Patent ID: 8205824

Claim:
An aircraft fuselage structure for a flying-wing aircraft, comprising: a central area of slight curvature and side areas of greater curvature, wherein the aircraft fuselage structure forms a pressure body having an outer skin supported by integrated structure reinforcements, wherein the structure reinforcements comprising three-dimensional first and second truss bending supports comprising a plurality of polyhedron units forming an integrated structure extending over the area of slight curvature, wherein the plurality of first truss bending supports being provided running in a first direction and the plurality of second truss bending supports being provided running in a second direction, transversely with respect to the former, wherein the truss bending supports comprise polyhedrons with a base and a tip, and wherein the rectangular base of the truss bending supports comprises first straps running close to the outer skin, and the tip of the truss bending support comprises second straps running at a distance from the outer skin, and the first and second straps are connected to one another by coupling elements.