| 摘要 |
A structuring construction for an aircraft fuselage is provided having an outer skin as well as a plurality of formers extending at a spacing side by side crosswise to the longitudinal direction of the fuselage wherein at least a partial number of the formers include a main former portion which is channel-like in cross section and the channel edges of which are adjacent to the outer skin and wherein the channel space of the main former portion serves to accommodate at least one supply air line which may be formed, for example, by a separate pipe line. |
