An aircraft for the transport of cargo and/or passengers, comprising a fuselage extending in longitudinal direction and having an upper deck, in particular main deck, and a lower deck separated from each other by a floor, wherein the fuselage comprises a barrel section with a cross-sectional profile for accommodating cargo and/or passengers, wherein the cross-sectional profile is essentially formed by several, in particular four, circular arc sections, which have radii (R1, R2, R3) with centers (M1, M2, M3′, M3″) differing from one another, so that the cross-sectional profile is designed in such a way that cargo items with different size dimensions, in particular cargo containers with different height and width dimensions, can be accommodated in the upper deck and the lower deck.

A cabin lining element for an aircraft cabin which is arranged in the interior of an aircraft fuselage structure, having a fuselage structure side and a cabin side. The cabin lining element comprises an electrically contactable heating lacquer layer at least in regions on its fuselage structure side. A rib is provided for an aircraft fuselage structure, having at least one foot portion on the outer skin facing side and a cabin facing side head portion. The rib comprises an electrically contactable heating lacquer layer at least in regions on a side of the head portion facing the cabin. As a result of the heating lacquer layer, it is possible to omit insulation which otherwise surrounds the rib heads and, as a consequence, to enlarge the width of the cabin.

A modular faucet system for an aircraft comprising a faucet outlet, a flow valve, and an actuator. The faucet outlet is configured to be installed on the aircraft. The flow valve is configured to be installed on the aircraft separately from the faucet outlet, to be connected by a first water line to a water supply comprising a water tank on the aircraft, and to be connected by a second water line to the faucet outlet. The actuator is configured to be installed on the aircraft separately from the faucet outlet and the flow valve. The actuator comprises a touchless sensor that is configured to detect a user of the modular faucet system. The actuator is configured to generate a control signal to open the flow valve to provide water from the water supply to the faucet outlet in response to detection of the user by the touchless sensor.

The present invention achieves technical advantages as an aircraft having an augmented reality flight control system integrated with and operable from the pilot seat and an associated pilot headgear unit, wherein the flight control system is supplemented by flight-assisting artificial intelligence and geo-location systems. The present invention includes an augmented reality flight control system incorporating real-world objects with virtual elements to provide relevant data to a pilot during aircraft flight. A translucent substrate is disposed in the pilot's field of view such that the pilot can see therethrough, and observe virtual elements displayed on the substrate. The system includes a headgear that is worn by the pilot. A flight assistance module is configured to receive data related to the aircraft and provide predictive assistance to the pilot during flight based on the received data based in part on a pilot profile having preferences related to the pilot.

A system for operating a configuration platform. The system comprising a conversion pipeline, the conversion pipeline allowing converting a first set of data associated with a computer-aided design (CAD) system into polygon meshes suitable for rendering of the portion of a monument and configuration data. The system also comprising a content management system, the content management system storing the polygon meshes and the configuration data; and a 3D real-time engine, the 3D real-time engine allowing to determine, based on the configuration data, at least one of the positioning of the monument, the material surface associated with the monument, the material grain direction associated with the monument, the lighting associated with the monument, the annotations associated with the monument, the alternate states associated with the monument and the kinematic sequence associated with the monument; and to render the portion of the monument by the 3D real-time engine.

A method for configuring an interior of a reconfigurable vehicle using one or more cabin modules. The method comprises providing, by a user interface system, a plurality of possible cabin configuration options to a plurality of users for selection by the plurality of users so as to generate selection data indicative of cabin configuration options selected by the users. The cabin configuration options relate to types of configuration of the one or more cabin modules. The method comprises determining an availability of cabin configuration options based on inventory data which relates to types of configuration of cabin modules that are currently available for use so as to generate availability data, and generating a forecast of cabin modules predicted to be loaded on the reconfigurable vehicle based on the selection data and the availability data. The method further comprises updating the availability data and the selection data substantially in real time based on the inventory data and user input to the user interface system so as to generate updated availability data and updated selection data, and modifying the forecast based on the updated availability data and the updated selection data. The method comprises finalizing the forecast so as to generate commissioning data indicative of cabin modules to be loaded on the reconfigurable vehicle, loading the reconfigurable vehicle with one or more cabin modules based on the commissioning data, and updating the inventory data based on the cabin modules that are loaded on the reconfigurable vehicle.

A cabin module deployable inside a vehicle so as to form at least a portion of an interior of the vehicle. The cabin module comprises a main body and a plurality of external walls. One or more of the plurality of external walls are moveable with respect to the main body. The module has a closed configuration for storage outside the vehicle, in which the plurality of external walls define at least a part of a first form factor of the module. The module has an open configuration for operational deployment in the vehicle, in which the plurality of external walls define at least a part of a second form factor of the module. The cabin module is reversibly changeable between the closed configuration and the open configuration by movement of the one or more external walls. The first form factor is different from the second form factor.

In an example, an overhead payload module is described. The overhead payload module comprises a ceiling assembly, an aisle floor assembly, a first payload assembly attached to the ceiling assembly and the aisle floor assembly to form a first side of the overhead payload module, and a second payload assembly attached to the ceiling assembly and the aisle floor assembly to form a second side of the overhead payload module. The first payload assembly comprises a first payload module and a first overhead stowbin module structurally integrated with the first payload module and having a first stowage area configured to receive stowbins. The second payload assembly is positioned opposite the first payload assembly to form an aisle therebetween and comprises a second payload module and a second overhead stowbin module structurally integrated with the second payload module and having a second stowage area configured to receive stowbins.

A floor arrangement for a cabin of a vehicle, in particular of an aircraft or spacecraft, comprises a carrier plate formed with a multiplicity of first fastening perforations and a multiplicity of reinforcing notches. The first fastening perforations are arranged one behind another in fastening rows at a uniform longitudinal distance. The fastening rows are oriented parallel at a uniform transverse distance from one another at an angle of orientation of 45 with respect to a longitudinal direction of the floor arrangement. The reinforcing notches run along the angle of orientation in a manner offset with respect to the fastening rows. A floor panel is formed with a multiplicity of second fastening perforations and is arranged above the carrier plate such that the second fastening perforations are arranged above the first fastening perforations to fasten cabin elements through the floor panel to the carrier plate.

A monument arrangement for a cabin of a vehicle has a first monument, with a washroom formed therein, a second monument and an aisle. The first and second monuments enclose the aisle, wherein an access opening to the washroom is directed toward a side wall of the second monument and is adjacent to the aisle. The distance between the access opening and the relevant side wall of the second monument is at most 1 m, and the side wall of the second monument has a first, rigid side wall portion and at least one second side-wall portion, which is mounted on the first side wall portion such that it can be pivoted about a vertical axis and which can be pivoted from a neutral position, running in the direction toward the first side wall portion, into an angled position, directed away from the first monument and the aisle.