期刊文献+
共找到1篇文章
< 1 >
每页显示 20 50 100
Optimization of press bend forming path of aircraft integral panel 被引量:6
1
作者 阎昱 万敏 +1 位作者 王海波 黄霖 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2010年第2期294-301,共8页
In order to design the press bend forming path of aircraft integral panels,a novel optimization method was proposed, which integrates FEM equivalent model based on previous study,the artificial neural network response... In order to design the press bend forming path of aircraft integral panels,a novel optimization method was proposed, which integrates FEM equivalent model based on previous study,the artificial neural network response surface,and the genetic algorithm.First,a multi-step press bend forming FEM equivalent model was established,with which the FEM experiments designed with Taguchi method were performed.Then,the BP neural network response surface was developed with the sample data from the FEM experiments.Furthermore,genetic algorithm was applied with the neural network response surface as the objective function. Finally,verification was carried out on a simple curvature grid-type stiffened panel.The forming error of the panel formed with the optimal path is only 0.098 39 and the calculating efficiency has been improved by 77%.Therefore,this novel optimization method is quite efficient and indispensable for the press bend forming path designing. 展开更多
关键词 aircraft integral panel press bend forming path neural network response surface genetic algorithm optimization
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部