Abstract: 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.

Abstract: A system and method. The system may include a monitor implemented as a virtual window, a camera, and a pivot motor. The pivot motor may be configured to change an orientation of a field of view of the camera relative to a vehicle based on a position of a passenger.

Abstract: An aircraft suite may include a passenger compartment disposed on a main deck of an aircraft. The passenger compartment may be partitioned from a main passenger cabin of the main deck by at least one bulkhead. The passenger compartment may include an aircraft seat and a hatch set within an opening in a floor of the passenger compartment. The aircraft suite may include a lower lobe rest compartment integrated in a cargo deck below the main deck. The lower lobe rest compartment may be proximate to the passenger compartment. The lower lobe rest compartment may include a passenger rest compartment and a device proximate to the hatch. The device may be configured to assist a passenger to at least one of descend into the lower lobe rest compartment from the passenger compartment, or ascend into the passenger compartment from the lower lobe rest compartment, via the hatch.

Abstract: A bi-directional entry vestibule for a passenger aircraft provides passenger access to overhead rest cabins and lower-lobe rest cabins (e.g., on a lower cargo deck) via separate enclosed chambers incorporating ascending and descending staircases respectively. The ascent and descent chambers may be accessed from the main passenger cabin via access doors (one door or separate doors); the ascending and descending access doors may be on opposing sides of the aircraft (e.g., accessible from port-side and starboard-side aisles) or adjacent to each other and accessible via the same aisle. The ascent chamber may include a further transitional space transitioning into an overhead corridor-based cabin, the transitional space including a crew station comprising a fold-down jump seat, communications equipment, and emergency supply storage.

Abstract: 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).

Abstract: 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.

Abstract: 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).

Abstract: An aircraft suite may include a passenger compartment disposed on a main deck of an aircraft. The passenger compartment may be partitioned from a main passenger cabin of the main deck by at least one bulkhead. The passenger compartment may include an aircraft seat and a hatch set within an opening in a floor of the passenger compartment. The aircraft suite may include a lower lobe rest compartment integrated in a cargo deck below the main deck. The lower lobe rest compartment may be proximate to the passenger compartment. The lower lobe rest compartment may include a passenger rest compartment and a device proximate to the hatch. The device may be configured to assist a passenger to at least one of descend into the lower lobe rest compartment from the passenger compartment, or ascend into the passenger compartment from the lower lobe rest compartment, via the hatch.

Abstract: A bi-directional entry vestibule for a passenger aircraft provides passenger access to overhead rest cabins and lower-lobe rest cabins (e.g., on a lower cargo deck) via separate enclosed chambers incorporating ascending and descending staircases respectively. The ascent and descent chambers may be accessed from the main passenger cabin via access doors (one door or separate doors); the ascending and descending access doors may be on opposing sides of the aircraft (e.g., accessible from port-side and starboard-side aisles) or adjacent to each other and accessible via the same aisle. The ascent chamber may include a further transitional space transitioning into an overhead corridor-based cabin, the transitional space including a crew station comprising a fold-down jump seat, communications equipment, and emergency supply storage.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: A system and method. The system may include a monitor implemented as a virtual window, a camera, an additional camera, a processor, and a switch. The processor may be configured to: receive video from the additional camera; manipulate the video from the additional camera based on a position of the passenger to provide an additional camera manipulated video stream; and output the additional camera manipulated video stream. The switch may be configured to: when the passenger is in a first position, feed video from the camera to the monitor; and when the passenger is in a second position, feed the additional camera manipulated video stream to the monitor.

Abstract: A system. The system may include at least one monitor mounted on a wall panel. The wall panel may be within an interior of an aircraft. Each of the at least one monitor may be configured to mimic an aircraft window. Each of the at least one monitor may include a shade feature.

Abstract: A system and method. The system may include a monitor implemented as a virtual window, a camera, and a pivot motor. The pivot motor may be configured to change an orientation of a field of view of the camera relative to a vehicle based on a position of a passenger.

Abstract: A system and method. The system may include a monitor implemented as a virtual window, a camera, an additional camera, a processor, and a switch. The processor may be configured to: receive video from the additional camera; manipulate the video from the additional camera based on a position of the passenger to provide an additional camera manipulated video stream; and output the additional camera manipulated video stream. The switch may be configured to: when the passenger is in a first position, feed video from the camera to the monitor; and when the passenger is in a second position, feed the additional camera manipulated video stream to the monitor.

Abstract: 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.

Abstract: In one aspect, the present disclosure relates to video system and methods for emulating a view through an aircraft window to a passenger in an interior passenger suite. The view may be emulated by determining a perspective view of the seated passenger relative to each monitor of at least one monitor mounted to a side wall of the interior passenger suite, and capturing video data of scenery exterior to the aircraft at the perspective view(s) for display on the monitor(s).

Abstract: An apparatus adapted to provide visual attitude reference to occupants seated in an inboard area of a cabin of a vehicle, that includes at least one interior partition positioned in the cabin in proximity to the occupants and at least one video camera mounted on the vehicle for capturing an electronic image of an environment exterior to the vehicle. At least one video monitor is adapted to serve as a virtual window mounted on the at least one interior partition in a substantially vertical and substantially parallel direction relative to a direction of forward travel of the vehicle in viewing proximity to the occupant, and further adapted to receive the electronic image from the at least one video camera and provide to the occupant an image of the environment external to the vehicle to the occupant.