Door surrounding structure of an aircraft fuselage with integrated SHM network
Door surrounding structure of an aircraft fuselage with integrated SHM network
Integrated structural health monitoring (SHM) with Lamb waves is a promising technique for continuously checking fibre composite structures for damage during operation. Reliable detection and localisation of damage poses a particular challenge, especially in complex aerospace structures. For this reason, a door surrounding structure with an integrated SHM network is being developed and manufactured in order to verify the capabilities of an SHM system in real, complex aviation structures.
