Angled brush seal and gas turbine engine component combination
US-11879340-B1 · Jan 23, 2024 · US
US10260370B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10260370-B2 |
| Application number | US-201414565732-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 10, 2014 |
| Priority date | Dec 10, 2014 |
| Publication date | Apr 16, 2019 |
| Grant date | Apr 16, 2019 |
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An article, for example a turbomachinery article is presented. The article includes a weldable first component having a base portion and a flange portion. The flange portion is outwardly projecting normal to a surface of the base portion; and is joined with the base portion by a solid state joint. The base portion comprises a nanostructured ferritic alloy; and the flange portion comprises a steel substantially free of oxide nanofeatures. The first component is joined to a second component through the flange portion of the first component by a weld joint.
Opening claim text (preview).
The invention claimed is: 1. An article comprising: a first component having a circular base portion extending from an inner periphery to an outer periphery, and a circular flange portion concentric to the circular base portion and is outwardly projecting normal to a surface between the inner periphery and the outer periphery of the circular base portion, wherein the circular base portion comprises a nanostructured ferritic alloy and the circular flange portion comprises a steel substantially free of oxide nanofeatures, and wherein the circular flange portion is joined with the circular base portion by a solid state joint; and a second component that is joined with the flange portion of the first component by a weld joint. 2. The article of claim 1 , wherein the nanostructured ferritic alloy comprises a metal matrix and oxide nanofeatures dispersed within the metal matrix. 3. The article of claim 2 , wherein the metal matrix comprises iron, chromium, cobalt, tungsten, molybdenum, titanium, or a combination thereof. 4. The article of claim 2 , wherein the metal matrix comprises a steel selected from ferritic steel, martensitic steel, austenitic steel, duplex steel and precipitation hardened steel. 5. The article of claim 2 , wherein the oxide nanofeatures comprises yttrium, zirconium, silicon, titanium, hafnium, or a combination thereof. 6. The article of claim 2 , wherein the oxide nanofeatures comprises particles of a median size less than about 20 nanometers. 7. The article of claim 1 , wherein the flange portion comprises ferritic steel, martensitic steel, austenitic steel, duplex steel or precipitation hardened steel. 8. The article of claim 1 , wherein the first component comprises a turhomachinery component selected one or more of a shaft, a wheel, a spacer and an engine disk. 9. The article of claim 1 , wherein the second component comprises a metallic material. 10. The article of claim 9 , wherein the metallic material comprises a steel, a nickel based super alloy, or a nanostructured ferritic alloy. 11. The article of claim 1 , wherein the second component comprises a turbomachinery component selected one or more from a shaft, a wheel, a spacer and an engine disk.
containing silicon · CPC title
Products made by additive manufacturing · CPC title
Processes of additive manufacturing · CPC title
containing N · CPC title
with one or more layers not made from powder, e.g. made from solid metal · CPC title
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