Adhesive bonding of composite aircraft structures:Challenges and recent developments

作     者：PANTELAKIS Sp. TSERPES K.I. 

作者机构：Laboratory of Technology & Strength of Materials Department of Mechanical Engineering & Aeronautics University of Patras Patras 26500 Greece 

出 版 物：《Science China(Physics,Mechanics & Astronomy)》 (中国科学：物理学、力学、天文学（英文版）)

年 卷 期：2014年第57卷第1期

页      码：2-11页

摘      要：In this review paper,the challenges and some recent developments of adhesive bonding technology in composite aircraft structures are *** durability of bonded joints is defined and presented for parameters that may influence bonding *** is also,a numerical design approach for composite joining profiles used to realize adhesive *** is shown that environmental ageing and pre-bond contamination of bonding surfaces may degrade significantly fracture toughness of bonded ***,it is obvious that additional research is needed in order to design joining profiles that will enable load transfer through shearing of the *** findings,together with the limited capabilities of existing non-destructive testing techniques,can partially explain the confined use of adhesive bonding in primary composite aircraft structural parts.

主 题 词：adhesive bonding fracture toughness finite element analysis 

学科分类：08[工学] 082503[082503] 0825[工学-环境科学与工程类] 

核心收录：

D　O　I：10.1007/s11433-013-5274-3

馆 藏 号：203158061...