Such a fuselage includes cross-members adapted for the formation of a floor, at least one of said cross-members including an upper part, a lower part, linkage for the lower part to the upper part, and at least one opening for the passage of systems which is delimited between the lower part and the upper part. The upper part of the cross-member is fastened to the fuselage and is dimensioned so as to bear the stresses to which said cross-member may be subjected when the aircraft remains on the ground. The lower part is fastened to the upper part so as to reinforce it such that when assembled, the upper part and the lower part are adapted to bear the stresses to which the cross-member may be subjected in flight conditions of the aircraft.
Aircraft fuselage and method for constructing a floor in such a fuselage
2018-06-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft fuselage section, aircraft fuselage and aircraft
European Patent Office | 2023
|European Patent Office | 2015
|Lintel structure for aircraft fuselage and fuselage comprising such a lintel
European Patent Office | 2022
|LINTEL STRUCTURE FOR AIRCRAFT FUSELAGE AND FUSELAGE COMPRISING SUCH A LINTEL
European Patent Office | 2018
|Method for producing an aircraft fuselage and aircraft fuselage
European Patent Office | 2016
|