首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于铸件热应力及变形的人工神经网络和遗传算法优化方法
引用本文:张丹,张卫红.基于铸件热应力及变形的人工神经网络和遗传算法优化方法[J].航空学报,2006,27(4):697-702.
作者姓名:张丹  张卫红
作者单位:西北工业大学,现代设计与集成制造技术教育部重点实验室,陕西,西安,710072
基金项目:国家自然科学基金 , 国家自然科学基金
摘    要: 将神经网络与遗传算法相结合,以有限元分析得到的样本集合作为教师样本,通过神经网络的训练建立设计参数与控制目标的非线性映射关系,并以此代替后续的有限元分析,获得遗传算法求解优化问题迭代中所需的目标函数近似值。以Al-4.5%Cu应力框为例,在分析铸件热应力及变形机理的基础上,对应力杆的高度、宽度和粗细杆截面比、浇注温度、界面换热系数和砂型的预热温度6个参数进行优化,从而有效地控制铸件内部的热应力及变形。优化结果表明:此方法在较少的有限元计算情况下即可获得较好的优化解,与初始设计相比,弯曲变形和热应力分别降低了58.5%和40.6%。

关 键 词:应力框  神经网络  遗传算法  热应力  变形  
文章编号:1000-6893(2006)04-0697-06
修稿时间:2005年1月12日

Optimization of Thermal Stress and Deformation of the Casting During Solidification by Neural Network and Genetic Algorithm
ZHANG Dan,ZHANG Wei-hong.Optimization of Thermal Stress and Deformation of the Casting During Solidification by Neural Network and Genetic Algorithm[J].Acta Aeronautica et Astronautica Sinica,2006,27(4):697-702.
Authors:ZHANG Dan  ZHANG Wei-hong
Institution:The Key Laboratory of Contemporary Design &; Integrated Manufacturing Technology, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:An artificial neural network is combined with the genetic algorithm.Based on some specimens given by FEM,a non-linear mapping function between multiple design variables and multiple control objects is constructed with BP neural networks (NN) in order to obtain the approximate objective function values that are necessary in optimum design using genetic algorithms(GA).An example of a frame-shape specimen(Al-4.5%Cu) is provided in the present work.By analyzing the deformation and thermal stress of the casting,an optimization process is performed for six design parameters including the height of the specimen,the width and the area ratio of the two stress bars,initial temperatures of the casting and the sand mould,and the heat-transfer coefficient as well.Results indicate that an improved solution can be obtained using less finite element analyses.Moreover,the deformation and the thermal stress decrease,respectively,by 58.5% and 40.6% compared with the initial design.
Keywords:stress-frame specimen  neural network  genetic algorithm  thermal stress  deformation
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号