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基于叶脉分枝结构的飞机盖板结构仿生设计

刘良宝 陈五一

刘良宝, 陈五一. 基于叶脉分枝结构的飞机盖板结构仿生设计[J]. 北京航空航天大学学报, 2013, 39(12): 1596-1600.
引用本文: 刘良宝, 陈五一. 基于叶脉分枝结构的飞机盖板结构仿生设计[J]. 北京航空航天大学学报, 2013, 39(12): 1596-1600.
Liu Liangbao, Chen Wuyi. Structural bionic design for aircraft cover plate based on leaf vein branched structure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(12): 1596-1600. (in Chinese)
Citation: Liu Liangbao, Chen Wuyi. Structural bionic design for aircraft cover plate based on leaf vein branched structure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(12): 1596-1600. (in Chinese)

基于叶脉分枝结构的飞机盖板结构仿生设计

基金项目: 国家自然科学基金资助项目(50975012)
详细信息
  • 中图分类号: TH122;TB17

Structural bionic design for aircraft cover plate based on leaf vein branched structure

  • 摘要: 针对薄壁件的轻量化设计要求,在对王莲叶脉分枝结构形态和构型规律分析基础上,以飞机盖板原型为对象,应用结构仿生设计方法,对盖板内部的筋板分布形式进行结构仿生设计,利用ANSYS APDL参数化设计语言建立仿生型结构的参数化模型并进行筋板结构参数优化.有限元分析结果表明,相对于原型盖板,结构参数优化后的仿生型盖板质量减小,比强度结构效能有较大提高,静力学性能明显改善.

     

  • [1] Diaz R C.The ongoing bionic revolution[J].Current Opinion in Otolaryngology & Head and Neck Surgery, 2012, 20(5):385
    [2] Liu J S, Hollaway L.Design optimization of composite panel str-uctures with stiffening ribs under multiple loading cases[J].Computers & Structure, 2000, 78(4):637-647
    [3] 王飞, 何景武.基于仿生学的机翼结构刚度和强度设计研究[J].飞机设计, 2010, 30(4):1-4 Wang Fei, He Jingwu.Research into aerofoil structure rigidity and intensity design based on bionics[J].Aircraft Design, 2010, 30(4):1-4(in Chinese)
    [4] 杨建霞.冰模板法制备层状多级孔仿生复合材料的研究[D].武汉:华中科技大学生命科学与技术学院, 2010 Yang Jianxia.Research on fabrication of bionic composite materials with hierarchical structure by using ice-templating[D].Wuhan:School of Life Science and Technology, Huazhong University of Science and Technology, 2010(in Chinese)
    [5] 岑海堂, 陈五一.小型翼结构仿生设计与试验分析[J].机械工程学报, 2009, 45(3):286-290 Cen Haitang, Chen Wuyi.Structural bionic design and experime-ntal analysis for small wing[J].Journal of Mechanical Engineeri-ng, 2009, 45(3):286-290(in Chinese)
    [6] Xing Denghai, Chen Wuyi, Zhao Lin, et al.Structural bionic de-sign for high-speed machine tool working table based on distributi-on rules of leaf veins[J].Science China Technological Science, 2012, 55(8):2091-2098
    [7] 丁晓红, 李国杰, 蔡戈坚, 等.薄板结构的加强筋自适应成长设计法[J].中国机械工程, 2005, 16(12):1057-1060 Ding Xiaohong, Li Guojie, Cai Gejie, et al.Adaptive growth m-ethod of rib distribution for thin plate structure[J].China Mechanical Engineering, 2005, 16(12):1057-1060(in Chinese)
    [8] 赵岭.基于结构仿生的机床运动构件高比刚度设计[D].北京:北京航空航大学机械工程及自动化学院, 2009 Zhao Ling.Design of machine tool moving structures for high sp-ecific stiffness based on structural bionic[D].Beijing:School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, 2009(in Chinese)
    [9] 周庆源, 傅德志, 靳晓白.克鲁兹王莲(睡莲科)的开花生物学研究[J].西北植物学报, 2006, 26(8):1526-1533 Zhou Qingyuan, Fu Dezhi, Jin Xiaobai.Floral biology of victoria cruziana(nymphaeaceae)[J].Acta Botanica Boreali-Occidentalia Sinica, 2006, 26(8):1526-1533(in Chinese)
    [10] 王志谨, 姚卫星.飞机结构设计[M].北京:国防工业出版社, 2009 Wang Zhijin, Yao Weixing.Aircraft structure design[M].Beijing:National Defence Industry Press, 2009(in Chinese)
    [11] 喻懋林.基于结构仿生的高比强度、比刚度结构设计研究[D].北京:北京航空航大学机械工程及自动化学院, 2005 Yu Maolin.Research on the high specific strength and specific sti-ffness structure design based on the structural bionic theory[D].Beijing:School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, 2005(in Chinese)
    [12] Karl J N.The mechanical roles of clasping leaf sheaths:evidence from Arundinaria tecta(Poaceae) shoots subjected to bending and twisting forces[J].Annals of Botany, 1998, 81:23-24
    [13] Hidetoshi K, Mashasi D, Kaori K.Venation pattern of butuerbur leaf and its mechanical contribution[J].J Soc Mat Sci, 2000, 49(12):1318-1323
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出版历程
  • 收稿日期:  2013-01-22
  • 网络出版日期:  2013-12-30

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