Aircraft door an aircraft fitted with such a door

Abstract

The door (10) of an aircraft incorporates a housing (14) able to receive a slide, in a folded up state. The housing (14) is delimited between a cover (16) facing outwards from the door (10) and an intermediate bulkhead (18). The cover (16) is jettisonable outside the aircraft or able to swivel by its lower edge on a threshold of the door, by the use of setting de-setting means. In one embodiment, the housing occupies the greater part of the door surface.

Description

[0001] The invention concerns an aircraft door. More exactly, it concerns a door allowing passengers to access the interior of the aircraft, said door incorporating an emergency evacuation slide.[0002] The invention also concerns an aircraft fitted with at least one door of this type.THE PRIOR ART[0003] On aircraft intended for transporting passengers, the regulations lay down that emergency evacuation slides must be present which are able to allow the rapid evacuation of passengers in the event of an accident.[0004] Emergency evacuation slides are usually constituted by inflatable structures, which are stored in the folded up state, in a location provided for this purpose within the aircraft.[0005] Furthermore, the locations in which the slides are stored are selected in order that, in the event of an accident, the slides are deployed underneath at least some of the exits from the aircraft, able to be opened under accident conditions. These exits may be doors usually used for the l...

AI Technical Summary

Benefits of technology

[0018] This original design makes it possible to provide a very rapid deployment of the slide, whatever its size, which makes the invention particularly adapted to the case of aircraft of very large size, in which the passenger cabin floor is a long way from the ground.

[0023] Furthermore, tightness means are provided, in a usual way, around the door. According to circumstances, these tightness means may be located either approximately in the extension of the intermediate bulkhead, or approximately in the extension of the cover. This latter solution is preferred, since it allows the aerodynamic noises generated by the cavity formed by the door-fuselage interstice to be reduced.

[0024] To advantage, the door also includes a lower stepped edge, comprising a closed inner part and an open outer part, communicating with the volume in which the slide is received and offset downwards relative to the closed inner part, so as to form a step. This arrangement makes it possible to increase slightly the volume available for the slide, without increasing too much the size of the aperture made in the aircraft fuselage.

Problems solved by technology

The particular drawback of this conventional solution is its requirement for the slide to be passed through a slot formed in the bottom of the door, when the latter is opened in an emergency evacuation situation.

The time required for the slide to be deployed therefore increases its volume.

These bulges translate into a loss of room and prevent seats from being placed immediately behind doors designed in this way.

Moreover, in the case of very long slides, the volume taken up by the bulges formed at the bottom of the doors may render the mechanisms usually providing the opening of the doors unusable.

Indeed, the projection serving to house the slide would then interfere with the door frame.

However, it leads to additional apertures being made in the aircraft fuselage, on the same cross-section as the door apertures.

To avoid embrittlement of the aircraft structure at this level, braces have to be provided, which is not without consequence on the mass and the cost of the plane.

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