滑轮结构的多工况拓扑优化
详细信息 查看官网全文
- 英文论文题名：Multiple Load Cases Topology Optimization of Pulley Structure
- 论文作者：胡平 ; 张兴金 ; 孙拴利 ; 陈磊
- 英文论文作者：Hu Ping ; Zhang Xingjin ; Sun Shuanli ; Chen Lei ; R&D Center ; AVIC Aircraft CO.LTD.
- 年：2016
- 作者机构：中航飞机研发中心;
- 论文关键词：滑轮结构 ; 多工况 ; 拓扑优化 ; 折中规划法
- 英文论文关键词：pulley structure ; multiple load cases ; topology optimization ; compromise programming approach
- 会议召开时间：2016-10-31
- 会议录名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛文集（上册）
- 英文会议录名称：Discovery,Innovation and Communication——Proceedings of 7th CSAA Science and Technology Youth Forum
- 语种：中文
- 分类号：V229
- 学会代码：ZGHU
- 会议名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛
- 会议地点：中国广东中山
- 主办单位：中国航空学会
- 学会名称：中国航空学会
- 页数：6
- 文件大小：1224k
- 原文格式：O
- 会议级别：全国
摘要
针对滑轮结构的多工况情况,以刚度为目标函数进行拓扑优化设计,本文通过将多工况优化问题转化为多目标优化问题,分别采用线性加权法和折中规划法来研究多目标拓扑优化问题。使用OptiStruct模块滑轮结构优化求解,并且对比两种方法的优化效果,经过重新建模,使结构重量由7.213kg减小到6.652kg。
According to the situation of multiple load cases,the topology optimization design of the pulley structure with stiffness as the objective function is carried out.In this paper,the multiple load cases optimization problem is transformed into multiobjective optimization problems with the use of linear weighting and compromising programming approach to study the multiobjective topology optimization problems.Using Optistruct module to optimize the solution,we compate the optimization effect of two methods,and reduce the weight of the structure by re-modeling from the original 7.231 to 6.652 Kg.
According to the situation of multiple load cases,the topology optimization design of the pulley structure with stiffness as the objective function is carried out.In this paper,the multiple load cases optimization problem is transformed into multiobjective optimization problems with the use of linear weighting and compromising programming approach to study the multiobjective topology optimization problems.Using Optistruct module to optimize the solution,we compate the optimization effect of two methods,and reduce the weight of the structure by re-modeling from the original 7.231 to 6.652 Kg.
引文
[1]夏天翔,姚卫星.连续体结构拓扑优化方法评述[J].航空工程进展,2011,(1).
[2]Mlejnek H P,R Schirrmacher.An Engineers Approach to Optimal Material Dist Ribution and Shape Finding Computer Method in Applied Mechanic and Engineering[J].Computer Methods in Applied Mechanics and Engineering,1993,106(1-2):1-26.
[3]吴顶峰.基于变密度法的连续体结构拓扑优化研究[D].西安电子科技大学:西安电子科技大学,2010.
[4]邱亚玲,伊海洋,王维,伍建川.基于人工制造约束的三维拓扑优化设计方法[J].机械设计与制造,2015,(1).
[5]方子帆,杨磊,杜道佳,何孔德,张屹.支撑结构多目标拓扑优化设计研究[J].中国机械工程,2010,(15).
[6]范文杰,范子杰,苏瑞意.汽车车架结构多目标拓扑优化方法研究[J].中国机械工程,2008(19):1505-1508.
[7]刘铁钢.传动滚筒简体结构有限元分析[D].大连理工大学:大连理工大学,2015.
[2]Mlejnek H P,R Schirrmacher.An Engineers Approach to Optimal Material Dist Ribution and Shape Finding Computer Method in Applied Mechanic and Engineering[J].Computer Methods in Applied Mechanics and Engineering,1993,106(1-2):1-26.
[3]吴顶峰.基于变密度法的连续体结构拓扑优化研究[D].西安电子科技大学:西安电子科技大学,2010.
[4]邱亚玲,伊海洋,王维,伍建川.基于人工制造约束的三维拓扑优化设计方法[J].机械设计与制造,2015,(1).
[5]方子帆,杨磊,杜道佳,何孔德,张屹.支撑结构多目标拓扑优化设计研究[J].中国机械工程,2010,(15).
[6]范文杰,范子杰,苏瑞意.汽车车架结构多目标拓扑优化方法研究[J].中国机械工程,2008(19):1505-1508.
[7]刘铁钢.传动滚筒简体结构有限元分析[D].大连理工大学:大连理工大学,2015.