Process for manufacturing a nickel-based alloy product
US-2024384383-A1 · Nov 21, 2024 · US
US2016376685A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016376685-A1 |
| Application number | US-201514748788-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jun 24, 2015 |
| Priority date | Jun 24, 2015 |
| Publication date | Dec 29, 2016 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method of melting and refining an alloy comprises vacuum induction melting starting materials to provide a vacuum induction melted alloy. At least a portion of the vacuum induction melted alloy is electroslag remelted to provide an electroslag remelted alloy. At least a portion of the vacuum arc remelted alloy is vacuum arc remelted to provide a singly vacuum arc remelted alloy. At least a portion of the singly vacuum arc remelted alloy is vacuum arc remelted to provide a doubly vacuum arc remelted alloy. In various embodiments, a composition of the vacuum induction melted alloy comprises primarily one of vanadium, chromium, manganese, iron, cobalt, nickel, copper, niobium, molybdenum, technetium, ruthenium, rhodium, palladium, silver, tantalum, tungsten, rhenium, osmium, iridium, platinum, and gold.
Opening claim text (preview).
We claim: 1 . A method of melting and refining an alloy, the method comprising: vacuum induction melting starting materials to provide a vacuum induction melted alloy; electroslag remelting at least a portion of the vacuum induction melted alloy to provide an electroslag remelted alloy; vacuum arc remelting at least a portion of the electroslag remelted alloy to provide a singly vacuum arc remelted alloy; and vacuum arc remelting at least a portion of the vacuum arc remelted alloy to provide a doubly vacuum arc remelted alloy. 2 . The method of claim 1 , wherein the vacuum induction melted alloy comprises primarily one of vanadium, chromium, manganese, iron, cobalt, nickel, copper, niobium, molybdenum, technetium, ruthenium, rhodium, palladium, silver, tantalum, tungsten, rhenium, osmium, iridium, platinum, and gold. 3 . The method of claim 1 , wherein the vacuum induction melted alloy is a nickel base alloy. 4 . The method of claim 1 , wherein the vacuum induction melted alloy has a composition of Alloy 718. 5 . The method of claim 1 , wherein the vacuum induction melted alloy comprises, in weight percentages based on total alloy weight: 50.0-55.0 Ni; up to 1.0 Co; 17.0-21.0 Cr; up to 0.35 Mn; 2.8-3.3 Mo; 4.75-5.50 Nb; 0.65-1.15 Ti; 0.2-0.8 Al; up to 0.35 Si; up to 0.08 C; up to 0.006 B; and Fe. 6 . The method of claim 1 , wherein the vacuum induction melted alloy has a composition of Alloy 720. 7 . The method of claim 1 , wherein the vacuum induction melted alloy comprises, in weight percentages based on total alloy weight: 50.0-55.0 Ni; up to 1.0 Co; 17.0-21.0 Cr; up to 0.35 Mn; 2.8-3.3 Mo; 4.75-5.50 Nb; 0.65-1.15 Ti; 0.2-0.8 Al; up to 0.35 Si; up to 0.08 C; up to 0.006 B; and Fe. 8 . The method of claim 1 , wherein the vacuum induction melted alloy has a composition of Rene 65 alloy. 9 . The method of claim 1 , wherein the vacuum induction melted alloy comprises, in weight percentages based on total alloy weight: 12.5-13.5 Co; 15.5-16.5 Cr; 0.75-1.20 Fe; 3.8-4.2 Mo; 3.8-4.2 W; 0.6-0.8 Nb; 3.55-3.90 Ti; 1.95-2.30 Al; 0.03-0.06 Zr; 0.005-0.011 C; 0.01-0.02 B; and Ni. 10 . The method of claim 1 , wherein the vacuum induction melted alloy is a nickel-cobalt base alloy. 11 . The method of claim 1 , wherein the vacuum induction melted alloy has a composition of MP35N alloy. 12 . The method of claim 1 , wherein the vacuum induction melted alloy comprises, in weight percentages based on total alloy weight: 33.0-37.0 Ni; 19.0-21.0 Cr; up to 1.0 Fe; up to 0.15 Mn; 9.0-10.5 Mo; up to 1.0 Ti; up to 0.15 Si; up to 0.025 C; and Co. 13 . The method of claim 1 , wherein the vacuum induction melted alloy is a cobalt base alloy. 14 . The method of claim 1 , wherein the vacuum induction melted alloy is a nickel-chromium-molybdenum alloy. 15 . The method of claim 1 , wherein the vacuum induction melted alloy has a composition of C-22 alloy. 16 . The method of claim 1 , wherein the vacuum induction melted alloy comprises, in weight percentages based on total alloy weight: up to 2.5 Co; 20.0-22.5 Cr; 2.0-6.0 Fe; up to 0.50 Mn; 12.5-14.5 Mo; 2.5-3.5 W; up to 0.08 Si; up to 0.015 C; and Ni. 17 . The method of claim 1 , wherein vacuum arc remelting comprises forming a vacuum arc remelted ingot in a crucible, and wherein in at least one of the vacuum arc remelting steps an inert gas is introduced into a gap between the crucible and the ingot. 18 . A method of melting and refining an alloy, the method comprising: vacuum induction melting starting materials to provide an alloy; electroslag remelting at least a portion of the alloy to provide a first ingot; vacuum arc remelting at least a portion of the first ingot to provide a second ingot; and vacuum arc remelting at least a portion of the second ingot. 19 . The method of claim 18 , wherein the alloy comprises primarily one of vanadium, chromium, manganese, iron, cobalt, nickel, copper, niobium, molybdenum, technetium, ruthenium, rhodium, palladium, silver, tantalum, tungsten, rhenium, osmium, iridium, platinum, and gold. 20 . The method of claim 18 , wherein the alloy is a nickel base alloy. 21 . The method of claim 18 , wherein the alloy has a composition of Alloy 718. 22 . The method of claim 18 , wherein the alloy comprises, in weight percentages based on total alloy weight: 50.0-55.0 Ni; up to 1.0 Co; 17.0-21.0 Cr; up to 0.35 Mn; 2.8-3.3 Mo; 4.75-5.50 Nb; 0.65-1.15 Ti; 0.2-0.8 Al; up to 0.35 Si; up to 0.08 C; up to 0.006 B; and Fe. 23 . The method of claim 18 , wherein the alloy has a composition of Alloy 720. 24 . The method of claim 18 , wherein the alloy comprises, in weight percentages based on total alloy weight: 50.0-55.0 Ni; up to 1.0 Co; 17.0-21.0 Cr; up to 0.35 Mn; 2.8-3.3 Mo; 4.75-5.50 Nb; 0.65-1.15 Ti; 0.2-0.8 Al; up to 0.35 Si; up to 0.08 C; up to 0.006 B; and Fe. 25 . The method of claim 18 , wherein the alloy has a composition of Rene 65 alloy. 26 . The method of claim 18 , wherein the alloy comprises, in weight percentages based on total alloy weight: 12.5-13.5 Co; 15.5-16.5 Cr; 0.75-1.20 Fe; 3.8-4.2 Mo; 3.8-4.2 W; 0.6-0.8 Nb; 3.55-3.90 Ti; 1.95-2.30 Al; 0.03-0.06 Zr; 0.005-0.011 C; 0.01-0.02 B; and Ni. 27 . The method of claim 18 , wherein the alloy is a nickel-cobalt base alloy. 28 . The method of claim 18 , wherein the alloy has a composition of MP35N alloy. 29 . The method of claim 18 , wherein the alloy comprises, in weight percentages based on total alloy weight: 33.0-37.0 Ni; 19.0-21.0 Cr; up to 1.0 Fe; up to 0.15 Mn; 9.0-10.5 Mo; up to 1.0 Ti; up to 0.15 Si; up to 0.025 C; and Co. 30 . The method of claim 18 , wherein the alloy is a cobalt base alloy. 31 . The method of claim 18 , wherein the alloy is a nickel-chromium-molybdenum alloy. 32 . The method of claim 18 , wherein the alloy has a composition of C-22 alloy. 33 . The method of claim 18 , wherein the vacuum induction melted alloy comprises, in weight percentages based on total alloy weight: up to 2.5 Co; 20.0-22.5 Cr; 2.0-6.0 Fe; up to 0.50 Mn; 12.5-14.5 Mo; 2.5-3.5 W; up to 0.08 Si; up to 0.015 C; and Ni. 34 . The method of claim 18 , wherein vacuum arc remelting comprises forming a vacuum arc remelted ingot in a crucible, and wherein in at least one of the vacuum arc remelting steps an inert gas is introduced into a gap between the crucible and the ingot.
Related publications grouped by family.
Answers are generated from the same data shown on this page.