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点蚀损伤7075-T6铝合金弹性性能计算模型的理论与实验研究
引用本文:毋玲,孙秦,郭英男.点蚀损伤7075-T6铝合金弹性性能计算模型的理论与实验研究[J].航空学报,2007,28(5):1272-1275.
作者姓名:毋玲  孙秦  郭英男
作者单位:西北工业大学,航空学院,陕西,西安,710072
基金项目:航天支撑技术基金 , 西北工业大学校科研和教改项目
摘    要: 点蚀坑是高强度铝合金材料中广泛存在的一种腐蚀形式,这种点蚀损伤会导致材料性能的下降,严重地威胁着结构的承载能力。根据点蚀损伤的特点,在细观力学的理论基础上,建立了点蚀损伤材料弹性性能计算的孔隙率模型。使用7075-T6铝合金,在连续酸性盐雾环境下进行预腐蚀。根据预腐蚀件的拉伸实验结果,对模型的正确性进行验证。模型计算与实验结果的对比证明了本文方法的可行性与正确性。

关 键 词:点蚀坑  铝合金  细观力学  
文章编号:1000-6893(2007)06-1272-04
修稿时间:2006年10月18

Theoretical and Experimental Research for the Elastic Properties of Corroded 7075-T6 Al Alloy
Wu Ling,Sun Qin,Guo Yingnan.Theoretical and Experimental Research for the Elastic Properties of Corroded 7075-T6 Al Alloy[J].Acta Aeronautica et Astronautica Sinica,2007,28(5):1272-1275.
Authors:Wu Ling  Sun Qin  Guo Yingnan
Institution:School of Aeronautics, Northwestern Polytechnical University
Abstract:The researches were aimed at assessing the elastic properties of material with pre-existing corrosion damage.Corrosion in the form of pitting in certain classes of aluminum alloys,e.g.7075-T6,is considered here.Based on the characteristics of corrosion metrics and micromechanics,the paper describes a mechanical property prediction procedure for corroded aluminum alloy.The model was developed in the framework of micro-mechanics,in combination with the existing corroded coupon tensile test results.The existing data included the weight loss rates of 7075-T6 sheet exposed to acid salt spray(fog)for various time periods.Tensile tests were taken for corroded "dog bone" coupons.The paper describes the test procedures and mechanical test results.The results provide a database for verifying the analysis model.The accuracy of the method is assessed by comparing the predicted results with those of tests of corroded 7075-T6 specimens.The results indicate that corrosion can be represented by voids damage in the material as the elastic properties of corroded aluminum alloy are concerned.
Keywords:corrosion pit  aluminum alloy  micromechanics
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