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.

A system of monitoring carry-on items for a flight of an aircraft includes one or more cameras positioned to capture images of carry-on items associated with passengers of an aircraft. The system includes an interface configured to receive image data from the one or more cameras. The system also includes one or more processors coupled to the interface. The one or more processors are configured to analyze the image data to determine characteristics of a carry-on item. The one or more processors are configured to determine that one or more alert conditions are satisfied based on a comparison of one or more alert criteria to the characteristics of the carry-on item and data associated with the aircraft. The one or more processors are also configured to send, to one or more devices, an output based on satisfaction of the one or more alert conditions.

A system comprises a plurality of RFID readers distributed throughout an aircraft cabin. The RFID readers are configured to read RFID tags attached to luggage items. The system also includes a controller operatively connected to the plurality of RFID readers. The controller includes machine readable instructions configured to cause the controller to receive RFID readings from the plurality of RFID readers and track locations of the luggage items within the aircraft cabin. A method comprises tracking RFID tags affixed to luggage items within an aircraft cabin to monitor distribution and/or movement of the luggage items within the aircraft cabin. Tracking RFID tags includes detecting the RFID tags using a plurality of RFID readers located in overhead bins of the aircraft cabin.

A room for an aircraft cabin is a hollow box shaped room and installed in the aircraft cabin. The room includes a floor wall portion that is configured to face a seat of the cabin, a side wall portion that extends from the floor wall portion in a direction away from the seat and has an opening portion for entering and leaving the room, a ladder portion extending in a direction toward the seat from a periphery of the opening portion, and a ceiling wall portion that extends to couple the floor wall portion and the side wall portion and has an engagement structure with an inner wall of the cabin.

A lavatory system within an internal cabin of a vehicle includes an enclosure defining an interior chamber, a first lavatory unit within the interior chamber, and a second lavatory within the interior chamber. The first lavatory unit is adjacent to the second lavatory unit. In at least one embodiment, a lavatory within an internal cabin of a vehicle includes an interior chamber defined by one or more outer walls, and a storage compartment extending outwardly from at least one of outer walls. The storage compartment defines an internal storage space that connects to the interior chamber. In at least one embodiment, a lavatory includes a first lavatory unit, a second lavatory adjacent to the first lavatory unit, and a containment compartment common to the first lavatory unit and the second lavatory unit.

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.

An aircraft sanitization system is disclosed. The aircraft sanitization system includes a frame. The aircraft sanitization system further includes a tray operatively coupled to at least first two corners of the frame and is rotatable about a pivot axis. The tray is configured to be in one of a locked state and an unlocked state based on rotation about the pivot axis. In the unlocked state the tray is at an angle greater than zero with respect to the frame and in the locked state the tray is at an angle equal to zero with respect to the frame. The aircraft sanitization system further includes a set of Ultraviolet (UV) Light Emitting Diodes (LEDs) attached on an exposed surface of the frame, wherein the set of UV LEDs is configured to sanitize the tray when the tray is in the locked state.

A hinge assembly for an aircraft overhead storage bin that includes a housing having a hinge space and a hinge opening defined therein, an arm pivotably connected to the housing within the hinge space, and a dampener. The hinge opening communicates the hinge space with an exterior of the housing. The arm is pivotable between a closed position and an open position and extends through the hinge opening such that the first end of the arm is positioned outside of the housing. The dampener includes first and second ends. The first end is connected to the housing and the second end is connected to the arm. The dampener biases the arm from the closed position to the open position.

An air deflector that includes a vane with a vane top, a vane bottom, a vane first side, and a vane second side, where the vane first side and the vane second side define a vane longitudinal axis extending therebetween and a closure with a closure top. The air deflector also includes a closure bottom, a closure first side, and a closure second side, where the closure first side and the closure second side define a closure longitudinal axis extending therebetween. The vane longitudinal axis intersects the closure longitudinal axis. The vane is disposed at a predetermined angle with respect to the closure longitudinal axis.

A door mechanism for a compartment on an aircraft that includes a door with a first lower guide, a second lower guide, a first upper guide, and a second upper guide. The door mechanism includes a first lower track, a second lower track, a first upper track, and a second upper track, each having a guide track. The first lower guide, second guide, first upper guide, and second upper guide being configured to travel along the corresponding guide track to enable the door to move between open and closed positions. The door in the open position may be positioned within a portion the compartment or may be positioned above the compartment. The first and second lower tracks may include a first a second gap that enables the door to be selectively uncoupled from the first and second lower track guides permitting the door to swing away from the compartment.