An internal cladding part for cladding a fuselage structure of an aircraft comprises a first cover layer that extends in a planar manner, a second cover layer that extends in a planar manner, a core layer which is disposed between the first and the second cover layer and is connected to the first and the second cover layer and defines a receptacle cavity, and an insulation structure having a porous insulation core and an evacuated film sheath (51) that encases the insulation core (50) in a gas-tight manner, wherein the insulation structure is disposed in the receptacle cavity between the first and the second cover layer.
INTERNAL CLADDING PART FOR CLADDING A FUSELAGE STRUCTURE OF AN AIRCRAFT
PARTIE DE REVETEMENT INTERNE POUR LE GAINAGE D'UNE STRUCTURE DE FUSELAGE D'UN AERONEF
17.10.2020
Patent
Elektronische Ressource
Englisch
Internal cladding part for cladding fuselage structure of aircraft
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