Structuring construction for an aircraft fuselage
First Claim
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1. Structuring construction for an aircraft fuselage of an aircraft, 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 formed as a channel in cross section, channel edges of which are adjacent to the outer skin,wherein at least one air line forming a riser of an air conditioning system of the aircraft and serving to convey supply air to an aircraft cabin of the aircraft is disposed or formed in a space between the main former portion and the outer skin at least in the formers constructed as the main former portions.
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Abstract
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.
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Citations
15 Claims
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1. Structuring construction for an aircraft fuselage of an aircraft, comprising:
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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 formed as a channel in cross section, channel edges of which are adjacent to the outer skin, wherein at least one air line forming a riser of an air conditioning system of the aircraft and serving to convey supply air to an aircraft cabin of the aircraft is disposed or formed in a space between the main former portion and the outer skin at least in the formers constructed as the main former portions. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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Specification