The experience gained in the last decades on the development of crashworthiness helicopter structures indicates that occupants’ protection can be achieved integrating different energy absorbing systems in landing gears, subfloor and seats. However, the mutual interactions between these different subsystems must be considered to achieve higher overall performances in case of crash events. This work proposes a numerical approach for the evaluation of the overall undercarriage performance, basing on an hybrid multi-body and finite element approach. A hybrid scheme of the subfloor lay-out is integrated with a multibody model of a crashworthy seat and an anthropomorphic dummy model. The modelling technique has been used to investigate and optim...