A system may include a vestibule disposed in a passenger cabin of an aircraft, the vestibule including a staircase for accessing a passenger rest cabin, the passenger rest cabin implemented above or below the passenger cabin of the aircraft. The system may also include a plurality of passenger rest compartments implemented in the passenger rest cabin, each of the plurality of the passenger rest compartments including a bed and a passenger service unit (PSU).

Passenger rest compartments may be incorporated into remote areas of an aircraft, either in the overhead crown region or in lower lobe cargo decks. Each passenger rest compartment includes two-way audio communication with the flight deck and non-intrusive non-visual monitoring of the compartments and surrounding environment to determine passenger presence, absence, and general well-being as well as environmental safety. Rest compartments may be integrated into rest cabins in the overhead or lower lobe areas, the rest cabins accessible from the main passenger cabin via an entry vestibule providing dedicated enclosed paths to the overhead and lower cabins. Additional deployable egress hatches may allow passengers to rapidly return to the main deck from the overhead and lower lobe cabins in the event of an emergency. Selected passenger seats (e.g., partitioned or other premium seats) may include private access to passenger rest compartments.

A system. The system may include a glare shield positioned between an exterior pane of an aircraft window and an interior portion of an aircraft. The glare shield may include at least one anti-reflective mask and at least one viewing aperture. Each of the at least one anti-reflective mask may be positioned adjacent one of the at least one viewing aperture.

A panelling part for a cabin of a means of transportation is proposed, which includes at least one display unit and at least one control unit, which are produced by printing and equipping at least one film, which is applied to a panelling element. The control unit can communicate wirelessly with an external electronics unit, so that the panelling part only requires a power terminal to implement electronic functions. Functions can be retrofitted easily by replacing the at least one film.

An imaging system includes a first imaging device and a second imaging device disposed flanking the main wing of an aircraft. The first imaging device and the second imaging device are disposed so that at least part of a first imaging range of the first imaging device overlaps a second imaging range of the second imaging device. The first imaging device and the second imaging device are also disposed so that the first imaging range and the second imaging range overlap an extension of the pitch axis of the aircraft and do not overlap the roll axis of the aircraft or an extension thereof.

A system and method. The system may include a monitor implemented as a virtual window, two cameras, and a switch. The switch may be configured to: when a passenger is in a first position, feed video from a first camera to the monitor; and when the passenger is in a second position, feed video from the second camera to the monitor.

An aerospace vehicle system, preferably including one or more capsules, and optionally including one or more propulsion modules and/or safety modules. A capsule, preferably including a pressure vessel including a structural frame and one or more windows, and optionally including a cabin. In alternate embodiments, the system can additionally or alternatively function as a terrestrial vehicle, a watercraft, and/or any other suitable vehicle. A method of operation, preferably including operating the aerospace vehicle system in flight, while maintaining a pressure differential between the pressure vessel interior and an environment surrounding the system.

A passenger cabin monitoring system includes infrared cameras disposed in respective passenger rest compartments, a flight attendant information system including at least one display and at least one speaker, and a computing device in communication with the infrared cameras and the flight attendant information system. The computing device is configured to detect a temperature of a portion of passenger rest compartment based on one or more thermal images generated by a respective infrared camera of the passenger rest compartment. The computing device is further configured to compare the temperature of the portion of the passenger rest compartment with a predetermined critical temperature and provide an audible alert and/or a visual alert via the flight attendant information system to indicate a critical status of the passenger rest compartment when the temperature of the portion of the passenger rest compartment is above the predetermined critical temperature.

A lighting arrangement for a passenger cabin of an aircraft having a display surface for image content having at least two surface portions for content portions contains at least two luminaires in a lighting environment of the display surface for light in accordance with at least one lighting parameter, and a control unit in which each luminaire is assigned part of the display surface as evaluation region and a mapping rule, wherein the mapping rule assigns image content of the evaluation region values of the lighting parameters, wherein the control unit, for each of the luminaires, assigns the image content of its evaluation region values of its lighting parameters using the mapping rule and actuates them with the values with regard to the assigned lighting parameters.

A passenger cabin contains the lighting arrangement and the display surface, wherein the luminaires are arranged in the lighting environment.

In a method for actuating the luminaires, the image content is depicted on the display surface, each of the luminaires is assigned its evaluation region and its mapping rule and, for each of the luminaires, the image content of its evaluation region is assigned values of its lighting parameters using the mapping rule, and each of the luminaires is actuated with the values with regard to the assigned lighting parameters.

A video data distributor for distribution of image and video data onboard an aircraft, has a central processing unit, at least one graphics processor coupled to the central processing unit, at least one display unit interface coupled to the graphics processor, a high-speed data transfer interface, and a buffer memory coupled to the central processing unit. An external display unit is connectable to the display unit interface. Via the high-speed data transfer interface, image and video data can be communicated from a network control device to the central processing unit. The buffer memory is designed to buffer-store image and video data received via the high-speed data transfer interface.