Using foam for structural components of a seat assembly

US11530044B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11530044-B2
Application numberUS-201616332580-A
CountryUS
Kind codeB2
Filing dateSep 20, 2016
Priority dateSep 20, 2016
Publication dateDec 20, 2022
Grant dateDec 20, 2022

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  1. Title

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  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  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.

Seat assemblies ( 200 ) including structural components ( 212, 222, 232 ) made of foam are described. A seat sub-assembly ( 210, 220, 230 ) can include a frame ( 214, 224, 234 ) and a foam support ( 212, 222, 232 ). The foam support ( 212, 222, 232 ) can be coupled to the frame ( 214, 224, 234 ) for receiving a load on the seat sub-assembly ( 210, 220, 230 ), dissipating at least half of the load, and dispersing the load through the frame ( 214, 224, 234 ).

First claim

Opening claim text (preview).

That which is claimed is: 1. A seat assembly comprising: a seat pan comprising: a bottom frame; and a bottom support coupled to the bottom frame for bearing at least half of a first load on the seat assembly and dispersing a portion of the first load across the bottom support to the bottom frame; a seat back coupled to the seat pan, the seat back comprising: a back frame; and a back support coupled to the back frame for bearing at least half of a second load on the seat assembly and for dispersing a portion of the second load across the back support to the back frame; and a leg rest coupled to the seat pan, the leg rest comprising: a leg frame; and a leg support coupled to the leg frame for bearing at least half of a third load on the seat assembly and for dispersing a portion of the third load across the leg support to the leg frame, and wherein the bottom support, the back support, and the leg support each include a load-bearing foam for receiving a corresponding load, dissipating at least half of the load, and dispersing a portion of the load through the corresponding frame, wherein the back frame defines a back-receiving area, wherein the foam of the back support is positioned within the back-receiving area, wherein the foam of the back support is larger than the back-receiving area, and wherein the back frame is positioned in a groove in the foam of the back support, wherein the leg frame defines a leg-rest area, wherein the foam of the leg support is positioned within the leg-rest area, wherein the foam of the leg support is larger than the leg-rest area, and wherein the leg frame is positioned in a groove in the foam of the leg support, and wherein the bottom frame comprises four frame segments defines a sitting area, wherein the foam of the bottom support is positioned within the sitting area, wherein the foam of the bottom support is larger than the sitting area, and wherein each of the four frame segments of the bottom frame are encompassed by the foam of the bottom support. 2. The seat assembly of claim 1 , wherein the seat assembly is a passenger seat on a passenger aircraft, wherein the first load, the second load, and the third load include a weight of a passenger sitting in the passenger seat. 3. The seat assembly of claim 1 , wherein the load-bearing foam comprises: a foam structural layer for dissipating the first load, the second load, or the third load; a foam comfort layer coupled to the foam structural layer for providing a cushion; and a covering for encompassing the foam structural layer and the foam comfort layer to protect the foam structural layer and the foam comfort layer. 4. The seat assembly of claim 3 , wherein the foam structural layer includes a reinforcing grid having a series of ridges and gaps such that the foam structural layer provides greater support to an area of the seat assembly closer to the ridges than the gaps. 5. The seat assembly of claim 3 , wherein the foam structural layer can include at least one of neopor, polyolefin, ethylene-vinyl acetate (“EVA”), polyethylene, polyform, polyurethane, or ethafoam. 6. The seat assembly of claim 1 , wherein the load-bearing foam is a structural foam that is molded, machined, formed, or constructed to act as a load-bearing part of the seat assembly. 7. The seat assembly of claim 1 , wherein foam is usable as a replacement for metal load-bearing components that support cushions.

Assignees

Inventors

Classifications

  • Seats characterised by special upholstery or cushioning features · CPC title

  • Upholstery springs {; Upholstery} · CPC title

  • with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash · CPC title

  • Seats characterised by special features for reducing weight · CPC title

  • Weight reduction · CPC title

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Frequently asked questions

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What does patent US11530044B2 cover?
Seat assemblies ( 200 ) including structural components ( 212, 222, 232 ) made of foam are described. A seat sub-assembly ( 210, 220, 230 ) can include a frame ( 214, 224, 234 ) and a foam support ( 212, 222, 232 ). The foam support ( 212, 222, 232 ) can be coupled to the frame ( 214, 224, 234 ) for receiving a load on the seat sub-assembly ( 210, 220, 230 ), dissipating at least half of the lo…
Who is the assignee on this patent?
Safran Seats Usa Llc
What technology area does this patent fall under?
Primary CPC classification B64D11/0647. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 20 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).