The present invention relates to a lavatory unit disposed in a passenger cabin of an aircraft.
A lavatory unit disposed in a passenger cabin of an aircraft has a structure where a bottom surface having a planar shape is surrounded by rectangular box-shaped panels. A lavatory unit disposed at a center area of the passenger cabin has a housing formed of flat panels, but a lavatory unit disposed at a window side of the passenger cabin has a panel disposed on the window side formed in the shape of a curved surface matching a side wall shape of a body of the aircraft.
[PTL 1] Japanese Unexamined Patent Application Publication No. 2002-154489
[PTL 2] Japanese Unexamined Patent Application Publication No. 2004-203167
In order to arrange a greater number of seats within the passenger cabin and improve efficiency, a floor space that the lavatory unit occupies must be downsized.
A lavatory unit 1 includes a main body 15 formed of a lightweight panel with a honeycomb structure. A door is provided on a front side of the drawing, and a toilet unit 10 is installed on a depth side. A sink, i.e., wash basin, 20 is attached to a side wall on an inner side of the main body 15. A space S1 is required for the user to use the sink 20.
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The object of the present invention is to provide a lavatory unit of an aircraft capable of reducing a width dimension of the lavatory unit while ensuring usability, which is effective in increasing the number of passenger seats.
In order to achieve the above-described objects, the lavatory unit provided in a passenger cabin of an aircraft includes, as basic means, a box-shaped main body formed of panels and having a bottom surface with a rectangular shape having short sides and long sides, a door provided on one of the short sides of the main body, a toilet unit provided on the other one of the short sides opposed to the door, and a foldable sink provided on an upper portion of the toilet unit.
Further, the main body of the lavatory unit is characterized in that it has the short sides of the bottom surface arranged in parallel with an axis of the aircraft.
The lavatory unit according to the present invention having the configuration illustrated above does not require any space for installing a sink on the side wall, so that a dimension of the lavatory unit in the axial direction of the body of the aircraft can be reduced. Therefore, the number of seats arranged in the passenger cabin can be increased, and the operating efficiency can be improved.
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The toilet unit 110 is disposed at a depth side of the main body 105 opposed to the door. A foldable sink 200 is attached to an upper portion of the toilet unit 110. FIG. 1 shows the foldable sink 200 in the opened state, and the passenger can use the sink in this state.
The main body 105 of the lavatory unit 100 has a rectangular shape with the planar shape of the bottom surface formed of short sides with a width dimension W2 and long sides with a depth dimension L2. An entrance D is formed on one of the short sides, and a door 160 is mounted thereto. The toilet unit 110 is disposed on the depth side of the main body 105 at a short side opposed to the door 160.
The foldable sink 200 is mounted to an upper portion of the toilet unit 110.
A sump sink 220 is provided at a mounting portion of the foldable sink 200. The sump sink 220 is connected to a bottom surface of the sink portion 205, and receives a water M accumulated in the sink portion 205. The water received by the sump sink 220 is discharged through a drain hose 230 connected to the lower end of the sump sink 220.
An overflow drain 225 is provided on the sump sink 220. When a water level of water pooled in the sump sink 220 reaches a plane of the drain 225, the water is discharged through the overflow drain 225 to the drain hose 230.
The lavatory unit 100 according to the present invention has the foldable sink 200 disposed in a space at the upper portion of the toilet unit 110, so that the sink 200 can be folded to form a wide space in the height direction of the lavatory unit 100 during use of the toilet unit, so that a user will not feel any inconvenience when using the toilet both in a sifting position and in a standing position. Further, the foldable sink 200 can be expanded when using the sink, so that the sink can be used in the space at the upper portion of the toilet unit 110.
Since the foldable sink 200 is arranged in a space above the toilet unit 110, which is an available space at a height direction in the lavatory unit 100, it becomes possible to prevent interference between the sink and the user of the toilet unit 110, so that a width dimension W2 in an axis F direction of the toilet unit 110 can be reduced.
According to the configuration described above, a number of rows of passenger seats arranged in the axis direction F can be increased, and an operating efficiency of the aircraft can be improved.
Number | Date | Country | Kind |
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2014-072685 | Mar 2014 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2014/071748 | 8/20/2014 | WO | 00 |