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US4083734A Expired / Lapsed US ⏱️ 0.0 years remaining

Nickel base alloy

Assignee: ALLEGHENY INTERNATIONAL ACCEPTANCE Corp
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Filing: 1976-06-09
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Granted: 1978-04-11
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Expires: 1996-06-09
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Abstract

Abstract A gamma prime strengthened nickel base alloy having a 1650 DEG F impact strength of at least 6 ft.-lbs. after 35,000 hours exposure at 1600 DEG F. The alloy consists essentially of, by weight, from 12.0 to 20.0% chromium, from 4.75 to 7.0% titanium, from 1.3 to 3.0% aluminum, from 13.0 to 19.0% cobalt, from 2.0 to 3.5% molybdenum, from 0.5 to 2.5% tungsten, from 0.005 to 0.03% boron, from 0.005 to 0.045% carbon, up to 0.75% manganese, up to 0.08% zirconium, up to 0.5% 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 0.02% of elements from the group consisting of magnesium, calcium, strontium and barium, balance essentially nickel.

Inventors

  • 👤 William J. Boesch

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 11:55
CPC Classifications
C; C22; C22C; C22C19/00; C22C19/03; C22C19/05; C22C19/051; C22C19/055

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 207 words
A gamma prime strengthened nickel base alloy consisting essentially of, by weight, from 12.0 to 20.0% chromium, from 4.75 to 7.0% titanium, from 1.3 to 3.0% aluminum, from 13.0 to 19.0% cobalt, from 2.0 to 3.5% molybdenum, from 0.5 to 2.5% tungsten, from 0.005 to 0.03% boron, from 0.005 to 0.045% carbon, up to 0.75% manganese, (up) from 0.01 to 0.08% zirconium, up to 0.5% 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 0.02% of elements from the group consisting of magnesium, calcium, strontium and barium, balance essentially nickel; said titanium plus said aluminum content being from 6.5 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 alloy having a 1650° F impact strength of at least 6 ft.-lbs. after 35,000 hours exposure at 1600° F; said alloy forming substantially fewer M 23 C 6 carbides than similar alloys of higher carbon content after long term service at elevated temperatures; said gamma prime being characterized as gamma prime which is substantially spheroidal.
Claim 2
Dependent Claim 207 words
A gamma prime strengthened nickel base alloy consisting essentially of, by weight, from 12.0 to 20.0% chromium, from 4.75 to 7.0% titanium, from 1.3 to 3.0% aluminum, from 13.0 to 19.0% cobalt, from 2.0 to 3.5% molybdenum, from 0.5 to 2.5% tungsten, from 0.005 to 0.03% boron, from 0.005 to 0.045% carbon, up to 0.75% manganese, (up) from 0.01 to 0.08% zirconium, up to 0.5% 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 0.02% of elements from the group consisting of magnesium, calcium, strontium and barium, balance essentially nickel; said titanium plus said aluminum content being from 6.5 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 alloy having a 1650° F impact strength of at least 6 ft.-lbs. after 35,000 hours exposure at 1600° F; said alloy forming substantially fewer M 23 C 6 carbides than similar alloys of higher carbon content after long term service at elevated temperatures; said gamma prime being characterized as gamma prime which is substantially spheroidal.
Claim 3
Dependent Claim 14 words
A nickel base alloy according to claim 1, having from 0.01 to 0.04% carbon.
Claim 4
Dependent Claim 14 words
A nickel base alloy according to claim 1, having from 0.02 to 0.06% zirconium.
Claim 5
Dependent Claim 163 words
A gamma prime strengthened nickel base alloy consisting essentially of, by weight, from 12.0 to 20.0% chromium, from 4.75 to 7.0% titanium, from 1.3 to 3.0% aluminum, from 13.0 to 19.0% cobalt, from 2.0 to 3.5% molybdenum from 0.5 to 2.5% tungsten, from 0.005 to 0.03% boron, from 0.01 to 0.04% carbon, up to 0.75% manganese, (up) from 0.02 to 0.06% zirconium, up to 0.5% iron, up to 0.2% of rare earth elements that will now lower the incipient melting temperature below the solvus temperature of the gamma prime present in the alloy, up to 0.02% of elements from the group consisting of magnesium, calcium, strontium and barium, balance essentially nickel; said titanium plus said aluminum content being from 6.5 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 spheroidal.
Claim 6
Dependent Claim 163 words
A gamma prime strengthened nickel base alloy consisting essentially of, by weight, from 12.0 to 20.0% chromium, from 4.75 to 7.0% titanium, from 1.3 to 3.0% aluminum, from 13.0 to 19.0% cobalt, from 2.0 to 3.5% molybdenum from 0.5 to 2.5% tungsten, from 0.005 to 0.03% boron, from 0.01 to 0.04% carbon, up to 0.75% manganese, (up) from 0.02 to 0.06% zirconium, up to 0.5% iron, up to 0.2% of rare earth elements that will now lower the incipient melting temperature below the solvus temperature of the gamma prime present in the alloy, up to 0.02% of elements from the group consisting of magnesium, calcium, strontium and barium, balance essentially nickel; said titanium plus said aluminum content being from 6.5 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 spheroidal.

References Cited (Backward Citations)

CA921733A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-04-10 1981-10-10 1982-04-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-04-10 1985-10-10 1986-04-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-04-10 1989-10-10 1990-04-11 $7700.00 Window Closed / Lapsed

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