Graded metallic structures and method of forming; and related articles
Abstract
A metallic structure having a graded microstructure is provided. The metallic structure comprises a graded region comprising a plurality of grains having a gradient in grain size varying as a function of position between a first median grain size at an outer region and a second median grain size at an inner region and a plurality of dispersoids dispersed within the microstructure. The first median grain size is different from the second median grain size. A method of forming a metallic structure having a graded microstructure is also provided. The method comprises: providing a metallic structure comprising at least one reactive species; diffusing at least one reactant at a controlled rate from an outer region of the metallic structure towards an inner region of the metallic structure to form a gradient in reactant activity; reacting the reactant with the reactive species to form a plurality of dispersoids; and heat treating the metallic structure to achieve grain growth so as to form a graded microstructure.
Claims
exact text as granted — not AI-modified1 . A metallic structure having a graded microstructure comprising:
a graded region comprising a plurality of grains having a gradient in grain size varying as a function of position between a first median grain size at an outer region and a second median grain size at an inner region, wherein the first median grain size is different from the second median grain size; and
a plurality of dispersoids dispersed within the microstructure.
2 . The metallic structure of claim 1 , wherein the metallic structure comprises a material selected from the group consisting of cobalt, nickel, iron, and titanium.
3 . The metallic structure of claim 2 , wherein the metallic structure comprises a material selected from the group consisting of a cobalt-based super alloy, a nickel-based super alloy, and a titanium-based alloy.
4 . The metallic structure of claim 3 , wherein the metallic structure comprises a nickel-based super alloy.
5 . The metallic structure of claim 1 , wherein the metallic structure comprises an alloy selected from the group selected from the group consisting of UNS N07718, UNS N13100, UNS N09706, MX4, RENE104, RENE95, RENE88DT, and UDIMET 720.
6 . The metallic structure of claim 1 , wherein the first median grain size has a value in the range from about 100 nanometers to about 1 micrometer.
7 . The metallic structure of claim 6 , wherein the first median grain size has a value in the range from about 100 nanometers to about 500 nanometers.
8 . The metallic structure of claim 1 , wherein the second median grain size has a value in the range from about 10 micrometers to about 100 micrometers.
9 . The metallic structure of claim 8 , wherein the second median grain size has a value in the range from about 10 micrometers to about 50 micrometers.
10 . The metallic structure of claim 1 , wherein the dispersoid comprises a material selected from the group consisting of an oxide, a nitride, a boride, a carbide, an oxynitride, a carbo-nitride.
11 . The metallic structure of claim 10 , wherein the dispersoid comprises an oxide.
12 . The metallic structure of claim 11 , wherein the oxide comprises an oxide selected from the group consisting of alumina, yttria, hafnia, lanthanum oxide, nickel oxide, thoria, titania, zirconia, erbium oxide, ceria, and yttrium aluminum oxide.
13 . The metallic structure of claim 12 , wherein the dispersoids comprise yttria.
14 . The metallic structure of claim 1 , wherein the dispersoids have a median size in the range from about 10 nanometers to about 1 micrometer.
15 . The metallic structure of claim 1 , wherein the dispersoids have a median size in the range from about 10 nanometers to about 100 nanometers
16 . The metallic structure of claim 1 , wherein the metallic structure is structurally stable in a temperature about 600° C. to about 1100° C.
17 . The metallic structure of claim 1 , wherein the metallic structure is a bulk monolithic structure.
18 . A gas turbine component comprising the metallic structure of claim 1 .
19 . A turbine airfoil comprising the metallic structure of claim 1 .
20 . An aircraft engine disc comprising the metallic structure of claim 1 .
21 . A method of forming a metallic structure having a graded microstructure, comprising:
providing a metallic structure comprising at least one reactive species; diffusing at least one reactant, at a controlled rate, from an outer region of the metallic structure towards an inner region of the metallic structure, to form a gradient in reactant activity; reacting the reactant with the reactive species to form a plurality of dispersoids; and heat treating the metallic structure to achieve grain growth, so as to form a graded microstructure, wherein the graded microstructure comprises a graded region comprising a plurality of grains having a gradient in grain size varying as a function of position between a first median grain size at an outer region and a second median grain size at an inner region, wherein the first median grain size is different from the second median grain size; and a plurality of dispersoids dispersed within the microstructure.
22 . The method of claim 21 , wherein the metallic structure comprises a material selected from the group consisting of a cobalt-based super alloy, a nickel-based super alloy, and a titanium-based alloy.
23 . The method of claim 22 , wherein the metallic structure comprises a titanium-based alloy.
24 . The method of claim 21 , wherein diffusing a reactant comprises exposing the metallic structure to an effective activity of the reactant.
25 . The method of claim 24 , wherein exposing the metallic structure to an effective activity of the reactant comprises exposing the metallic structure to a gaseous phase of the reactant.
26 . The method of claim 24 , wherein exposing the metallic structure to an effective activity of the reactant comprises exposing the metallic structure to a liquid phase of the reactant.
27 . The method of claim 21 , wherein diffusing the reactant, at a controlled rate, comprises providing the reactant at a controlled partial pressure.
28 . The method of claim 21 , wherein heat treating the metallic structure to achieve grain growth comprises heating at a temperature in a range from about 600° C. to about 1200° C.
29 . The method of claim 21 , wherein the reactive species comprises a material selected from the group consisting of an oxide former, a carbide former, a nitride former, and a boride former.
30 . The method of claim 29 , wherein the reactive species comprises a plurality of oxide formers.
31 . The method of claim 21 , wherein the reactive species comprises at least one selected from the group consisting of aluminum, yttrium, hafnium, lanthanum, erbium, thorium, titanium, magnesium, cerium, and erbium.
32 . The method of claim 21 , wherein the reactant comprises a material selected from the group consisting of oxygen, boron, carbon, and nitrogen.
33 . The method of claim 21 , wherein the dispersoids comprise a material selected from the group consisting of an oxide, a nitride, a boride, a carbide, a oxynitride, an intermetallic, and a carbo-nitride.
34 . The method of claim 21 , wherein the first median grain size has a value in the range from about 100 nanometers to about 1 micrometer.
35 . The method of claim 21 , wherein the second median grain size has a value in the range from about 10 micrometers to about 50 micrometers.
36 . The method of claim 21 , wherein reacting the reactant with the reactive species comprises:
decomposing a precursor particles, dispersed within the metallic structure, into a product comprising a secondary reactive species and a secondary reactant; and reacting the secondary reactant with the reactive species.Cited by (0)
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