螺栓连接
复合数
结构工程
材料科学
复合材料
有限元法
工程类
出处
期刊:Journal of Aircraft
[American Institute of Aeronautics and Astronautics]
日期:1985-11-01
卷期号:22 (11): 993-1000
被引量:157
摘要
Various aspects of the combination of adhesive bonding and mechanical fastening for fibrous composite structures are considered. The factors accounted for in the theories are explained and the source of the complete derivations is given. Analyses of undamaged structures show that, because the adhesive bond load path is so much stiffer than the load path through bolts or rivets, the combination is no stronger than a well-designed bonded joint alone. However, the combination of bonding and bolting is shown to be particularly useful for repair and to prevent damage from spreading. The issues raised are illustrated by specific analyses of large stepped-lap composite to metal joints.
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