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Nickel-base alloy

Assignee: General Electric Co
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Filing: 1988-07-20
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Granted: —
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Expires: 2008-07-20
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Abstract

Abstract A high temperature-resistant nickel-base alloy adapted for use in turbine nozzle components contains carefully balanced amount of aluminum and titanium to render the alloy repair weldable. The levels of carbon and zirconium are also carefully controlled to improve the castability of the alloy so that large turbine components may be cast without hot tearing or microshrinkage. The alloy consists essentially of, by weight percent, about 0.08% to 0.12% carbon, 0.005% to 0.02% zirconium, 0.005% to 0.015% boron, 0.9% to 1.1% tantalum, 0.7% to 0.9% columbium, 2.2% to 2.4% titanium, 1.1% to 1.3% aluminium, the sum of aluminium plus titanium being about 3.2% to 3.8%, 1.8% to 2.2% tungsten, 22.2% to 22.8% chromium, 18.5% to 19.5% cobalt, with the remainder essentially nickel.

Inventors

  • 👤 John Hebert Wood
  • 👤 John Stuart Haydon

Bibliographic Details

Application Number —
Jurisdiction EP
Data Source google_patents
Last Synchronized 2026-11-06 04:24
CPC Classifications
C; C22; C22C; C22C19/00; C22C19/03; C22C19/05; C22C19/051; C22C19/055

Claims Analysis

Total Claims: 18
Claim 1
Independent Claim 69 words
A nickel-base alloy adapted for welding, consisting essentially of, by weight percent, about 0.08% to 0.12% carbon, 0.005% to 0.02% zirconium, 0.005% to 0.015% boron, 0.9% to 1.1% tantalum, 0.7% to 0.9% columbium, 2.2% to 2.4% titanium, 1.1% to 1.3% aluminum, the sum of aluminum plus titanium being about 3.2% to 3.8%, 1.8% to 2.2% tungsten, 22.2% to 22.8% chromium, 18.5% to 19.5% cobalt, with the remainder essentially nickel.
Claim 2
Dependent Claim 69 words
A nickel-base alloy adapted for welding, consisting essentially of, by weight percent, about 0.08% to 0.12% carbon, 0.005% to 0.02% zirconium, 0.005% to 0.015% boron, 0.9% to 1.1% tantalum, 0.7% to 0.9% columbium, 2.2% to 2.4% titanium, 1.1% to 1.3% aluminum, the sum of aluminum plus titanium being about 3.2% to 3.8%, 1.8% to 2.2% tungsten, 22.2% to 22.8% chromium, 18.5% to 19.5% cobalt, with the remainder essentially nickel.
Claim 3
Dependent Claim 22 words
The alloy of claim 1, wherein said alloy is heat treated at 2100F for 4 hours and at 1475F for 8 hours.
Claim 4
Dependent Claim 12 words
The alloy of claim 1, containing about 6 atomic percent gamma-prime-forming elements.
Claim 5
Dependent Claim 17 words
The alloy of claim 1, wherein said gamma-prime-forming elements consist essentially of aluminum, titanium, tantalum and columbium.
Claim 6
Dependent Claim 15 words
The alloy of claim 1, containing about 28 volume percent of a gamma-prime precipitate phase.
Claim 7
Dependent Claim 25 words
The alloy of claim 1, wherein a ratio of the atomic percent of said aluminum to the atomic percent of said titanium is about 0.91%.
Claim 8
Dependent Claim 47 words
A nickel-base alloy adapted for welding, consisting essentially of, by weight percent, about 0.1% carbon, 0.01% zirconium, 0.01% boron, 1.0% tantalum, 0.8% columbium, 2.3% titanium, 1.2% aluminum, the sum of aluminum plus titanium being about 3.5%, 2.0% tungsten, 22.5% chromium, 19% cobalt, with the remainder essentially nickel.
Claim 9
Dependent Claim 47 words
A nickel-base alloy adapted for welding, consisting essentially of, by weight percent, about 0.1% carbon, 0.01% zirconium, 0.01% boron, 1.0% tantalum, 0.8% columbium, 2.3% titanium, 1.2% aluminum, the sum of aluminum plus titanium being about 3.5%, 2.0% tungsten, 22.5% chromium, 19% cobalt, with the remainder essentially nickel.
Claim 10
Dependent Claim 22 words
The alloy of claim 7, wherein said alloy is heat treated at 2100F for 4 hours and at 1475F for 8 hours.
Claim 11
Dependent Claim 12 words
The alloy of claim 7, containing about 6 atomic percent gamma-prime-forming elements.
Claim 12
Dependent Claim 17 words
The alloy of claim 7, wherein said gamma-prime-forming elements consist essentially of aluminum, titanium, tantalum and columbium.
Claim 13
Dependent Claim 15 words
The alloy of claim 7, containing about 28 volume percent of a gamma-prime precipitate phase.
Claim 14
Dependent Claim 25 words
The alloy of claim 7, wherein a ratio of the atomic percent of said aluminum to the atomic percent of said titanium is about 0.91.
Claim 15
Dependent Claim 12 words
The alloy of claim 8, containing about 6 atomic percent gamma-prime-forming elements.
Claim 16
Dependent Claim 17 words
The alloy of claim 8, wherein said gamma-prime-forming elements consist essentially of aluminum, titanium, tantalum and columbium.
Claim 17
Dependent Claim 15 words
The alloy of claim 8, containing about 28 volume percent of a gamma-prime precipitate phase.
Claim 18
Dependent Claim 25 words
The alloy of claim 8, wherein a ratio of the atomic percent of said aluminum to the atomic percent of said titanium is about 0.91.

References Cited (Backward Citations)

US2766156A Cited
US4039330A Cited
EP0053948A1 Cited
DE3427206C2 Cited

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