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US3767385A Expired / Lapsed US ⏱️ 0.0 years remaining

Cobalt-base alloys

Assignee: Latrobe Steel Co
•
Filing: 1971-08-24
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Granted: 1973-10-23
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Expires: 1991-08-24
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Abstract

Abstract Work-hardened cobalt-base alloys having high strength and ductility combined with excellent corrosion resistance, characterized by an iron content from 6 to 25 percent by weight but free of embrittling phases often associated with high iron content, the percent by weight of the other principal alloy constituents being: nickel, 18 - 40; molybdenum, 6 - 12; and chromium, 15 - 25. Further alloy embodiments comprising titanium and aluminum or columbium in a total amount up to 8 percent by weight and iron in an amount from 6 to 10 percent retain ductility at elevated temperatures to 900* F.

Inventors

  • 👤 J Slaney

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 17:25
CPC Classifications
C; C22; C22C; C22C19/00; C22C19/07

Claims Analysis

Total Claims: 15
Claim 1
Independent Claim 254 words
A cobalt-base alloy having a hexagonal close-packed platelet phase dispersed in a face-centered cubic matrix phase, said alloy being substantially free of embrittling phases and consisting essentially of the following elements in percent by weight: Carbon 0 - 0.05 Nickel 18 - 40 Molybdenum6 - 12Chromium 15 - 25 Iron 6 - 25 Boron 0 - 0.1 Titanium 0 or 1-5 Aluminum 0 or 0-1 Columbium 0 or 0-2 Cobalt Balance, said alloy either being free of titanium, aluminum, and columbium, or comprising 1 - 5 percent by weight of titanium together with at least aluminum or columbium and not more than 10 percent by weight of iron, the electron vacancy number of the alloy, Nv, defined by Nv 0.61 Ni + 1.71 Co + 2.66 Fe + 4.66 Cr + 5.66 Mo, wherein the chemical symbols represent the effective atomic fractions (as defined) of the respective element present in the alloy, being no greater than 2.55 in those alloys containing from 16 to 25 percent by weight of iron and not exceeding the value Nv 2.82 - 0.017 WFe , where WFe is the percent by weight of iron in the alloy, in those alloys containing from 6 to 16 percent by weight of iron; said alloy having been homogenized by heating at 2,050* - 2,150* F., then haVing been cold-worked at a temperature below the hcp-fcc transformation zone to achieve a reduction in cross-section between about 5 percent and about 70 percent, and then having been heat-aged at 800* - 1,350* F.
Claim 2
Independent Claim 248 words
The method of making a cobalt-base alloy having a hexagonal close-packed platelet phase dispersed in a face-centered cubic matrix phase, said alloy being substantially free of embrittling phases, which comprises forming a melt consisting essentially of the following elements in percent by weight: Carbon 0 - 0.05 Nickel 18 - 40 Molybdenum 6 - 12 Chromium 15 -25 Iron 6 - 25 Boron 0 - 0.1 Titanium 0 or 1-5 Aluminum 0 or 0-1 Columbium 0 or 0-2 Cobalt Balance, said alloy either being free of titanium, aluminum, and columbium, or comprising 1 - 5 percent by weight of titanium together with at least aluminum or columbium and not more than 10 percent by weight of iron, the electron vacancy number of the alloy, Nv, defined by Nv 0.61 Ni + 1.71 Co + 2.66 Fe + 4.66 Cr + 5.66 Mo, wherein the chemical symbols represent the effective atomic fractions (as defined) of the respective elements present in the alloy, being no greater than 2.55 in those alloys containing from 16 to 25 percent by weight of iron and not exceeding the value Nv 2.82 - 0.017 WFe , where WFe is the percent by weight of iron in the alloy, in those alloys containing from 6 to 16 percent by weight of iron; cooling said melt, and cold-working said alloy at a temperature below the lower temperature of the hcp-fcc phase-transformation zone to achieve a reduction in cross-section between about 5 percent and about 70 percent.
Claim 3
Independent Claim 259 words
The method of making a cobalt-base alloy having a hexagonal close-packed platelet phase dispersed in a face-centered cubic matrix phase, said alloy being substantially free of embrittling phases, which comprises forming a melt consisting essentially of the following elements in percent by weight: Carbon 0 - 0.05 Nickel 18 - 40 Molybdenum 6 - 12 Chromium 15 -25 Iron 6 - 25 Boron 0 - 0.1 Titanium 0 or 1-5 Aluminum 0 or 0-1 Columbium 0 or 0-2 Cobalt Balance, said alloy either being free of titanium, aluminum, and columbium, or comprising 1 - 5 percent by weight of titanium together with at least aluminum or columbium and not more than 10 percent by weight of iron, the electron vacancy number of the alloy, Nv, defined by Nv 0.61 Ni + 1.71 Co + 2.66 Fe + 4.66 Cr + 5.66 Mo, wherein the chemical symbols represent the effective atomic fractions (as defined) of the respective elements present in the alloy, being no greater than 2.55 in those alloys containing from 16 to 25 percent by weight of iron and not exceeding the value Nv 2.82 - 0.017 WFe , where WFe is the percent by weight of iron in the alloy, in those alloys containing from 6 to 16 percent by weight of iron; cooling said melt; homogenizing said alloy by heating; cold working said alloy at a temperature below the lower temperature of the hcp-fcc phase-transformation zone to achieve a reduction in cross-section between about 5 percent and about 70 percent; and then heat-aging said cold-worked alloy.
Claim 4
Dependent Claim 185 words
A cobalt-base alloy consisting essentially of the following elements in percent by weight: Carbon 0 - 0.05 Nickel 18 - 40 Molybdenum 6 - 12 Chromium 15 -25 Iron 6 - 25 Boron 0 - 0.1 Titanium 0 or 1-5 Aluminum 0 or 0-1 Columbium 0 or 0-2 Cobalt Balance, said alloy either being free of titanium, aluminum, and columbium, or comprising 1 - 5 percent by weight of titanium together with at least aluminum or columbium and not more than 10 percent by weight of iron, the electron vacancy number of the alloy, Nv, defined by Nv 0.61 Ni + 1.71 Co + 2.66 Fe + 4.66 Cr + 5.66 Mo, wherein the chemical symbols represent the effective atomic fractions (as defined) of the respective elements present in the alloy, being no greater than 2.55 in those alloys containing from 16 to 25 percent by weight of iron and not exceeding the value Nv 2.82 - 0.017 WFe , where WFe is the percent by weight of iron in the alloy, in those alloys containing from 6 to 16 percent by weight of iron.
Claim 5
Dependent Claim 14 words
An alloy as in claim 1 which is homogenized by heating prior to cold-working.
Claim 6
Dependent Claim 13 words
An alloy as in claim 1 which is additionally heat-aged after cold working.
Claim 7
Dependent Claim 14 words
An alloy as in claim 1 which is free of titanium, aluminum, and columbium.
Claim 8
Dependent Claim 18 words
An alloy as in claim 1 in which titanium is present together with at least aluminum or columbium.
Claim 9
Dependent Claim 13 words
An alloy as in claim 2 which has been cold-worked at ambient temperatures.
Claim 10
Dependent Claim 16 words
The method as in claim 3 wherein said alloy is homogenized by heating prior to cold-working.
Claim 11
Dependent Claim 13 words
The method as in claim 3 wherein said alloy is heat-aged after cold-working.
Claim 12
Dependent Claim 15 words
The method as in claim 3 wherein said alloy is powdered prior to cold working.
Claim 13
Dependent Claim 24 words
The method as in claim 13 wherein said powdered alloy is formed into a desired shape by compression and sintering prior to cold working.
Claim 14
Dependent Claim 24 words
The method as in claim 13 wherein said powdered alloy, prior to cold working, is sprayed hot onto a substrate to which it adheres.
Claim 15
Dependent Claim 15 words
The method as in claim 4 wherein said alloy is cold worked at ambient temperature.

References Cited (Backward Citations)

US3356542A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-10-22 1977-04-23 1977-10-23 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-10-22 1981-04-23 1981-10-23 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-10-22 1985-04-23 1985-10-23 $7700.00 Window Closed / Lapsed

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