Deployable floor panel arrangement for aircraft cabin area

US9511847B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9511847-B2
Application numberUS-201514699401-A
CountryUS
Kind codeB2
Filing dateApr 29, 2015
Priority dateApr 29, 2014
Publication dateDec 6, 2016
Grant dateDec 6, 2016

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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 deployable floor panel arrangement for an aircraft cabin area comprising a substantially planar floor panel with at least one foldable seat arrangement mounted thereto. The seat arrangement comprises at least one backrest which is configured to be moveable between a stowed position in which it extends at an angle of approximately 0° to 40° to the plane of the floor panel and a deployed position in which it extends at an angle of approximately 80° to 180° to the plane of the floor panel.

First claim

Opening claim text (preview).

The invention claimed is: 1. An aircraft cabin area, comprising: at least one deployable floor panel arrangement comprising: a substantially planar floor panel with at least one foldable seat arrangement mounted thereto, wherein the seat arrangement comprises at least one backrest which is configured to be movable between a stowed position in which it extends at an angle of approximately 0° to 40° to the plane of the floor panel and a deployed position in which it extends at an angle of approximately 80° to 180° to the plane of the floor panel, wherein the floor panel is movable between a deployed position in which it extends substantially in parallel to the floor area of the aircraft cabin area and a stowed position in which it extends substantially transverse thereto. 2. The aircraft cabin area according to claim 1 , wherein the floor panel is pivotable relative to a floor area of the aircraft cabin area. 3. The aircraft cabin area according to claim 1 , wherein the floor panel arrangement is lockable to components of the aircraft cabin area when arranged in its deployed position and/or in its stowed position. 4. The aircraft cabin area according to claim 1 , wherein the aircraft cabin area further comprises at least one sidewall area, wherein the floor panel is movable into its stowed position by pivoting it towards the sidewall area, and wherein the seat arrangement is located between the sidewall area and the floor panel when the floor panel is in its stowed position. 5. The aircraft cabin area according to claim 1 , wherein the aircraft cabin area comprises at least two floor panel arrangements that are arranged adjacent to each other along a transverse axis of the aircraft cabin area which extends in the floor area and perpendicularly to a longitudinal axis of the aircraft cabin area, and wherein the floor panels are movable into their stowed positions by pivoting them towards oppositely arranged sidewall areas. 6. An aircraft cabin area, comprising: at least one deployable floor panel arrangement comprising: a substantially planar floor panel with at least one foldable seat arrangement mounted thereto, wherein the seat arrangement comprises at least one backrest which is configured to be movable between a stowed position in which it extends at an angle of approximately 0° to 40° to the plane of the floor panel and a deployed position in which it extends at an angle of approximately 80° to 180° to the plane of the floor panel, wherein the floor panel is movable between a deployed position in which it extends substantially in parallel to the floor area of the aircraft cabin area and a stowed position in which it extends at an angle of approximately 50° to 130° to the floor area. 7. The aircraft cabin area according to claim 6 , wherein the floor panel is pivotable relative to a floor area of the aircraft cabin area. 8. The aircraft cabin area according to claim 6 , wherein the floor panel arrangement is lockable to components of the aircraft cabin area when arranged in its deployed position and/or in its stowed position. 9. The aircraft cabin area according to claim 6 , wherein the aircraft cabin area further comprises at least one sidewall area, wherein the floor panel is movable into its stowed position by pivoting it towards the sidewall area, and wherein the seat arrangement is located between the sidewall area and the floor panel when the floor panel is in its stowed position. 10. The aircraft cabin area according to claim 6 , wherein the aircraft cabin area comprises at least two floor panel arrangements that are arranged adjacent to each other along a transverse axis of the aircraft cabin area which extends in the floor area and perpendicularly to a longitudinal axis of the aircraft cabin area, and wherein the floor panels are movable into their stowed positions by pivoting them towards oppositely arranged sidewall areas. 11. An aircraft cabin area, comprising: at least one deployable floor panel arrangement comprising: a substantially planar floor panel with at least one foldable seat arrangement mounted thereto, wherein the seat arrangement comprises at least one backrest which is configured to be movable between a stowed position in which it extends at an angle of approximately 0° to 40° to the plane of the floor panel and a deployed position in which it extends at an angle of approximately 80° to 180° to the plane of the floor panel, wherein the aircraft cabin area further comprises at least one barrier wall which is configured to be movable along the longitudinal axis of the area craft cabin area, and wherein the barrier wall comprises at least one retractable portion that is retractable to such a degree that the barrier wall may pass by at least one floor panel arrangement with the floor panel in its stowed position.

Assignees

Inventors

Classifications

  • 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

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

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

  • Equipment for handling freight; Equipment for facilitating passenger embarkation or the like · CPC title

  • Cross-Sectional Technologies · mapped topic

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Frequently asked questions

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What does patent US9511847B2 cover?
A deployable floor panel arrangement for an aircraft cabin area comprising a substantially planar floor panel with at least one foldable seat arrangement mounted thereto. The seat arrangement comprises at least one backrest which is configured to be moveable between a stowed position in which it extends at an angle of approximately 0° to 40° to the plane of the floor panel and a deployed positi…
Who is the assignee on this patent?
Airbus Operations Gmbh
What technology area does this patent fall under?
Primary CPC classification B64C1/20. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 06 2016 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).