Disclosed is a modular seat for aircraft. The system has a frame that is able to be interconnected with other frames laterally. Since each lateral frame has the same pivot points (when viewed from the side), the linked seats rotate together. The seats also include buckle lugs which enable a particular seat to be used on either side of the aircraft.

An aircraft viewing platform system that enables passengers to view the exterior of the aircraft while in flight includes a canopy assembly, a platform assembly supporting at least one seat, and an elevating mechanism to facilitate raising the platform into a volume of the canopy assembly extending through a fuselage cutout beyond the fuselage periphery. The system may include an actuating mechanism such as a jack screw or a telescoping system. The platform can have integrated rollers slide configured to roll in guide rails. The system can include a control panel that regulates the elevating mechanism motion. The control panel allows the viewer to move the platform. The platform can include a rotating pedestal to allow passengers have a 360 degree view of the aircraft exterior.

A sleeping box for installation in an aircraft includes a casing which is suitable for accommodating a person located in a reclining position parallel to a longitudinal axis of the casing and which has an access aperture in the area of a front side which extends perpendicularly to the longitudinal axis of the casing. The sleeping box also includes a fastening apparatus which is configured to fasten the sleeping box within a passenger cabin of the aircraft in such a way that the longitudinal axis of the casing extends perpendicularly to a longitudinal axis of the passenger cabin and the access aperture of the casing borders on an aisle which is present within the passenger cabin.

An aircraft including a cabin inside which a floor is installed, and at least one arranging module which is fixed solely to the floor and which includes a front wall, a rear wall, a port-side wall and a starboard-side wall which are rigidly connected to one another. The port-side and starboard-side walls each have a door, a roof and a deck fixed to each of the front, rear, port-side and starboard-side walls, and a separating system which makes it possible to separate the internal volume of the arranging module into two volumes, each being accessible through one of the doors. Such an aircraft therefore provides an arranging module which is fixed solely to the floor of the cabin, thereby facilitating the set-up thereof.

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.

A sleeping module and a modular sleeping structure with a plurality of sleeping modules. The sleeping modules has a housing which defines a space dimensioned to accommodate a user in at least a lie-flat position, an entrance to permit access to and exit from the space of the housing, an openable closure member provided with the housing to at least partially obstruct the entrance for isolating the space from the surroundings and a holder useful with the openable closure member is provided at the housing to releasably hold the openable closure member in a closed position by way of an attractive force.

An isolation section assembly includes a section housing defining an interior space. The section housing includes a door with access to the interior space. The isolation section assembly includes an enclosure abutting the door. The airlock enclosure defines an interior airlock space. The interior airlock space is configured and adapted to be at a negative pressure relative to a cabin area. An air recirculation system in fluid communication with at least one of the interior space of the section housing or the interior airlock space.

An enclosed patient suite may include a plurality of suite walls, a patient bed positioned in a patient area defined within the plurality of suite walls, a plurality of medical systems with at least some of the plurality of medical systems mounted to the plurality of suite walls, a plurality of support members coupled to the plurality of suite walls, a plurality of wheels with a particular wheel of the plurality of wheels coupled to a corresponding support member of the plurality of support members, a rail brake configured to engage a floor-mounted rail in a floor of at least one of a cargo hold or a cabin of an aircraft, and a controller coupled to the plurality of medical systems and configured to receive data from and transmit data to the plurality of medical systems. The enclosed patient suite may be dimensioned to fit within the aircraft.

The present invention relates to a seat array (100), comprising a first (1) and a second (2) seat, arranged with their backrests opposite one another, said first (1) and second (2) seats being able to move from a sitting position to a lying position, possibly with possibility of stopping at each of the intermediate positions, a portion of dividing wall (respectively 3, 4) being arranged laterally with respect to said seats (1, 2), said portion of dividing wall (3, 4) being provided extending laterally at one side of said first and second seats (1, 2) and ending, on one side, in a portion containing a footrest (5, 6), arranged in front of the respective seat (1, 2), and on the other side at a distance from the respective side of the dividing wall (3, 4) of the seat (2, 1), in such a way as to leave an entry/exit passage (7), and thus access, to the seats (1, 2), said entry/exit passage (7) leading to a lane (respectively 8, 9) for reaching the first (1) or the second (2) seat, said dividing walls (3, 4), on their respective end constituting the entry/exit passage (7) provide, externally, a respective footrest (10, 11), which is positioned in front of a respective third (12) and fourth (13) seats, which are arranged in an opposite direction with respect to the respective seat (1, 2) arranged on the opposite side of the same dividing wall (3, 4), said third (12) and fourth (13) seats also being able to move from a sitting position to a lying position, possibly with possibility of stopping at each of the intermediate positions.

A multifunctional container system for producing a container for a cargo compartment of an aircraft includes a first lateral container component, which forms a first lateral surface of the container that is at least partially beveled, a first lower resting surface having first fastening devices and a first top side, a second lateral container component, which forms a second lateral surface of the container that is at least partially beveled, a second lower resting surface having second fastening devices and a second top side, and a floor cladding. The cladding is selectively positionable between the first resting surface and the second resting surface, which enclose a continuous gap to each other and comprise a predetermined distance to each other and to create a protrusion that faces away from the first and second top side. The protrusion extends into a recess of a floor in a cargo compartment.