This kind of panelling, of composite material, was the first to be produced by McLore in 1997. Key coefficients were considered, such as the specific weight of each element, collision-resistance (breaking load), factors of expansion, and the costs of the materials and of autoclave processing.
By combining aluminium honeycomb (6-mm honeycomb cell) and carbon fibre, we thus self-produce composite carbon fibre panels with unrivalled resistance and lightness specifications (weight is 60% less than the same flight cases when manufactured in aluminium or multilayer wood). Thanks to this solution type, this flight case is suitable for air transport, with a reduction of the “tare”, thus cutting transport costs.
Recommended for large flight cases.