초록 ▼

An aircraft component assembly system for the assembly of an interior component, a pipe or an electric line in an aircraft includes at least one arc-shaped frame element, a connection element that extends between a first and a second end of the frame element, and a fastening apparatus for fastening

An aircraft component assembly system for the assembly of an interior component, a pipe or an electric line in an aircraft includes at least one arc-shaped frame element, a connection element that extends between a first and a second end of the frame element, and a fastening apparatus for fastening the interior component, the pipe or the electric line to the frame element or the connection element. The system also includes a first guide device that is provided on the frame element or the connection element and is devised to interact with a second guide device, which is complementary to the first guide device and provided on an aircraft structure, in such a way that the aircraft component assembly system is connectable to the aircraft structure in a manner displaceable relative to the aircraft structure.

대표청구항 ▼

1. An aircraft component assembly system for use in the assembly of at least one of an interior component, a pipe and an electric line in an aircraft, the aircraft including aircraft structure having a fuselage extending in a longitudinal direction, the aircraft component assembly system comprising:

1. An aircraft component assembly system for use in the assembly of at least one of an interior component, a pipe and an electric line in an aircraft, the aircraft including aircraft structure having a fuselage extending in a longitudinal direction, the aircraft component assembly system comprising: at least one arc-shaped frame element, which comprises a plurality of spaced apart struts that are disposed at least in sections substantially parallel to one another and within a vertical plane transverse to the longitudinal direction, the plurality of struts spanning both side walls and a ceiling of an aircraft cabin structure in a fully assembled state,a connection element that extends between a first and a second end of the frame element and is devised, in the assembled state of the aircraft component assembly system in an aircraft, to form an element of a floor of a cabin of the aircraft,a fastening apparatus for fastening at least one of the interior component, the pipe and the electric line to the frame element or to the connection element, anda first guide device that is provided on the frame element or the connection element and is devised to interact with a second guide device, which is complementary to the first guide device and provided on an aircraft structure, in such a way that the aircraft component assembly system is connectable to the aircraft structure in a manner slideable within the fuselage in the longitudinal direction. 2. The aircraft component assembly system according to claim 1, further comprising: a fixing device that is devised to fix the aircraft component assembly system in a desired position on the aircraft structure. 3. The aircraft component assembly system according to claim 2, wherein the fixing device takes the form of a detent mechanism that is devised to interlock the aircraft component assembly system with the aircraft structure when the aircraft component assembly system is situated in the desired position relative to the aircraft structure. 4. The aircraft component assembly system according to claim 3, wherein the detent mechanism includes first and second detent apparatuses, the first detent apparatus being located on the aircraft component assembly system and being integrated with each of a first interface connected to at least one electric line fastened to the aircraft component assembly system and a first connector for pipes fastened to the aircraft component assembly system, the second detent apparatus being located on the aircraft structure and integrated with a second interface and a second connector for pipes, the first and second interfaces and the first and second connectors being automatically coupled with the first and second detent apparatuses. 5. The aircraft component assembly system according to claim 1, wherein on the frame element at least one force introduction apparatus is formed for fitting the frame element on a rib of the aircraft structure, and wherein the first guide device comprises a guide rail, which extends from the connection element and is devised to interact with a receiver of the second guide device that is provided in cross-members of the aircraft structure. 6. The aircraft component assembly system according to claim 1, wherein at least one of the first and the second guide device comprises a device for the acoustic decoupling of the aircraft component assembly system from the aircraft structure. 7. The aircraft component assembly system according to claim 1, wherein on the aircraft component assembly system at least one first interface is provided, which is connected to at least one electric line fastened to the aircraft component assembly system and is electrically connectable to a second interface, which is complementary to the first interface, when the aircraft component assembly system is situated in the desired position relative to the aircraft structure. 8. The aircraft component assembly system according to claim 1, wherein a first connector of a pipe, which is fastened to the aircraft component assembly system or integrated into the aircraft component assembly system, is connectable to a second connector, which is complementary to the first connector, when the aircraft component assembly system is situated in the desired position relative to the aircraft structure. 9. The aircraft component assembly system according to claim 1, wherein at least one strut of the frame element is of a hollow-cylindrical construction. 10. The aircraft component assembly system according to claim 1, further comprising: a further fastening apparatus for fastening an insulation package to at least one of the frame element and the connection element. 11. A method of assembling at least one of an interior component, a pipe and an electric line in an aircraft, comprising: providing an aircraft component assembly system according to claim 1,fastening the at least one of the interior component, the pipe and the electric line to at least one of the frame element or the connection element of the aircraft component assembly system,connecting the first guide device provided on the at least one of the frame element or the connection element to the second guide device, which is complementary to the first guide device and provided on the aircraft structure, anddisplacing the aircraft component assembly system relative to the aircraft structure while the first and second guide devices are connected until the aircraft component assembly system is situated in a desired position relative to the aircraft structure. 12. The method according to claim 11, further comprising: fixing the aircraft component assembly system in the desired position on the aircraft structure with a fixing device. 13. The method according to claim 12, wherein fixing the aircraft component assembly system in the desired position further comprises: connecting a first detent apparatus on the aircraft component assembly system with a second detent apparatus on the aircraft structure;electrically connecting a first interface provided on the aircraft component assembly system and integrated into the first detent apparatus to a second interface integrated with the second detent apparatus as the first and second detent apparatuses are connected; andconnecting a first connector of pipes, which is fastened to the aircraft component assembly system and integrated into the first detent apparatus to a second connector integrated with the second detent apparatus as the first and second detent apparatuses are connected. 14. The method according to claim 11, further comprising: electrically connecting a first interface provided on the aircraft component assembly system to a second interface, which is complementary to the first interface, when the aircraft component assembly system is situated in the desired position relative to the aircraft structure. 15. The method according to claim 11, further comprising: connecting a first connector of the pipe, which is fastened to the aircraft component assembly system or integrated into the aircraft component assembly system, to a second connector, which is complementary to the first connector, when the aircraft component assembly system is situated in the desired position relative to the aircraft structure. 16. The method according to claim 11, further comprising: prior to connecting of the first guide device to the second guide device, fastening an insulation package to at least one of the frame element and the connection element of the aircraft component assembly system.