Structuring construction for an aircraft fuselage
AssigneeAirbus Deutschland GmbH
InventorHendrik Verweyen
Life of this patent
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Abstract
A structuring construction (10) for an aircraft fuselage comprises an outer skin (12) as well as a plurality of formers (14) extending at a spacing side by side crosswise to the longitudinal direction of the fuselage. According to the invention, at least a partial number of the formers comprise a main former portion (18) which is channel-like in cross section and the channel edges of which are adjacent to the outer skin (12). In a preferred development the channel space of the main former portion (18) serves to accommodate at least one supply air line which may be formed, for example, by a separate pipe line (28).
Claims15
Structuring construction for an aircraft fuselage, with comprising:
- an outer skin;
- and
- 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 channel-like in cross section and the channel edges of which are adjacent to the outer skin, wherein at least one air line serving to convey supply air is disposed or formed in the space between the main former portion and the outer skin at least in the case of a partial number of the formers constructed with a channel-like main former portion.
Dependencies are inferred from the claim text.