大型翼面玻璃钢蜂窝夹层结构设计  

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

作　　者：魏志毅[1] 

机构地区：[1]南京航空航天大学飞机系

出　　处：《航空学报》1994年第6期731-734,共4页Acta Aeronautica et Astronautica Sinica

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。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.

关 键 词：蜂窝结构 玻璃钢纤维 飞机 

分 类 号：V262.415[航空宇航科学与技术—航空宇航制造工程]