STRUCTURAL ELEMENT OF AN AIRCRAFT FUSELAGE

摘要

The structural element of an aircraft fuselage, with stringers (20, 30; 40; 50; 60) running in the longitudinal direction of the aircraft fuselage and ribs (80) running transversely to the stringers (20, 30; 40; 50; 60) in the circumferential direction of the fuselage. According to the invention, at least one of the stringers (30; 40; 50; 60) running in the longitudinal direction of the aircraft fuselage is designed as a fastening rail for elements (100, 110) to be installed in the aircraft fuselage.