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Volume 38 Issue 3
Mar.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (3): 285-290,296.
Feng Haocheng, Luo Mingqiang, Liu Hu, et al. Rapid cockpit configuration design method research[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (3): 285-290,296. (in Chinese)
Citation: Feng Haocheng, Luo Mingqiang, Liu Hu, et al. Rapid cockpit configuration design method research[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (3): 285-290,296. (in Chinese)
shu

Rapid cockpit configuration design method research

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

  • Received Date: 14 Feb 2011
  • Publish Date: 30 Mar 2012
    Abstract
  • In order to improve the efficiency of civil airplane design in conceptual design phase, the design method of civil airplane-s cockpit was studied. The functionality was achieved in an open aircraft conceptual/preliminary design system. The coordinate of fuselage was defined. The method of defining eye design position of cockpit was studied. The method of cockpit layout and the parametric design and modeling method of windshield was presented. Based on these methods an interactive rapid design environment of civil airplane-s cockpit was constructed. Automatic adjustment for the cockpit was implemented, which was the basis for multidisciplinary design optimization in conceptual design phase.A design instance is given to illustrate the effectiveness of the methods.

     

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