Finite Element Analysis on the Effect of Activation Time on Cervical Spine Biomechanical Response During Pilot Ejection.

Abstract

This study uses finite element analysis (FEA) to investigate different muscle activation times on the cervical spine biomechanical responses in pilot ejection. A validated C0-T1 cervical spine model, incorporating vertebrae, intervertebral discs, ligaments, and 13 major active muscles, was subjected to simulated ejection conditions of 10G vertical acceleration over 150 ms. Activation times ranging from 26 to 92 ms were analyzed to evaluate their impact on vertebral rotation, disc stress, and injury risk. Results demonstrated that shorter activation times (26-46 ms) reduced excessive flexion at C3-C4 and C4-C5; these earlier muscle engagements enhance spinal stability. Conversely, longer delays (76-92 ms) increased rotational angles at C5-C7, exacerbating hyperflexion-related injury risks. An optimal activation time of approximately 46 ms minimized flexion without inducing compensatory hyperextension, balancing load distribution across cervical segments. These findings emphasize the critical role of neuromuscular response timing in mitigating cervical spine injuries during high-G ejection. The study provides insights for optimizing pilot safety through tailored muscle activation strategies, sophisticated artificial intelligence (AI) protective equipment design, and training protocols.