Structure formed from composite material

US10167074B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10167074-B2
Application numberUS-201615381946-A
CountryUS
Kind codeB2
Filing dateDec 16, 2016
Priority dateDec 18, 2015
Publication dateJan 1, 2019
Grant dateJan 1, 2019

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  1. Title

    What the patent document calls the invention.

  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 structure formed from composite material and method of forming a structure composite material is disclosed in which one or more metal layers are disposed on the composite material.

First claim

Opening claim text (preview).

The invention claimed is: 1. A composite structure comprising: a composite structural member formed from a synthetic composite material; a sealant layer disposed on a surface of the composite structural member; a first metallic layer disposed on the sealant layer; and a second metallic layer comprising a fastener region, in which one or more fasteners are located, an extent of the first metallic layer being spaced from the fastener region by a predetermined distance, wherein the second metallic layer is disposed in or on a surface of the composite structural member and is overlapped by the first metallic layer, and wherein the sealant layer overlaps the second metallic layer. 2. A composite structure according to claim 1 , wherein the sealant layer is discrete from the composite structural member. 3. A composite structure according to claim 1 , wherein the sealant layer is resiliently deformable. 4. A composite structural member according to claim 1 , wherein the sealant layer comprises one or more polyurethanes. 5. A composite structure according to claim 1 , wherein the sealant layer is configured as a barrier between the composite structural member and the first metallic layer. 6. A composite structure according to claim 1 , wherein the extent of the first metallic layer is restricted to within a predetermined distance of an edge of the composite structural member. 7. A composite structure according to claim 1 , wherein the first metallic layer comprises a thermally applied metal film. 8. A composite structure according to claim 1 , wherein a portion of the first metallic layer overlapping the second metallic layer is configured to provide electrical continuity between the first metallic layer and the second metallic layer. 9. A composite structure according to claim 1 , wherein an overlap of the sealant layer over the second metallic layer is substantially equal to or greater than an overlap of the first metallic layer over the second metallic layer. 10. A composite structure according to claim 1 , wherein an overlap of the second metallic layer and the first metallic layer has a generally uniform width. 11. A composite structure comprising: a composite structural member formed from a synthetic composite material; a metal layer disposed in or on a surface of the composite structural member; a sealant layer disposed on the surface of the composite structural member; and a metallic layer comprising a fastener region, in which one or more fasteners are located, an extent of the metallic layer being spaced from the fastener region by a predetermined distance, wherein the metallic layer is disposed on the sealant layer and overlaps the metal layer, and wherein the sealant layer overlaps the metallic layer. 12. A method for forming a composite structure comprising: forming a composite structural member from a synthetic composite material; disposing a sealant layer on a surface of the composite structural member; disposing a first metallic layer on the sealant layer; disposing a second metallic layer in or on a surface of the composite structural member, wherein the second metallic layer comprises a fastener region, in which one or more fasteners is located, an extent of the first metallic layer being spaced from the fastener region by a predetermined distance, wherein the first metallic layer overlaps the second metallic layer, and wherein the sealant layer overlaps the second metallic layer. 13. A method for forming a composite structure comprising: forming a composite structural member from a synthetic composite material; providing a second metallic layer in or on a surface of the composite structural member, the second metallic layer comprising a fastener region, in which one or more fasteners are located; disposing a sealant layer on the surface of the composite structural member; disposing a first metallic layer on the sealant layer, the first metallic layer being disposed to overlap the second metallic layer; and spacing the first metallic layer from the fastener region by a predetermined distance, wherein the sealant layer overlaps the second metallic layer.

Assignees

Inventors

Classifications

  • comprising polyurethanes · CPC title

  • B32B15/08Primary

    of synthetic resin · CPC title

  • comprising polyurethanes · CPC title

  • with incorporated metallic wires, nets, films or plates (as lost heating elements B29C35/0272, B29C61/0625) · CPC title

  • B64C3/20Primary

    Integral or sandwich constructions · CPC title

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Frequently asked questions

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What does patent US10167074B2 cover?
A structure formed from composite material and method of forming a structure composite material is disclosed in which one or more metal layers are disposed on the composite material.
Who is the assignee on this patent?
Airbus Operations Ltd
What technology area does this patent fall under?
Primary CPC classification B32B15/08. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jan 01 2019 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).