FINITE ELEMENT PEEN FORMING SIMULATION

被引:0
|
作者
Gariepy, Alexandre [1 ]
Larose, Simon [2 ]
Perron, Claude [2 ]
Bocher, Philippe [3 ]
Levesque, Martin [1 ]
机构
[1] Ecole Polytech, Dept Genie Mecan, CREPEQ, CP 6079,Succ Ctr Ville, Montreal, PQ H3C 3A7, Canada
[2] Natl Res Council Canada, Aerosp Mfg Technol Ctr, Montreal, PQ H3T 2B2, Canada
[3] Ecole Technol Super, Montreal, PQ H3C 1K3, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Peen forming; Shot peening; Finite element; Aerospace; Residual stress;
D O I
暂无
中图分类号
TF [冶金工业];
学科分类号
0806 ;
摘要
Shot peening consists of projecting multiple small particles onto a ductile part in order to induce compressive residual stresses near the surface. Peen forming, a derivative of shot peening, is a process that creates an unbalanced stress state which in turn leads to a deformation to shape thin parts. This versatile and cost-effective process is commonly used to manufacture aluminum wing skins and rocket panels. This paper presents the finite element modelling approach that was developed by the authors to simulate the process. The method relies on shell elements and calculated stress profiles and uses an approximation equation to take into account the incremental nature of the process. Finite element predictions were in good agreement with experimental results for small-scale tests. The method was extended to a hypothetical wing skin model to show its potential applications.
引用
收藏
页码:681 / 686
页数:6
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