The adhesive bonding of three unidirectional carbon.fibre composites -
with thermoplastic polyetheretherketone, thermoplastic polyphenylene
sulfide and, for comparative purposes, thermosetting epoxy matrices -
has been examined. The adhesives were a room-temperature-curing epoxy
paste and a hot-curing epoxy film; composite substrates were pretreate
d by light abrasion and solvent cleaning, followed by either an oxygen
-plasma or corona treatment. It is shown that good adhesive bonding of
the thermoplastic composites can be achieved if a plasma treatment is
used prior to bonding. For the oxygen-plasma and corona treatments em
ployed, the adhesive fracture energy, G(c), for the thermoplastic comp
osite joints increases steadily with the intensity of the treatment un
til a plateau value of G(c) is reached. On the other hand, the thermos
etting-based composite needs only light abrasion and solvent cleaning
to give high values of G(c). Without the oxygen-plasma or corona treat
ment, the thermoplastic composite joints fail at the adhesive/composit
e interface at a very low applied load. The oxygen-plasma and corona t
reatments lead to an increase in the surface concentration of polar, o
xygen-containing groups, resulting in both increased wetting by the ep
oxy adhesive on the substrate and greater intrinsic adhesion across th
e adhesive/composite interface. The enhancement in intrinsic adhesion
is reflected in the locus of failure of the joints moving away from th
e adhesive/composite interface, and in far higher values of G(c).