The structural integrity of thermoplastic composite parts varies significan
tly with the local polymer morphology, fibre distribution, and fibre orient
ation. Reductions of 30% in the ultimate stress and impact properties of kn
it lines in composite filled parts are common, with much greater losses bei
ng reported for many material systems.(1-3) A method is presented for incre
asing the knit line strength to or beyond the nominal strength of the part
without requiring additional investment in tooling or processing. In additi
on, the fundamental concept of this technique should lead to additional str
ategies for dynamically controlling the polymer flow and fibre orientation
to deliver optimum part properties for composite material systems. PRCPA/14
17 (C) 1998 The Institute of Materials.