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US4093476A Expired / Lapsed US ⏱️ 0.0 years remaining

Nickel base alloy

Assignee: ALLEGHENY INTERNATIONAL ACCEPTANCE Corp
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Filing: 1976-12-22
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Granted: 1978-06-06
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Expires: 1996-12-22
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Abstract

Abstract A gamma prime strengthened nickel base alloy characterized by good hot corrosion resistance, strength, creep resistance, phase stability and stress rupture life. The alloy consists essentially of, by weight, from 12.0 to 20.0% chromium, from 4.0 to 7.0% titanium, from 1.2 to 3.5% aluminum, from 12.0 to 20.0% cobalt, from 2.0 to 4.0% molybdenum, from 0.5 to 2.5% tungsten, from 0.031 to 0.048% boron, from 0.005 to 0.15% carbon, up to 0.75% manganese, up to 0.5% silicon, up to 1.5% hafnium, up to 0.1% zirconium, up to 1.0% iron, up to 0.2% of rare earth elements that will not lower the incipient melting temperature below the solvus temperature of the gamma prime present in the alloy, up to 0.1% of elements from the group consisting of magnesium, calcium, strontium and barium, up to 6.0% of elements from the group consisting of rhenium and ruthenium, balance essentially nickel.

Inventors

  • 👤 William J. Boesch

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 16:05
CPC Classifications
C; C22; C22C; C22C19/00; C22C19/03; C22C19/05; C22C19/051; C22C19/055

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 222 words
A gamma prime strengthened nickel base alloy consisting essentially of, by weight, from 12.0 to 20.0% chromium, from 4.0 to 7.0% titanium, from 1.2 to 3.5% aluminum, from 12.0 to 20.0% cobalt, from 2.0 to 4.0% molybdenum, from 0.5 to 2.5% tungsten, from 0.031 to 0.048% boron, from 0.005 to 0.045% carbon, up to 0.75% manganese, up to 0.5% silicon, up to 1.5% hafnium, up to 0.1% zirconium, up to 1.0% iron, up to 0.2% of rare earth elements that will not lower the incipient melting temperature below the solvus temperature of the gamma prime present in the alloy, up to 0.1% of elements from the group consisting of magnesium, calcium, strontium and barium, up to 6.0% of elements from the group consisting of rhenium and ruthenium, balance essentially nickel; said titanium plus said aluminum content being from 6.0 to 9.0%; said titanium and aluminum being present in a titanium to aluminum ratio of from 1.75:1 to 3.5:1; said alloy being substantially free of deleterious acicular, sigma and mu phases; said gamma prime being characterized as gamma prime which is substantially speroidal; said alloy being characterized by a highly desirable combination of hot corrosion resistance, strength, creep resistance, phase stability and stress rupture life; said desirable combination of properties being, in part, attributable to said boron content of from 0.031 to 0.048%.
Claim 2
Dependent Claim 222 words
A gamma prime strengthened nickel base alloy consisting essentially of, by weight, from 12.0 to 20.0% chromium, from 4.0 to 7.0% titanium, from 1.2 to 3.5% aluminum, from 12.0 to 20.0% cobalt, from 2.0 to 4.0% molybdenum, from 0.5 to 2.5% tungsten, from 0.031 to 0.048% boron, from 0.005 to 0.045% carbon, up to 0.75% manganese, up to 0.5% silicon, up to 1.5% hafnium, up to 0.1% zirconium, up to 1.0% iron, up to 0.2% of rare earth elements that will not lower the incipient melting temperature below the solvus temperature of the gamma prime present in the alloy, up to 0.1% of elements from the group consisting of magnesium, calcium, strontium and barium, up to 6.0% of elements from the group consisting of rhenium and ruthenium, balance essentially nickel; said titanium plus said aluminum content being from 6.0 to 9.0%; said titanium and aluminum being present in a titanium to aluminum ratio of from 1.75:1 to 3.5:1; said alloy being substantially free of deleterious acicular, sigma and mu phases; said gamma prime being characterized as gamma prime which is substantially speroidal; said alloy being characterized by a highly desirable combination of hot corrosion resistance, strength, creep resistance, phase stability and stress rupture life; said desirable combination of properties being, in part, attributable to said boron content of from 0.031 to 0.048%.
Claim 3
Dependent Claim 14 words
A nickel base alloy according to claim 1, having from 0.032 to 0.045% boron.
Claim 4
Dependent Claim 14 words
A nickel base alloy according to claim 1, having from 0.01 to 0.04% carbon.
Claim 5
Dependent Claim 14 words
A nickel base alloy according to claim 1, having from 0.015 to 0.05% zirconium.
Claim 6
Dependent Claim 14 words
A nickel base alloy according to claim 4, having from 0.02 to 0.035% zirconium.
Claim 7
Dependent Claim 53 words
A nickel base alloy according to claim 1, having from 0.032 to 0.045% boron and from 0.02 to 0.04% carbon; said alloy additionally having a 1650° F impact strength of at least 6 ft.-lbs. after 35,000 hours exposure at 1600° F and an 1800° F/16 ksi stress rupture life at least 120 hours.
Claim 8
Dependent Claim 14 words
A nickel base alloy according to claim 6, having from 0.015 of 0.05% zirconium.
Claim 9
Dependent Claim 14 words
A nickel base alloy according to claim 7, having from 0.02 to 0.035% zirconium.

References Cited (Backward Citations)

US3667938A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-06-05 1981-12-05 1982-06-06 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-06-05 1985-12-05 1986-06-06 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-06-05 1989-12-05 1990-06-06 $7700.00 Window Closed / Lapsed

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