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民用飞机机身结构快速设计及自动化调整

陈稗 罗明强 武哲

陈稗, 罗明强, 武哲等 . 民用飞机机身结构快速设计及自动化调整[J]. 北京航空航天大学学报, 2014, 40(6): 782-787. doi: 10.13700/j.bh.1001-5965.2013.0391
引用本文: 陈稗, 罗明强, 武哲等 . 民用飞机机身结构快速设计及自动化调整[J]. 北京航空航天大学学报, 2014, 40(6): 782-787. doi: 10.13700/j.bh.1001-5965.2013.0391
Chen Bai, Luo Mingqiang, Wu Zheet al. Rapid structure design and automated adjustment of civil aircraft fuselage[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(6): 782-787. doi: 10.13700/j.bh.1001-5965.2013.0391(in Chinese)
Citation: Chen Bai, Luo Mingqiang, Wu Zheet al. Rapid structure design and automated adjustment of civil aircraft fuselage[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(6): 782-787. doi: 10.13700/j.bh.1001-5965.2013.0391(in Chinese)

民用飞机机身结构快速设计及自动化调整

doi: 10.13700/j.bh.1001-5965.2013.0391
基金项目: 

工业和信息化部“民用飞机总体设计支撑软件”基金资助项目

详细信息
    作者简介:

    陈 稗(1987- ),女,北京人,博士生,chenbai214@126.com.

  • 中图分类号: V221

Rapid structure design and automated adjustment of civil aircraft fuselage

  • 摘要: 为了在飞机设计前期对结构进行较详细的考虑,满足在设计前期进行以强度为约束的重量特性评估、方案评估等方面的需求,研究了民用飞机机身结构快速设计、建模以及模型自动化调整的方法,并运用该方法在一个开放式飞机总体设计环境中开发实现了此功能.定义了飞机机身坐标系,提出了机身各类结构件的参数化描述及构建模型的方法,建立了交互式机身结构设计环境,可自动获取结构的体积、重量和惯性矩等信息.在此基础上实现了模型自动化调整和重量特性的同步更新,为总体设计阶段进行飞机重量、气动和结构的多学科设计优化奠定了基础.最后,用设计实例验证了该方法的有效性.

     

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出版历程
  • 收稿日期:  2013-07-02
  • 网络出版日期:  2014-06-20

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