Turbine engine seal for high erosion environment
US-10294962-B2 · May 21, 2019 · US
US10829647B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10829647-B2 |
| Application number | US-201816216672-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 11, 2018 |
| Priority date | Dec 11, 2018 |
| Publication date | Nov 10, 2020 |
| Grant date | Nov 10, 2020 |
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.
Disclosed is a corrosion inhibition coating, comprising: a base comprising a matrix and a metal within the matrix; and an inhibitor comprising: zinc molybdate, cerium citrate, magnesium metasilicate, a metal phosphate silicate, or a combination thereof, wherein the metal within the matrix comprises aluminum, an aluminum alloy, zinc, a zinc alloy, magnesium, a magnesium alloy, or a combination thereof. Also disclosed is a substrate coated with the corrosion inhibition coating.
Opening claim text (preview).
What is claimed is: 1. A corrosion inhibition coating composition, comprising: a base comprising a matrix and a metal within the matrix; and an inhibitor comprising two or more of: zinc molybdate, cerium citrate, magnesium metasilicate, a metal phosphate silicate, wherein the metal within the matrix comprises aluminum, an aluminum alloy, zinc, a zinc alloy, magnesium, a magnesium alloy, or any combination(s) thereof. 2. The corrosion inhibition coating composition of claim 1 , wherein the matrix comprises silicate, epoxy, ceramic, or any combination(s) thereof. 3. The corrosion inhibition coating composition of claim 1 , wherein the corrosion inhibition coating composition comprises: about 70% to about 95% base by volume; and about 5% to about 30% inhibitor by volume. 4. The corrosion inhibition coating composition of claim 1 , wherein the corrosion inhibition coating composition comprises less than or equal to about 10% inhibitor by volume. 5. The corrosion inhibition coating composition of claim 1 , wherein the inhibitor comprises three or more of: zinc molybdate; cerium citrate; magnesium metasilicate; a metal phosphate silicate. 6. The corrosion inhibition coating composition of claim 1 , wherein the corrosion inhibition coating composition comprises 0% chromium. 7. The corrosion inhibition coating composition of claim 1 , wherein the corrosion inhibition coating composition comprises 0% magnesium molybdate. 8. The corrosion inhibition coating composition of claim 1 , wherein the metal phosphate silicate comprises aluminum phosphate silicate, zinc phosphate silicate, calcium phosphate silicate, strontium phosphate silicate, or any combination(s) thereof. 9. The corrosion inhibition coating composition of claim 1 , wherein the inhibitor is a powder. 10. The corrosion inhibition coating composition of claim 1 , wherein the inhibitor is mixed within the base. 11. The corrosion inhibition coating composition of claim 1 , wherein the base and the inhibitor are two distinct layers. 12. The corrosion inhibition coating composition of claim 11 , wherein the inhibitor is coated on the base. 13. The corrosion inhibition coating composition of claim 11 , further comprising a second matrix, wherein the inhibitor is mixed within the second matrix. 14. The corrosion inhibition coating composition of claim 13 , wherein the second matrix comprises silicate, epoxy, ceramic, or any combination(s) thereof. 15. A substrate coated with the corrosion inhibition coating composition of claim 1 . 16. The substrate of claim 15 , wherein the substrate comprises steel, aluminum, zinc, magnesium, or any combination(s) thereof. 17. The substrate of claim 15 , wherein the substrate is an aircraft component. 18. The substrate of claim 17 , wherein the aircraft component is a propeller blade, a propeller shank, a propeller hub, a propeller barrel, a propeller tulip, a landing gear component, an engine gear, an engine disc, a shaft, a strut, or a counterweight. 19. A corrosion inhibition coating composition comprising: a base comprising a matrix and a metal within the matrix; and an inhibitor comprising: zinc molybdate; cerium citrate; magnesium metasilicate; and a metal phosphate silicate, wherein the metal within the matrix comprises aluminum, an aluminum alloy, zinc, a zinc alloy, magnesium, a magnesium alloy, or any combination(s) thereof. 20. A corrosion inhibition coating composition comprising: a base comprising a matrix and a metal within the matrix; and an inhibitor comprising: zinc molybdate; and cerium citrate, wherein the metal within the matrix comprises aluminum, an aluminum alloy, zinc, a zinc alloy, magnesium, a magnesium alloy, or any combination(s) thereof.
containing Al · CPC title
using reducing agents for coating with metallic material not provided for in a single one of groups C23C18/32 - C23C18/50 · CPC title
Metal salts of carboxylic acids · CPC title
of molybdenum · CPC title
Phosphorous, arsenic, antimony or bismuth containing compounds · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.