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

以可靠性为约束的结构优化
引用本文:裴忠秀,詹承禹,黄文敏,张树林.以可靠性为约束的结构优化[J].航空学报,1989,10(6):330-334.
作者姓名:裴忠秀  詹承禹  黄文敏  张树林
作者单位:北京航空航天大学 (裴忠秀,詹承禹,黄文敏),北京航空航天大学(张树林)
摘    要: 常规结构优化设计存在以下两个根本缺陷:首先,没有确切考虑载荷及元件强度实际存在的不确定性,而用安全系数给以笼统的概括。安全系数取值一般较大,元、对结构带来的影响往往比经过优化设计所得到的效益还要大。第二,它是用元件的应力约束来保证结构系统安全,因此,它是结构元件安全基础上的优化设计。从系统论的观点看,元部件功能好整体功能不一定好。

关 键 词:结构系统可靠度  载荷增量法  结构优化  大步长插值法  
收稿时间:1988-04-27;

STRUCTURAL OPTIMIZATION WITH CONSTRAINT OF STRUCTURAL SYSTEM RELIABILITY
Beijing University of Aeronautics and AstronauticsPei Zhongxiu Zhan Chengyu Huang Wenmin and Zhang Shulin.STRUCTURAL OPTIMIZATION WITH CONSTRAINT OF STRUCTURAL SYSTEM RELIABILITY[J].Acta Aeronautica et Astronautica Sinica,1989,10(6):330-334.
Authors:Beijing University of Aeronautics and AstronauticsPei Zhongxiu Zhan Chengyu Huang Wenmin and Zhang Shulin
Institution:Beijing University of Aeronautics and AstronauticsPei Zhongxiu Zhan Chengyu Huang Wenmin and Zhang Shulin
Abstract:In this paper the problem of optimized structure design with the constraint of structure system reliability is investigated. In the reliability analysis of structure systems, the incremental load approach proposed by Fred Moses is applied to multi- loading situations. In the optimized design, a large step search method based on the concept of gradient projection is proposed. The method fully takes the advantages of the large step search method and the interpolating method and overcomes the defect of large step search method, i.e., its convergence rate is rather slow a't the end of each iteration. Several examples are computed.The results show that this method can really increase the convergence rate remarkably.
Keywords:structural system reliability  incremental load approach  structural optimzation  large step interpolating method    
本文献已被 CNKI 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