INTERNAL CLADDING PART FOR CLADDING A FUSELAGE STRUCTURE OF AN AIRCRAFT

摘要

An internal cladding part for cladding a fuselage structure of an aircraftcomprises a first cover layer that extends in a planar manner, a secondcover layer that extends in a planar manner, a core layer which is disposedbetween the first and the second cover layer and is connected to the firstand the second cover layer and defines a receptacle cavity, and aninsulation structure having a porous insulation core and an evacuated filmsheath (51) that encases the insulation core (50) in a gas-tight manner,wherein the insulation structure is disposed in the receptacle cavitybetween the first and the second cover layer.