In order to simplify a system integration in a fuselage of an aircraft, the disclosure herein provides a production method for producing a load-bearing fuselage panel for a fuselage section of an aircraft fuselage in an area of an aircraft cabin, including manufacturing the fuselage panel to have a sandwich construction with an inner panel and an outer skin as shells and a filling panel embedded between the shells as a core, while configuring the outer skin as a part of a fuselage structure and the outer delimitation of the aircraft fuselage, configuring the inner panel for an interior space delimitation of the cabin, and integrating functional elements of the fuselage structure and the cabin and/or the aircraft into the filling panel. Preferably, the shells and the filling panel are connected to each other by a joining process while producing covalent bonds.
PRODUCTION METHOD FOR PRODUCING A LOAD-BEARING FUSELAGE PANEL AND FUSELAGE PANEL PRODUCIBLE THEREWITH
2016-12-22
Patent
Electronic Resource
English
PRODUCTION METHOD FOR PRODUCING A SUPPORTING FUSELAGE PANEL AND FUSELAGE PANEL PRODUCIBLE THEREWITH
European Patent Office | 2015
|Aircraft fuselage assembling jig and method of handling aircraft fuselage panel
European Patent Office | 2022
|Assembly method for assembling aircraft fuselage panel, fuselage part and aircraft
European Patent Office | 2024
|AIRCRAFT FUSELAGE ASSEMBLY JIG AND METHOD FOR HANDLING AIRCRAFT FUSELAGE PANEL
European Patent Office | 2017
|Full-scale fuselage panel tests
TIBKAT | 1998
|