Aircraft seal

US9340291B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9340291-B2
Application numberUS-201414338747-A
CountryUS
Kind codeB2
Filing dateJul 23, 2014
Priority dateJul 26, 2013
Publication dateMay 17, 2016
Grant dateMay 17, 2016

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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

    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.

The invention is a seal assembly, including a polyvinyl fluoride (PVF) film bonded to a polyvinylidene fluoride (PVDF) substrate and attached to a plastic retainer element for being mounted to an aircraft passenger fixture by mounting holes formed in the retainer element through which fasteners extend into the seat. The seal is sufficiently flexible to bend into an inner sidewall of an aircraft cabin and to seal a space between the aircraft cabin fixture and the inner sidewall.

First claim

Opening claim text (preview).

We claim: 1. An aircraft seal assembly comprising: a. a retainer, made of a plastic, having a plurality of mounting elements for being mounted to an aircraft cabin fixture; b. an elongate seal bonded to the retainer and comprising a flexible film bonded to a flexible substrate; and c. wherein the elongate seal is flexible and is positioned in a space between the aircraft cabin fixture and an inner sidewall of an aircraft cabin to seal the space between the aircraft cabin fixture and the inner sidewall; and d. wherein the retainer further comprises a pair of overlapping reciprocal retainer elements. 2. The aircraft seal assembly of claim 1 wherein the flexible film is made from a polyvinyl fluoride (VDF), and the flexible substrate is made from a polyvinylidene difluoride (PVDF). 3. The aircraft seal assembly of claim 1 wherein the flexible film is bonded to the flexible substrate with a contact adhesive. 4. The aircraft seal assembly of claim 1 wherein the elongate seal is bonded to the retainer with an epoxy bonding material. 5. The aircraft seal assembly of claim 1 wherein the elongate seal comprises a generally planar shape when not in contact with the inner sidewall. 6. The aircraft seal assembly of claim 1 wherein the plurality of mounting elements comprises holes through which a plurality of fasteners extend into the aircraft cabin fixture. 7. The aircraft seal assembly of claim 1 wherein the aircraft cabin fixture is selected from the group consisting of: aircraft passenger shells, aircraft passenger seats, aircraft cabin monuments, aircraft cabin partitions, aircraft cabin lavatories, and aircraft cabin storage components. 8. The aircraft seal assembly of claim 1 wherein the elongate seal forms a rounded V shape. 9. The aircraft seal assembly of claim 1 wherein the pair of overlapping reciprocal retainer elements are bonded to each other with an epoxy bonding material and wherein the elongate seal is bonded to the plastic retainer with an epoxy bonding material. 10. An aircraft seal assembly comprising: a. a plastic retainer having a plurality of holes through which a plurality of fasteners pass for being mounted to an aircraft cabin fixture; b. an elongate seal bonded with an epoxy bonding material to the plastic retainer and comprising a polyvinyl fluoride (PVD) film bonded with a contact adhesive to a polyvinylidene fluoride substrate; and c. wherein the elongate seal comprises a generally planar shape when not in contact with an inner sidewall of an aircraft cabin, is flexible, and is positioned in a space between the aircraft cabin fixture and an inner sidewall of an aircraft cabin to seal the space between the aircraft cabin fixture and the inner sidewall. 11. The aircraft seal assembly of claim 10 wherein the polyvinylidene fluoride substrate is polyvinylidene difluoride (PVDF). 12. The aircraft seal assembly of claim 11 wherein the aircraft cabin fixture is selected from the group consisting of: aircraft passenger shells, aircraft passenger seats, aircraft cabin monuments, aircraft cabin partitions, aircraft cabin lavatories, and aircraft cabin storage components. 13. An aircraft seal assembly comprising; a. a plastic retainer having a pair of overlapping reciprocal retainer elements, bonded to each other with an epoxy bonding material, and a plurality of holes through which a plurality of fasteners pass for being mounted to an aircraft cabin fixture; b. an elongate seal having a rounded V shaped bonded with an epoxy bonding material at each terminus of the rounded V shape to the plastic retainer and comprising a polyvinyl fluoride film (PVF) bonded with a contact adhesive to a polyvinylidene fluoride substrate; c. wherein the elongate seal is flexible and is positioned in a space between the aircraft fixture and an inner sidewall of an aircraft cabin to seal a space between the aircraft cabin fixture and the inner sidewall. 14. The aircraft seal assembly of claim 13 wherein the polyvinylidene fluoride substrate is polyvinylidene difluoride (PVDF). 15. The aircraft seal assembly of claim 14 wherein the aircraft cabin fixture is selected from the group consisting of: aircraft passenger shells, aircraft passenger seats, aircraft cabin monuments, aircraft cabin partitions, aircraft cabin lavatories, and aircraft cabin storage components.

Assignees

Inventors

Classifications

  • F16J15/022Primary

    characterised by structure or material · CPC title

  • and with a hollow profile · CPC title

  • B64D11/06Primary

    Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title

  • Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title

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Frequently asked questions

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What does patent US9340291B2 cover?
The invention is a seal assembly, including a polyvinyl fluoride (PVF) film bonded to a polyvinylidene fluoride (PVDF) substrate and attached to a plastic retainer element for being mounted to an aircraft passenger fixture by mounting holes formed in the retainer element through which fasteners extend into the seat. The seal is sufficiently flexible to bend into an inner sidewall of an aircraft…
Who is the assignee on this patent?
Be Aerospace Inc
What technology area does this patent fall under?
Primary CPC classification F16J15/022. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 17 2016 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).