Patent attributes
An aircraft cabin floor structure which makes it possible to avoid the appearance of blisters in the carpets covering the floor panels in an aircraft cabin is disclosed. The aircraft cabin floor structure comprises a rigid carpet that is impermeable to air having a top face and a bottom face, an adhesive layer having an adhesive top face and an adhesive bottom face, said top face adhering to the bottom face of the carpet, and a floor panel that is impermeable to air having a top face and a bottom face, the bottom face of the adhesive layer adhering to the top face of the floor panel. The bottom face of the carpet comprises grooves and at least one air evacuation channel over its periphery. The adhesive layer comprises a plurality of through holes.
