Cabin monument for an aircraft

US10836489B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10836489-B2
Application numberUS-201815878627-A
CountryUS
Kind codeB2
Filing dateJan 24, 2018
Priority dateFeb 9, 2017
Publication dateNov 17, 2020
Grant dateNov 17, 2020

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  1. Title

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  2. Abstract

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  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

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A cabin monument for an aircraft includes a floor panel, which forms a base surface of the cabin monument, and a surrounding sidewall which defines an interior space of the cabin monument. The surrounding sidewall is assembled from a first wall part and a second wall part which is coupled to this. Provision is made on at least one of the wall parts for a fixing section which is overlapped by the floor panel. Also described is an aircraft which features such a cabin monument.

First claim

Opening claim text (preview).

The invention claimed is: 1. An aircraft, comprising: a body; an inner floor, which extends in an interior space of the aircraft which is delimited by the body; and a cabin monument comprising: a floor panel, which forms a base surface of the cabin monument, and has an inner lateral surface and a rear lateral surface; and a surrounding sidewall, extending transversely to the floor panel, which defines an interior space of the cabin monument; wherein the surrounding sidewall is assembled from a first wall part and a second wall part which is coupled to the first wall part; and wherein at least one of the wall parts comprises a fixing section having a top surface and a bottom surface, wherein the fixing section is overlapped by the floor panel such that the rear lateral surface of the floor panel rests on the top surface of the fixing section, and wherein the fixing section is clamped in between the floor panel and the inner floor. 2. The aircraft according to claim 1 , wherein the first and the second wall parts are configured as half-shells. 3. The aircraft according to claim 2 , wherein the first wall part comprises a first fixing section and the second wall part comprises a second fixing section, wherein the first and the second fixing sections are overlapped in each case by the floor panel. 4. The aircraft according to claim 1 , wherein the first wall part has a first connecting section which extends transversely to a main section of the first wall part which delimits the interior space, and the second wall part has a second connecting section which extends transversely to a main section of the second wall part which delimits the interior space, and wherein the first connecting section and the second connecting section are interconnected. 5. The aircraft according to claim 4 , wherein the first connecting section and the second connecting section are clamped inside a clamping device. 6. The aircraft according to claim 1 , wherein the first and the second wall parts have in each case an outer cover layer, an inner cover layer and a spacing layer which connects the inner cover layer and the outer cover layer, wherein the spacing layer has a hollow structure. 7. The aircraft according to claim 1 , wherein a bearing device for the fixing of functional units is arranged on the inner lateral surface of the floor panel which faces the interior space. 8. The aircraft according to claim 1 , wherein a spacing device is arranged on the rear lateral surface of the floor panel which is located in a manner facing away from the interior space. 9. The aircraft according to claim 1 , wherein a bearing device for the fixing of functional units is arranged on an inner surface of at least one of the wall parts. 10. The aircraft according to claim 1 , wherein the fixing section is perpendicular to the at least one of the wall parts. 11. The aircraft according to claim 1 , wherein the fixing section and the rear lateral surface are parallel to the inner floor.

Assignees

Inventors

Classifications

  • B64D11/00Primary

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

  • Toilet fittings · CPC title

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

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Frequently asked questions

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What does patent US10836489B2 cover?
A cabin monument for an aircraft includes a floor panel, which forms a base surface of the cabin monument, and a surrounding sidewall which defines an interior space of the cabin monument. The surrounding sidewall is assembled from a first wall part and a second wall part which is coupled to this. Provision is made on at least one of the wall parts for a fixing section which is overlapped by th…
Who is the assignee on this patent?
Airbus Operations Gmbh
What technology area does this patent fall under?
Primary CPC classification B64D11/00. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Nov 17 2020 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 6 related publications on this page (citations in our corpus or others sharing the same primary CPC).