Composites have a widespread use in airframe components and helicopter blades. DVI has investigated accidents involving both of these uses. The failure behavior in composites is complex and can be influenced by the composition of the matrix and fibre, the fibre content, the nature of the interfacial bond, fibre orientation,stacking and sequence, void level,and type of loading.

Possible failure modes include matrix cracking, fibre buckling, pull-out, and breaking, interfacial-bond failure, and delamination. Manufacturing defects could include voids, resin-rich zones, pockets of undispersed crosslinker, misaligned fibres, and regions of poorly wetted fibres.  

DVI's staff has designed and tested large complex composite structures for military applications, and has the experience and depth of knowledge to investigate and determine the cause of composite material failures.

Please contact General Aviation Experts at 630-556-9702 to retain the services of Mr. Meyers or email: smeyers@generalaviationexperts.com