AZ31镁合金早期力学性能退化非线性超声检测

吴斌;颜丙生;何存富;焦敬品

航空材料学报 ›› 2011, Vol. 31 ›› Issue (1) : 87-92.

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航空材料学报 ›› 2011, Vol. 31 ›› Issue (1) : 87-92.
论文

AZ31镁合金早期力学性能退化非线性超声检测

  • 吴斌;颜丙生;何存富;焦敬品
作者信息 +

AZ31 Magnesium early Mechanical Performance Degradation Nondestructive Testing Using Nonlinear Ultrasonic

  • WU Bin;YAN Bing-sheng;HE Cun-fu;JIAO Jing-pin
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文章历史 +

摘要

针对镁合金材料早期力学性能退化问题,研究发展了一套可靠的非线性超声系数的测量实验系统,利用该系统测量了AZ31镁合金拉伸和疲劳试件的超声非线性系数。实验结果表明,在拉伸试件进入塑性应变阶段,疲劳试件在疲劳寿命的55%左右之前,超声非线性系数对镁合金材料力学性能退化具有很高的灵敏度。同时利用光学显微镜对拉伸试件的位错滑移带进行了原位微观观察,位错滑移带在塑性阶段随加载应力增大而增多。宏观力学、非线性超声检测和微观观察实验结果表明超声非线性系数作为宏观和微观的桥梁可以表征材料的早期力学性能退化情况。另外在中低周疲劳范围内,加载应力的大小以及拉-拉和拉-压疲劳模式的变化对实验结果没有明显的影响。

Abstract

Toward the problem of the metal material early degradation of mechanical properties,this research developed a robust experimental procedure.Using this system,ultrasonic nonlinearity parameters of AZ31magnesium monotonic load and fatigue samples were measured.The experimental results show that there is a significant increase inβlinked to magnesium mechanical performance degradation,into plastic deformation stage and before the fatigue life of 55%.Monotonic load sample was observed by optical microscopy in the same place,dislocation slip bands increase with stress.Macro-mechanics,nonlinear ultrasonic testing and microscopic observation results show that ultrasonic nonlinearity parameters as a bridge between micro and macro can characterize the mechanical properties of early degradation.However,in the context of low-cycle fatigue,changes of loading stress and the fatigue model with tension-tension fatigue and tension-compression fatigue had no significant effect to the experimental results.

关键词

非线性超声 / AZ31镁合金 / 力学性能退化 / 微观观察

Key words

nonlinear ultrasonic / AZ31magnesium / mechanical performan / observation of micro

引用本文

导出引用
吴斌;颜丙生;何存富;焦敬品. AZ31镁合金早期力学性能退化非线性超声检测[J]. 航空材料学报, 2011, 31(1): 87-92
WU Bin;YAN Bing-sheng;HE Cun-fu;JIAO Jing-pin. AZ31 Magnesium early Mechanical Performance Degradation Nondestructive Testing Using Nonlinear Ultrasonic[J]. Journal of Aeronautical Materials, 2011, 31(1): 87-92

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基金

北京市教委科技计划重点资助项目(KZ200810005001);国家自然科学基金资助项目(10772008)
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