Abstract: A system and method for transporting a cargo container in a cabin of an aircraft are provided. The system comprises a guide rail spanning a length of a seat track and being releasably coupled to the seat track at one or more locations on a bottom surface of the guide rail. A plurality of rollers are coupled to the guide rail where the rollers positioned to engage a surface of the cargo container. The system also comprises a lateral rail comprising a rail member configured to abut a side surface of the cargo container and prevent lateral movement of the cargo container in the cabin. The rail member is slidably mounted on a base to move the rail member laterally within the cabin. When the cargo container deviates from a path defined by the guide rail, the rail member abuts one of the side surfaces of the cargo container.

Abstract: A system for restraining a cargo container in a cabin of an aircraft is disclosed. The system may include a guide rail, a rail and a plurality of rollers. The guide rail spans a length of a seat track and is releasably coupled to the seat track at one or more locations on a bottom surface of the guide rail. The rail is attached to a surface of the cargo container. The rail engages with the guide rail. The plurality of roller are coupled to the guide rail. The rollers engage a surface of the rail. The rail has two side surfaces that partially enclose two side surfaces of the rollers. When the cargo container deviates from a path defined by the guide rail, one of the side surfaces of the rollers abuts one of the side surfaces of the rail.

Abstract: A system for restraining a cargo container in a cabin of an aircraft is disclosed. The system may include a guide rail, a rail and a plurality of rollers. The guide rail spans a length of a seat track and is releasably coupled to the seat track at one or more locations on a bottom surface of the guide rail. The rail is attached to a surface of the cargo container. The rail engages with the guide rail. The plurality of roller are coupled to the guide rail. The rollers engage a surface of the rail. The rail has two side surfaces that partially enclose two side surfaces of the rollers. When the cargo container deviates from a path defined by the guide rail, one of the side surfaces of the rollers abuts one of the side surfaces of the rail.

Abstract: The invention provides a system, for providing the distribution of electrical power and data signal communication inside a passenger aircraft to each seat on each seat assembly, the passenger seat assembly comprising a leg frame secured to a floor seat track and a lateral beam spanning between the leg frame and a side wall seat track, the lateral beam supporting a passenger seat and having an outboard end secured in the side wall seat track, the system comprising: a hub secured to the side wall seat track, the hub being connected to both: a source of electrical power; and a source of data signal communication, via a side wall mounted conduit; and an outlet secured to the passenger aircraft seat assembly and communicating with the hub via an outlet conduit.

Abstract: The invention provides a system, for providing the distribution of electrical power and data signal communication inside a passenger aircraft to each seat on each seat assembly, the passenger seat assembly comprising a leg frame secured to a floor seat track and a lateral beam spanning between the leg frame and a side wall seat track, the lateral beam supporting a passenger seat and having an outboard end secured in the side wall seat track, the system comprising: a hub secured to the side wall seat track, the hub being connected to both: a source of electrical power; and a source of data signal communication, via a side wall mounted conduit; and an outlet secured to the passenger aircraft seat assembly and communicating with the hub via an outlet conduit.

Abstract: The invention provides a means by which AC or USB power/data outlets can be installed onto aircraft passenger seats by an underhung mounting bracket that can be quickly installed with flexible cable ties or adjustable straps to the beams of a passenger aircraft seat, and provides sufficient adjustment in length to accommodate a variety of aircraft seat structures.

Abstract: The invention provides a means by which AC or USB power/data outlets can be installed onto aircraft passenger seats by an underhung mounting bracket that can be quickly installed with flexible cable ties or adjustable straps to the beams of a passenger aircraft seat, and provides sufficient adjustment in length to accommodate a variety of aircraft seat structures.

Abstract: A support bracket for mounting wires, cables, conduits and the like to floor beams of an aircraft passenger cabin floor without modification to the floor beams, the floor beams having a top flange, a bottom flange, and a vertical web. The support bracket has a support body with cable support cradles where each cradle has a cradling surface and a tie wrap passage; and at least clamping block connected to the support body with at least one adjustable tension bolt, the clamping block having a beam engaging surface wherein tension in the at least one bolt urges the beam engaging surface toward the support body.