Structural material for structure, fuel tank, main wing, and aircraft
US-2015274316-A1 · Oct 1, 2015 · US
US2016196891A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016196891-A1 |
| Application number | US-201414497576-A |
| Country | US |
| Kind code | A1 |
| Filing date | Sep 26, 2014 |
| Priority date | Sep 26, 2014 |
| Publication date | Jul 7, 2016 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
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.
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.
Intrinsically conductive polymers · CPC title
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
Related publications grouped by family.
Answers are generated from the same data shown on this page.