INTERIOR COMPONENT CARRIER SYSTEM, AIRCRAFT INTERIOR COMPONENT MODULE AND ASSEMBLY METHOD

摘要

The invention relates to an interior component carrier system (22) for use in the assembly of aircraft interior components (12, 14, 16, 68, 78) in an aircraft, said system comprising a retaining system (24) with at least one retaining element (26, 28), and a first connection device (30) for connecting the retaining element (26, 28) to a first aircraft interior component (12) and also a second connection device (56) being provided on said retaining element (26, 28). Additionally, on said retaining element (26, 28), a structural retainer (80) is provided for fixing said retaining element (26, 28) to an aircraft structure. The interior component carrier system (22) also comprises a hinge (38) that can be connected to a second and a third aircraft interior component (14, 16) such that the third aircraft interior component (16) is able to be pivoted about a longitudinal axis (L) of said hinge (38) and relative to the second aircraft interior component (14). The second connection device (56) mounted on the retaining element (26, 28) is configured to be connected to the hinge (38) and/or to a region of the second or third aircraft interior component (14, 16) which is adjacent to said hinge (38).