In the current effort towards sustainability, the aviation industry faces challenges in repurposing carbon fiber reinforced plastic (CFRP) components effectively. Traditional "downcycling" methods fail to maintain CFRP integrity, as they involve cutting load-bearing fibers and re-embedding them with new polymers, which leads to fragmentation and loss of properties.
Innovative solutions like non-destructive disassembly or dismanteling offer precise separation without compromising fiber integrity. This method allows for the direct reuse of materials in similar or new applications and highlights the importance of advanced recycling technologies for fiber-reinforced plastics.
Finite element method (FEM) analysis shows the basic separation mechanism functions without damaging the base material in simulated shell structures. Safety margins are within acceptable ranges, and additional damping forces enhance process safety. Thinner wedges are recommended as they generate lower loads, exhibit less dependency on plate stiffness, and require shorter crack lengths. Fracture risk is influenced by specific parameters.
Critical parameters must be determined during structure development, as they cannot be varied in existing components without design considerations for recyclability. However, green inputs can be directly modified to improve the process. Targeted force applications, such as pressing at the crack tip and relieving force at the wedge contact point, reduce structural load. A cable force mechanism, supported by a lateral roller, effectively relieves wedge contact force.
In summary, the wedge separation process is suitable for non-destructive disassembly of stiffeners, representing a promising approach for developing practical test stands.