WO2016162918A1 - Module de toilette pour avion - Google Patents

Module de toilette pour avion Download PDF

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Publication number
WO2016162918A1
WO2016162918A1 PCT/JP2015/060727 JP2015060727W WO2016162918A1 WO 2016162918 A1 WO2016162918 A1 WO 2016162918A1 JP 2015060727 W JP2015060727 W JP 2015060727W WO 2016162918 A1 WO2016162918 A1 WO 2016162918A1
Authority
WO
WIPO (PCT)
Prior art keywords
side wall
unit
lavatory unit
module
aircraft lavatory
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2015/060727
Other languages
English (en)
Japanese (ja)
Inventor
晃一 大井
義久 筒井
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jamco Corp
Original Assignee
Jamco Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Jamco Corp filed Critical Jamco Corp
Priority to PCT/JP2015/060727 priority Critical patent/WO2016162918A1/fr
Publication of WO2016162918A1 publication Critical patent/WO2016162918A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/02—Toilet fittings

Definitions

  • the present invention relates to a lavatory unit that is applied to passenger aircraft and the like.
  • An aircraft restroom unit mounted on a passenger aircraft or the like is generally known in which a toilet bowl, a urinal, a sink equipped with a mirror, and the like are integrated in a box-shaped room (for example, a patent) Reference 1).
  • an object of the present invention is to provide an aircraft lavatory unit that can easily cope with a change in specifications and shape inside the unit and can reduce the work burden associated with the change.
  • an aircraft lavatory unit is formed by separately forming a ceiling portion, a floor portion, and a side wall portion, and assembling them, and the side wall portion is composed of a plurality of side wall modules. By forming and joining the plurality of side wall modules, a space enclosed inside was formed.
  • At least one of the plurality of side wall modules is formed to have a shape corresponding to a passenger seat arranged outside the aircraft lavatory unit.
  • at least one of the plurality of side wall modules may be formed to include an additional sheet on an outer wall surface of the aircraft lavatory unit.
  • the aircraft lavatory unit of the present invention it is possible to easily cope with changes in specifications and shapes inside the unit, and to reduce the work burden related to the changes.
  • the design can be changed in units of side wall modules, the strength and the like can be guaranteed not in the whole box-shaped unit but in units of modules, and the design burden can be reduced.
  • FIG. 1 is a plan view showing an outline of an aircraft lavatory unit according to Embodiment 1 of the present invention.
  • the ceiling of the unit is not shown.
  • the aircraft lavatory unit 10 according to the first embodiment includes a first side wall module 11, a second side wall module 12, a third side wall between a ceiling part and a floor part (not shown).
  • the side wall module 13 and the fourth side wall module 14 are assembled so as to be substantially rectangular when viewed from above.
  • the coupling part can employ any coupling means such as bolt fastening, adhesion, or insertion structure. A structure that can be easily attached and detached so as to be exchangeable is applied.
  • a toilet unit 11a is attached to a first side wall module 11 integrally with a wall surface, for example.
  • the water supply system and the drainage system of the toilet unit 11a are configured to be connected to the water supply system and the drainage system provided on the floor during assembly.
  • the second side wall module 12 has a wash unit 12a attached integrally with a wall surface, for example.
  • the water supply system and the drainage system of the wash unit 12a are configured to be connected to the water supply system and the drainage system provided on the floor during assembly. .
  • the third side wall module 13 is provided with a door (not shown) for entering and exiting the aircraft lavatory unit 10 after assembly.
  • the fourth side wall module 14 is attached with a multi-purpose unit 24a such as a shelf for placing small items and a hook for hooking an object integrally with the wall surface.
  • FIG. 2 is a plan view showing a modification of the aircraft lavatory unit shown in FIG. In FIG. 2 as well, the ceiling of the unit is not shown.
  • Fig.2 (a) has shown the 2nd side wall module 22 which changed the washing
  • the second side wall module 22 for example, by changing the base part of the upper surface of the washbasin unit 22 a to a material having a marble-like surface with a high design property, it is configured to add a sense of quality and texture to the interior of the lavatory unit Has been.
  • FIG. 2B shows a fourth side wall module 24 in which the outside of the wall surface of the fourth side wall module 14 shown in FIG. 1 is changed.
  • a seat for a crew member is additionally attached, so that it has not only a function as a part of the lavatory unit but also a function as an attachment part of the additional seat. It can also be made.
  • the second side wall shown in FIGS. 2A and 2B is used instead of the second side wall module 12 and the fourth side wall module 14 in FIG.
  • a modified aircraft lavatory unit 20 is formed. With such a change, it is possible to easily make a change that reflects the user's preference or adds a function by performing an operation of replacing the side wall module.
  • the aircraft lavatory unit of the present invention can be changed by replacing some side wall modules of the unit without changing the entire unit when changing a part of the interior. It is possible to easily cope with changes in specifications and shapes inside the unit, and to reduce the work burden associated with the changes.
  • FIG. 3 is a plan view showing an outline of an aircraft lavatory unit according to Embodiment 2 of the present invention. In FIG. 3 as well, the ceiling of the unit is not shown.
  • FIG. 3A shows the first sidewall module 31 and the third sidewall module 33 in which the widths of the wall surfaces of the first sidewall module 11 and the third sidewall module 13 shown in FIG. 1 are extended. .
  • the aircraft lavatory unit 30 having an expanded width toward the doorway and the toilet unit is formed.
  • the ceiling portion and the floor portion are also changed to those having an expanded width.
  • the size (width and depth) of the aircraft lavatory unit can be easily changed by performing an operation of replacing the side wall module.
  • FIG. 4 is a plan view showing an outline of an aircraft lavatory unit according to Embodiment 3 of the present invention.
  • the unit ceiling is not shown.
  • FIG. 4A shows a recess for receiving an external structure such as a seat on the wall surface of the second side wall module 11 shown in FIG. 1, and a wash unit 42a corresponding to the shape of the recess is provided on the wall surface.
  • a second side wall module 42 is shown integrally mounted therein.
  • the shape of the wall surface for example, one having a recess for receiving a special specification sheet 50 for business class or the like is used.
  • the modified aircraft lavatory unit 40 is formed.
  • the ceiling part and the floor part are also changed to those having an expanded shape.
  • the aircraft lavatory unit according to the present invention is formed by separately forming the ceiling portion, the floor portion, and the side wall portion, and forming the side wall portion from a plurality of side wall modules.
  • the structure it is possible to easily cope with a layout change or a specification change of the lavatory unit, and it is not necessary to change or replace the entire unit. Therefore, it is possible to reduce the work load and the parts cost.
  • the design can be changed in units of side wall modules, the strength and rigidity of the unit can be guaranteed not in the whole box-shaped unit but in units of modules, and the design burden can be reduced.
  • the aircraft lavatory unit of the present invention is not limited to the above-described embodiment, and includes various modifications.
  • the aircraft lavatory unit of the present invention can add, delete, and replace other configurations within a range that does not depart from the technical idea of the present invention.
  • the configuration in which the ceiling portion and the floor portion are respectively provided is illustrated.
  • the ceiling portion and the floor portion is also used as the ceiling member or floor member of the aircraft.
  • the lavatory unit can be formed at an arbitrary position simply by attaching the module, the degree of freedom of layout inside the aircraft can be further increased.
  • the lavatory unit can have a function as a part of a member that increases the strength and rigidity of the aircraft.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Sanitary Device For Flush Toilet (AREA)

Abstract

L'objectif de la présente invention est de proposer un module de toilette pour avion qui peut facilement s'adapter à des modifications de forme et de spécifications de l'intérieur du module, et qui est capable de réduire la charge de travail associée à ces changements. Par conséquent, la présente invention concerne un module de toilette pour avion dans lequel une partie plafond, une partie sol et des parties paroi latérale sont formées séparément, et qui est formé par l'assemblage de ces parties. Les parties paroi latérale sont formées à partir d'une pluralité de modules de paroi. La pluralité de modules de paroi est couplée pour former un espace fermé formé à l'intérieur desdits modules de paroi.
PCT/JP2015/060727 2015-04-06 2015-04-06 Module de toilette pour avion Ceased WO2016162918A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/JP2015/060727 WO2016162918A1 (fr) 2015-04-06 2015-04-06 Module de toilette pour avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2015/060727 WO2016162918A1 (fr) 2015-04-06 2015-04-06 Module de toilette pour avion

Publications (1)

Publication Number Publication Date
WO2016162918A1 true WO2016162918A1 (fr) 2016-10-13

Family

ID=57071875

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2015/060727 Ceased WO2016162918A1 (fr) 2015-04-06 2015-04-06 Module de toilette pour avion

Country Status (1)

Country Link
WO (1) WO2016162918A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3643612A1 (fr) * 2018-10-26 2020-04-29 The Boeing Company Structure de toilettes améliorée pour aéronef
EP3643613A1 (fr) * 2018-10-26 2020-04-29 The Boeing Company Paroi arrière améliorée pour une structure de toilettes d'un aéronef

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6007025A (en) * 1996-12-23 1999-12-28 The Boeing Company Stowable module airplane lavatory
US6079669A (en) * 1997-03-24 2000-06-27 The Boeing Company Dual pivot expandable lavatory
US6101766A (en) * 1996-01-19 2000-08-15 Daimlerchrysler Rail Systems (Denmark) A/S Sanitary cell
JP2002154489A (ja) * 2000-11-22 2002-05-28 Jamco Corp 航空機用拡張式ラバトリーユニット
JP2003267296A (ja) * 2002-02-20 2003-09-25 Boeing Co:The マルチモード洗面所、洗面所システム、洗面所とシャワーとのモジュール、および、モジュールによるマルチモード洗面所の動作方法
US6889936B1 (en) * 2003-11-17 2005-05-10 The Boeing Company Apparatus and methods for increasing useable space within aircraft lavatories
US20050230550A1 (en) * 2003-10-21 2005-10-20 Armando Dominguez Cockpit security door/restroom
US20120119029A1 (en) * 2009-07-23 2012-05-17 Airbus Operations Gmbh Monument for a cabin of a vehicle
US20130001359A1 (en) * 2010-02-19 2013-01-03 Airbus Operations Gmbh Toilet arrangement for a vehicle
JP2013525178A (ja) * 2010-04-20 2013-06-20 ビーイー・インテレクチュアル・プロパティー・インコーポレイテッド 航空機内部のラバトリー
US20140359934A1 (en) * 2012-02-24 2014-12-11 Airbus Operations Gmbh Toilet module for a vehicle and a vehicle comprising a vehicle cabin and at least one toilet module

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6101766A (en) * 1996-01-19 2000-08-15 Daimlerchrysler Rail Systems (Denmark) A/S Sanitary cell
US6007025A (en) * 1996-12-23 1999-12-28 The Boeing Company Stowable module airplane lavatory
US6079669A (en) * 1997-03-24 2000-06-27 The Boeing Company Dual pivot expandable lavatory
JP2002154489A (ja) * 2000-11-22 2002-05-28 Jamco Corp 航空機用拡張式ラバトリーユニット
JP2003267296A (ja) * 2002-02-20 2003-09-25 Boeing Co:The マルチモード洗面所、洗面所システム、洗面所とシャワーとのモジュール、および、モジュールによるマルチモード洗面所の動作方法
US20050230550A1 (en) * 2003-10-21 2005-10-20 Armando Dominguez Cockpit security door/restroom
US6889936B1 (en) * 2003-11-17 2005-05-10 The Boeing Company Apparatus and methods for increasing useable space within aircraft lavatories
US20120119029A1 (en) * 2009-07-23 2012-05-17 Airbus Operations Gmbh Monument for a cabin of a vehicle
US20130001359A1 (en) * 2010-02-19 2013-01-03 Airbus Operations Gmbh Toilet arrangement for a vehicle
JP2013525178A (ja) * 2010-04-20 2013-06-20 ビーイー・インテレクチュアル・プロパティー・インコーポレイテッド 航空機内部のラバトリー
US20140359934A1 (en) * 2012-02-24 2014-12-11 Airbus Operations Gmbh Toilet module for a vehicle and a vehicle comprising a vehicle cabin and at least one toilet module

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3643612A1 (fr) * 2018-10-26 2020-04-29 The Boeing Company Structure de toilettes améliorée pour aéronef
EP3643613A1 (fr) * 2018-10-26 2020-04-29 The Boeing Company Paroi arrière améliorée pour une structure de toilettes d'un aéronef
CN111099020A (zh) * 2018-10-26 2020-05-05 波音公司 用于飞行器的盥洗室区块的改进的后壁
CN111099019A (zh) * 2018-10-26 2020-05-05 波音公司 用于飞行器的改进盥洗室区块
US11472555B2 (en) 2018-10-26 2022-10-18 The Boeing Company Aft wall for a lavatory monument of an aircraft
CN111099020B (zh) * 2018-10-26 2024-06-18 波音公司 用于飞行器的盥洗室区块的改进的后壁
CN111099019B (zh) * 2018-10-26 2024-08-06 波音公司 用于飞行器的改进盥洗室区块

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