| 摘要 |
The invention relates to a fuselage (2) for an aircraft, which fuselage is produced of a fiber-reinforced composite material and comprises a skin (4) and a plurality of peripheral reinforcements (12) and only a small number of longitudinal reinforcements (10), the skin (4) having a plurality of locally reinforced sections (14), and to a skin section (6) for forming such a fuselage. |
