PRODUCTION METHOD FOR PRODUCING A LOAD-BEARING FUSELAGE PANEL AND FUSELAGE PANEL PRODUCIBLE THEREWITH

摘要

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.

主权项

1. 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, comprising:
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.