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2A12铝合金试件中空间斜裂纹在线止裂及性能分析
引用本文:付宇明,吴杰,康玮明,何大川. 2A12铝合金试件中空间斜裂纹在线止裂及性能分析[J]. 航空学报, 2008, 29(4): 1073-1078
作者姓名:付宇明  吴杰  康玮明  何大川
作者单位:燕山大学,机械工程学院,河北,秦皇岛,066004;燕山大学,电气工程学院,河北,秦皇岛,066004
摘    要: 选择带有空间斜裂纹的2A12铝合金试件进行了拉伸载荷作用下电磁热在线止裂研究。采用数值分析方法确定了止裂工艺参数,并求得了放电后试件内的温度场及热应力场;通过自制加载装置,应用ZL-2超强脉冲电流放电装置完成了空间裂纹在线止裂试验;对止裂前后的铝合金试件进行了微观组织分析和宏观力学性能测试。研究表明:脉冲放电瞬时,裂纹尖端熔化、钝化,并形成了高压应力区,提高了裂纹的扩展功,在一定的拉伸载荷下,试件也不会开裂,达到了裂纹在线止裂的目的。

关 键 词:电磁热效应  空间裂纹  止裂  微观组织  力学性能

On-line Crack Prevention and Performance Analysis of Aluminum Alloy 2A12 Specimen with Oblique Crack
Fu Yuming,Wu Jie,Kang Weiming,He Dachuan. On-line Crack Prevention and Performance Analysis of Aluminum Alloy 2A12 Specimen with Oblique Crack[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(4): 1073-1078
Authors:Fu Yuming  Wu Jie  Kang Weiming  He Dachuan
Affiliation:1.College of Mechanical Engineering, Yanshan University 2.College of Electrical Engineering, Yanshan University
Abstract:A study of crack prevention under tensile load is performed on an aluminum alloy 2A12 specimen with an oblique spatial crack by using electromagnetic heating on-line.Crack preventing technical parameters are determined by numerical analysis,and the temperature field and thermal stress field are obtained after discharge.By using a self-prepared homemade loading device and the super pulse current generating equipment of ZL-2,the spatial crack preventing experiment is carried out by electromagnetic heating on-line.Microstructure analysis and macroscopical mechanical property test are performed on the aluminum alloy specimen pre-and post prevention.Results show that at the time of pulse current discharging,the crack tip melts,dulls and forms a compressed stress area,which increases the propagation work of the crack.The crack will not propagate even with a certain amount of tensile load;thus the formation of the main crack source will be prevented.
Keywords:electromagnetic heating  spatial crack  crack preventing  microstructure  mechanical property
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