Aircraft interior lavatory

US10259558B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10259558-B2
Application numberUS-201615258529-A
CountryUS
Kind codeB2
Filing dateSep 7, 2016
Priority dateApr 20, 2010
Publication dateApr 16, 2019
Grant dateApr 16, 2019

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A lavatory for an aircraft cabin includes a wall having a forward wall portion disposed immediately aft of and substantially conforming to an exterior aft surface of an aircraft cabin structure, such as a passenger seat, that is substantially not flat in a vertical plane. The forward wall portion includes a forward projection over an aft portion of the adjacent passenger seat. The forward wall portion can define a secondary space in the interior lavatory space, which can provide an amenity stowage space, and can include design elements providing visual space.

First claim

Opening claim text (preview).

The invention claimed is: 1. An aircraft lavatory unit for a cabin area of a passenger aircraft, the aircraft lavatory unit comprising: an aft wall; and a contoured forward wall that is substantially not flat, wherein the contoured forward wall is configured to receive a portion of an exterior aft surface of a seat back of a forward-installed passenger seat when the seat back is in an unreclined seat position; wherein a width of a lavatory space disposed between the forward wall and the aft wall comprises an upper width, a lower width, and a mid-width measured at a height above the cabin floor corresponding substantially to a head rest of the forward-installed passenger seat when the seat back is in the unreclined position, wherein  the upper width and the lower width are both substantially wider than the mid-width; and wherein the contoured forward wall permits a forward-installed passenger seat to be positioned in a manner that reduces a volume of unusable space in the cabin area by reducing or eliminating gaps that would exist between a substantially flat forward wall and the forward-installed passenger seat; and wherein the contoured forward wall permits an aft-extending seat support of the forward-positioned passenger seat to be positioned closer to the contoured forward wall than a position permitted by the substantially flat forward wall. 2. The aircraft lavatory unit of claim 1 , wherein the forward wall comprises: a forward-extending upper portion; an aft-extending mid-portion; and a forward-extending lower portion; wherein the forward-extending upper portion, the aft-extending mid-portion, and the forward-extending lower portion combine to define a first aft-extending recess disposed between the forward-extending upper portion and the forward-extending lower portion for receiving the portion of the exterior aft surface of the seat back. 3. The aircraft lavatory unit of claim 2 , wherein the upper recess extends along substantially a full width of the contoured forward wall. 4. The aircraft lavatory unit of claim 1 , wherein a bottom width of the aircraft lavatory unit is narrower than the lower width. 5. The aircraft lavatory unit of claim 4 , wherein the forward wall further defines a second aft-extending recess proximate to a lower end of the forward wall, the second aft-extending recess being configured to receive at least a portion of the aft-extending seat support of the forward-positioned passenger seat therein. 6. The aircraft lavatory unit of claim 5 , wherein the second aft-extending recess extends along substantially a full width of the contoured forward wall. 7. The aircraft lavatory unit of claim 1 , wherein the contoured forward wall further comprises an upper projection that, upon installation, protrudes forward over a top of the seat back. 8. The aircraft lavatory unit of claim 7 , wherein the upper projection is configured to abut an upper surface of the cabin area. 9. The aircraft lavatory unit of claim 7 , wherein the upper projection defines a secondary space in the interior lavatory space above the passenger seat back. 10. The aircraft lavatory unit of claim 1 , wherein the contoured forward wall is configured to accept loads from the forward-positioned passenger seat.

Assignees

Inventors

Classifications

  • B64D11/02Primary

    Toilet fittings · CPC title

  • B64C1/10Primary

    Bulkheads · CPC title

  • Adjustable inclination or position of seats · CPC title

  • Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title

  • Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for · CPC title

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Frequently asked questions

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What does patent US10259558B2 cover?
A lavatory for an aircraft cabin includes a wall having a forward wall portion disposed immediately aft of and substantially conforming to an exterior aft surface of an aircraft cabin structure, such as a passenger seat, that is substantially not flat in a vertical plane. The forward wall portion includes a forward projection over an aft portion of the adjacent passenger seat. The forward wall …
Who is the assignee on this patent?
Be Aerospace Inc
What technology area does this patent fall under?
Primary CPC classification B64D11/02. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 16 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).