A process for electrochemical deposition of copper with different current densities
US-2024183052-A1 · Jun 6, 2024 · US
US10017860B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10017860-B2 |
| Application number | US-201414183617-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 19, 2014 |
| Priority date | Feb 19, 2014 |
| Publication date | Jul 10, 2018 |
| Grant date | Jul 10, 2018 |
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.
A component is provided including a body formed at least partially from a composite material. At least a portion of the composite material is covered by a plating. The plating includes a layer of electroless copper, a layer of electrolytic copper, a layer of nickel strike, and a finishing layer.
Opening claim text (preview).
The invention claimed is: 1. An engine-mounted actuator for an aircraft comprising, a body formed at least partially from a thermal plastic material, a portion of the thermal plastic material being covered by a plating, the plating including a layer of electroless copper, a layer of electrolytic copper, a layer of nickel strike, and a finishing layer, the body comprising one of a housing, an endcap or a piston rod of the engine-mounted actuator, the layer of nickel strike having a thickness between 0.00005 inches and 0.0001 inches; wherein the engine-mounted actuator is a hydraulic linear actuator of a thrust reverser actuation system. 2. The engine-mounted actuator according to claim 1 , wherein the layer of electroless copper is arranged directly in contact with an exterior surface of the thermal plastic material. 3. The engine-mounted actuator according to claim 2 , wherein the layer of electrolytic copper is positioned adjacent the layer of electroless copper. 4. The engine-mounted actuator according to claim 3 , wherein the layer of nickel strike is positioned between the layer of electrolytic copper and the finishing layer. 5. The engine-mounted actuator according to claim 1 , wherein the finishing layer includes an additive to enhance the wear resistance of the finishing layer.
Electroplating characterised by the article coated · CPC title
Roughening, e.g. by etching · CPC title
Two or more layers with at least one layer obtained by electroless plating and one layer obtained by electroplating · CPC title
at least one layer being of nickel or chromium · CPC title
Coating with copper · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.