Shell structure of a fuselage

摘要

Shell structure of a fuselage comprising a plurality of ribs (110) arranged in predetermined intervals; an outer skin (120) fastened to each of the plurality of ribs (110); a plurality of fastening means (240) coupled to the outer skin between the ribs (110) and facing inwards into the fuselage; and an interior structural element (220) being mounted to the outer skin (120) in a load transmitting manner using the fastening means (240).