Abstract: This adjustable partitioning mechanism for an aircraft comprises a more or less straight upper rod (34) of variable length and assumed to be horizontal. The rod (34) comprises at its ends connection means allowing the rod (34) to pivot around a vertical axis. The mechanism further comprises a curtain (36) having attachment means intended to cooperate with complementary attachment means mounted on the rod (34). The invention also relates to an aircraft equipped with at least one such partitioning mechanism.

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: A front portion of a fuselage of an aircraft including a cockpit, a washroom, an access corridor to the cockpit alongside the washroom, and a rest compartment with at least one berth for at least one pilot. The corridor alongside the washroom includes a mechanism separating the corridor from the cockpit and a door for blocking access to the passenger cabin. The rest compartment can be accessed from the access corridor to the cockpit, between the separation mechanism between the corridor and the cockpit and the corridor door. The washroom includes two access doors, a first access door for accessing the washroom from the access corridor to the cockpit in the area located between the separation mechanism between the corridor and the cockpit and the corridor door, and a second access door for accessing the washroom from the passenger cabin.

Abstract: An aircraft fuselage including a front part including a cockpit, a central part, and a rear part. The central part of the fuselage includes a first zone located at the front part and that increases in width to a maximum width towards the rear of the aircraft, a second zone that decreases in width, and a third zone that has an essentially constant width and is located behind the second zone, width begin measured along the pitch axis.

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.