TiB2, pyrolytic carbon (C-pyr) and C-pyr + TiB2 double layer coatings have
been envisaged as potential protective coatings to prevent the deleterious
interface reactions between the carbon fibre and the aluminium matrix durin
g composite manufacturing. These coatings have been obtained by low pressur
e chemical vapour deposition on T800H carbon fibre yarns. In spite of a 20%
increase in the coated monofilaments tensile strength observed for very th
in C-pyr coatings, a strength decrease as a function of the coating thickne
ss is recorded for single C-pyr or TiB2 layers. For the TiB2 coatings, this
decrease fits well with Ochiai's model which simulates the notch effect in
duced by a cracked brittle layer. Concerning the C-pyr coatings, a lower da
maging effect is observed as compared to TiB2, it may be explained by the d
ifference between the Young's moduli of both layers. Although the initial f
ibre properties are not perfectly maintained in the case of the double laye
r, the crack deviation role of the C-pyr coating succeeds in preserving the
coated fibres from the TiB2 notch effect, thus leading to a noticeable str
ength increase. (C) 1998 Kluwer Academic Publishers.