Curtain support assembly, in a framework design, in a cabin of a vehicle

1. A curtain support assembly to receive a curtain for separating at least two regions in a cabin of an aircraft, comprising:

a pair of lateral covering parts for covering a space between the curtain and a ceiling in the cabin and

at least one load-bearing frame structure for carrying the curtain, the at least one load-bearing frame structure comprising an elongate profile component and a plurality of profile components extending from the elongate profile component at a predetermined spacing from one another, the elongate profile component comprising a first side and a second side opposite the first side, the second side facing the curtain, some of the plurality of profile components extending from the first side of the elongate profile component, the remainder of the plurality of profile components extending from the second side of the elongate profile component,

wherein at least one of the profile components extending from the first side of the elongate profile component extends upwardly and away from the elongate profile component; wherein at least one of the plurality of profile components extending from the second side of the elongate profile component extends downwardly and away from the elongate profile component; wherein the elongate profile component and the plurality of profile components each compromise an identical profile; wherein the elongate profile component and the plurality of profile components each compromise a square cross section comprising an undercut recess along each of the four sides of the cross section

wherein the elongate profile component is configured as a curtain rail for receiving the curtain, and

wherein the pair of lateral covering parts are arranged on the at least one load-bearing frame structure on opposed sides of the at least one load-bearing frame structure.

2. The assembly of claim 1 ,

wherein the at least one load-bearing frame structure is adapted for bearing the curtain load completely.

3. The assembly of claim 1 ,

wherein the profile components are made from an extruded aluminium alloy, or a steel alloy.

4. The assembly of claim 1 ,

wherein the profile components are made from a fibre-reinforced plastic.

5. An aircraft comprising a cabin and at least one assembly to receive a curtain for separating at least two regions in the cabin of the aircraft, wherein the at least one assembly comprises:

a pair of lateral covering parts for covering a space between the curtain and a ceiling in the cabin; and

at least one load-bearing frame structure comprising an elongate profile component and a plurality of profile components extending from the elongate profile component at a predetermined spacing from one another, the elongate profile component comprising a first side and a second side opposite the first side, the second side is proximal to the curtain, some of the plurality of profile components extending from the first side of the elongate profile component, the remainder of the plurality of profile components extending from the second side of the elongate profile component the plurality of profile components,

wherein at least one of the profile components extending from the first side of the elongate profile component extends upwardly and away from the elongate profile component; wherein at least one of the plurality of profile components extending from the second side of the elongate profile component extends downwardly and away from the elongate profile component; wherein the elongate profile component and the plurality of profile components each comprise an identical profile; wherein the elongate profile component and the plurality of profile components each comprise a square cross section comprising an undercut recess along each of the four sides of the cross section

wherein the elongate profile component is configured as a curtain rail for mounting the curtain; and

wherein the pair of lateral covering parts are arranged on the at least one load-bearing frame structure on opposed sides of the at least one load-bearing frame structure.

6. The assembly of claim 1 ,

wherein the at least one upwardly extending profile component extends toward the ceiling when the assembly is mounted.

7. The assembly of claim 1 , further comprising, among the plurality of profile components, a second profile component having a longitudinal axis;

wherein said second profile component extends along said longitudinal axis away from the elongate profile component.

8. The assembly of claim 1 , wherein the lateral covering parts extend upwardly from the at least one load-bearing frame structure towards the ceiling, when the curtain support assembly is mounted in the cabin.

9. The assembly of claim 8 , wherein the pair of lateral covering parts each has an arcuate edge to conform with the ceiling when the assembly is mounted in the cabin.

10. The assembly of claim 8 ,

wherein the at least one upwardly extending profile components extends toward the ceiling when the assembly is mounted in the cabin.

11. The assembly of claim 5 , wherein the pair of the lateral covering parts extend upwardly from the at least one load-bearing frame structure towards the ceiling, when the curtain support assembly is mounted in the cabin.

12. The assembly of claim 11 , wherein the

at least one lateral covering part has an arcuate edge to conform with the cabin when the assembly is mounted in the cabin.