An aircraft cabin comprising a credenza and a lounge chair disposed above the credenza is disclosed. The lounge chair is adjustable between a first configuration defining a first seating arrangement and a second configuration defining a second seating arrangement. Also disclosed is a mechanism to facilitate the adjustment of the lounge chair.

The present invention generally relates to bed structures having an inflatable and/or collapsible/deflatable component. More particularly, it relates to bed construction configurations that can include multiple adaptations for enhanced safety in situations of rapid loss of aircraft cabin pressure to meet airflow requirements for emergency decompression events as well as to provide overall better airflow for in-cabin air filtration systems. The bed configurations can include cross-welded structures and bowing-prevention stabilizers to control bulging of the bed when inflated.

An adjustable bed assembly for a vehicle includes a contoured bed frame, a foundation disposed in the bed frame and coupled to an articulated frame having a support platform with a plurality of sectional support members. A linkage mechanism couples the support platform to the foundation and a drive mechanism operably coupled to the linkage assembly adjusts the position of at least one sectional support member. A mattress is disposed on the support platform and configured to conform with the plurality of sectional support members. A monitor mounted on the bed frame is movable between a retracted position and an extended position. A control device has a first preset for concurrently adjusting the articulated frame and moving the monitor.

A seat array that includes a first and a second seat arranged with their backrests opposite one another, seats being able to move from a sitting position to a lying position, a portion of a dividing wall being arranged laterally with respect to the seats, the portion of dividing wall being provided in such a way as to leave an entry/exit passage, and thus access, to the seats, the entry/exit passage leading to a lane for reaching the first or the second seat, the dividing walls, on their respective end constituting the entry/exit passage provide, externally, a respective footrest, which is positioned in front of a respective third and fourth seats, which are arranged in an opposite direction with respect to the respective seat arranged on the opposite side of the same dividing wall.

An aircraft cabin comprising a credenza and a lounge chair disposed above the credenza is disclosed. The lounge chair is adjustable between a first configuration defining a first seating arrangement and a second configuration defining a second seating arrangement. Also disclosed is a mechanism to facilitate the adjustment of the lounge chair.

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.

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.

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).

In a cargo hold module for an aircraft, in particular a passenger aircraft, with exterior dimensions that are adjusted to a respective cargo hold of the aircraft, and suitable for securing the cargo hold module in a predetermined position in a cargo hold of the aircraft, the cargo hold module has an accessway, via which it can be accessed from a cabin of the aircraft. The cargo hold module can be hooked up to onboard electrical systems of the aircraft for power, water and/or air supply. The cargo hold module has a massage facility with at least one massage table for treating passengers or crew.