xiaogang, DONG Chaofang, DU Cuiwei, Fractography: Observing Measuring and Interpreting Fracture Surface Topography (Beijing, Science Press, 2009) p.9(赫尔(Derek Hull), 李晓刚, 董超芳, 杜翠薇译, 断口形貌学: 观察、测量和分析断口形貌学的科学 (北京, 科学出版社, 2009) p.9)13 JIAN Haigen, JIANG Feng, WEN Kang, HUANG Hongfeng, WEI Lili, JIANG Long, Fatigue fracture of 7B04 aluminum alloy under different stresses, Journal of Central South University(Science and Technology), 24(3), 23(2009)(蹇海根, 姜 锋, 文 康, 黄宏锋, 韦莉莉, 蒋 龙, 不同应力下7B04铝合金的疲劳断口, 中南大学学报(自然科学版), 41(1), 132(2010))14 JIAN Haigen, JIANG Feng, ZHENG Xiuyuan, Study on fatigue fractography of high strength and toughness aluminum alloy for aviation, Journal of Aeronautical Materials, 30(4), 97(2010)(蹇海根, 姜 锋, 郑秀媛, 航空用高强高韧铝合金疲劳断口特征的研究, 航空材料学报, 30(4), 97(2010))15 CAO Changnian, WANG Zhizhi, ZHAO Xuanmin, Evaluation and coincidence check for initial fatigue quality of fastener hole, Journal of Northwestern Polytechnical University, 1, 15(2000)(曹昌年, 王志智, 赵选民, 紧固孔原始疲劳质量评定及符合性检查, 西北工业大学学报, 1, 15(2000))16 HU Renwei, LIU Wenting, Advanced method of durability analysis, Journal of Beijing University of Aeronautics And Astronautics, 1, 41(1999)(胡仁伟, 刘文珽, 结构原始疲劳质量分布方法的改进, 北京航空航天大学学报, 1, 41(1999)) |
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