Combination energy impact attenuation, vibration mitigation and flotation device for aircraft seating applications

US11708164B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11708164-B2
Application numberUS-202117234998-A
CountryUS
Kind codeB2
Filing dateApr 20, 2021
Priority dateApr 20, 2021
Publication dateJul 25, 2023
Grant dateJul 25, 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.

A combination adaptive energy absorption and emergency flotation device for positioning beneath a plurality of seat pans of a seat assembly in an aircraft seating application. The device includes a plurality of fluidly coupled inflatable elastic bladders, at least one constrictor valve fluidly coupling at least two adjacent ones of the plurality of inflatable elastic bladders allowing fluid flow therethrough in response to predetermined pressure on the device from the plurality of seat pans, and a fluid supply source fluidly coupled to the plurality of inflatable elastic bladders for outputting a positive flow of fluid to the plurality of inflatable elastic bladders, wherein the adaptive energy absorption device is detached from the plurality of seat pans to allow removal from beneath the plurality of seat pans for use as an emergency flotation device.

First claim

Opening claim text (preview).

What is claimed is: 1. A seating system for an aircraft, comprising: a seat frame defining at least one seat position, each seat position including a seat back and a seat pan coupled to the seat frame; an adaptive energy absorption device disposed beneath the seat pan of the at least one seat position, the adaptive energy absorption device comprising a plurality of fluidly coupled inflatable elastic bladders and at least one constrictor valve for allowing fluid to flow from one of the plurality of inflatable elastic bladders in response to predetermined pressure on the adaptive energy absorption device from the seat pan of the at least one seat position; and a fluid supply source fluidly coupled to the at least one inflatable elastic bladder operable for outputting a positive flow of fluid to the at least one inflatable elastic bladder; wherein the adaptive energy absorption device is detached from the seat frame to allow removal from beneath the seat pan of the at least one seat position for use as an emergency flotation device. 2. The seating system according to claim 1 , wherein the seat frame defines at least two laterally adjacent seat positions and the adaptive energy absorption device spans continuously across the at least two laterally adjacent seat positions. 3. The seating system according to claim 1 , wherein the plurality of fluidly coupled inflatable elastic bladders are to form a vertical stack. 4. The seating system according to claim 1 , wherein the at least one constrictor valve is disposed between fluidly coupled adjacent ones of the plurality of inflatable elastic bladders to allow fluid to flow between the fluidly coupled adjacent ones of the plurality of inflatable elastic bladders. 5. The seating system according to claim 1 , wherein the at least one constrictor valve is disposed in one of the plurality of inflatable elastic bladders to allow fluid escape out of the adaptive energy absorption device. 6. The seating system according to claim 1 , further comprising a controller communicatively coupled to the fluid supply source operable for activating the fluid supply source to output fluid to the adaptive energy absorption device to maintain a predetermined fluid pressure in the adaptive energy absorption device. 7. The seating system according to claim 1 , wherein the seat pan is pivotally and/or translatably coupled to the seat frame and the adaptive energy absorption device is positioned in direct physical contact with the seat pan of the at least one seat position. 8. The seating system according to claim 1 , wherein fluid supplied by the fluid supply source is helium. 9. The seating system according to claim 1 , wherein the seat frame defines a plurality of laterally adjacent seat positions, and wherein the seat pans of the laterally adjacent seat positions are coupled together. 10. The seating system according to claim 1 , wherein the adaptive energy absorption device is expandable from a partially inflated condition when disposed beneath the seat pan of the at least one seat position to a fully inflated condition when removed from beneath the seat pan of the at least one seat position for use as the emergency flotation device.

Assignees

Inventors

Classifications

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

  • Seat modifications · CPC title

  • Flotation gear · CPC title

  • for devices other than life vests and intended for external use, e.g. parachutes or life rafts · CPC title

  • inflatable · CPC title

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Frequently asked questions

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What does patent US11708164B2 cover?
A combination adaptive energy absorption and emergency flotation device for positioning beneath a plurality of seat pans of a seat assembly in an aircraft seating application. The device includes a plurality of fluidly coupled inflatable elastic bladders, at least one constrictor valve fluidly coupling at least two adjacent ones of the plurality of inflatable elastic bladders allowing fluid flo…
Who is the assignee on this patent?
Be Aerospace Inc
What technology area does this patent fall under?
Primary CPC classification B64D11/0619. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jul 25 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).