Alloy

US11898228B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11898228-B2
Application numberUS-202117402699-A
CountryUS
Kind codeB2
Filing dateAug 16, 2021
Priority dateAug 20, 2020
Publication dateFeb 13, 2024
Grant dateFeb 13, 2024

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A nickel-cobalt based superalloy composition consisting of by weight (wt.): 33.5 to 54 percent Ni; 19.5 to 36 percent Co; 9 to 12 percent Cr; 3.9 to 5.5 percent Al; 4.5 to 9.5 percent W; up to 5.5 percent Fe; 2 to 3.5 percent Mo; 0.6 to 5 percent Ta; 0.15 to 2.2 percent Ti; up to 1.75 percent Nb; up to 0.1 percent Hf; 0.005 to 0.03 percent C; 0.001 to 0.02 percent B; 0.005 to 0.06 percent Zr; up to 0.3 percent Si; up to 0.6 percent Mn; and the balance being impurities.

First claim

Opening claim text (preview).

The invention claimed is: 1. A nickel-cobalt based superalloy composition consisting of, by weight: 33.5 to 54 percent nickel; 19.5 to 36 percent cobalt; 9.0 to 12.0 percent chromium; 3.9 to 5.5 percent aluminium; 5.39 to 9.5 percent tungsten; up to 5.5 percent iron; 2 to 3.5 percent molybdenum; 0.6 to 5 percent tantalum; 0.15 to 2.2 percent titanium; up to 1.75 percent niobium; up to 0.1 percent hafnium; 0.005 to 0.03 percent carbon; 0.001 to 0.02 percent boron; 0.005 to 0.06 percent zirconium; up to 0.3 percent silicon; up to 0.6 percent manganese; and the balance being impurities. 2. A nickel-cobalt based superalloy according to claim 1 , wherein the nickel and cobalt (Ni:Co) are present in the ratio between 1:1 and about 2.6:1 in atomic percent. 3. A nickel-cobalt based superalloy as claimed in claim 1 comprising by atomic percentage: 9-11.5 percent aluminium; 1.5 to 3 percent tungsten; 0.25-1.6 percent tantalum; 0.3-2.5 percent titanium; and up to 1 percent niobium; wherein a combined atomic percentage of aluminium, tantalum, titanium, niobium and 0.62 of tungsten in the nickel-cobalt based superalloy is between 12.5 and 16.25 percent to provide substantially 50 to 65 percent by volume gamma prime precipitates. 4. A nickel-cobalt based superalloy according to claim 1 comprising by atomic percentage: 1.5-3 percent tungsten; 1.3-2 percent molybdenum; wherein a combined atomic percentage of Mo+0.38 of W in the nickel-cobalt based superalloy is at least 2.44 percent. 5. A nickel-cobalt based superalloy as claimed in claim 1 , wherein: the density at ambient temperature is less than 8.5 grams per cubic centimetre; and a combined atomic percentage of Mo+0.38 is no greater than 2.5 percent and a combined atomic percentage of W+Ta+Nb is no greater than 3.8 percent. 6. A nickel-cobalt based superalloy according to claim 1 , wherein the nickel-cobalt based superalloy has a gamma prime solvus temperature of 1020 to 1125° C. 7. A nickel-cobalt based superalloy as claimed in claim 1 , and comprising by weight: 47 to 54 percent nickel; and 19.5 to 25 percent cobalt. 8. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 35.5% cobalt; 10.5% chromium; 5.4% tungsten; 2.9% molybdenum; 4.15% aluminium; 3% tantalum; 1.5% niobium; 1.5% titanium; 0.015% carbon; 0.009% boron; 0.039% zirconium; and the balance being nickel and impurities. 9. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 31.1% cobalt; 10.5% chromium; 5.4% tungsten; 2.9% molybdenum; 4.15% aluminium; 3% tantalum; 1.5% niobium; 1.5% titanium; 0.015% carbon; 0.009% boron; 0.039% zirconium; and the balance being nickel and impurities. 10. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 28.1% cobalt; 10.5% chromium; 5% iron; 5.4% tungsten; 2.9% molybdenum; 4.15% aluminium; 3% tantalum; 1.5% niobium; 1.5% titanium; 0.015% carbon; 0.009% boron; 0.039% zirconium; and the balance being nickel and impurities. 11. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 28.0% cobalt; 10.5% chromium; 5% iron; 5.4% tungsten; 2.9% molybdenum; 4.15% aluminium; 3% tantalum; 1.5% niobium; 1.5% titanium; 0.5% manganese; 0.1% silicon; 0.015% carbon; 0.009% boron; 0.039% zirconium; and the balance being nickel and impurities. 12. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 19.8% cobalt; 10.5% chromium; 6.2% tungsten; 2.8% molybdenum; 4.4% aluminium; 3.8% tantalum; 0.8% niobium; 0.8% titanium; 0.015% carbon; 0.009% boron; 0.030% zirconium; and the balance being nickel and impurities. 13. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 31.0% cobalt; 10.6% chromium; 5.5% tungsten; 2.9% molybdenum; 4.2% aluminium; 3.1% tantalum; 1.9% titanium; 0.015% carbon; 0.009% boron; 0.039% zirconium; and the balance being nickel and impurities. 14. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 34.5% cobalt; 10.3% chromium; 8.4% tungsten; 3.2% molybdenum; 4.5% aluminium; 3.75% tantalum; 1.0% titanium; 0.020% carbon; 0.008% boron; 0.030% zirconium; and the balance being nickel and impurities. 15. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 34.0% cobalt; 10.4% chromium; 8.4% tungsten; 3.2% molybdenum; 4.5% aluminium; 3.75% tantalum; 1.8% titanium; 0.020% carbon; 0.008% boron; 0.030% zirconium; and the balance being nickel and impurities. 16. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 34.5% cobalt; 10.3% chromium; 8.3% tungsten; 3.2% molybdenum; 4.45% aluminium; 3.7% tantalum; 0.8% niobium; 0.25% titanium; 0.020% carbon; 0.007% boron; 0.030% zirconium; and the balance being nickel and impurities. 17. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 34.2% cobalt; 10.3% chromium; 8.3% tungsten; 3.2% molybdenum; 4.4% aluminium; 3.7% tantalum; 1.5% niobium; 0.25% titanium; 0.020% carbon; 0.007% boron; 0.030% zirconium; and the balance being nickel and impurities. 18. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 20.3% cobalt; 10.7% chromium; 6.3% tungsten; 2.9% molybdenum; 4.5% aluminium; 0.8% tantalum; 0.4% niobium; 0.8% titanium; 0.25% silicon; 0.015% carbon; 0.009% boron; 0.030% zirconium; and the balance being nickel and impurities. 19. A nickel-cobalt based superalloy as claimed in claim 1 , wherein the nickel-cobalt based superalloy consists of, by weight: 34.1% cobalt; 11.3% chromium; 8.4% tungsten; 3.2% molybdenum; 5.2% aluminium; 3.8% tantalum; 0.015% carbon; 0.015% boron; 0.060% zirconium; and the balance being nickel and impurities. 20. A nickel-cobalt based superalloy composition consisting of, by weight: 33.5 to 54 percent nickel; 19.5 to 36 percent cobalt; 9.0 to 12.0 percent chromium; 3.9 to 5.5 percent aluminium; 4.5 to 9.5 percent tungsten; up to 5.5 percent iron; 2 to 3.5 percent molybdenum; 0.6 to 3.4 percent tantalum; 0.15 to 2.2 percent titanium; up to 1.75 percent niobium; up to 0.1 percent hafnium; 0.005 to 0.03 percent carbon; 0.001 to 0.02 percent boron; 0.005 to 0.06 percent zirconium; up to 0.3 percent silicon; up to 0.6 percent manganese; and the balance being impurities. 21. A nickel-cobalt based superalloy composition consisting of, by weight: 33.5 to 54 percent nickel; 19.5 to 36 percent cobalt; 9.0 to 12.0 percent chromium; 3.9 to 5.5 percent aluminium; 4.5 to 9.5 percent tungsten; up to 5.5 percent iron; 2 to 3.5 percent molybdenum; 0.6 to 3.80 percent tantalum; 0.15 to 2.2 percent titanium; up to 1.75 percent niobium; up to 0.1 percent hafnium; 0

Assignees

Inventors

Classifications

  • C22C30/00Primary

    Alloys containing less than 50% by weight of each constituent · CPC title

  • with the maximum Cr content being at least 10% but less than 20% · CPC title

  • with the maximum Cr content being less 10% · CPC title

  • C22C19/05Primary

    with chromium · CPC title

  • of nickel or cobalt or alloys based thereon · CPC title

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What does patent US11898228B2 cover?
A nickel-cobalt based superalloy composition consisting of by weight (wt.): 33.5 to 54 percent Ni; 19.5 to 36 percent Co; 9 to 12 percent Cr; 3.9 to 5.5 percent Al; 4.5 to 9.5 percent W; up to 5.5 percent Fe; 2 to 3.5 percent Mo; 0.6 to 5 percent Ta; 0.15 to 2.2 percent Ti; up to 1.75 percent Nb; up to 0.1 percent Hf; 0.005 to 0.03 percent C; 0.001 to 0.02 percent B; 0.005 to 0.06 percent Zr; u…
Who is the assignee on this patent?
Rolls Royce Plc
What technology area does this patent fall under?
Primary CPC classification C22C30/00. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Feb 13 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).