Installation system for an airplane
View Patent ↗An exemplary embodiment of the present invention indicates an installation system for an airplane for securing interior equipment, which exhibits longitudinal and transverse rails. The transverse rails are designed as peripheral rails, and exhibit perforations to which the interior equipment can be secured.
1. A rail for cabin and system installation in an aircraft, the rail comprising:
a cable installation space;
an attachment area arranged at a first side of the cable installation space;
a mounting area arranged at a second side of the cable installation space, which second side is arranged opposite to the first side, such that the cable installation space is arranged between the attachment area and the mounting area and
at least one mechanical bonding point;
wherein the attachment area comprises a first perpendicular area, which first perpendicular area extends in a longitudinal direction of the rail along the whole rail;
wherein the attachment area is configured to attach the rail to a primary structure of the aircraft;
wherein the mounting area extends as a horizontal area in a longitudinal direction of the rail along the whole rail and accommodates the at least one mechanical bonding point;
wherein the at least one mechanical bonding point is configured to mechanically attach loads to the rail;
wherein the cable installation space is configured to provide an integrated, expanded functionality;
wherein the mounting area extends generally orthogonally to the attachment area, and
wherein the attachment area comprises a generally planar face and is configured such that the planar face directly attaches to the primary structure for attaching the rail to the primary structure.
2. The rail of claim 1 ,
wherein the expanded functionality is an electrical functionality.
3. The rail of claim 1 ,
wherein the cable installation space comprises at least partially an electrically conductive jacket;
wherein the jacket is configured to electromagnetically screen an electrical conductor inside the cable installation space.
4. The rail of claim 1 ,
wherein at least portions of the rail are configured as part of a return line network.
5. The rail of claim 1 ,
wherein the rail comprises an expanded H-profile in cross section perpendicular to a longitudinal axis of the rail;
wherein the expanded H-profile comprises, at a boundary section, the first perpendicular area abutted by a first horizontal area up to a second perpendicular area;
wherein the first horizontal area comprises a first width between the first and the second perpendicular area, thereby forming a cable installation space both on an upper side and lower side of the horizontal area;
wherein the mounting area comprises a second, final, horizontal area abuting the second perpendicular area, and accommodating the at least one mechanical bonding point;
wherein the first horizontal area is perpendicular to the first and the second perpendicular areas and extends parallel to the longitudinal axis of the rail; and
wherein the second, final, horizontal area is perpendicular to the second perpendicular area and extends parallel to the longitudinal axis of the rail.
6. The rail of claim 1 ,
wherein the rail comprises the first and the second perpendicular areas in cross section perpendicular to a longitudinal axis of the rail;
wherein the cable installation space is arranged between the perpendicular areas as a load-bearing element of the rail; and
wherein the mounting area comprises a final, horizontal area abuting the second perpendicular area, and accommodating the at least one mechanical bonding point; and
wherein the final, horizontal area is perpendicular to the second perpendicular area and extends parallel to the longitudinal axis of the rail.
7. The rail of claim 1 ,
wherein the rail comprises at least partially an electrically conductive material.