A cabin structural segment is provided for an aircraft that includes, but is not limited to a fuselage structure and a floor structure. The fuselage structure defines an interior and separating it from an environment. The fuselage structure includes, but is not limited to an opening for a door. It i
A cabin structural segment is provided for an aircraft that includes, but is not limited to a fuselage structure and a floor structure. The fuselage structure defines an interior and separating it from an environment. The fuselage structure includes, but is not limited to an opening for a door. It is possible to provide via the opening a connection between the interior and the environment. The cabin structural segment is designed to be self-supporting. The cabin structural segment is fastenable exclusively to the floor structure. The cabin structural segment is constructed in such a way that the one cabin structural segment frames the opening.
대표청구항▼
1. An aircraft comprising: a fuselage structure that at least partially defines an interior and separates the interior from an environment, the fuselage structure comprising a door opening and a connection between the interior and the environment that is providable via the door opening;a floor struc
1. An aircraft comprising: a fuselage structure that at least partially defines an interior and separates the interior from an environment, the fuselage structure comprising a door opening and a connection between the interior and the environment that is providable via the door opening;a floor structure,the cabin structural segment that is self-supporting, the cabin structural segment including two frame longitudinal profiles and a frame transverse profile that cooperate to frame mutually opposing longitudinal sides of the door opening and an upper side, opposing the floor structure, of the door opening,wherein the two frame longitudinal profiles of the cabin structural segment are fastened exclusively to the floor structure of the aircraft. 2. The cabin structural segment according to claim 1, wherein the cabin structural segment is configured to frame two mutually opposing door openings. 3. The cabin structural segment according to claim 1, further comprising at least one transition segment in an aircraft longitudinal direction, the transition segment rigidly connected to the cabin structural segment. 4. The cabin structural segment according to claim 1, wherein the mutually opposing longitudinal sides of the door opening extend substantially transverse to the floor structure. 5. The cabin structural segment according to claim 4, further comprising a frame part that frames the upper side, the frame part extending in a screen-like manner towards the fuselage structure. 6. The cabin structural segment according to claim 1, further comprising: an arch segment; anda cover segment rigidly interconnected to the arch segment,wherein the arch segment extending substantially along an inner face of the fuselage structure from the floor structure to the cover segment, andwherein the cover segment is spaced apart from the floor structure. 7. The cabin structural segment according to claim 6, wherein the cover segment comprises an outer face, the outer face being adjacent to the fuselage structure, and configured for an electric unit for supplying a passenger cabin with power to be fastened to the outer face. 8. The cabin structural segment according to claim 1, wherein the cabin structural segment is dividable substantially centrally in an aircraft longitudinal direction to form a first cabin structural segment and a second cabin structural segment. 9. The cabin structural segment according to claim 8, wherein the first cabin structural segment and the second cabin structural segment are substantially identical. 10. An aircraft comprising: a fuselage structure that at least partially defines an interior and separates the interior from an environment, the fuselage structure comprising a door opening and a connection between the interior and the environment that is providable via the door opening;a floor structure;a cabin structural unit that is configured to attach to a cabin built-in element and formed to self-support; anda cabin structural segment connectable to the cabin structural unit, the cabin structural segment including two frame longitudinal profiles and a frame transverse profile that define an opening such that the cabin structural segment frames mutually opposing longitudinal sides of the door opening and an upper side, opposing the floor structure, of the door opening when the two frame longitudinal profiles of the cabin structural segment are fastened to the floor structure of the aircraft,wherein the cabin structural unit is fastenable only to the floor structure of the aircraft, andwherein the cabin structural unit is supportable on the fuselage structure in a moment-free manner. 11. A method for installing a cabin structural segment for an aircraft comprising a fuselage structure and a floor structure, the fuselage structure defining an interior and separating it from an environment, the fuselage structure comprising a door opening, a connection between the interior and the environment is possible via the door opening; the method comprising: pre-assembling the cabin structural segment in an environment of the fuselage structure the cabin structural segment including two frame longitudinal profiles and a frame transverse profile;guiding the pre-assembled cabin structural segment through the door opening of the fuselage structure into the interior;positioning the pre-assembled cabin structural segment at a predetermined location in the interior such that the door opening is framed by the cabin structural segment;fastening the two frame longitudinal profiles of the cabin structural segment exclusively to the floor structure of the aircraft, andforming the cabin structural segment to be self-supporting. 12. The method according to claim 11, further comprising dividing the pre-assembled cabin structural segment into a first cabin structural subsegment and a second cabin structural subsegment in the environment. 13. The method according to claim 12, assembling the first cabin structural subsegment and the second cabin structural subsegment to form the cabin structural segment. 14. The method according to claim 12, wherein the guiding the pre-assembled cabin structural segment through the door opening of the fuselage structure into the interior comprises guiding the first cabin structural subsegment and the second cabin structural subsegment through the door opening of the fuselage structure into the interior. 15. The method according to claim 14, wherein the positioning the pre-assembled cabin structural segment at the predetermined location in the interior such that the door opening is framed by the cabin structural segment comprises: positioning the first cabin structural subsegment and the second cabin structural subsegment at a predetermined location in the interior such that the door opening is framed by the first cabin structural subsegment. 16. The method according to claim 14, wherein the positioning the pre-assembled cabin structural segment at the predetermined location in the interior such that the door opening is framed by the cabin structural segment comprises: positioning the first cabin structural subsegment and the second cabin structural subsegment at a predetermined location in the interior such that the door opening is framed by the second cabin structural element.
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