Patent ID: 8146860
Filing Date: 2012-04-03
Classification: B64C

Abstract:
1. A fuselage section comprising an interior that forms a passenger cabin comprising an interior lining that spans the longitudinal length of the fuselage and which in horizontal projection is geometrically defined by a first exterior skin region and a second exterior skin region, which second exterior skin region faces the first exterior skin region, wherein the two exterior skin regions in longitudinal direction of the passenger cabin comprise a circular-arc-shaped contour of uniform curvature, wherein the interior lining lines at least one of the two facing exterior skin regions, wherein the interior lining in horizontal projection in longitudinal direction of the fuselage comprises a circular arc shape of uniform curvature, and wherein the interior lining is comprised of a plurality of interior lining segments that are designed for using one and the same interior lining segment alternatively for lining the first exterior skin region or the second exterior skin region.