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: 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 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 module for aircraft passenger(s) is provided with two seats disposed beside one another and oriented in the same direction, each of these seats being a seat that can be converted to a berth. The module also includes a side wall surrounding the two seats, at least partly, an opening provided in the side wall to permit access to the module, and a partition intended to achieve separation between the two seats. The partition is displaceable from a first position, in which it achieves separation of the two seats, to a second stored position, in which it does not form a barrier between the two seats.

Abstract: This door is intended for a compartment, such as an aircraft baggage compartment. The door can be moved between a first position, in which it closes an opening of the compartment, and a second position, in which the opening is accessible. This door is provided with a guide system on both sides of the opening of the compartment to guide the door in a substantially vertical translational movement.

Abstract: An aircraft cabin segment includes at least one longitudinally extending aisle, seats disposed in rows, at least two assemblies of baggage compartments, and ventilation outlets. The seats disposed in rows are transversal relative to the longitudinal aisle. The at least two assemblies of baggage compartments are aligned and positioned overhead. The baggage compartments of each of the two assemblies are aligned in a transversal direction and are positioned above the seats such that bottom surfaces of the baggage compartments form a sinusoidal wave along a longitudinal direction of the aircraft cabin segment. The ventilation outlets are disposed between the two assemblies of the baggage compartments.

Abstract: An aircraft cabin includes a longitudinal cabin wall, seats, transversal accesses, and at least one storage space. The seats are disposed in rows that are transversal relative to a longitudinal aisle. The transversal accesses permit access to the seats of the transversal rows closest to the cabin wall. At least one storage space is disposed in an immediate proximity of the longitudinal cabin wall and at a dead end of one of the transversal accesses. The dead end of the one of the transversal accesses is not entered by passengers of the aircraft cabin.

Abstract: The invention relates to a medical block associated with a couchette (2) for a patient to lie on, said block comprising: a water supply; a power supply; a stop region for at least one trolley (12); at least one trolley (12) located in the stop region and comprising drawers containing medical equipment; and an access flap corresponding to each trolley (12), provided with locking means and enabling the drawers of the trolley to be accessed.

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 seat for an aircraft includes a seating surface, a backrest and two armrests. The seat also includes a mechanism for guiding at least one of the armrests in translation in an essentially-vertical direction.

Abstract: A seat for a vehicle includes a sitting portion, a movable back; and a first guide mechanism configured to move the back from a first edge of the sitting portion to an opposite second edge of the sitting portion. The back is assembled on the sitting portion by a movable element including a base configured to move between the first edge of the sitting portion and the opposite second edge, and a support assembled pivoting on the movable base. The movable base is in a form of a stirrup, a base of the stirrup extending from a first lateral edge to a second latent edge of the sitting portion. Each branch of the stirrup extends substantially parallel to the first lateral edge and is curved at a free end under the sitting portion.

Abstract: An aircraft fuselage includes an outer skin and at least one main deck separating an interior space of the aircraft fuselage longitudinally into a first space and a second space. At least one portion of the first space is divided into at least three longitudinal zones, and the at least three longitudinal zones include at least one central zone and at least two lateral zones. The at least one central zone is divided into three sectors, and the three sectors include a front sector, a central sector, and a rear sector. The at least two lateral zones include a first and second lateral zone configuration, the front sector includes a first and second front sector configuration, the central sector includes a first and second central sector configuration, and the rear sector includes a first and second rear sector configuration.

Abstract: This layout shows a set or assembly of aircraft seats to outfit an aircraft cabin, comprising at least two columns of neighboring seats. The seats are arranged one behind the other in each of the columns of seats. Moreover, each seat can be converted into a sleeper so as to present a considerably stretched out sleeping surface. Each seat when converted into a sleeper, has a first sleeping portion and at least a second sleeping portion that is narrower than the first. In two neighboring columns, the seats are staggered, in such a way that the first part of a seat of a column is facing a second portion of a seat of the second column that is narrower in width.

Abstract: A convertible seat to accommodate an aircraft passenger. The seat includes a frame, a sitting portion borne by the frame, a back, and a jointed footrest along the transverse edge of the sitting portion. The seat can change from a so-called seated position in which the back forms an angle with the sitting portion and its base is close to the rear transverse edge of the sitting portion to a so-called lying-down position in which it has a more or less level surface intended to accommodate a passenger in the lying down position. The frame is a fixed frame. At most two of the elements of the whole constituted by the sitting portion, the back, and the footrest form the more or less level surface of the seat in lying-down position. At least one additional berth is provided to cooperate with the sitting portion and/or the back and/or the footrest to form the more or less level surface intended to accommodate a passenger in the lying-down position.

Abstract: An aircraft cabin that includes a main structure being the structure of the aircraft and enclosing the cabin; a bridge forming a flat surface on which the seats are secured; an aisle extending longitudinally in cabin and elevated with respect to bridge, and beds or cots accessed by said aisle and arranged above seats of bridge, transversally with respect to aisle and on both sides of such aisle.

Abstract: The invention relates to a seat which is intended for an aircraft and which comprises a seating surface (2), a backrest (4) and two armrests (8). The inventive seat also comprises means for guiding at least one of the armrests (8) in translation in an essentially-vertical direction.

Abstract: This module (8) for aircraft passenger(s) is provided with: two seats (10) disposed beside one another and oriented in the same direction, each of these seats (10) being a seat that can be converted to a berth, a side wall (14) surrounding the two seats (10), at least partly, an opening (16) provided in the side wall (14) to permit access to the module (8), and a partition (18) intended to achieve separation between the two seats (10), this partition (18) being displaceable from a first position, in which it achieves separation of the two seats (10), to a second stored position, in which it does not form a barrier between the two seats (10).

Abstract: A process for adjusting the interior space of a vehicle and a seat for implementation of the process. The process makes it possible to adjust the interior space of a vehicle including seats each having a sitting portion and a back. The process includes, for at least one seat, moving the back of the seat from a first position in which a lower edge of the back is facing a first transverse edge of the sitting portion to a second position in which the lower edge of the back is facing a second transverse edge opposite the first transverse edge. A seat implements the process. Such a process and seat may find application to the interior layout of aircraft.

Abstract: An aircraft cabin according to the invention is provided with: a longitudinal cabin wall (2), seats (8) disposed in rows that are transversal relative to a longitudinal aisle (18), transversal accesses (20) permitting access to the seats (8) of the transversal rows closest to the cabin wall (2), and at least one storage space (24) disposed in the immediate proximity of the longitudinal cabin wall (2) and at the dead end of a transversal access (20).