飞机活动翼面的结构布局方法研究  

STRUCTURE LAYOUT FOR AIRCRAFT MOVABLE WING

作　　者：邓扬晨[1] 张卫红[1] 万敏[1] 章怡宁[2] 

机构地区：[1]西北工业大学中法并行工程联合实验室,西安710072 [2]沈阳飞机设计研究所,沈阳110035

出　　处：《力学与实践》2004年第5期14-17,共4页Mechanics in Engineering

基　　金：中国博士后科学基金(2002032222);航空科学基金(03853003);西北工业大学研究生创业种子基金(Z20030057);2004年西北工业大学本科毕业设计重点扶持项目

摘　　要：为探讨飞机活动翼面结构布局方法,提供一种用于结构方案论证时的新方法.采用模块化策略作为技术途径,表现为将CAD,CAE和结构拓扑优化组合使用,以UG作为CAD几何造型平台,以ANSYS作为CAE建模平台,利用“敏度阀值”概念和“约束补偿”措施构造出一种拓扑优化新算法.以实际飞机型号作为算例,优化结果与真实的结构布局形式相比较,能够指出传统设计的不足之处,既验证了建立的物理模型的合理性,又考核了该优化算法的有效性.In order to study the structure layout of movable wing of future aircraft and to provide an integrated design method, the author uses a modular strategy and several technical tools, including CAD/CAE and structural topology optimization. We use UG as CAD platform, ANSYS as CAE platform. A new algorithm based on the gradient threshold concept and a sort of constraint compensation technique is obtained. A practical aircraft wing is used as an example and optimal results show the weakness of the practical one. This can be seen from Fig.8 and Fig.12 and it is shown that this physical model is reasonable. By Fig.9 and Fig.13, we can say that the proposed algorithm is effective and reliable.

关 键 词：CAD CAE 几何造型 UG 新算法 平台 建模 活动 实际 结构布局 

分 类 号：O241.82[理学—计算数学] TP391[理学—数学]