Contoured passenger seat privacy shell shape of aircraft passenger compartment suites

US11299273B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11299273-B2
Application numberUS-202016744653-A
CountryUS
Kind codeB2
Filing dateJan 16, 2020
Priority dateJan 16, 2020
Publication dateApr 12, 2022
Grant dateApr 12, 2022

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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

    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.

An aircraft passenger compartment suite may include a privacy shell element proximate to an aircraft seat installed within the aircraft passenger compartment suite. The privacy shell element may include a first section configured to conform to a primary section of the aircraft seat, and a second section configured to conform to an auxiliary section of the aircraft seat. The privacy shell element may include a first profile configured to conform with the aircraft seat when the aircraft seat is in a first position, and a second profile configured to conform with the aircraft seat when the aircraft seat is in a second position. The second profile of the privacy shell element may be configured to occupy a greater amount of passenger aircraft living space surrounding the aircraft passenger compartment suite than an amount of passenger aircraft living space occupied by the first profile of the privacy shell element.

First claim

Opening claim text (preview).

What is claimed: 1. An aircraft passenger compartment suite, comprising: a privacy shell element proximate to an aircraft seat installed within the aircraft passenger compartment suite, a first section of the privacy shell element being configured to conform to a primary section of the aircraft seat, a second section of the privacy shell element being configured to conform to an auxiliary section of the aircraft seat, the primary section positioned substantially parallel to the auxiliary section of the aircraft seat, where an edge of the primary section is substantially flush with an edge of the auxiliary section of the aircraft seat to form a combined area of the aircraft seat, the privacy shell element including a first profile configured to conform with the aircraft seat when the aircraft seat is in a first position, the privacy shell element including a second profile configured to conform with the aircraft seat when the aircraft seat is in a second position, the second profile of the privacy shell element being configured to occupy a greater amount of passenger aircraft living space surrounding the aircraft passenger compartment suite than an amount of passenger aircraft living space occupied by the first profile of the privacy shell element. 2. The aircraft passenger compartment suite of claim 1 , the first position including an upright position. 3. The aircraft passenger compartment suite of claim 2 , the primary section of the aircraft seat and the auxiliary section of the aircraft seat forming a wide seating area when the aircraft seat is in the upright position, the wide seating area configured to seat one or more passengers. 4. The aircraft passenger compartment suite of claim 3 , the primary section of the aircraft seat being configured for a first passenger in the aircraft passenger compartment suite when the aircraft seat is in the upright position. 5. The aircraft passenger compartment suite of claim 4 , the auxiliary section of the aircraft seat being configured for a second passenger in the aircraft passenger compartment suite when the aircraft seat is in the upright position. 6. The aircraft passenger compartment suite of claim 2 , the first section of the privacy shell element being configured to conform to a seat back of the primary section of the aircraft seat when the aircraft seat is in the upright position, the second section of the privacy shell element being configured to conform to a seat back of the auxiliary section of the aircraft seat when the aircraft seat is in the upright position. 7. The aircraft passenger compartment suite of claim 6 , the first profile of the privacy shell element including a first flat surface configured to conform to the seat back of the primary section of the aircraft seat when the aircraft seat is in the upright position, the first profile of the privacy shell element including a second flat surface configured to conform to the seat back of the auxiliary section of the aircraft seat when the aircraft seat is in the upright position. 8. The aircraft passenger compartment suite of claim 2 , the second position including a lie-flat position. 9. The aircraft passenger compartment suite of claim 8 , the primary section of the aircraft seat and the auxiliary section of the aircraft seat forming a wide lie-flat area when the aircraft seat is in the lie-flat position, the wide lie-flat area configured to provide increased width for a passenger when in the lie-flat position. 10. The aircraft passenger compartment suite of claim 9 , the primary section of the aircraft seat and the auxiliary section of the aircraft seat being configured for a passenger in the aircraft passenger compartment suite when the aircraft seat is in the lie-flat position. 11. The aircraft passenger compartment suite of claim 9 , the first section of the privacy shell element being configured to conform to a headrest of the primary section of the aircraft seat when the aircraft seat is in the lie-flat position, the second section of the privacy shell element being configured to conform to an edge of a seat back of the auxiliary section of the aircraft seat when the aircraft seat is in the lie-flat position. 12. The aircraft passenger compartment suite of claim 11 , the second profile of the privacy shell element including a notch configured to conform to the headrest of the primary section of the aircraft seat when the aircraft seat is in the lie-flat position, the second profile of the privacy shell element including a surface configured to conform to the seat back of the auxiliary section of the aircraft seat when the aircraft seat is in the lie-flat position, the notch being configured to occupy the greater amount of passenger aircraft living space surrounding the aircraft passenger compartment suite than the amount of passenger aircraft living space occupied by the surface configured to conform to the seat back of the auxiliary section of the aircraft seat. 13. The aircraft passenger compartment suite of claim 11 , a portion of the auxiliary section of the aircraft seat being coupled to the privacy shell element when the auxiliary section of the aircraft seat transitions between the upright position and the lie-flat position. 14. The aircraft passenger compartment suite of claim 8 , the aircraft seat being configured to be positioned within a reclined position, the aircraft seat being configured to transition from the upright position to the lie-flat position through the reclined position. 15. A passenger compartment aircraft suite system, comprising: a first aircraft passenger compartment suite, comprising: a first privacy shell element proximate to a first aircraft seat installed within the first aircraft passenger compartment suite, a first section of the first privacy shell element being configured to conform to a primary section of the first aircraft seat, a second section of the first privacy shell element being configured to conform to an auxiliary section of the first aircraft seat, the primary section positioned substantially parallel to the auxiliary section of the aircraft seat, where an edge of the primary section is substantially flush with an edge of the auxiliary section of the aircraft seat to form a combined area of the aircraft seat, the first privacy shell element including a first profile configured to conform with the first aircraft seat when the first aircraft seat is in a first position, the first privacy shell element including a second profile configured to conform with the first aircraft seat when the first aircraft seat is in a second position, the second profile of the first privacy shell element being configured to occupy a greater amount of passenger aircraft living space surrounding the first aircraft passenger compartment suite than an amount of passenger aircraft living space occupied by the first profile of the first privacy shell element; and a second aircraft passenger compartment suite, comprising: a second privacy shell element proximate to a second aircraft seat installed within the second aircraft passenger compartment suite, a first section of the second privacy shell element being configured to conform to a primary section of the second aircraft seat, a second section of the second privacy shell element being configured to conform to an auxiliary section of the second aircraft seat, the second privacy shell element including a first profile configured to conform with the aircraft seat when the aircraft seat is in a first position, the second privacy shell element including a second profile configured to conform with the aircraft seat when the aircraft seat is in

Assignees

Inventors

Classifications

  • Seats convertible into beds · CPC title

  • including tables or desks · CPC title

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

  • with privacy shells, screens, separators or the like (class dividers B64D11/0023) · CPC title

  • 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

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Frequently asked questions

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What does patent US11299273B2 cover?
An aircraft passenger compartment suite may include a privacy shell element proximate to an aircraft seat installed within the aircraft passenger compartment suite. The privacy shell element may include a first section configured to conform to a primary section of the aircraft seat, and a second section configured to conform to an auxiliary section of the aircraft seat. The privacy shell elemen…
Who is the assignee on this patent?
Be Aerospace Inc
What technology area does this patent fall under?
Primary CPC classification B64D11/0606. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 12 2022 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 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).