摘要:
The invention relates to a front portion of the fuselage of an aircraft including a cockpit (2), a washroom (6) and an access corridor (8) to the cockpit alongside the washroom (6). It further comprises a rest compartment with at least one berth (36) for at least one pilot. The corridor (8) alongside the washroom (6) includes means (26) for separating the corridor (8) from the cockpit (2) and a door (24) for blocking access to the passenger cabin. The rest compartment can be accessed from the access corridor (8) to the cockpit (2), between the separation means (26) between the corridor (8) and the cockpit (2) and said corridor door (24). Finally, the washroom (6) includes two access doors, i.e. a first access door (20) for accessing the washroom (6) from the access corridor (8) to the cockpit (2) in the area located between the separation means (26) between the corridor (8) and the cockpit (2) and said corridor door (24), and a second access door (229) for accessing the washroom (6) from the passenger cabin.
摘要:
The present invention relates to a module for an aircraft. The aircraft having a fuselage structure (6) and a floor element (5).The floor element (5) defining a floor plane. The module comprises a frame device (2), wherein the frame device (2) is adapted for mounting a functional element (4) and wherein the frame device (2) is adapted for attachment to the floor element (5) of the aircraft at a first location in the floor plane (7). The frame device (2) is adapted for attachment to the fuselage structure (6) of the aircraft at a second location (7'), wherein the second location is not in the floor plane.
摘要:
The invention relates to an aircraft fuselage comprising a front part (2) with a cockpit, a central part (4) and a rear part (6). The central part of the fuselage includes a first zone (10) which is located at the front part and which increases in width to a maximum width towards the rear of the aircraft, a second zone (12) that decreases in width, and a third zone (14) which has an essentially constant width and which is located behind the second zone (12), width being measured along the pitch axis.
摘要:
The invention relates to an aircraft fuselage comprising a front part (2) with a cockpit, a central part (4) and a rear part (6). The central part of the fuselage includes a first zone (10) which is located at the front part and which increases in width to a maximum width towards the rear of the aircraft, a second zone (12) that decreases in width, and a third zone (14) which has an essentially constant width and which is located behind the second zone (12), width being measured along the pitch axis.
摘要:
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.
摘要:
The invention relates to an internal layout for an aircraft cabin, comprising an assembly (18) of aircraft seats. Each seat assembly comprises two rows of seats (8) which are disposed transversely in relation to the longitudinal axis (2) of the cabin, and a single longitudinal aisle (16) provides access to said transverse rows. The two transverse rows are disposed opposite one another and are separated by means of a transverse passageway (20). In each row of seats, at least one seat (8) is disposed on one side of the longitudinal aisle (16) and at least two seats (8) are disposed on the other side of said longitudinal aisle (16).