A power rail system including a rail assembly, which includes a sidewall, a first interior compartment at least partially enclosed by the sidewall, the first interior compartment extending longitudinally along the first rail assembly, an opening in communication with the first interior compartment, the opening positioned along the sidewall, and a second interior compartment at least partially enclosed by the sidewall, the second interior compartment extending longitudinally along the first rail assembly and configured to receive the connector member therein. The power rail system can further include an electrical outlet assembly positionable within the first interior compartment. Further, various accessories, such as privacy screens, can be supported by the rail assembly. Still further, multiple rail assemblies can be connected together to customize the size and/or configuration of the power rail system.

A power rail system including a rail assembly, which includes a sidewall, a first interior compartment at least partially enclosed by the sidewall, the first interior compartment extending longitudinally along the first rail assembly, an opening in communication with the first interior compartment, the opening positioned along the sidewall, and a second interior compartment at least partially enclosed by the sidewall, the second interior compartment extending longitudinally along the first rail assembly and configured to receive the connector member therein. The power rail system can further include an electrical outlet assembly positionable within the first interior compartment. Further, various accessories, such as privacy screens, can be supported by the rail assembly. Still further, multiple rail assemblies can be connected together to customize the size and/or configuration of the power rail system.

A wire trough is provided that includes a main body, caps closing ends of the main body, and a cover. The main body has four longitudinally extending walls defining an access opening between edges of two of the four walls. The cover selectively close the access opening.

A cable management system includes a mounting bracket configured for mounting to a wall surface and a detached snap-on type cover member. The mounting bracket includes vertically spaced support ledges for supporting one or more cables in multiple regions of the bracket. The bracket and cover member include mating connection element protrusions which become mutually engaged to snap fit the cover to the bracket in a readily removable manner to access the cable runs. The cables are fully concealed by the cover member. In one embodiment, the bracket and cover member are configured to simulate baseboard molding in appearance and are mounted at the bottom of the wall at the interface with the floor. Coupler members complementary configured to match the profile of the cover members may be detachably coupled thereto to bridge joints or gaps between adjacent sections of cover members.

There is provided a sidewall closeout area assembly for an aircraft. The assembly includes a raceway with a first end to attach to a sidewall assembly, a second end to attach to aircraft floor structure(s), and a raceway body with first access opening(s) providing access to one or more of, a crown area and an underfloor area, for conductive elements routed along the raceway. The assembly further includes a raceway cover removably coupled to the raceway and having second access opening(s) providing access to the cabin and to an overfloor area in the cabin for the conductive elements. The assembly further includes a closeout area formed between the raceway body and the raceway cover, to house and protect the conductive elements. The assembly facilitates accessibility to the conductive elements, and provides a routing path for the conductive elements that does not need to be reconfigured for different aircraft cabin layouts.

A decorative interior trim piece is provided for use in a low voltage power transmission system, and includes an outer, decorative surface, an opposite inner surface facing a substrate, a first end surface and an opposite second end surface. At least one conductive element extends from the first end surface to said second end surface on the inner surface. Each conductive element has a connector surface at each of the first end and second ends. At least one magnetic fastener is secured to the inner surface for releasably attaching the trim piece to the substrate. A complementary low voltage power transmission system is also disclosed.

There is provided a sidewall closeout area assembly for an aircraft. The assembly includes a raceway with a first end to attach to a sidewall assembly, a second end to attach to aircraft floor structure(s), and a raceway body with first access opening(s) providing access to one or more of, a crown area and an underfloor area, for conductive elements routed along the raceway. The assembly further includes a raceway cover removably coupled to the raceway and having second access opening(s) providing access to the cabin and to an overfloor area in the cabin for the conductive elements. The assembly further includes a closeout area formed between the raceway body and the raceway cover, to house and protect the conductive elements. The assembly facilitates accessibility to the conductive elements, and provides a routing path for the conductive elements that does not need to be reconfigured for different aircraft cabin layouts.

There is provided a raceway cover assembly for installing conductive element(s) in an aircraft. The raceway cover assembly includes a raceway cover for removable coupling to a raceway. The raceway is configured for attachment to a sidewall assembly for use in a cabin of the aircraft. The raceway cover includes a first cover side, a second cover side, and retaining element(s) disposed on the first cover side. The raceway cover assembly further includes the conductive element(s) coupled and retained to the first cover side, with the retaining element(s), to form the raceway cover assembly. The conductive element(s) and the raceway cover are assembled together at a location off of the aircraft, prior to installing the raceway cover assembly with the one or more conductive elements in the aircraft, which allows for routing of the one or more conductive elements in the raceway cover at the location off of the aircraft.

A system for crown molding that enables safely incorporating electrical and communications cabling within crown molding by creating one or more protected paths which inherently prevent overly sharp bends in crown molding corners and by mitigating damage from penetrating punctures through a decorated face designed to fracture when improperly penetrated by a screw or nail, and enables the secure installation of hardware either concealed within the molding or securely and favorably positioned through the decorative face to view or sense a room, and enables additional cable capacity that is concealed within a light reflector to increase lighting efficacy as well as power and data delivery capacity.

A system for crown molding that enables safely incorporating electrical and communications cabling within crown molding by creating one or more protected paths which inherently prevent overly sharp bends in crown molding corners and by mitigating damage from penetrating punctures through a decorated face designed to fracture when improperly penetrated by a screw or nail, and enables the secure installation of hardware either concealed within the molding or securely and favorably positioned through the decorative face to view or sense a room, and enables additional cable capacity that is concealed within a light reflector to increase lighting efficacy as well as power and data delivery capacity.