A cabin lining element for an aircraft cabin which is arranged in the interior of an aircraft fuselage structure, having a fuselage structure side and a cabin side. The cabin lining element comprises an electrically contactable heating lacquer layer at least in regions on its fuselage structure side. A rib is provided for an aircraft fuselage structure, having at least one foot portion on the outer skin facing side and a cabin facing side head portion. The rib comprises an electrically contactable heating lacquer layer at least in regions on a side of the head portion facing the cabin. As a result of the heating lacquer layer, it is possible to omit insulation which otherwise surrounds the rib heads and, as a consequence, to enlarge the width of the cabin.
CABIN LINING ELEMENT FOR AN AIRCRAFT CABIN AND RIB FOR AN AIRCRAFT FUSELAGE STRUCTURE
08.04.2021
Patent
Elektronische Ressource
Englisch
CABIN LINING ELEMENT FOR AN AIRCRAFT CABIN AND RIB FOR AN AIRCRAFT FUSELAGE STRUCTURE
Europäisches Patentamt | 2025
|Cabin lining element for an aircraft cabin and rib for an aircraft fuselage structure
Europäisches Patentamt | 2024
|Aircraft cabin air distribution system, aircraft and method of feeding air into cabin of fuselage
Europäisches Patentamt | 2025
|Europäisches Patentamt | 2018
|