Dimensional stability of complex shapes manufactured by the VARTM process

摘要

The vacuum assisted resin transfer molding (VARTM)process is a cost effective, innovative method that is being considered for manufacture of large aircraft-quality components where high mechanical properties and dimensional tolerance are essential. In the present work, carbon fiber SAERTEX fabric/SI-ZG-5A epoxy resin C-shaped laminates were manufactured by VARTM using different cure cycles followed by the same post-cure cycle. The final part thickness was uniform except at the corner were thinning was observed. The cure cycle selected is shown to significantly affect the part spring-in and a long cycle at 66°C followed by a 178°C post-cure produced apart with negligible spring-in.