In summary, the present application relates to an aircraft interior paneling (10) comprising: —a planar replaceable surface element (40); —a structural element (20); —at least one connection element (30); wherein the replaceable surface element (40) is detachably fastened to the structural element (20) by means of the at least one connection element (30), and wherein the replaceable surface element (40) comprises: —a support element (42), wherein, in the thickness direction of the support element (42), the support element (42) comprises a plurality of successive layers which comprise woven fabrics; —a decorative element (50) which is attached to a decorative connection surface (52) of the support element (42), wherein the support element (42) is dimensionally stable; and a replaceable surface element (40) for an aircraft interior paneling (10); the use of a replaceable surface element (40) for an aircraft interior paneling (10); a method for producing a replaceable surface element (40) for an aircraft interior paneling (10); and a method for updating an existing aircraft interior paneling (100).
FLUGZEUGINTERIEURVERKLEIDUNG, OBERFLÄCHENWECHSELELEMENT FÜR EINE FLUGZEUGINTERIEURVERKLEIDUNG, VERWENDUNG, VERFAHREN ZUR HERSTELLUNG UND VERFAHREN ZUM ÜBERARBEITEN
AIRCRAFT INTERIOR CLADDING, SURFACE CHANGE MEMBER FOR AIRCRAFT INTERIOR CLADDING, USE, METHOD OF PRODUCTION AND METHOD OF REVISION
REVÊTEMENT INTÉRIEUR D'AVION, ÉLÉMENT DE CHANGEMENT DE SURFACE POUR UN REVÊTEMENT INTÉRIEUR D'AVION, UTILISATION, PROCÉDÉ DE FABRICATION ET PROCÉDÉ DE RÉVISION
2021-09-15
Patent
Electronic Resource
German
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