Coated round wire
US-2024368794-A1 · Nov 7, 2024 · US
US9719353B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9719353-B2 |
| Application number | US-201214111417-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 13, 2012 |
| Priority date | Apr 13, 2011 |
| Publication date | Aug 1, 2017 |
| Grant date | Aug 1, 2017 |
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An article may include a substrate, a diffusion barrier layer formed on the substrate, and a protective layer formed on the diffusion barrier coating. The diffusion barrier layer may include iridium.
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The invention claimed is: 1. An article comprising: a nickel-based superalloy substrate including between about 2 wt. % and about 5 wt. % aluminum and between about 2 wt. % and about 5 wt. % titanium, wherein the nickel-based superalloy substrate comprises between 40 volume percent and 55 volume percent gamma-prime precipitate phase; a diffusion barrier layer on the substrate, wherein the diffusion barrier layer comprises an alloy comprising iridium and silicon, and wherein the alloy comprises a majority iridium; and a nickel-based protective layer comprising nickel and at least one of aluminum or chromium on the diffusion barrier layer. 2. The article of claim 1 , further comprising an oxide scale formed on the protective layer, wherein the oxide scale comprises an oxide of the at least one of aluminum or chromium. 3. The article of claim 1 , wherein the alloy of the diffusion barrier layer further comprises chromium, wherein the alloy comprises less than 1 weight percent (wt. %) silicon. 4. The article of claim 1 , wherein the alloy of the diffusion barrier layer further comprises at least one of platinum, palladium, rhenium, ruthenium, or rhodium. 5. The article of claim 1 , wherein a thickness of the diffusion barrier layer and the protective layer, measured in a direction substantially normal to a surface of the substrate on which the diffusion barrier layer and the protective layer are formed, is between about 6.35 μm and about 127 μm. 6. The article of claim 5 , wherein a thickness of the diffusion barrier layer is between about 5 percent and about 50 percent of the thickness of the diffusion barrier layer and the protective layer. 7. The article of claim 1 , wherein the diffusion barrier layer as deposited is essentially free of Ti and Co. 8. The article of claim 1 , wherein the alloy of the diffusion barrier layer comprises less than about 1 weight percent (wt. %) of the silicon and greater than 50 wt. % iridium. 9. A method comprising: forming a diffusion barrier layer on a nickel-based superalloy substrate, wherein the diffusion barrier layer comprises an alloy comprising iridium and silicon, wherein the alloy comprises a majority iridium, wherein the nickel-based superalloy substrate includes between about 2 wt. % and about 5 wt. % aluminum and between about 2 wt. % and about 5 wt. % titanium, and wherein the nickel-based superalloy substrate comprises between about 40 volume percent and about 55 volume percent gamma-prime precipitate phase; and forming a nickel-based protective layer comprising nickel and at least one of aluminum or chromium on the diffusion barrier layer. 10. The method of claim 9 , further comprising forming an oxide scale on the protective layer, wherein the oxide scale comprises at least one of alumina or chromia. 11. The method of claim 9 , wherein the alloy of the diffusion barrier layer further comprises chromium, wherein the alloy comprises less than 1 weight percent (wt. %) silicon. 12. The method of claim 9 , wherein the alloy of the diffusion barrier layer further comprises at least one of Pt, Pd, Re, Ru, or Rh on the substrate. 13. The method of claim 9 , wherein a thickness of the diffusion barrier layer and the protective layer, measured in a direction substantially normal to a surface of the substrate on which the diffusion barrier layer and the protective layer are formed, is between about 6.35 μm inch and about 127 μm. 14. The method of claim 9 , wherein forming the diffusion barrier layer on the substrate comprises forming a diffusion barrier layer essentially free of Ti and Co. 15. The method of claim 9 , wherein forming the diffusion barrier layer on the substrate comprises forming the diffusion barrier layer on the substrate using at least one of directed vapor deposition, electroplating, or nano-electroplating. 16. An article comprising: a nickel-based superalloy substrate including between about 2 wt. % and about 5 wt. % aluminum and between about 2 wt. % and about 5 wt. % titanium, wherein the nickel-based superalloy substrate comprises between 40 volume percent and 55 volume percent gamma-prime precipitate phase; a diffusion barrier layer on the substrate, wherein the diffusion barrier layer comprises an alloy comprising iridium and silicon, and wherein the alloy comprises a predominance of iridium; and a nickel-based protective layer comprising nickel and at least one of aluminum or chromium on the diffusion barrier layer. 17. The article of claim 16 , wherein the alloy of the diffusion barrier layer comprises less than about 1 weight percent (wt. %) of the silicon and between about 10 wt. and about 40 wt. % iridium. 18. The article of claim 17 , wherein the alloy of the diffusion barrier layer comprises between about 26 wt. % and about 65 wt. % Ni, between about 15 wt. % and about 30 wt. % Fe, between about 10 wt. % and about 30 wt. % Cr, less than about 1 wt. % Mn, less than about 2 wt. % Al. 19. The article of claim 18 , wherein the diffusion barrier layer as deposited is essentially free of Ti and Co.
only coatings of metal elements only · CPC title
the rotor disc being formed of sheet laminae (rotor blade aggregates of unitary construction F01D5/34) · CPC title
on metallic substrates or on substrates of boron or silicon · CPC title
with at least one oxide layer · CPC title
including layers graded in composition or physical properties · CPC title
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