Systems and methods for wireless unlocking of lock systems on enclosures within a vehicle are provided. A lock system may be unlocked via a digital key communicated to the lock system via any suitable communication protocol, for example, a short range communication protocol. The digital key can be embedded or otherwise stored and accessed in an application accessible via a user interface device.

A modular element for an electrical power distribution network of an aircraft comprises a section of a bus comprising connection points at different locations distributed along its length. The bus section comprises interconnection points making it possible to link the modular element to other modular elements arranged longitudinally in series with the modular element. Electrical conductors of the bus section are housed in an enclosure corresponding to a structural part of the aircraft. This enclosure comprises openings facing the connection points of the bus section, so as to allow the connection of at least one electrical equipment item of the aircraft to the bus section by means of a local electrical link.

An aircraft door mechanism includes an aircraft structure (14) delimiting an opening (24); an aircraft door (26) movable between a position closing off the opening (24) and a released position of the opening (24); and a guide system (28) for moving the door (26) between the closed off and released positions. The guide system (28) includes a main rail (46) that is fixed relative to the structure and a main carriage (48) mechanically connected to the door (26) and able to slide on the main rail (46) during the movement between said closed off and released positions. The main rail (46) is positioned between the door (26) and the structure during at least part of the movement of the door (26) between said closed off and released positions.

An adjustable bed assembly for a vehicle includes a contoured bed frame, a foundation disposed in the bed frame and coupled to an articulated frame having a support platform with a plurality of sectional support members. A linkage mechanism couples the support platform to the foundation and a drive mechanism operably coupled to the linkage assembly adjusts the position of at least one sectional support member. A mattress is disposed on the support platform and configured to conform with the plurality of sectional support members. A monitor mounted on the bed frame is movable between a retracted position and an extended position. A control device has a first preset for concurrently adjusting the articulated frame and moving the monitor.

An example system for determining space availability in an aircraft includes a plurality of laser sensors configured to be positioned in a baggage container at a first wall and a second wall, and the first wall and the second wall face each other. The plurality of laser sensors emit signals within the baggage container and detect reflected responses to generate outputs. The system also includes one or more processors in communication with the plurality of laser sensors for executing instructions stored in non-transitory computer readable media to perform functions including receiving the outputs from the plurality of laser sensors, mapping contents of the baggage container based on the outputs from the plurality of laser sensors, and based on said mapping, outputting data indicative of occupied space in the baggage container.

Mirror displays, mirror display and compartment assemblies, and methods for making mirror displays are provided. In one example, the mirror display includes a transparent mirror having a front surface facing in a forward direction and a back surface opposite the front surface. When a user is present in front of the front surface, the transparent mirror is configured to reflect a first image of the user from the transparent mirror back towards the user. A display panel is disposed adjacent to the back surface of the transparent mirror and is configured to display a second image that is transmitted through the transparent mirror to be viewable from the front surface.

A bidirectional latching device for securing a cargo in a vehicle may have a latch catch assembly and a latch head. The latch catch assembly may selectably engage with the latch head. When engaged with the latch head, the latch catch assembly may lock the latch head in position to resist movement and the latch head may secure the cargo in the vehicle. When disengaged from the latch head, the latch catch assembly may release the latch head and the latch head may move to a stowed position. The latch catch assembly may lock the latch head to resist movement in one or more directions of movement. The latch head may be shaped to secure the cargo in the vehicle in at least two directions. Thus, cargo may be secured more efficiently by requiring a reduced number of latch devices because the disclosed latch device is bidirectional.

A system and method are disclosed for displaying the storage status of overhead luggage storage bins in an aircraft. A camera is provided that is mounted with a field of view directed at an inner portion of a group of open bins. The camera is communicatively coupled to a controller and selectively provides images of the inner portion of the bins immediately prior to when the bins are closed to the controller. A projector is also provided for each group of bins. The projector is communicatively coupled to the controller and is mounted such that an image received from the controller is projected onto an outer surface of the closed bins. The controller receives images from each of the cameras and selectively provides such images to the projector associated with each camera so that a storage status display is projected on an outer surface of the bins.

In an example, an overhead payload module is described. The overhead payload module comprises a ceiling assembly, an aisle floor assembly, a first payload assembly attached to the ceiling assembly and the aisle floor assembly to form a first side of the overhead payload module, and a second payload assembly attached to the ceiling assembly and the aisle floor assembly to form a second side of the overhead payload module. The first payload assembly comprises a first payload module and a first overhead stowbin module structurally integrated with the first payload module and having a first stowage area configured to receive stowbins. The second payload assembly is positioned opposite the first payload assembly to form an aisle therebetween and comprises a second payload module and a second overhead stowbin module structurally integrated with the second payload module and having a second stowage area configured to receive stowbins.

An illuminated handle mounted to a surface of a crew work area includes an illuminated portion is disposed on an interior surface. A structural portion is integrated into work area stowage compartments, disposed between two stowage compartments, such that the illuminated portion illuminates the stowage compartments and their contents when opened. The illuminated handle includes an illuminated coat hook protrusion extending from a top portion of the illuminated handle. The illuminated portion of the illuminated coat hook is disposed on an interior surface to further illuminate the stowage compartments and indicate the location of the illuminated coat hook, while the hook extension prevents the illuminated portion from directly illuminating a crew member's face and potentially blinding the crew member momentarily.