Aircraft fuselage structure
An aircraft fuselage structure is described for a flying-wing aircraft, having a central area of slight curvature and side areas of greater curvature, which forms a pressure body and has an outer skin and structure reinforcements which support the outer skin. According to the invention, the structure reinforcements contain three-dimensional truss bending supports which extend over the area of light curvature and comprise first straps, which run close to the outer skin 9 , and second straps, which run at a distance from the outer skin, and are connected to one another by coupling elements.
1. 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.
2. The aircraft fuselage structure according to claim 1 , wherein the base of the truss bending supports is at a distance from the outer skin.
3. The aircraft fuselage structure according to claim 1 , wherein the coupling elements which connect the straps of the truss bending supports are formed by segments of plates.
4. The aircraft fuselage structure according to claim 1 , wherein the coupling elements which connect the straps of the truss bending supports are formed by rods.
5. The aircraft fuselage structure according to claim 1 , wherein the first truss bending supports are arranged running in the aircraft lateral direction.
6. The aircraft fuselage structure according to claim 1 , wherein the first truss bending supports are arranged running in the aircraft longitudinal direction.
7. The aircraft fuselage structure according to claim 1 , wherein the truss bending supports are produced from metal.
8. The aircraft fuselage structure according to claim 1 , wherein the truss bending supports are produced from fibre-reinforced plastic.
9. The aircraft fuselage structure according to claim 1 , wherein the first truss bending supports are connected to one another and supported by the second truss bending supports.
10. The aircraft fuselage structure according to claim 9 , wherein the first truss bending supports are arranged running in the aircraft lateral direction and the second truss bending supports are arranged running in the aircraft longitudinal direction.
11. The aircraft fuselage structure according to claim 10 , wherein the second truss bending supports are arranged to run in the aircraft longitudinal direction in the area of slight and greater curvatures, and
wherein the first truss bending supports are arranged to run in the aircraft lateral direction covering the central area of the aircraft fuselage.