US2023151459A1PendingUtilityA1
Nickel-based alloy embodiments and method of making and using the same
Individually held — no corporate assignee on recordPriority: May 11, 2018Filed: Jan 2, 2023Published: May 18, 2023
Est. expiryMay 11, 2038(~11.8 yrs left)· nominal 20-yr term from priority
C22C 19/055C22C 1/023C22F 1/10C22C 19/058C22C 19/051C22C 19/056C22C 19/053
70
PatentIndex Score
0
Cited by
0
References
0
Claims
Abstract
Disclosed herein are embodiments of a nickel-based alloy. In particular embodiments, the nickel-based alloy is configured for use in applications involving supercritical fluids. The disclosed nickel-based alloy embodiments are highly resistant to corrosion and exhibit high stability and thus are suited for use in vessels, boilers, piping, and other receptacles that contain or are used with supercritical fluids. Method embodiments of making the nickel-based alloy also are disclosed.
Claims
exact text as granted — not AI-modifiedWe claim:
1 . An alloy, comprising:
greater than 0 wt % to 80% nickel; greater than 0 wt % to 30% chromium; greater than 0 wt % to 25% cobalt; greater than 0 wt % to 10% aluminum; and greater than 0 wt % to 1% carbon; wherein the alloy does not comprise
(i) 16 wt % Cr, 4.5 wt % Al, 3.5 wt % Fe, 0.05 wt % C, 0.01 wt % B, 0.2 wt % Mn, 0.1 wt % Si, 0.01 wt % Y, 0.02 wt % Zr, and a balance wt % made up of Ni and trace impurities;
(ii) 22 wt % Cr, 5 wt % Co, 2 wt % Mo, 14 wt % W, 0.3 wt % Al, 3 wt % Fe, 0.1 wt % C, 0.015 wt % B, 0.5 wt % Mn, 0.4 wt % Si, 0.02 wt % La, and a balance wt % made up of Ni and trace impurities;
(iii) 25 wt % Cr, 20 wt % Co, 0.5 wt % Mo, 2 wt % Nb, 1.8 wt % Ti, 0.9 wt % Al, 0.7 wt % Fe, 0.03 wt % C, 0.3 wt % Mn, 0.5 wt % Si, and a balance wt % made of Ni and trace impurities;
(iv) 20 wt % Cr, 8 wt % Mo, 3.15 wt % Nb, and a balance wt % made up of Ni and trace impurities;
(v) 23 wt % Cr, 1 wt % Co, 10 wt % Mo, 4.15 wt % Nb, 0.4 wt % Ti, 0.4 wt % Al, 5 wt % Fe, 0.1 wt % C, 0.5 wt % Mn, 0.5 wt % Si, 0.015 wt % P, 0.015 wt % S, and a balance wt % made of Ni and trace impurities; or
(vi) 25 wt % Cr, 3 wt % or less Co, 2.5 wt % or less Mo, 0.7 wt % Nb, 0.1 wt % Al, 37 wt % Ni, 0.03 wt % C, 0.7 wt % Mn, 0.6 wt % Si, 0.2 wt % N, 0.05 wt % C, 0.004 wt % B, and a balance wt % made of Fe and trace impurities.
2 . The alloy of claim 1 , further comprising greater than 0 wt % to 20% Mo, greater than 0 wt % to 20% W, greater than 0 wt % to 5% Ti, greater than 0 wt % to 15% Fe, greater than 0 wt % to 1% B, greater than 0 wt % to 5% Mn, greater than 0 wt % to 5% Si, greater than 0 wt % to 1% Cu, greater than 0 wt % to 1% P, greater than 0 wt % to 1% S, greater than 0 wt % to 10% niobium, or any and all combinations thereof.
3 . The alloy of claim 1 , wherein the alloy comprises 34 wt % to 75 wt % Ni.
4 . The alloy of claim 1 , wherein the alloy comprises 15 wt % to 30 wt % Cr.
5 . The alloy of claim 1 , wherein the alloy comprises 5 wt % to 18 wt % Co.
6 . The alloy of claim 1 , wherein the alloy comprises 0.5 wt % to 4 wt % Nb.
7 . The alloy of claim 1 , wherein the alloy comprises 0.05 wt % to 5 wt % Al.
8 . The alloy of claim 1 , wherein the alloy comprises 0.02 wt % to 0.5 wt % C.
9 . The alloy of claim 1 , wherein the alloy comprises 5 wt % to 10% Mo, 5 wt % to 10% W, 0.5 wt % to 4% Ti, 0.5 wt % to 4% Fe, 0.001 wt % to 0.02% B, greater than 0 wt % to 2% Mn, greater than 0 wt % to 2% Si, greater than 0 wt % to 1% Cu, greater than 0 wt % to 0.1% P, greater than 0 wt % to 0.1% S, 0.5 wt % to 4% niobium, or any and all combinations thereof.
10 . The alloy of claim 1 , wherein the alloy has a microstructure comprising at least one secondary phase.
11 . The alloy of claim 10 , wherein the at least one secondary phase comprises precipitates.
12 . The alloy of claim 10 , wherein the microstructure comprises phase having a grain size of 50 μm to 150 μm.
13 . The alloy of claim 10 , wherein the microstructure comprises a substantially uniformly distributed γ′-phase, a carbide-containing phase, or a combination thereof.
14 . The alloy of claim 1 , wherein the alloy has an exterior surface and the exterior surface is oxidized.
15 . The alloy of claim 14 , wherein the exterior surface is carburized.
16 . A method for making the alloy of claim 1 , comprising:
determining a set of properties for the alloy; determining an initial composition of constituent alloy elements of the alloy; calculating the set of properties for the initial composition of the alloy using thermodynamic and kinetic analysis; and fabricating the alloy of claim 1 .
17 . The method of claim 16 , wherein the alloy is configured for use with a supercritical fluid.
18 . The method of claim 16 , wherein the method further comprises altering the initial composition of constituent alloy elements if the alloy fails to satisfy the set of properties for a solid metallic material as evidenced by substantial cracking and/or fracturing of the alloy.
19 . The method of claim 16 , wherein the set of properties of the alloy comprises a solvus temperature, a liquidus temperature, a solidus temperature, or a combination thereof of a secondary phase of alloy.
20 . The method of claim 16 , wherein the set of properties of the alloy comprises a partition coefficient of the alloy, a yield strength of the alloy, a tensile strength of the alloy, a creep rupture stability of the alloy, or any combination thereof.
21 . The method of claim 16 , further comprising determining at least one subsequent treatment to which the alloy can be subject to improve the set of properties.
22 . The method of claim 21 , wherein the at least one subsequent treatment comprises solution-treating the alloy, homogenizing the alloy, aging the alloy, strain-hardening the alloy, forming a protective coating on the alloy, or any combination thereof.
23 . The method of claim 21 , further comprising exposing the alloy to the at least one subsequent treatment.
24 . The method of claim 16 , further comprising analyzing a microstructure of the alloy using scanning electron microscopy (SEM), scanning electron microscopy-back scattered electron imaging (SEM-BSE), secondary-electron imaging (SE), transmission electron microscopy (TEM), selected area diffraction (SAED), high resolution X-ray diffraction (XRD), energy-dispersive X-ray spectroscopy (EDX), electron energy loss spectroscopy (EELS), or any combination thereof.
25 . The method of claim 16 , further comprising exposing the alloy to a supercritical fluid and measuring corrosion resistance of the alloy.
26 . The method of claim 25 , wherein measuring corrosion resistance of the alloy comprises measuring a change in mass following exposure of the alloy to the supercritical fluid.
27 . A method for fabricating a nickel-based alloy, comprising:
determining a set of properties for the nickel-based alloy; determining an initial composition of constituent alloy elements of the nickel-based alloy; calculating the set of properties selected from a partition coefficient of the alloy, a yield strength of the alloy, a tensile strength of the alloy, a creep rupture stability of the alloy, or any combination thereof for the initial composition of the nickel-based alloy using thermodynamic analysis, a kinetic analysis, or a combination thereof; fabricating the nickel-based alloy; subjecting the nickel-based alloy to at least one subsequent treatment selected from homogenization, aging, strain-hardening, solution-treating, protective coating formation, or combinations thereof at a particular temperature, treatment time period, applied stress, or combinations thereof; analyzing a microstructure of the nickel-based alloy using scanning electron microscopy (SEM), scanning electron microscopy-back scattered electron imaging (SEM-BSE), secondary-electron imaging (SE), transmission electron microscopy (TEM), selected area diffraction (SAED), high resolution X-ray diffraction (XRD), energy-dispersive X-ray spectroscopy (EDX), electron energy loss spectroscopy (EELS), or any combination thereof; analyzing at least one mechanical property of the nickel-based alloy; and exposing the nickel-based alloy to a supercritical fluid;
wherein calculating the set of properties using thermodynamics analysis, kinetics analysis, or combinations thereof is conducted utilizing the Scheil-Gulliver equation and utilizing computer-aided software to generate a solidification plot, an equilibrium plot, a coarsening plot, a stress-strain plot, a partition coefficient, a simulated homogenization treatment, a simulated binding energy, or combinations thereof.Join the waitlist — get patent alerts
Track US2023151459A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.