帮助 关于我们

返回检索结果

喷丸对激光辅助成形铝合金样件拉-拉疲劳性能的影响
Influence of Shot Peening on Tension-Tension Fatigue Property of Laser Aided Forming Aluminum Alloy Samples

查看参考文献15篇

文摘 为了研究激光辅助成形样件的疲劳性能及喷丸处理的作用规律,以2024铝合金板材为对象,对原始、激光辅助成形以及激光辅助成形后再喷丸等样件的微观组织、显微硬度、残余应力和拉-拉疲劳性能进行了对比分析研究。结果表明:激光辅助成形后,样件的组织和微结构未发现明显变化,但其硬度和残余拉应力水平有所下降;喷丸处理的激光辅助成形样件表层组织改变、显微硬度提高、其拉-拉疲劳寿命显著提高,不仅高于激光辅助成形样件,也高于初始样件。
其他语种文摘 In order to study the fatigue properties of laser aided forming samples and realize the effects of shot peening treatment on these samples,with aluminum alloy plate 2024 as the test object,the microstructure,microhardness,residual stress and tension-tension fatigue properties of as-machined aluminum samples,samples of laser aided forming and shot peened samples are studied.The results show that the microstructures of laser aided forming samples are not varied obviously,but their microhardness and extensive residual stress decrease,while after shot peening the surface microstructures of the laser aided forming samples become varied,their microhardness is raised and their fatigue properties are greatly improved.The tension-tension fatigue lives of shot peened samples are not only higher than the laser aided forming samples,but also higher than the as-machined aluminum samples.
来源 航空学报 ,2011,32(7):1351-1356 【核心库】
关键词 铝合金 ; 疲劳 ; 激光 ; 喷丸 ; 微观组织 ; 残余应力
地址

中国科学院力学研究所, 北京, 100190

语种 中文
文献类型 研究性论文
ISSN 1000-6893
学科 金属学与金属工艺;航空
基金 国家自然科学基金 ;  中国博士后科学基金
文献收藏号 CSCD:4277696

参考文献 共 15 共1页

1.  Yan Y. Optimization of press bend forming path of aircraft integral panel. Transactions of Nonferrous Metals Society of China,2010,20(2):294-301 被引 4    
2.  Massa L. Spatial linear analysis of the flow in a solid rocket motor with burning walls. Combustion and Flame,2009,156(4):865-888 被引 2    
3.  Kolich M. A conceptual framework proposed to formalize the scientific investigation of automobile seat comfort. Applied Ergonomics,2008,39(1):15-27 被引 6    
4.  Yoon J W. Childs buckling analysis for an integrally stiffened panel structure with a friction stir weld. Thin-Walled Structures,2009,47(12):1608-1622 被引 8    
5.  Huang L. FEM Analysis of Spring-backs in Age Forming of Aluminum Alloy Plates. Chinese Journal of Aeronautics,2007,20(6):564-569 被引 20    
6.  Harburn B. Shot peen forming of compound contours:US Patent,4329862,1982 被引 1    
7.  Zerbst U. Fracture and damage mechanics modelling of thin-walled structures-an overview. Engineering Fracture Mechanics,2009,76(1):5-43 被引 7    
8.  Majzoobi G H. The effects of multiple re-shot peening on fretting fatigue behavior of Al 7075-T6. Surface and Coatings Technology,2010,205(1):102-109 被引 3    
9.  陈光南. 压弯激光复合成形方法:中国,ZL2007100629102,2009 被引 1    
10.  陈光南. 飞机外壳成形件激光精调方法:中国,ZL2007100629117,2008 被引 1    
11.  彭青. 一种基于预应力的激光和喷丸复合成形方法:中国,ZL2008101156030,2009 被引 1    
12.  彭青. 整体壁板激光辅助预应力成形. 航空学报,2009,130(8):1544-1548 被引 6    
13.  Carpio F J. Fatigue behavior of laser machined 2024 T3 aeronautic aluminum alloy. Applied Surface Science,2003,208/209:194-198 被引 4    
14.  Zhai T. The grain boundary geometry for optimum resistance to growth of short fatigue cracks in high strength Al-alloys. International Journal of Fatigue,2005,27(10/12):1202-1209 被引 12    
15.  张定铨. 残余应力对金属疲劳强度的影响. 理化检验:物理分册,2002,38(6):231-235 被引 19    
引证文献 3

1 何卫锋 激光冲击叶片榫头变形控制与疲劳试验 航空学报,2014,35(7):2041-2048
被引 6

2 钟丽琼 残余应力场和不同应力比下TC11钛合金的高周疲劳性能 稀有金属材料与工程,2015,44(5):1224-1228
被引 7

显示所有3篇文献

论文科学数据集
PlumX Metrics
相关文献

 作者相关
 关键词相关
 参考文献相关

版权所有 ©2008 中国科学院文献情报中心 制作维护:中国科学院文献情报中心
地址:北京中关村北四环西路33号 邮政编码:100190 联系电话:(010)82627496 E-mail:cscd@mail.las.ac.cn 京ICP备05002861号-4 | 京公网安备11010802043238号