Abstract: A door for aircraft is capable of blocking an aperture made in the aircraft. A framing of the door is connected to the fuselage by hinging means. The framing is mounted rotationally on the hinging means. The door is capable of taking two opposite stable positions, by 180° rotation about hinging means. The door comprises means to lock the framing in either of the stable positions. A first face of the framing is fitted with an observation dome, a second face comprising an access hole to the dome.

Abstract: A door for aircraft is capable of blocking an aperture made in the aircraft. A framing of the door is connected to the fuselage by hinging means. The framing is mounted rotationally on the hinging means. The door is capable of taking two opposite stable positions, by 180° rotation about hinging means. The door comprises means to lock the framing in either of the stable positions. A first face of the framing is fitted with an observation dome, a second face comprising an access hole to the dome.

Abstract: The present invention concerns an emergency opening control device for an aircraft door comprising: at least one triggering mechanism (10) for emergency opening, at least one door actuator (8), and means of power supply (14, 16) to the actuator driven by the triggering mechanism. The device also comprises means (20) for modification of the output delivered by the means of power supply to the actuator, to allow the door to be opened more slowly in an initial phase of opening and more rapidly in at least one subsequent opening phase.

Abstract: Fast evacuation device for an aircraft. An inflatable slide (18) is placed in a housing (20) close to an access door (16) to a cabin (14) of an aircraft. More precisely, the housing (20) is located in a pressurised area of the aircraft but outside the wall delimiting the cabin (14). Thus, there is no constraint for delimiting the housing (20) on the inside of the aircraft. On the outside, the housing (20) is closed by a hatch (24) capable of resisting the pressure. A lock (30) normally keeps the hatch (24) fixed in the closed position. A mechanism (32) connects this lock (30) to the door (16) when the slide arming system (33) is armed. Opening the door (16) then unlocks the hatch (24) that is then opened due to inflation of the slide (18).

Abstract: The present invention concerns an emergency opening control device for an aircraft door to allow the door to be opened more slowly in an initial phase of opening and more rapidly in at least one subsequent opening phase.

Abstract: The present invention concerns an emergency opening control device for an aircraft door comprising:

Abstract: The present invention concerns an emergency opening control device for an aircraft door comprising :

Abstract: Fast evacuation device for an aircraft.