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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1994, Vol. 15 ›› Issue (6): 731-734.

• 论文 • Previous Articles     Next Articles

DESIGN OF A HONEYCOMB SANDWISH STRUCTURE WITH GLASS FIBER REINFORCED PLASTICS FOR A LARGE SCALE WING PANEL

Wei Zhiyi   

  1. Depavtment of Aircraft Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing,210016
  • Received:1993-05-31 Revised:1993-08-04 Online:1994-06-25 Published:1994-06-25

Abstract: he structural designs of AD-series aircraft are described in detail,especially for AD-200 aircraft. Based on testing data a connective method with glue nails and toothed nails is recommended, which can solve the problem of connection between a metal joint and a honey-comb sandwich structure. The difficulty of direct connection between a metal structure and a honeycomb sandwich structure is solved by using a plywood transition structure. In addition,a set of reliable measure of fail-safe designs are proposed.

Key words: honeycomb structures, glass fibers, fail-safe system

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