Aircraft lavatory unit installation method and aircraft

Patent metadata

Field	Value
Publication number	US-9650144-B2
Application number	US-201314380661-A
Country	US
Kind code	B2
Filing date	Feb 20, 2013
Priority date	Feb 23, 2012
Publication date	May 16, 2017
Grant date	May 16, 2017

Abstract

A body frame of an aircraft lavatory unit includes a front wall having an entrance opened and closed off by a door, side walls on both sides, and a floor surface. The outer surface of the side wall positioned closer to the front constitutes a wall facing backrests of a rear seat row and extending in a latitudinal direction. The lavatory unit is capable of being disposed at a front position in which the wall is disposed behind and near the backrests of the seats of the rear seat rows with the backrests being in an upright position, and at a rear position in which the wall is disposed behind and near the backrests of the rear seat rows of the seats with the backrests being in a reclining position.

First claim

The invention claimed is:

1. An aircraft lavatory unit installation method, the aircraft comprising:
a longitudinal aisle extending along a longitudinal direction of a fuselage and positioned at an intermediate position with respect to a latitudinal direction of the fuselage;
a seat group in which a plurality of seat rows, the seat rows including a plurality of seats facing the front of the fuselage and arranged in rows along the latitudinal direction of the fuselage, is arranged in rows along the longitudinal direction of the fuselage on left and right sides of the longitudinal aisle;
a latitudinal aisle extending in the latitudinal direction from a boarding entrance of the fuselage behind the seat group and connecting to the longitudinal aisle; and
a lavatory unit provided between the latitudinal aisle and a rear seat row at a rearmost position in the seat group, the lavatory unit comprising a body frame having a plurality of walls and a toilet within the body frame, the plurality of walls including a wall extending in the latitudinal direction and facing backrests of the rear seat row and a wall extending in the latitudinal direction and facing the latitudinal aisle,
the method comprising the steps of:
disposing the lavatory unit at a front position in which the wall facing the backrests of the rear seat row is positioned near the backrests of the seats of the rear seat row with the backrests set to an upright position and the wall facing the latitudinal aisle is positioned at a front of the latitudinal aisle along the latitudinal direction of the fuselage, during takeoff and landing;
disposing the lavatory unit at a rear position in which the wall facing the backrests of the rear seat row is positioned near the backrests of the seats of the rear seat row with the backrests set to a reclining position and the wall facing the latitudinal aisle is positioned on the latitudinal aisle, when the aircraft is not taking off or landing;
using an excess space formed behind the backrests of the seats of the rear seat rows, when the backrests are in the upright position during takeoff and landing, as a space for disposing the lavatory units at the front position, and using a part of the space of the latitudinal aisle which is not frequently used, when the aircraft is not taking off or landing, as a space for disposing the lavatory units at the rear position; and
utilizing the excess space behind the backrests of the seats of the rear seat rows and the part of the space of the latitudinal aisle, and reducing spacings between seat rows in the longitudinal direction for each spacing to obtain more seat rows arranged in the longitudinal direction as compared with a number of seat rows in a fuselage of an aircraft in which a lavatory unit is immovably disposed.

2. The aircraft lavatory unit installation method according to claim 1 , wherein a plurality of lavatory units is provided in a row in the latitudinal direction, and the plurality of lavatory units is disposed at the front position during takeoff and landing and at the rear position when not taking off or landing.

3. The aircraft lavatory unit installation method according to claim 1 , wherein a plurality of lavatory units is provided in a row in the longitudinal direction, the plurality of lavatory units forming an integrated whole,
a forward-facing wall of the lavatory unit positioned furthest to the front among the integrated plurality of lavatory units constitutes the wall facing the backrests of the rear seat row, and
the plurality of lavatory units are disposed as an integrated whole at the front position during takeoff and landing and at the rear position when not taking off or landing.

Assignees

• Yokohama Rubber Co Ltd

Inventors

• Koyama Takashi

Classifications

• B64D11/0696

  Means for fastening seats to floors, e.g. to floor rails · CPC title

• B64C1/20

  specially adapted for freight · CPC title

• B64D11/02 Primary

  Toilet fittings · CPC title

• B64D11/0601

  Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight · CPC title

• B64D2011/0046

  Modular or preassembled units for creating cabin interior structures · CPC title