| CAD/CAE在飞机改型设计中的应用 |
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| 引用本文： | 伍厚军,郑国磊,闫勇,柳泽,罗乖林. CAD/CAE在飞机改型设计中的应用[J]. 飞机设计, 2003, 0(2): 10-12,16 |
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| 作者姓名： | 伍厚军 郑国磊 闫勇 柳泽 罗乖林 |
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| 作者单位： | 1. 北京航空航天大学,北京,100083
2. 空军第一研究所,北京,100076 |
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| 摘 要： | 结合某试验机承力密封框结构件的研制 ,开展先进CAD/CAE系统在飞机改型设计中的应用研究 ,其中包括 :简要介绍应用先进的CAD/CAE系统 ,进行承力密封框的三维数字化建模 ,包括建立三维结构模型和有限元分析模型 ;根据承力密封框的使用环境和设计要求 ,确定对其进行刚度和强度分析时所需的各种主要参数 ;应用CAE系统计算承力密封框的刚度和强度 ,分析计算结果。最后 ,总结了先进CAD/CAE系统在飞机改型设计中的应用效果
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| 关 键 词： | 机身承力框 计算机辅助设计 有限元分析 |
The Application of CAD/CAE Technology to the Design of a Certain Test Aircraft |
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| Wu Houjun ,Zheng Guolei ,Yan Yong ,Liu Zhe ,Luo Guailin. The Application of CAD/CAE Technology to the Design of a Certain Test Aircraft[J]. Aircraft Design, 2003, 0(2): 10-12,16 |
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| Authors: | Wu Houjun Zheng Guolei Yan Yong Liu Zhe Luo Guailin |
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| Affiliation: | Wu Houjun 1,Zheng Guolei 1,Yan Yong 2,Liu Zhe 2,Luo Guailin 2 |
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| Abstract: | A study of the application of an advanced CAD/CAE system to the redesign of a load-bearing airtight bulkhead for a certain test aircraft has been performed. The CAD/CAE system was used for the three-dimensional digital modeling of the airtight bulkhead, including the three-dimensional structure model and finite element analysis model; the principle parameters required for the stiffness and strength analysis were determined by accounting for the operation environment constraints and design requirements; and the CAE system was used to conduct the stiffness and strength computation and computation result analysis for the load-bearing airtight bulkhead. Finally, the application of the system to the design change of airframe structural members was summarized. |
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| Keywords: | load-bearing bulkhead computer aided design finite element analysis |
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