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Volume 40 Issue 6
Jun.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(6): 782-787.
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)
shu

Rapid structure design and automated adjustment of civil aircraft fuselage

doi: 10.13700/j.bh.1001-5965.2013.0391

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

  • Received Date: 02 Jul 2013
  • Publish Date: 20 Jun 2014
    Abstract
  • To improve the quality and efficiency of civil aircraft design, it would be better to take structure design into account earlier, instead of beginning structure design in later preliminary design phase or detail design phase. A method to implement fuselage structure rapid design, modeling, and automated adjustment for civil aircraft was studied. The parametric modeling method of fuselage structure was represented， and a functionality of rapid fuselage structure design for civil aircraft, which can obtain the characteristics including mass, centre of gravity and inertia, was developed in an open aircraft conceptual/preliminary design system. In addition, the automatic adjustment of fuselage structure model and automatic update of mass property data were implemented, which contribute to multidisciplinary optimization work. An instance was presented to illustrate that this implementation method is feasible and effective.

     

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