阳极氧化对7475铝合金疲劳性能和断口形貌的影响Effects of anodic oxidation on fatigue property and fracture of 7475 aluminum alloy
王进春,孔德军
摘要(Abstract):
利用阳极氧化对7475铝合金进行表面改性处理,通过拉伸疲劳试验,用罗卡提法求出阳极氧化前后7475铝合金的疲劳极限。采用SEM、XRD等手段对阳极氧化前后7475铝合金的断口形貌和组成物相进行了分析,并对阳极氧化前后7475铝合金疲劳断裂机理进行了探讨。结果表明,阳极氧化膜主要是由γ-Al2O3和α-Al2O3组成,膜层越厚,α-Al2O3相含量越多;氧化膜降低了铝合金的疲劳性能,与原始试样相比,膜层厚度为6、8和10μm的试样疲劳极限分别下降了3.2%、3.9%和4.5%;氧化膜在基体原位生长,在界面处基体中产生的残留拉应力促进了疲劳源的萌生,使铝合金的疲劳性能有所降低。
关键词(KeyWords): 阳极氧化;7475铝合金;疲劳性能;断口形貌
基金项目(Foundation): 江苏省科协首席专家(工程师)项目(2013-216)
作者(Author): 王进春,孔德军
DOI: 10.13289/j.issn.1009-6264.2015.11.021
参考文献(References):
- [1]Tomasz Brynk,Zbigniew Pakiela,Mariusz Kulczyk,et al.Fatigue crack growth rate in ultrafine-grained Al 5483 and 7475 alloys processed by hydroextrusion[J].Mechanics of Materials,2013,67:46-52.
- [2]孔德军,王进春,刘浩.7475铝合金阳极氧化膜表面-界面组织与特征[J].中国有色金属学报,2014,24(7):1744-1751.KONG De-jun,WANG Jin-chun,LIU Hao.Structures and characteristics of 7475 aluminium alloy surface-interface by anodic oxidation[J].The Chinese Journal of Nonferrous Metals,2014,24(7):1744-1751.
- [3]张林,张豪,朱玉桂.喷射成形7475铝合金组织和性能演变[J].材料热处理学报,2014,35(12):67-73.ZHANG Lin,ZHANG Hao,ZHU Yu-gui.Evolution of microstructure and properties of spray-deposited 7475 alloy[J].Transactions of Materials and Heat Treatment,2014,35(12):67-73.
- [4]Chung-Youb Kim,Jae-Man Choi,Ji-Ho Song.Fatigue crack growth and closure behavior under random loadings in 7475-T7351 aluminum alloy[J].International Journal of Fatigue,2013,47:196-204.
- [5]Hiroki TANAKA,Tadashi MINODA.Mechanical properties of 7475 aluminum alloy sheets with fine subgrain structure by warm rolling[J].Transactions of Nonferrous Metals Society of China,2014,24(7):2187-2195.
- [6]陈勃,高玉魁,吴学仁,等.喷丸强化7475-T7351铝合金的小裂纹行为和寿命预测[J].航空学报,2010,31(3):519-525.CHEN Bo,GAO Yu-kui,WU Xue-ren,et al.Small crack behavior and fatigue life prediction for shot peening aluminum alloy 7475-T7351[J].Acta Aeronautica Et Aeronautica Sinica,2010,31(3):519-525.
- [7]Nursen Saklakoglu,Simge Gencalp Irizalp,Erhan Akman,et al.Near surface modication of aluminum alloy induced by laser shock processing[J].Optics&Laser Technology,2014,64:235-241.
- [8]Saeedikhani M,Javidi M,Yazdani A.Anodizing of 2024-T3 aluminum alloy in sulfuric-boric-phosphoric acids and its corrosion behavior[J].Transactions of Nonferrous Metals Society of China,2013,23(9):2551-2559.
- [9]王文昌,张垒,孔德军,等.YL113铝合金阳极氧化膜表面-界面形貌与能谱分析[J].材料热处理学报,2014,35(3):177-183.WANG Wen-chang,ZHANG Lei,KONG De-jun,et al.Surface-interface morphologies and EDS analysis of anodic oxide film on surface of aluminum alloy YL113[J].Transactions of Materials and Heat Treatment,2014,35(3):177-183.
- [10]汝继刚,李超,王亮,等.喷丸强化对7A12铝合金微观组织和疲劳性能的影响[J].航空材料学报,2013,33(6):51-56.RU Ji-gang,LI Chao,WANG Liang,et al.Effect of shot peening on microstructure and fatigue life of 7A12 aluminum[J].Journal of Aeronautical Materials,2013,33(6):51-56.
- [11]GAO Y K,WU X R.Experimental investigation and fatigue life prediction for 7475-T7351 aluminum alloy with and without shot peening-induced residual stresses[J].Acta Materialia,2011,59(9):3737-3747.
- [12]王声波,范勇,吴鸿兴,等.7050航空铝合金结构材料激光冲击强化处理研究[J].中国激光,2004,31(1):125-128.WANG Sheng-bo,FAN Yong,WU Hong-xing,et al.Research of strengthening 7050 aerial aluminum alloy structural material with laser shock processing[J].Chinese Journal of Lasers,2004,31(1):125-128.
- [13]乔艳江,孙强,李春旺,等.合金钢与铝合金疲劳极限的理论估算方法分析[J].力学与实践,2007,29(4):47-50.QIAO Yan-jiang,SUN Qiang,LI Chun-wang,et al.The fatigue limit estimation methods for alloy steels and aluminum alloys[J].Mechanics in Engineering,2007,29(4):47-50.
- [14]刘建秀,丁遂栋.铝合金光试样非对称循环疲劳极限的估算[J].机械强度,1999,21(2):157-158.LIU Jian-xiu,DING Sui-dong.The estimation of nonsymmetry cycle fatigue limits for aluminium alloy smooth specimens[J].Journal of Mechanical Strength,1999,21(2):157-158.
- [15]蹇海根,姜锋,文康,等.不同应力下7B04铝合金的疲劳断口[J].中南大学学报:自然科学版,2010,41(1):132-137.JIAN Hai-gen,JIANG Feng,WEN Kang,et al.Fatigue fracture of 7B04 aluminum alloy under different stresses[J].Journal of Central South University-Science and Technology,2010,41(1):132-137.
- [16]徐超.7075铝合金的低周疲劳行为及其损伤演化机理研究[D].上海:上海工程技术大学,2012.XU Chao.Research on low cycle fatigue behavior and damage mechanism of 7075 aluminum alloy[D].Shanghai:Shanghai University of Engineering Science,2012.
文章评论(Comment):
|
||||||||||||||||||
|
||||||||||||||||||