Expandable aircraft monument

Patent metadata

Field	Value
Publication number	US-9428274-B2
Application number	US-201414278310-A
Country	US
Kind code	B2
Filing date	May 15, 2014
Priority date	May 15, 2013
Publication date	Aug 30, 2016
Grant date	Aug 30, 2016

Abstract

An aircraft monument for installation in an aircraft cabin including a first functional module, the first functional module including a side wall for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module and/or from a region of the aircraft monument adjacent to the first functional module. The side wall is movable between a first and a second operational position and comprises a side-wall region which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, so that a movement of the side wall out of its first operational position into its second operational position results in an enlargement of a base area of the first functional module.

First claim

The invention claimed is:

1. An aircraft region, comprising:
at least one main aisle extending along a longitudinal axis of an aircraft cabin,
a door aisle extending substantially perpendicular to the at least one main aisle between a first and a second aircraft door, and
an aircraft monument arranged in the door aisle comprising a first functional module,
the first functional module including a side wall for delimiting the first functional module from at least one of a region of the aircraft cabin adjacent to the first functional module and a region of the aircraft monument adjacent to the first functional module,
the side wall being movable between a first and a second operational position and comprises a side-wall region which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, so that a movement of the side wall out of its first operational position into its second operational position results in an enlargement of a base area of the first functional module,
wherein the side wall of the first functional module is adapted to serve in its first operational position as a guidance device for passengers moving in the course of disembarking from the aircraft, or in the event of an emergency evacuation of the aircraft in the direction of at least one of the first and the second aircraft door.

2. The aircraft region according to claim 1 , wherein the aircraft monument is arranged in the door aisle in such a manner that the side wall of the first functional module faces towards a rear region of the aircraft cabin, relative to the flight direction of an aircraft equipped with the aircraft region.

3. The aircraft region according to claim 1 , wherein the aircraft monument is arranged in the door aisle in such a manner that the side wall of the first functional module faces towards a front region of the aircraft cabin, relative to the flight direction of an aircraft equipped with the aircraft region.

4. The aircraft region according to claim 1 , wherein the aircraft monument is arranged substantially centrically in the door aisle.

5. The aircraft region according to claim 1 , wherein the side wall of the first functional module is adapted to serve in its second operational position as at least one of a privacy screen and a separating device between two portions of the aircraft region.

6. The aircraft region according to claim 1 , wherein the first functional module of the aircraft monument is configured in the form of a sanitary module.

7. The aircraft region according to claim 1 , wherein the first functional module of the aircraft monument comprises a tapering base area, in particular a circular-segment-shaped base area.

8. The aircraft region according to claim 7 , wherein in the side wall of the first functional module of the aircraft monument a doorway that is capable of being closed by a door is formed, the door being capable of being swiveled between an open position and a closed position about a swivel axis.

9. The aircraft region according to claim 8 , wherein the swivel axis is arranged in the region of a vertex of the tapering base area of the first functional module of the aircraft monument.

10. The aircraft region according to claim 1 , wherein the side wall of the first functional module of the aircraft monument is movable between its first and its second operational position by swiveling of at least one portion of the side wall about a swivel axis.

11. The aircraft region according to claim 10 , wherein the swivel axis is arranged in the region of a vertex of the tapering base area of the first functional module of the aircraft monument.

12. The Aircraft region according to claim 1 , wherein the side-wall region of the side wall of the first functional module of the aircraft monument, which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, is designed in the form of a segment of an outer cylindrical surface.

13. The aircraft region according to claim 1 , wherein the side-wall region of the side wall of the first functional module of the aircraft monument, which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, in the first operational position of the side wall is arranged adjacent to a further side-wall region of the side wall of the first functional module in an interior space of the first functional module or outside the first functional module.

14. The aircraft region according to claim 13 , wherein at least two first functional modules are arranged in the region of portions of the aircraft monument situated substantially opposite one another.

15. The aircraft region according to claim 1 , wherein the aircraft monument includes at least one of a plurality of first functional modules and at least one further functional module serving for a function different from that of the first functional module.

16. The aircraft region according to claim 15 , wherein the at least two first functional modules are separated from one another by a further functional module.

Assignees

• Airbus Operations Gmbh

Inventors

• Moje Sabrina
• Breuer Matthias

Classifications

• B64C1/1423

  Passenger doors · CPC title

• B64D11/04

  Galleys · CPC title

• B64D11/02

  Toilet fittings · CPC title

• B64D11/0023

  Movable or removable cabin dividers, e.g. for class separation · CPC title

• B64D11/00 Primary

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title