Abstract: The disclosure provides for an aircraft galley and lavatory energy system capable of independent operation from a separate aircraft energy generating system. The galley and lavatory energy system comprises an energy source providing electrical energy, heat energy, and at least one by-product; a plurality of galley and lavatory devices for receiving the electrical energy, the heat energy, and the at least one by-product; and, a plurality of connectors for connecting the electrical energy, the heat energy, and the at least one by-product to the galley and lavatory devices. The energy source comprises a fuel cell, a fuel module, and optionally, a supplemental fuel source.

Abstract: A system for loading cargo containers into a storage hold, and offloading cargo containers from the storage hold, especially of a vehicle, such as an aircraft. The system includes at least one guide rail and a motorized platform, onto which cargo containers are loaded, cooperating mechanically with the guide rail. The guide rail guides the cargo laden motorized platform into the storage hold, and the motorized platform deposits the cargo upon remote command. The motorized platform has a chassis; a power source; a control module controlling drive motors of the wheels of the platform; and a device for reciprocating at least a portion of an upper surface of the platform sufficient to elevate a load placed thereon above the guide rail height.

Abstract: The disclosure provides for an aircraft galley and lavatory energy system capable of independent operation from a separate aircraft energy generating system. The galley and lavatory energy system comprises an energy source providing electrical energy, heat energy, and at least one by-product; a plurality of galley and lavatory devices for receiving the electrical energy, the heat energy, and the at least one by-product; and, a plurality of connectors for connecting the electrical energy, the heat energy, and the at least one by-product to the galley and lavatory devices. The energy source comprises a fuel cell, a fuel module, and optionally, a supplemental fuel source.

Abstract: A system for loading cargo containers into a storage hold, and offloading cargo containers from the storage hold, especially of a vehicle, such as an aircraft. The system includes at least one guide rail and a motorized platform, onto which cargo containers are loaded, cooperating mechanically with the guide rail. The guide rail guides the cargo laden motorized platform into the storage hold, and the motorized platform deposits the cargo upon remote command. The motorized platform has a chassis; a power source; a control module controlling drive motors of the wheels of the platform; and means for reciprocating at least a portion of an upper surface of the platform sufficient to elevate a load placed thereon above the guide rail height.

Abstract: Apparatus and methods for removably securing payloads are disclosed. In one embodiment, a method includes coupling the payload to a body of a locking assembly, engaging an insertion portion of the body into the channel, translating the insertion portion of the body along the track from a first position to a second position, the body being substantially constrained from movement away from the track in the second position, and actuating at least one engagement member from an unsecured position to a secured position, a portion of the track being clampably engaged by the at least one engagement member and the insertion portion of the body when the at least one engagement member is positioned in the secured position such that the body is substantially constrained from movement along the track by the at least one engagement member.

Abstract: A method of providing power and/or data to a seat in a seating area. A power distribution system having a continuous power bus is used to supply power and/or data to seats in a mobile platform or fixed structure. The power distribution system generally includes a bus strip that, in a mobile platform, extends along a length of a passenger cabin and a connector operable to provide a connection between the bus strip and the passenger seats. Power and/or data can be transmitted between the bus strip and the passenger seats, via the connector, at any point along the bus strip, thus eliminating the need to run separate connections between the power and/or data source and each seat.

Abstract: Systems and methods are provided for regulating the pressure within an aircraft flight crew area during and/or after a decompression event. For example, an aircraft may include a flight crew area, at least one pressure sensor for detecting the pressure of the atmosphere within the flight crew area, and at least one regulated decompression panel that is operatively associated with the pressure sensor, for regulating the pressure within the flight crew area during and/or after a decompression event.

Abstract: A supplemental oxygen system and method is set forth for providing oxygen to an occupant of a pressurized aircraft. A flexible hood may be adapted to be stowed in a small volume when the flexible hood is deflated and may be further adapted to cover at least a portion of the head of the occupant and to provide a flow of oxygen to the occupant when the flexible hood is inflated. A source of oxygen may be adapted to rapidly inflate and deploy the flexible hood.

Abstract: Methods and systems for a monitoring system for a vehicle are provided. The system includes at least one radio frequency identification (RFID) system comprising at least one transceiver and a plurality of RFID tags, the tags coupled to a plurality of vehicle components, a plurality of vehicle component retaining assemblies coupled to the plurality of components and operatively configured to substantially shield the amount of radio frequency (RF) energy received from the transceiver by each tag in a first position and unshield each tag in a second position, and an alert system for receiving information regarding the plurality of vehicle components and for generating an alert based on the information received.

Abstract: An overhead video system for an aircraft is disclosed. The overhead video system comprises a wireless overhead video unit; and at least one mounting rail detachably coupled to the wireless overhead video unit. The mounting rail provides structural support and electrical power to the wireless overhead video unit. A system in one embodiment may use mounting rails that double as power rails supplying power to the wireless overhead video unit. Video control and content streaming is accomplished over a wireless link. The power rail control may be accomplished remotely via a standard or solid state relay. Normal rail power for the rail mounted video system may come from the utility bus.

Abstract: A cabin services system for an aircraft is disclosed. The cabin services system comprises at least one wireless network, the at least one wireless network providing at least one cabin service. The cabin services system further includes a cabin attendant panel for communicating with the at least one wireless networks and configured to control the at least one cabin service.

Abstract: A mounting rail system for a cabin services system of an aircraft is disclosed. The mounting rail system comprises a mounting rail for providing power, and at least one circuit coupled to the mounting rail for allowing for operation of functionalities of a passenger services unit.

Abstract: A system for communicating electrical signals between two spaced apart seat assemblies on a mobile platform, for example an aircraft. The seat assemblies are secured to seat tracks mounted on a floor of the aircraft cabin. The seat tracks have a plurality of spaced apart holes that enable seat assembly mounting. A seat track cover is snap-fit onto one or more seat track mount devices. Each of the seat track mount devices includes one or more cleats or knobs that can be snap fit into the openings in the seat track to quickly and easily secure the seat track cover to the seat track. The seat track cover and mount devices enable a simple, planar seat track having spaced apart holes to be employed, rather than a C-shaped seat mounting track.

Abstract: A seat track cover for transferring at least one of electrical power and data between two seats. The cover has a housing and a cable. The housing is sized to extend between a first seat leg assembly of a first seat and a second seat leg assembly of a second seat. The housing comprises a channel forming a first aperture at one end and a second aperture at a second end opposite the first aperture. The cable is seated within the housing and has a length at least equal to the length of the housing. The cable comprises a first connector and a second connector. The cable is seated within the housing such that the first connector is at the first aperture of the housing and the second connector is at the second aperture of the housing. The first connector couples with the first seat leg assembly and the second connector couples with the second seat leg assembly when the housing is positioned between the first seat leg and the second seat leg.

Abstract: A seat track cover having telescopically engaged first and second portions that enables an overall length of the seat track cover to be adjusted as needed to cover a portion of a seat track that separates two adjacent seats mounted to the seat tracks. A cable can be routed within the first and second portions to enable electrical or optical signals to be conducted between data/power connection ports on the seats. One embodiment includes mating conductive elements formed along the lengths of each of the first and second portions.

Abstract: A power/data bus for conducting at least one of data and power signals to a variety of different locations on a mobile platform. The bus has a plurality of discrete connection ports, and at least one conductive cable. The power/data bus extends across an area where access to at least one of data and electricity is desired. The discrete connection ports are spaced apart at different locations along the power/data bus. The conductive cable extends through the power/data bus and is connected to at least one of the discrete connection ports. The conductive cable conducts at least one of power and data signals between the discrete connection ports and a data/power source. At least one of the connection ports are operable to cooperate with a connector of an external device to supply at least one of power and data signals to the external device. The power/data bus, when used in an aircraft passenger cabin, eliminates the need to extend individual data and/or power cables to or between each passenger seat group.

Abstract: An interior cabin configuration determination system (10) includes multiple objects (16), including two or more monuments or passenger service units, that are within an interior cabin (13). The objects (16) include card readers (12). Object controllers (18) are coupled to the card readers (12) and determine the position of the objects (18) in response to the position information on the cards (12). A remotely located controller (20) determines the configuration of the objects (18) in response to the position information.

Abstract: A seat having a seat leg assembly for use on a mobile platform, especially on an aircraft. The seat comprises a front seat leg, a rear seat leg, and a spreader bar coupled to and extending between the front seat leg and the rear seat leg. The spreader bar has a door. The door is movable between a closed position in which the door prevents access to areas beneath the spreader bar and an open position in which the door permits access to areas beneath the spreader bar. In this manner, the open door allows an installer to grasp electrical cabling beneath the spreader bar and feed the cabling through a hole in the door so that the cable can be connected a connection point on or adjacent to the seat track.

Abstract: A conductive bus device and method operable to distribute signals throughout a platform. The bus delivers signals to any number of select locations within the platform, such as to seats mounted to a seat track. The bus is mounted beneath a floor of the platform. The signals can be transmitted between the power bus and the passenger seats using a conductor that extends from the passenger seats to the bus through a opening in the seat track. The bus device and method eliminates the need to run separate connections between a signal source and each seat. This device and method significantly reduce the cost, energy, and time necessary to wire each seat individually.

Abstract: A power supply system operable to supply power and/or data to aircraft passenger seats that eliminates the need to extend individual cables to each seat and eliminates the need to rewire the passenger cabin when the seats are moved. The system includes a first connector housing secured to a first seat leg and a second connector housing secured to at least one of the first seat leg and the second leg. A first connector of a seat electronic subsystem is mounted to the first housing. A second connector of the seat electronic subsystem is mounted to the second housing. A conductor is operable to mate with at least one of the first connector and the second connector for conducting at least one of data and electricity to or from the seat.