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.

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.

An economy class cabin with sleeping berths in a passenger aircraft, includes cabin floor, multi-tier sleeping berths, an air duct, an overhead bin, seats, a baggage storage place, a shoe storage place and multi-tier baggage racks. The multi-tier sleeping berths are disposed in parallel to longitudinal axis of the aircraft; a longitudinal partition board is disposed between two abreast sleeping berths; and two latitudinal partition boards are respectively disposed at two opposite ends of each of the sleeping berths and a private space is formed by the longitudinal partition board, two latitudinal partition boards, a bed cushion and a slidable curtain. The present invention has simple structure and reasonable utilization of compact space, enables all or some of passengers of the economy class to be in a lie-flat sleeping state in half of the time in intercontinental flight.

An aircraft cabin includes an upper deck, and a cargo area. The cargo area is configured to accommodate at least one passenger and is situated at a different level than the upper deck. An accessway provides access between the upper deck and the cargo area. The upper deck has, at least locally, a raised floor in the vicinity of the accessway so that at least one part of the cargo area has a ceiling height higher than the ceiling height of the rest of the area cargo.

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.

The invention concerns a modular arrangement intended to accommodate at least one passenger of an aircraft, comprising A modular aircraft passenger accommodation includes at least one module, configured to be arranged in a removable manner in a cargo area of the aircraft. The module communication with an upper deck of the aircraft, and/or a comfort module. The comfort module includes at least one comfort device for improving the comfort of the passenger. The module is configured to be in communication with at least one space outside the module situated in the cargo area.

A three-place aircraft divan configured to be installed side-facing in an aircraft and track between an upright sitting position and a berth position. Seat bottom and backrest portions of the divan are movably supported on a static frame and track together. The divan includes inflatable passenger restraints at each seat place and a leg flail prevention device at one end of the frame triggered to actuate in response to an event sensed by a mechanical crash sensor. The inboard leg arrangement of the divan accommodates the installation of two containers for containing high-capacity life rafts under the seat bottom frame, among other equipment.

Passenger seating arrangements for an airliner or other conveyance including a plurality of individual suites arranged into longitudinal columns. Lateral aisles extending from longitudinal aisles lead to branch aisles that provide access to suites spaced apart from the longitudinal aisles, and each lateral aisle can be shared to provide access to two outboard suites. Suites are arranged to maximize seating density and privacy, and each suite is equipped with premium features and amenities for use by occupants during flight.

The invention relates to a system for remote monitoring of an area intended to accommodate at least one passenger of an aeroplane, notably a cargo area provisionally converted into cabin space, including: at least one control member configured to generate at least one signal relating to the safety of the passenger present in the area, and at least one interface means that is situated at a distance from the area and allows the cabin crew to have access to information relating to the area and/or to the passenger present in the area on the basis of the signal.