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大型翼面玻璃钢蜂窝夹层结构设计
引用本文:魏志毅.大型翼面玻璃钢蜂窝夹层结构设计[J].航空学报,1994,15(6):731-734.
作者姓名:魏志毅
作者单位:南京航空航天大学飞机系,南京,210016
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  
收稿时间:1993-05-31
修稿时间:1993-08-04

DESIGN OF A HONEYCOMB SANDWISH STRUCTURE WITH GLASS FIBER REINFORCED PLASTICS FOR A LARGE SCALE WING PANEL
Wei Zhiyi.DESIGN OF A HONEYCOMB SANDWISH STRUCTURE WITH GLASS FIBER REINFORCED PLASTICS FOR A LARGE SCALE WING PANEL[J].Acta Aeronautica et Astronautica Sinica,1994,15(6):731-734.
Authors:Wei Zhiyi
Institution:Depavtment of Aircraft Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing,210016
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.
Keywords:honeycomb structures  glass fibers  fail-safe system  
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