A method of managing media content on a vehicle comprises storing a media content library comprising a plurality of media content items in non-volatile data storage media disposed in the vehicle, storing access rule data in the non-volatile data storage media, establishing a connection with a remote computing device over a communication link, receiving, from the remote computing device over the communication link, an indication identifying a first subset of the media content library to be designated as active, updating the access rule data to indicate that the first subset of the media content library is designated as active, and presenting at least a portion of the first subset of the media content library on a media presentation device based at least in part on said updating.

A passenger seat includes a spreader frame structure and a seat back pivotally attached to the spreader frame structure. At least one cable can pass through apertures between the seat back and the spreader frame structure. The seat can rotate between an upright configuration wherein the seat back is in a deployed position, and a break over configuration wherein the seat back is in a stowed position. The length of the at least one cable between the aperture in the seat back and the aperture in the spreader frame structure is approximately the same in the upright configuration and in the break over configuration.

The present invention pertains an overhead unit (1) for presenting information, gathering information, transferring information, lighting and/or alarm signals in an individualized manner in a carriage or fuselage, comprising a function module (2), a fixation module (3) for removably attaching the overhead unit to a rail, two receival modules (5a, 5b) for receiving signals, two transmission modules (4a, 4b) for sending messages and a processing module (6) for processing messages, whereby the receival modules and the transmission modules are operationally connected to the processing module, wherein the fixation module comprises a mechanical fixation system (7) configured to interlock with a fixation system of the rail, wherein the overhead unit comprises a proximal longitudinal end (9) and a distal longitudinal end (10), wherein the receival modules comprise a proximal receival module located at the proximal end of the overhead unit and a distal receival module located at the distal end of the overhead unit, whereby the receival modules each comprise a sensor, wherein the transmission modules comprise a proximal transmission module located at the proximal end of the overhead unit and a distal transmission module located at the distal end of the overhead unit, whereby the transmission modules each comprise a transmission source, wherein the processing module of the overhead unit is configured to receive signals via the receival modules from a neighbouring overhead unit or from a neighbouring control unit, and/or wherein the processing module of the overhead unit is configured to cause the transmission modules to send out signals to a neighbouring overhead unit and/or the control unit.

The aircraft intercom employs beam steerable microphone arrays and speaker arrays deployed in each of a plurality of zones within the aircraft. A speech recognizer generates recognition text from utterances picked up by the microphone arrays. A direction control processor analyzes the arrival time of signals from the microphone arrays to identify utterance location, which is then used to control the beam direction of at least one steerable speaker array. A dialogue manager processor coupled to the speech recognizer and to each of the plurality of microphone arrays and plurality of speaker arrays responds to a set of predefined keywords to selectively route a voiced communication from a first selected zone to a second selected zone using the microphone array and speaker array disposed in each of the first and second selected zones.

In an aircraft seat power system, a Smart Power Distribution Connector (PDC) connects a power supply to multiple power outlets. Power to each outlet is monitored and controlled directly by the PDC that is in turn monitored and controlled by the power source. The power source and the PDC share a communication bus through which instructions and responses are communicated. The PDC has the ability to communicate with the outlets by sending instructions and monitoring and acting on the responses from the outlets. The system allows for power management from a supply of limited power. The PDC can provide current limiting, allowing the use of lighter weight and smaller wire and other components.

A super first-class cabin includes a monitor disposed in the ceiling structure, a controller to render images on the monitor, and cameras to capture real-time streaming environmental images and renders them on the monitor. At the passenger's request, or when the passenger reclines, the controller may render a selection of mood affective images, for example to promote sleep if desired. Such mood affective images may be organized into a schedule associated with phases of flight to gently wake the passenger and prepare them for the end of the flight. The monitor may be employed to reduce the effects of flight-base time-disassociation by varying a daylight color scheme over the course of long flights, simulating a day/night routine to align the time of day at the origin of the flight with the time of day at the destination.

Aircraft information systems, aircraft that include the aircraft information systems, methods of utilizing the aircraft information systems, and methods of configuring the aircraft information systems are disclosed herein. The aircraft information systems include a fixed computing device configured to be fixedly installed within an aircraft. The fixed computing device is programmed to provide a cabin function interface that provides cabin functionality for a cabin attendant of the aircraft and also to provide a mechanic function interface that provides mechanic functionality for a mechanic for the aircraft. The aircraft include a fuselage, at least one wing, at least one engine, and the aircraft information systems.

An aircraft workstation is disclosed that includes a table that is movable between a stowed position and a deployed position. In one implementation the workstation is incorporated by an aircraft within an exit row. Access to the workstation may be controlled by a latch that locks the table it is stowed position. The workstation may also include a power switch, one or more power sockets, and wire management. The table may incorporate one or more accessories, such as a cupholder, a mouse extender, a table extender, and a stand.

A magnetic pass-through controller of an in-helmet display includes internal components inside a helmet. The internal components include a magnet assembly holding one or more internal magnets and a swing arm affixed to the magnet assembly and affixed to the in-helmet display. External components outside the helmet include an external magnet housing holding one or more external magnets and an adjuster for manual rotation. The adjuster is coupled to the external magnet housing such that the manual rotation of the adjuster causes a corresponding rotation of the external magnet housing. Magnetic coupling between the one or more internal magnets and the one or more external magnets causes the corresponding rotation also in the magnet assembly and the swing arm.

A galley monument for an aircraft has a shelf structure, a pull-out member supported on the shelf structure so as to be able to be moved between an insertion position and a deployment position and has a carrier plate, and a display device supported on the pull-out member and having a display. A first surface of the carrier plate in the deployment position of the pull-out member is located in a deployment plane and protrudes with respect to the shelf structure and is located in the insertion position at least partially inside the shelf structure. The display device in the deployment position of the pull-out member can be pivoted about a centre of rotation between a storage position, in which the display device extends parallel with the deployment plane, and a position for use, in which the display device extends transversely relative to the deployment plane.