Forward interior space arrangement for an aircraft

US2018208316A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2018208316-A1
Application numberUS-201815878019-A
CountryUS
Kind codeA1
Filing dateJan 23, 2018
Priority dateJan 26, 2017
Publication dateJul 26, 2018
Grant date

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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.

An interior space for an aircraft includes a cockpit, a cockpit wall separating the cockpit from the remaining interior space, a cabin door arranged directly behind the cockpit wall for accessing the interior space of the aircraft from outside the fuselage, a modular installation space for installation equipment, a plurality of seat rows, a longitudinal aisle extending along the interior space through the seat rows to separate adjacent groups of seats from each other, and an access path for the cabin door. The access path extends from the cabin door to the longitudinal aisle to create an intersection region between the access path and the longitudinal aisle. The modular installation space is arranged directly forward of the seat rows. The access path extends at an angle of at least 100° to the longitudinal aisle in a forward direction.

First claim

Opening claim text (preview).

What is claimed is: 1 . A forward interior space arrangement for an aircraft, comprising: a cockpit arranged at a forward-most part of an interior space in a fuselage of the aircraft; a cockpit wall for separating the cockpit from a remaining part of the interior space; at least one forward cabin door, which is arranged directly behind the cockpit wall for accessing the interior space of the aircraft from outside the fuselage; at least one first modular installation space for receiving installation equipment; a plurality of first seat rows; at least one longitudinal aisle extending along the interior space through the first seat rows and thereby separating adjacent groups of seats from each other; and an access path for each of the at least one cabin door, extending from the respective cabin door to at least one of the at least one longitudinal aisle, thereby creating an intersection region between the respective access path and the respective longitudinal aisle; wherein the at least one first modular installation space is arranged directly forward of one of the first seat rows; and wherein the at least one access path extends at an angle of at least 100° to the at least one longitudinal aisle in a forward direction. 2 . The arrangement of claim 1 , wherein the at least one first modular installation space extends in a substantially lateral direction less than a subsequent first group of seats. 3 . The arrangement of claim 1 , wherein at least one of the at least one first modular installation space comprises at least a second group of seats having less seats than a first group of seats directly rearward of the first modular installation space. 4 . The arrangement of claim 1 , wherein at least one of the at least one first modular installation space comprises at least an additional first group of seats. 5 . The arrangement of claim 1 , wherein the at least one first modular installation space comprises a stowage module. 6 . The arrangement of claim 1 , wherein the at least one first modular installation space comprises a monument, in particular a galley module. 7 . The arrangement of claim 6 , further comprising at least one foldable seat arranged on a forward facing front of the monument. 8 . The arrangement of claim 6 , wherein the intersection region is asymmetrically shifted away from the monument. 9 . The arrangement of claim 1 , further comprising at least one second modular installation space between the cockpit wall and the at least one access path, wherein the at least one second modular installation space extends up to the intersection region. 10 . The arrangement of claim 9 , wherein the at least one second modular installation space comprises at least one lavatory module. 11 . The arrangement of claim 10 , wherein the at least one lavatory module comprises a lavatory door facing to the at least one longitudinal aisle. 12 . The arrangement of claim 11 , wherein a cabin attendant seat is arranged on the lavatory door. 13 . The arrangement of claim 1 , further comprising two forward cabin doors at two laterally opposite sides of the interior space, such that the at least one longitudinal aisle and the access paths to the at least one longitudinal aisle form an Y-aisle arrangement. 14 . The arrangement of claim 1 , further comprising at least one partition curtain extendable between a position in or at a rear end of the first installation space to a position forward of the at least one first modular installation space at least partially along the longitudinal aisle. 15 . An aircraft comprising: a fuselage having a front end and a rear end; and a forward interior space arrangement in the fuselage, the forward interior space comprising: a cockpit arranged at a forward-most part of an interior space in a fuselage of the aircraft; a cockpit wall for separating the cockpit from a remaining part of the interior space; at least one forward cabin door, which is arranged directly behind the cockpit wall for accessing the interior space of the aircraft from outside the fuselage; at least one first modular installation space for receiving installation equipment; a plurality of first seat rows; at least one longitudinal aisle extending along the interior space through the first seat rows and thereby separating adjacent groups of seats from each other; and an access path for each of the at least one cabin door, extending from the respective cabin door to at least one of the at least one longitudinal aisle, thereby creating an intersection region between the respective access path and the respective longitudinal aisle; wherein the at least one first modular installation space is arranged directly forward of one of the first seat rows; and wherein the at least one access path extends at an angle of at least 100° to the at least one longitudinal aisle in a forward direction.

Assignees

Inventors

Classifications

  • Width modification of seat assemblies, e.g. for class modification · CPC title

  • Passenger doors · CPC title

  • Galleys · CPC title

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

  • Stowage devices for passengers' personal luggage · CPC title

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Frequently asked questions

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What does patent US2018208316A1 cover?
An interior space for an aircraft includes a cockpit, a cockpit wall separating the cockpit from the remaining interior space, a cabin door arranged directly behind the cockpit wall for accessing the interior space of the aircraft from outside the fuselage, a modular installation space for installation equipment, a plurality of seat rows, a longitudinal aisle extending along the interior space …
Who is the assignee on this patent?
Airbus Operations Gmbh
What technology area does this patent fall under?
Primary CPC classification B64D11/0023. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Jul 26 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).