航空学报 > 1994, Vol. 15 Issue (6): 731-734

大型翼面玻璃钢蜂窝夹层结构设计

魏志毅   

  1. 南京航空航天大学飞机系,南京,210016
  • 收稿日期:1993-05-31 修回日期:1993-08-04 出版日期:1994-06-25 发布日期:1994-06-25

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

摘要: 全面地介绍了AD系列飞机,特别是AD200飞机的玻璃钢蜂窝夹层结构的设计思想和具体措施。以试验数据为依据,推荐采用胶钉和齿钉的紧固连接方式,解决了金属接头与蜂窝夹层结构的连接问题,并在金属件与蜂窝之间采用层板过渡办法,解决了金属件与蜂窝直接连接的困难。此外,提出一套可靠的抗破损安全设计的措施。

关键词: 蜂窝结构, 玻璃钢纤维, 故障-安全系统

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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