Abstract: An aircraft with an electric propulsion arrangement which includes a fuselage, a wing system attached to the fuselage, and a tail unit attached to a rear part of the fuselage. The electric propulsion arrangement is arranged on each side of the fuselage, an electrical energy generator and electricity storage and supply devices are arranged substantially along a longitudinal axis of symmetry of the fuselage. The aircraft thus incorporates a hybrid motorization.

Abstract: A medical block associated with a couchette for a patient to lie on. The block includes: a water supply; a power supply; a stop region for at least one trolley; at least one trolley located in the stop region and including drawers containing medical equipment; and an access flap corresponding to each trolley, provided with a locking mechanism and enabling the drawers of the trolley to be accessed.

Abstract: An aircraft including a fuselage, a cockpit and a cabin, wherein the cockpit is situated below the cabin and outside the nose, such as a lancet-shaped nose, of the aircraft and may extend to a front end of the aircraft, and the viewing surfaces in the cockpit may be entirely formed of digital display screens.

Abstract: An armrest for arrangement between two seats, especially two passenger seats of a vehicle such as an aircraft is provided, having at least one first support portion for an arm of a first person and at least one second support portion for an arm of a second person wherein the first and second support portions provide different height levels.

Abstract: The invention concerns an aircraft cockpit comprising at least one instrument panel (4) and a seat (2) for a pilot characterized in that the instrument panel forms a single unit and is carried by a hinged support (6) enabling the pilot to adjust the position of the instrument panel (4) relative to the pilot seat (2). Preferably, the instrument panel forms a single unit and is curved, for example along the arc of a circle, around the pilot seat.

Abstract: The invention concerns an aircraft including a cockpit comprising a viewing surface for piloting giving at least one pilot a view of an outside scene comprising the environment of the aircraft extending forward of the aircraft. At least part of said viewing surface for piloting is free of any glazed surface and is formed by display means for a digital image representing at least part of an outside scene comprising the environment of the aircraft extending forward of the aircraft.

Abstract: A device for stowage of carts including: a first compartment configured to receive carts lined up side by side; a second compartment configured to receive carts lined up side by side, including an aperture allowing cart entry and exit and arranged above the first compartment; a substantially horizontal platform capable of moving in a vertical direction between a lower position in which it is substantially at floor level and a higher position in which it is substantially level with a lower, substantially horizontal wall of the second compartment and facing the opening thereof; and a mechanism arranged in the second compartment for motorized transfer of at least one cart from the second compartment to the platform and vice versa.

Abstract: A layout for a cabin in a passenger transport vehicle, that includes at least one longitudinal aisle and seats for passengers arranged in rows, each accessible by a longitudinal aisle. At least one row of at least two seats is arranged so as to be inclined relative to a longitudinal aisle. The seats of the row are arranged side by side and oriented perpendicularly to the row and to the aisle enabling access to the row.

Abstract: A module for an aircraft has a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane.

Abstract: A seat arrangement for a passenger compartment of a vehicle, the passenger compartment having a floor and concave side walls. The seat arrangement has a plurality of seats arranged in at least one seat row with at least one gap to form an aisle between at least two of these seats wherein an armrest is arranged both on the left-hand side and on the right-hand side of each seat with an end armrest arranged on each of the both ends of the seat row. The width of the at least one seat row with the end armrests is larger than the width of the at least one seat row with the end armrest, and/or at least the end armrests and/or at least the end seats are arranged in a higher height level when compared with a middle armrest or a middle seat, respectively.

Abstract: An armrest for arrangement between two seats, especially two passenger seats of a vehicle such as an aircraft is provided, having at least one first support portion for an arm of a first person and at least one second support portion for an arm of a second person wherein the first and second support portions provide different height levels.

Abstract: A module for an aircraft having a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane. The frame device is adapted for attachment to the fuselage structure of the aircraft at a second location, wherein the second location is not in the floor plane.

Abstract: A collapsible staircase is provided with a set of flat parts, with each of the parts intended to function as steps. Each flat part can be moved between a first position and a second position. All of the flat parts are substantially coplanar when the parts are in the first position, and the parts are disposed above each other and at a distance from each other when the parts are in the second position. A retractable holding handle is also provided and driven together with the flat parts.

Abstract: An aircraft with an electric propulsion arrangement which includes a fuselage, a wing system attached to the fuselage, and a tail unit attached to a rear part of the fuselage. The electric propulsion arrangement is arranged on each side of the fuselage, an electrical energy generator and electricity storage and supply devices are arranged substantially along a longitudinal axis of symmetry of the fuselage. The aircraft thus incorporates a hybrid motorization.

Abstract: The invention concerns an aircraft comprising a cockpit situated outside the nose of the aircraft. The cockpit is situated in a lower part of a fin, the latter advantageously extending to a front end of the aircraft. Preferably, the aircraft has a lancet-shaped nose.

Abstract: The invention concerns an aircraft cockpit comprising at least one instrument panel (4) and a seat (2) for a pilot characterized in that the instrument panel forms a single unit and is carried by a hinged support (6) enabling the pilot to adjust the position of the instrument panel (4) relative to the pilot seat (2). Preferably, the instrument panel forms a single unit and is curved, for example along the arc of a circle, around the pilot seat.

Abstract: The invention concerns an aircraft including a cockpit comprising a viewing surface for piloting giving at least one pilot a view of an outside scene comprising the environment of the aircraft extending forward of the aircraft. At least part of said viewing surface for piloting is free of any glazed surface and is formed by display means for a digital image representing at least part of an outside scene comprising the environment of the aircraft extending forward of the aircraft.