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Volume 39 Issue 4
Apr.  2013
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Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  39(4): 463-468.
Yan Weitian, Luo Mingqiang, Liu Hu, et al. Layout optimization of civil airplane wing structure based on automated finite element modeling[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(4): 463-468. (in Chinese)
Citation: Yan Weitian, Luo Mingqiang, Liu Hu, et al. Layout optimization of civil airplane wing structure based on automated finite element modeling[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(4): 463-468. (in Chinese)
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Layout optimization of civil airplane wing structure based on automated finite element modeling

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 18 Apr 2012
  • Publish Date: 30 Apr 2013
    Abstract
  • Focusing on the widely-applied two spar wing structure on civil airplanes, a wing CAD model was created parametrically according to the numbers of its stringers and ribs. Then a wing structure finite element method(FEM) model was constructed automatically by Patran command language(PCL), it was realized by 4 major steps, which were geometry model segmentation, geometry segment renumbering, segment mesh definition and FEM model generation. A complete procedure was fulfilled to construct and analyze a wing structure FEM model automatically after the numbers of its stringers and ribs had been changed, then it was integrated into a wing structure layout optimization that could be applied in preliminary design. In the end, a case study model was constructed referring to a typical civil airplane wing. Under the constraints of static strength, stiffness and skin stability, the numbers of stringers and ribs were optimized to achieve a minimum structure weight. Results show that the optimal layout brought a 10.1% structure weight reduction, which indicates the effectiveness and feasibility of the optimization.

     

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    • References(14)
  • [1]
    Shen J Y,Ferguson F.Weight reduction through optimal arrangement of force-carrying components within wing box structures .AIAA-2004-4495,2004
    [2]
    Nawijn M,van Tooren M J L,Berends J P T J,et al.Automated finite element analysis in a knowledge based engineering environment .AIAA-2006-947,2006
    [3]
    王伟,常楠.飞机翼面结构多级布局优化设计思想及需要解决的问题[J].飞机设计,2007,27(5):1-6 Wang Wei,Chang Nan.Multi-level optimization in wing structural configuration design and future research aspects[J].Aircraft Design,2007,27(5):1-6(in Chinese)
    [4]
    刘颖卓,张永存,刘书田,等.考虑复合材料蒙皮稳定性的飞机翼面结构布局优化设计[J].航空学报,2010,31(10):1985-1992 Liu Yingzhuo,Zhang Yongcun,Liu Shutian,et al.Layout optimization design of wing structures with consideration of stability of composite skin[J].Acta Aeronautica et Astronautica Sinica,2010,31(10):1985-1992(in Chinese)
    [5]
    Wang Wei,Yang Wei,Chang Nan.Integration shape and sizing optimization of composite wing structure based on response surface Method[J].Transactions of Nanjing University of Aeronautics & Astronautics,2008,25(2):94-100
    [6]
    何林涛,万小朋,赵美英,等.布局优化和尺寸优化相结合的复合材料机翼优化设计[J].中国机械工程,2008,19(17):2077-2080 He Lintao,Wan Xiaopeng,Zhao Meiying,et al.Composite aircraft wing structure optimization using combination of layout and sizing[J].Chinese Journal of Mechanical Engineering,2008,19(17):2077-2080(in Chinese)
    [7]
    王伟,赵美英,常楠.基于两相法的机翼结构几何优化设计[J].飞机设计,2007,27(1):22-26 Wang Wei,Zhao Meiying,Chang Nan.Geometrical optimization of aircraft wing based on double-state technology[J].Aircraft Design,2007,27(1):22-26(in Chinese)
    [8]
    张仲桢,余雄庆,胡添元.飞翼式飞行器结构布局与构件尺寸的两级优化[J].计算机辅助工程,2009,18(1):27-30 Zhang Zhongzhen,Yu Xiongqing,Hu Tianyuan.Two-level optimization on structural layout and component size of flying wing aircraft[J].Computer Aided Engineering,2009,18(1):27-30(in Chinese)
    [9]
    邓扬晨,詹光,高彤,等.飞机翼面结构布局综合设计方法研究[J].飞机设计,2004(2):28-36 Deng Yangchen,Zhan Guang,Gao Tong,et al.Analysis and synthesis based aircraft wing structural layout study[J].Aircraft Design,2004(2):28-36(in Chinese)
    [10]
    Skillen M D,Crossley W A.A matlab-based object-oriented process architecture for rapid generation of unconventional wing finite element models .AIAA-2008-2160,2008
    [11]
    罗明强,冯昊成,刘虎,等.机翼结构有限元的快速建模及自动化调整[J].北京航空航天大学学报,2011,37(6):680-684 Luo Mingqiang,Feng Haocheng,Liu Hu,et al.Rapid wing structural finite element modeling and automated adjustment[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(6):680-684(in Chinese)
    [12]
    邓扬晨,廖家驹,章怡宁,等.面向设计的飞机翼面结构有限元自动建模技术[J].飞机设计,2002(1):9-13 Deng Yangchen,Liao Jiaju,Zhang Yining,et al.Design-oriented finite element auto-modeling to aircraft wing structures[J].Aircraft Design,2002(1):9-13(in Chinese)
    [13]
    Dassault Systèmes.Isight 4.5 Component Guide[M].USA:Dassault Systèmes,2010:621-623
    [14]
    王宝忠.飞机设计手册第10册:结构设计[M].北京:航空工业出版社,2000:410-411 Wang Baozhong.Aircraft design manual vol 10-structure design[M].Beijing:Aviation Industry Press,2000:410-411(in Chinese)
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