초록

A fuselage segment of an aircraft fuselage is provided with an outer skin and an inner skin that are spaced apart from one another by a core, wherein conduits for system installations are integrated into the core, as well as a method for manufacturing such a fuselage segment.

대표청구항 ▼

1. A fuselage segment of an aircraft fuselage, comprising: an inner skin on a cabin side of the aircraft fuselage; andan outer skin of the aircraft fuselage that covers a core, where conduits for system installations are integrated into the core,wherein at least the core consists of a foam material

1. A fuselage segment of an aircraft fuselage, comprising: an inner skin on a cabin side of the aircraft fuselage; andan outer skin of the aircraft fuselage that covers a core, where conduits for system installations are integrated into the core,wherein at least the core consists of a foam material wherein the material hardness of the foam material increases from a center region of the core to the outer skin and from the center region of the core to the inner skin. 2. The fuselage segment according to claim 1, wherein the inner skin and the outer skin are realized separately of the core. 3. The fuselage segment according to claim 1, wherein the fuselage segment is realized in one piece. 4. The fuselage segment according to claim 1, wherein the core is constructed from a multilayer foam material. 5. The fuselage segment according to claim 1, wherein the conduits are formed as tubular elements. 6. The fuselage segment according to claim 1, wherein a number of the conduits are integrated into the core such that an outer surface of each of the number of conduits engages the core. 7. The fuselage segment according to claim 1, wherein the inner skin forms a sidewall of a cabin. 8. A method for manufacturing a fuselage segment according to claim 1, wherein the conduits are produced in the core during the manufacture of the core. 9. A fuselage segment of an aircraft fuselage, comprising: an inner skin of the aircraft fuselage;an outer skin of the aircraft fuselage; anda core interposed between the inner skin and the outer skin, wherein the core comprises a foam material the material hardness of which increases in a direction extending from a portion proximate the inner skin towards a portion proximate the outer skin, wherein conduits for system installations are integrated within the core.