An internal cladding part for cladding a fuselage structure of an aircraft is disclosed having 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 that encases the insulation core in a gas-tight manner. The insulation structure is disposed in the receptacle cavity between the first and the second cover layer.
INNENVERKLEIDUNGSTEIL ZUR VERKLEIDUNG EINER RUMPFSTRUKTUR EINES LUFTFAHRZEUGS
INTERIOR CLADDING SECTION FOR COVERING A FUSELAGE STRUCTURE OF AN AIRCRAFT
PARTIE DE REVÊTEMENT INTÉRIEUR DESTINÉ AU REVÊTEMENT D'UNE STRUCTURE DE FUSELAGE D'UN AÉRONEF
2021-10-20
Patent
Elektronische Ressource
Deutsch
IPC: | B64C AEROPLANES , Flugzeuge |
INNENVERKLEIDUNGSTEIL ZUR VERKLEIDUNG EINER RUMPFSTRUKTUR EINES LUFTFAHRZEUGS
Europäisches Patentamt | 2020
|Europäisches Patentamt | 2021
|Europäisches Patentamt | 2021
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