Nondestructive Assessment of Aerospace Components by Means of Pulsed Thermography

Infrared (IR) thermography is a nondestructive, non-contact and non-intrusive technique that allows the fast inspection of large and complex structures with limited accessibility. Pulsed thermography is particularly interesting for the inspection of aerospace materials such as composites given that, after submitting the specimen surface to a thermal front, the most common types of subsurface discontinuities (e.g. porosity, de laminations, dis bonds, fiber breakage and inclusions) can be detected with an IR camera as regions showing abnormal temperature patterns. We present first the case of an aircraft door with water ingress and surface repairs on its honey comb structure. We also highlight the advantages and limitations of thermography for the inspection of aircraft composite parts, such as edge flaps, rotor blades and speed breaks. Finally, we expose some results from a Kevlar® non-planar specimen with Teflon® inclusions at different depths and locations.