Method for mitigating edge glow

US2016196891A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016196891-A1
Application numberUS-201414497576-A
CountryUS
Kind codeA1
Filing dateSep 26, 2014
Priority dateSep 26, 2014
Publication dateJul 7, 2016
Grant date

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

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Composite structures and methods for mitigating edge glow resulting from lightning strikes on composite structures, such as aerospace structures, containing carbon fiber reinforced plastic components. One or more thin layers of conductive coating material is applied over a cut edge or drop off of the carbon fiber reinforced plastic components to reduce inter-ply voltage potential between composite layers of the carbon fiber reinforced plastic component. The conductive coating material is made of a conductive doping material dispersed in a carrier medium.

First claim

Opening claim text (preview).

1 . A method for mitigating edge glow at an exposed fiber surface in a carbon fiber reinforced plastic component of a composite structure, the method comprising: applying a conductive coating material over the exposed fiber surface. 2 . The method of claim 1 , wherein the conductive coating material has a conductivity of at least about 10 Siemens/meter. 3 . The method of claim 1 , wherein the conductive coating material has a conductivity of at least about 10 4 Siemens/meter. 4 . The method of claim 1 , wherein the conductive coating material is applied in one or more layers having a total thickness of about 0.001 to 0.003 inch. 5 . The method of claim 1 , wherein the conductive coating material is applied in a layer having a thickness of about 0.002 inch. 6 . The method of claim 1 , wherein the conductive coating material comprises a conductive doping material and a carrier medium. 7 . The method of claim 6 , wherein the conductive doping material is a material selected from the group consisting of indium tin oxide solutions, carbon nanotubes, metallic nanowires, semiconducting nanowires, carbon black, graphene and intrinsically conductive polymers. 8 . The method of claim 6 , further comprising the steps of: selecting the carrier medium; selecting the conductive doping material; combining the carrier medium and doping material to form the conductive coating material. 9 . A method of fabricating a composite structure comprising: forming at least one carbon fiber reinforced plastic component with at least one exposed fiber surface; forming the composite structure from the at least one carbon fiber reinforced plastic component; and applying a conductive coating material over the exposed fiber surface. 10 . The method of claim 9 , wherein the conductive coating material has a conductivity of at least about 10 Siemens/meter. 11 . The method of claim 9 , wherein the conductive coating material has a conductivity of at least about 10 4 Siemens/meter. 12 . The method of claim 9 , wherein conductive coating material is applied in one or more layers to a total thickness of about 0.001 to 0.003 inch. 13 . The method of claim 9 , wherein the conductive coating material comprises a carrier medium and a conductive doping material. 14 . The method of claim 13 , wherein the conductive coating material is a material selected from the group consisting of indium tin oxide solutions, carbon nanotubes, metallic nanowires, semiconducting nanowires, carbon black, graphene and intrinsically conductive polymers. 15 . The method of claim 9 , wherein the composite structure defines a fuel environment. 16 . A composite structure comprising carbon fiber reinforced plastic components having at least one exposed fiber surface, and a conductive coating material applied over the at least one exposed fiber surface. 17 . The composite structure of claim 16 , wherein the conductive coating material has a conductivity of at least about 10 Siemens/meter. 18 . The composite structure of claim 16 , wherein the conductive coating material has a conductivity of at least about 10 4 Siemens/meter. 19 . The composite structure of claim 16 , wherein the conductive coating material has a total thickness of about 0.001 to 0.003 inch. 20 . The composite structure of claim 16 , wherein the conductive coating material comprises a conductive doping material and a carrier medium, the conductive doping material being selected from the group consisting of indium tin oxide solutions, carbon nanotubes, metallic nanowires, semiconducting nanowires, carbon black, graphene and intrinsically conductive polymers.

Assignees

Inventors

Classifications

  • Intrinsically conductive polymers · CPC title

  • H01B1/04Primary

    mainly consisting of carbon-silicon compounds, carbon or silicon · CPC title

  • characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced · CPC title

  • Lightning protectors; Static dischargers · CPC title

  • oxides · CPC title

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What does patent US2016196891A1 cover?
Composite structures and methods for mitigating edge glow resulting from lightning strikes on composite structures, such as aerospace structures, containing carbon fiber reinforced plastic components. One or more thin layers of conductive coating material is applied over a cut edge or drop off of the carbon fiber reinforced plastic components to reduce inter-ply voltage potential between compos…
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification H01B1/04. Mapped technology areas include Electricity.
When was this patent published?
Publication date Thu Jul 07 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).