Plasma surface treatment of aerospace materials for enhanced adhesive bonding

被引:55
作者
Leahy, W
Barron, V [1 ]
Buggy, M
Young, T
Mas, A
Schue, F
McCabe, T
Bridge, M
机构
[1] Univ Dublin Trinity Coll, Dept Phys, Dublin 2, Ireland
[2] Univ Limerick, Mat & Surface Sci Inst, Limerick, Ireland
[3] Univ Montpellier 2, Lab Chim Macromol, F-34095 Montpellier 5, France
[4] Univ Dublin Trinity Coll, Dept Chem, Dublin 2, Ireland
关键词
plasma treatment; adhesive bonding; aerospace materials; titanium; composites;
D O I
10.1080/00218460108030739
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
The increased use of polyphenylene sulphide (PPS) and polyetheretherketone based composites for aircraft structures has highlighted the need for reliable methods of bonding these materials to metallic components such as titanium. Both composite and titanium adhesive bonds exhibit poor long-term durability when exposed to hot/wet conditions, aerospace fluids and solvents. As a result, surface treatments are employed to enhance surface energy, surface roughness and alter surface chemistry to provide better long-term durability. In this initial study the adhesive bonding of glass fibre reinforced GFR-PPS and commercially pure titanium was investigated. Prior to bonding, both materials were plasma treated using argon and oxygen gases in a RF discharge. Surface characterisation was carried out to optimise these treatments. Surface energy and wettability were examined using contact angle analysis, surface roughness was examined using scanning electron microscopy and atomic force microscopy, while X-ray photoelectron spectroscopy (XPS) was employed to study the surface chemistry. Bond strengths were determined using lap shear tests. Initial results reveal that these optimum plasma treatments produce a significant increase in bond strength.
引用
收藏
页码:215 / 249
页数:35
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