Transformable monuments may be positioned proximate to aircraft exit doors to utilize the doorway spaces as temporary workspaces for cabin crew or destination spaces for passengers once cruising altitude is achieved. A transformable monument includes transforming portions that extend or pivot into an aircraft cross-aisle upon actuation of an exterior latch by either hand. The transforming portions extend or pivot into horizontal surfaces for crew or passenger use while protecting the exit doors from unauthorized access by passengers inflight. Transforming portions of a single monument may extend partially or fully across the cross-aisle, or a system of two transformable monuments on either side of the exit door may collectively define the temporary space. The upper and middle sections of the monument may include additional storage or self-service compartments for providing refreshments or other amenities to passengers.

A system may include a door installed within a vehicle. The system may further include an electronically actuated linear actuator latch mechanism (a) installed in or on the door or (b) installed within the vehicle in proximity to the door. The electronically actuated linear actuator latch mechanism may be configured to cause the door to be in a latched state and to cause the door to be in an unlatched state.

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.

A keep-out assembly for a stowage bin assembly positioned above at least a portion of one or more seats within a vehicle includes a keep-out lens and a keep-out bracket. The keep-out lens is pellucid and extends between an inner edge and an outer edge. The keep-out lens has a top surface and a bottom surface. The keep-out mounting bracket has a base configured to be mounted to the stowage bin assembly at a top of the stowage bin assembly. The keep-out mounting bracket has a support arm extending from the base. The support arm engages the keep-out lens and supports the bottom surface of the keep-out lens at an elevated position above the stowage bin assembly.

An aircraft that includes a cabin interior that is bifurcated into first and second sides and includes a pilot zone and a passenger zone aft of the pilot zone, a pilot seat positioned in the pilot zone and on a first side of the cabin interior, and first and second rows positioned in the passenger zone. The front row includes first and second front seats positioned on first and second sides of the cabin interior, respectively. The first and second front seats are angled away from one another and the second front seat is positioned forwardly of the first front seat. The back row includes first and second back seats positioned on first and second sides of the cabin interior, respectively.

Processes and systems for determining that a piece of luggage has been left behind in an overhead bin of a vehicle. When a passenger places a piece of luggage into the overhead bin, it is associated with that passenger by detecting that the passenger has sat down in a particular seat after the luggage has been placed into the overhead bin. When it has been determined that the passenger has deboarded the vehicle, and the luggage has not been removed, reminder signals are sent.

A locking system for an overhead stowage bin may comprise a latch and an electromechanical actuator configured to actuate the latch. A bin controller may be electrically coupled to the electromechanical actuator. A passenger input and a master controller may be in operable communication with the bin controller.

Example implementations relate to stowage bin lighting interfaces. An example apparatus includes a panel portion, and a set of fasteners configured to couple the panel portion to a stowage bin such that a curvature of the panel portion aligns with a curvature of the exterior of the stowage bin. Each fastener is configured to extend through the stowage bin into a back portion of the panel portion to couple the panel portion to the stowage bin. Aligning the curvature of the panel portion with the curvature of the exterior of the stowage bin enables the stowage bin to open and close when the panel portion is coupled. The apparatus further includes a lighting interface configured to couple between the panel portion and the exterior of the stowage bin at a position that enables the lighting interface to provide illumination through openings in the panel portion and ambient lighting.

A system and method for vehicle compartment item presence indication senses an item within a vehicle compartment and notifies a user if the item is expected or unexpected within the compartment based on a vehicle state. Should the item be expected in a compartment during a phase of flight where the compartment is expected to contain items, there is no abnormal indication. However, if a compartment is expected to be empty during a specific phase of flight and the sensors indicate an item is present, the system will alert the user to the unexpected item.

An overhead stowage bin assembly having a bin structure with a lower panel and an open side that defines a front of the stowage bin assembly. The lower panel has a leading edge that is arranged at the front of the stowage bin assembly. A cover is formed by base plates and a central plate and is secured to the lower panel to form a passage. The central plate has protruding ribs that are aligned to increase the stiffness of the cover and the rigidity of the lower panel. A threshold has walls that are connected to each other and define a channel. The leading edge of the lower panel is received within the channel such that the threshold walls mate with opposite surfaces of the lower panel so as to grip the leading edge of the panel and further enhance the stiffness of the lower panel.