Hull structure component for vehicles, particularly for aircraft and/or spacecraft

摘要

The fuselage structural component has ribs (30) that are arranged on inner side (11) of inner structure (10). The outer stringers (41) are arranged on outer side (12) of inner structure at same angle with respect to fuselage longitudinal axis (15). The inner stringers (42) are arranged on the inner side of the inner structure at same angle with respect to fuselage longitudinal axis. The included angles between stringers and fuselage longitudinal axis are same and the inner and outer stringers are symmetrically arranged in opposite to each other.