Angled brush seal and gas turbine engine component combination
US-11879340-B1 · Jan 23, 2024 · US
US9546566B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9546566-B2 |
| Application number | US-201214114680-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 24, 2012 |
| Priority date | Apr 29, 2011 |
| Publication date | Jan 17, 2017 |
| Grant date | Jan 17, 2017 |
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The invention relates to a part comprising a coating on a superalloy metal substrate, the coating comprising a metal underlayer covering said substrate, the part being characterized in that said metal underlayer contains a base of nickel aluminide and also contains 0.5 at % to 0.95 at % of one or more stabilizer elements M from the group formed by Cu and Ag for stabilizing the gamma and gamma prime phases.
Opening claim text (preview).
The invention claimed is: 1. A part comprising a coating on a superalloy metal substrate, the coating comprising a metal underlayer covering the substrate, wherein the metal underlayer comprises a base of nickel aluminide and 0.5 at % to 0.95 at % of Ag for stabilizing gamma and gamma prime phases. 2. The part according to claim 1 , wherein the metal underlayer further comprises Cu in the range from 0.5 at % to 0.95 at %. 3. The part according to claim 1 , wherein the metal underlayer further comprises a platinum group element in the range from 2 at % to 30 at % to form a metal underlayer with an NiPtAl type base. 4. The part according to claim 1 , wherein the metal underlayer further comprises at least one reactive element selected from the group consisting of a reactive element of a rare earth type: Hf, Zr, Y, Sr, Ce, La, Yb, Er, and a reactive element Si, wherein each reactive element has a content of from 0.05 at % to 0.25 at %. 5. The part according to claim 1 , wherein the metal underlayer farther comprises, as a reactive element: 0.05 at %≦Hf≦0.2 at %, 0.05 at %≦Y≦0.2 at %, 0.05 at %≦Si≦0.25 at %, or a combination thereof. 6. The part according to claim 1 , wherein the metal underlayer comprises: an NiPtAl type base; as reactive element 0.08 at %≦Hf≦0.20 at %, 0.10 at %≦Y≦0.20 at %, 0.15 at %≦Si≦0.25 at %, or a combination thereof, wherein the Ag content is from 0.75 at % to 0.9 at %. 7. The part according to claim 1 , wherein the metal substrate is made of a nickel-based superalloy. 8. The part according to claim 1 , wherein the coating farther comprises a layer of ceramic covering the metal underlayer. 9. The part according to claim 1 , forming a turbine part for a turbine engine. 10. The part according to claim 1 , constituting a turbine engine blade or vane. 11. The part according to claim 1 , wherein the metal underlayer comprises 0.6 at % to 0.9 at % of Ag. 12. The part according to claim 1 , wherein the metal underlayer comprises 0.7 at % to 0.85 at % of Ag. 13. The part according to claim 1 , wherein the metal underlayer further comprises at least one platinum group element. 14. The part according to claim 1 , wherein the metal underlayer has a thickness of less than 20 μm. 15. The part according to claim 1 , wherein the metal underlayer has a thickness of less than 15 μm. 16. The part according to claim 1 , wherein the metal underlayer further comprises at least one element selected from the group consisting of platinum, chromium, palladium, ruthenium, iridium, osmium and rhodium. 17. The part according to claim 1 , wherein the metal underlayer further comprises at least one element selected from the group consisting of zirconium, cerium, lanthanum, strontium, hafnium, silicon, ytterbium, erbium and yttrium. 18. A method of preparing the part according to claim 1 , comprising coating the superalloy metal substrate with the coating.
Solid state diffusion of only metal elements or silicon into metallic material surfaces · CPC title
with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer · CPC title
Plural oxides · CPC title
After-treatment · CPC title
Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process (C23C26/00, C23C28/00 take precedence) · CPC title
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