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

火焰筒浮动瓦块的壁温-结构一体化优化
引用本文:高建辉,温卫东,崔海涛.火焰筒浮动瓦块的壁温-结构一体化优化[J].航空动力学报,2012,27(3):588-594.
作者姓名:高建辉  温卫东  崔海涛
作者单位:南京航空航天大学能源与动力学院,南京,210016
摘    要:以火焰筒浮动瓦块结构为研究对象,提出了利用神经网络与遗传算法相结合的方法对浮动瓦块中冷却结构变量和安装位置变量进行同步优化.利用遗传算法分别对冷却结构变量和安装位置变量进行优化,将安装位置优化结果作为冷却结构变量优化中遗传操作的依据,最终实现冷却结构和安装位置的同步优化.为了通过计算效率,利用神经网络对安装位置的优化结果进行映射取代其优化过程.算例结果表明:该方法高效、精确,有很好的工程实用价值.

关 键 词:浮动瓦块  火焰筒  优化  神经网络  遗传算法
收稿时间:2011/4/17 0:00:00
修稿时间:2011/10/27 0:00:00

Optimal design for temperature and structure of the float-wall of flame tube
GAO Jian-hui,WEN Wei-dong and CUI Hai-tao.Optimal design for temperature and structure of the float-wall of flame tube[J].Journal of Aerospace Power,2012,27(3):588-594.
Authors:GAO Jian-hui  WEN Wei-dong and CUI Hai-tao
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:Taking the float-wall structure as the object of study,neural network and genetic algorithm were used to settle synchronistically the optimization of cooling structures and install position.Using genetic algorithm to perform cooling structures and install position optimization,and taking the result of install position optimization as the foundation of cooling structures optimization,thus finally realized the synchronized optimizations of cooling structures and install position.In order to enhance the efficiency of algorithm,neural network was used to perform mapping on the result of install position optimization so as to replace its optimization processes.The result of calculating example shows that the method being mentioned is highly active,accurate and possesses good application value to engineering.
Keywords:float-wall  flame tube  optimization  neural network  genetic algorithm
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》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