Physical modifications for improved peel strength in a high-temperature epoxy adhesive

被引:9
作者
Dixon, DG
Unger, W
Naylor, M
Dublineau, P
Figgures, CC
机构
[1] British Aerosp Operat Ltd, Sowerby Res Ctr, Bristol BS12 7QW, Avon, England
[2] Daimler Benz Aerosp, D-81663 Munchen, Germany
[3] British Aerosp Airbus Ltd, Bristol, Avon, England
[4] Aerospatiale, Ctr Commun Rech Louis Bleriot, F-92512 Suresnes, France
关键词
epoxides; aluminium and alloys; destructive testing by peel; fracture; physical modifications;
D O I
10.1016/S0143-7496(97)00058-4
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
The thermal performance of high-temperature thermoset adhesives is invariably gained at the expense of mechanical properties, particularly peel strength. A microscopic study of failure propagation in adhesive joints revealed that fibres within the bondline can affect the fracture path during peel failure in a commercially available modified epoxy adhesive, developed for high-temperature use. This adhesive has been further modified by the incorporation of polymer fibres and the resultant adhesive joints have shown significant increases in peel strength combined with both increases and decreases in lap-shear strength, depending on the fibre orientation. These effects were measured from - 55 degrees C to + 180 degrees C. Improvements were also seen when larger joints, more typical of aerospace structures, were tested. (C) 1998 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:125 / 130
页数:6
相关论文
共 16 条
[1]  
*BAC, 5555 BAC
[2]  
BAUER M, 1992, P EUR 92 KARLSR 20 2
[3]  
DAVIES RGH, 1996, P ADH 96 EUR 96 I MA, P733
[4]  
DIXON DA, UNPUB
[5]   The effect of PEEK fibres and powder on joints made with a high temperature adhesive [J].
Dixon, DG ;
Harris, SJ ;
Dempster, M ;
Nicholls, P .
JOURNAL OF ADHESION, 1998, 65 (1-4) :131-162
[6]   THE INTERLAMINAR FAILURE BEHAVIOR OF CARBON-FIBER POLYETHERETHERKETONE COMPOSITES [J].
DYSON, IN ;
KINLOCH, AJ ;
OKADA, A .
COMPOSITES, 1994, 25 (03) :189-196
[7]  
Hamerton I., 2012, Chemistry and Technology of Cyanate Ester Resins
[8]   THE EFFECTS OF GEOMETRY, RATE AND TEMPERATURE ON THE MODE-I, MODE-II AND MIXED-MODE I/II INTERLAMINAR FRACTURE OF CARBON-FIBRE/POLY(ETHER-ETHER KETONE) COMPOSITES [J].
HASHEMI, S ;
KINLOCH, AJ ;
WILLIAMS, JG .
JOURNAL OF COMPOSITE MATERIALS, 1990, 24 (09) :918-956
[9]   THE FRACTURE-RESISTANCE OF A TOUGHENED EPOXY ADHESIVE [J].
KINLOCH, AJ ;
SHAW, SJ .
JOURNAL OF ADHESION, 1981, 12 (01) :59-77
[10]  
KUHBANDER RJ, 1988, P 33 INT SAMPE S 7 1, P1582