Aircraft
An aircraft capable of hovering, and having a fuselage in turn having a nose, a tail portion at the opposite end to the nose, and a cabin interposed between the nose and the tail portion; the cabin has a loading opening at the opposite end to the nose, and a first wall movable between a closed position engaging at least one portion of the loading opening, and an open position allowing free access to the portion of the loading opening; and, working from the tail portion towards the nose, the first wall in the open position extends on the opposite side of a first edge of the loading opening with respect to a second edge, opposite the first edge, of the loading opening.
1. An aircraft capable of hovering, and comprising:
a fuselage in turn comprising a nose, a tail portion at the opposite end to said nose, and a cabin interposed between said nose and said tail portion; said cabin comprising a rear loading opening interposed between said nose and said tail portion, defining the cabin on the opposite side to the nose and delimited by a bottom edge and a top edge, opposite said bottom edge; and
at least a first wall movable between a closed position engaging at least one portion of said loading opening, and an open position allowing free access to said portion of said loading opening;
characterized in that, proceeding from the tail portion towards the nose, said first wall in said open position extends on the opposite side of said bottom edge of said loading opening with respect to said top edge, and is interposed between the nose and said bottom edge.
2. An aircraft as claimed in claim 1 , characterized in that, in said open position, said first wall at least partly faces a surface of said fuselage bounding the outside of said cabin and defining said bottom edge.
3. An aircraft as claimed in claim 1 , characterized in that said first wall slides with respect to said bottom edge between said closed and open positions.
4. An aircraft as claimed in claim 1 , characterized in that said bottom and top edge define said loading opening on the side facing said nose and on the side facing said tail portion respectively.
5. An aircraft as claimed in claim 2 , characterized in that said first wall comprises a curved convex first face facing outwards of said cabin; and in that said surface is convex; the curvatures of said first face and said surface matching at all points.
6. An aircraft as claimed in claim 5 , characterized in that said first wall comprises a curved, concave second face opposite said first face and facing said cabin; the concavity of said second face housing at least part of said surface.
7. An aircraft as claimed in claim 2 , characterized by comprising guide means fitted to said surface and for guiding said first wall.
8. An aircraft as claimed in claim 1 , characterized by comprising a second wall movable, with respect to said top edge, between a further closed position engaging a further portion of said loading opening, and a further open position, in which it allows free access to said further portion of said loading opening, and is housed inside said cabin.
9. An aircraft as claimed in claim 8 , characterized in that said second wall is hinged to a supporting beam of said tail portion of the aircraft.
10. An aircraft as claimed in claim 1 , characterized by comprising an access opening to said cabin, defined by a side of said fuselage alongside said loading opening.
11. An aircraft as claimed in claim 1 , characterized in that said fuselage comprises a main portion interposed between said nose and said tail portion; said main portion comprising a first region which supports said cabin and defines said surface, and a second region which is interposed between said first region and said tail portion, slopes with respect to the first region, and defines said loading opening.
12. An aircraft as claimed in claim 1 , characterized by being a helicopter.
13. An aircraft as claimed in claim 1 , characterized by being a convertiplane.