Aircraft seat with extendable and retractable rear section

US11753170B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11753170-B2
Application numberUS-202117216105-A
CountryUS
Kind codeB2
Filing dateMar 29, 2021
Priority dateMar 30, 2020
Publication dateSep 12, 2023
Grant dateSep 12, 2023

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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 aircraft seat may include a seat pan cushion coupled to a seat base. The aircraft seat may include a seat back cushion. The aircraft seat may include an auxiliary rear section. The auxiliary rear section may be configured to transition between an extended position and a retracted position. The seat pan cushion and the seat back cushion may be configured to transition between a first position and a second position. The auxiliary rear section may be configured to be in the extended position when the seat pan cushion and the seat back cushion are in the first position. The auxiliary rear section may be configured to be in the retracted position when the seat pan cushion and the seat back cushion are in the second position.

First claim

Opening claim text (preview).

What is claimed: 1. An aircraft seat, comprising: a seat pan cushion coupled to a seat base; a seat back cushion; a head rest coupled to the seat back cushion; and an auxiliary rear section positioned behind a rear surface of the head rest, the auxiliary rear section configured to transition between an extended position and a retracted position, the auxiliary rear section being extendable and retractable from a cavity defined within a primary rear section, when the auxiliary rear section is in the retracted position, the auxiliary rear section is stowed within the cavity defined by the primary rear section, the seat pan cushion and the seat back cushion configured to transition between an upright position and a bed position, the auxiliary rear section configured to be in the extended position when the seat pan cushion and the seat back cushion are in the upright position, the auxiliary rear section configured to be in the retracted position when the seat pan cushion and the seat back cushion are in the bed position. 2. The aircraft seat of claim 1 , wherein the auxiliary rear section being configured to transition from the extended position to the retracted position while the seat pan cushion and the seat back cushion transition from the upright position to the bed position. 3. The aircraft seat of claim 2 , wherein the auxiliary rear section being configured to transition from the retracted position to the extended position while the seat pan cushion and the seat back cushion transition from the bed position to the upright position. 4. The aircraft seat of claim 1 , wherein the auxiliary rear section being configured to transition from the extended position to the retracted position before the seat pan cushion and the seat back cushion transition from the upright position to the bed position. 5. The aircraft seat of claim 4 , wherein the auxiliary rear section being configured to transition from the retracted position to the extended position after the seat pan cushion and the seat back cushion transition from the bed position to the upright position. 6. The aircraft seat of claim 1 , wherein the aircraft seat comprises: the primary rear section, the auxiliary rear section coupled to the primary rear section, a surface of the auxiliary rear section being proximate to a surface of the head rest when the auxiliary rear section is in the extended position. 7. The aircraft seat of claim 6 , wherein a top edge of the auxiliary rear section being at an extended height relative to the head rest when the auxiliary rear section is in the extended position. 8. The aircraft seat of claim 7 , wherein the top edge of the auxiliary rear section being at a retracted height relative to the head rest when the auxiliary rear section is in the retracted position. 9. The aircraft seat of claim 6 , wherein the auxiliary rear section is configured to transition between the extended position and the retracted position via the cavity defined within the primary rear section. 10. The aircraft seat of claim 6 , wherein the auxiliary rear section is configured to transition between the extended position and the retracted position along an exterior surface of the primary rear section. 11. A passenger compartment of an aircraft cabin, comprising: a privacy shell; and an aircraft seat positioned within the privacy shell, the aircraft seat comprising: a seat pan cushion coupled to a seat base; a head rest coupled to the seat back cushion; and an auxiliary rear section positioned behind a rear surface of the head rest, the auxiliary rear section configured to transition between an extended position and a retracted position, the auxiliary rear section being extendable and retractable from a cavity defined within a primary rear section, when the auxiliary rear section is in the retracted position, the auxiliary rear section is stowed within the cavity defined by the primary rear section, the seat pan cushion and the seat back cushion configured to transition between an upright position and a bed position, the auxiliary rear section configured to be in the extended position when the seat pan cushion and the seat back cushion are in the upright position, the auxiliary rear section configured to be in the retracted position when the seat pan cushion and the seat back cushion are in the bed position. 12. The passenger compartment of claim 11 , wherein the passenger compartment further comprises: an ottoman, the ottoman positioned proximate to the aircraft seat within the privacy shell. 13. The passenger compartment of claim 12 , wherein the ottoman and the aircraft seat are configured to form a bed surface when the seat pan cushion and the seat back cushion are in the bed position.

Assignees

Inventors

Classifications

  • with features for adjustment or converting of seats · CPC title

  • Seats convertible into beds · CPC title

  • Seats characterised by special features of stationary arms, foot or head rests · CPC title

  • Adjustable headrests · 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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What does patent US11753170B2 cover?
An aircraft seat may include a seat pan cushion coupled to a seat base. The aircraft seat may include a seat back cushion. The aircraft seat may include an auxiliary rear section. The auxiliary rear section may be configured to transition between an extended position and a retracted position. The seat pan cushion and the seat back cushion may be configured to transition between a first position…
Who is the assignee on this patent?
Be Aerospace Inc
What technology area does this patent fall under?
Primary CPC classification B64D11/0639. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Sep 12 2023 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 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).