This project aims to design and evaluate the feasibility of a fiber optic inspection probe for real-time assessment of jet engine fan blades during post flight spool-down periods. Traditional inspection methods require manual visual checks post-shutdown, which are labor-intensive and prone to inconsistency and error. The proposed solution must deliver high-resolution imaging capable of detecting and characterizing Foreign Object Damage (FOD) including nicks, scratches, and dents. While also remaining within a strict dimensional envelope of 4 × 3 × 2 inches. This remote observation solution aims to improve inspection accuracy, reduce inspection times, and minimize reliance on manual visual checks.

Our team collaborated with Electrical and Computer Engineering 4 on this project.