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US4245698A Expired / Lapsed US ⏱️ 0.0 years remaining

Superalloys having improved resistance to hydrogen embrittlement and methods of producing and using the same

Assignee: ExxonMobil Technology and Engineering Co
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Filing: 1978-03-01
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Granted: 1981-01-20
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Expires: 1998-03-01
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Abstract

Abstract Cold-worked superalloys having improved resistance to hydrogen embrittlement are disclosed. These new superalloys are nickel- or cobalt-chromium-molybdenum superalloys and possess improved resistance to hydrogen embrittlement rendering them useful in deep sour gas wells.

Inventors

  • 👤 Barry J. Berkowitz
  • 👤 Russell D. Kane

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 00:44
CPC Classifications
C; C22; C22C; C22C19/00; C22C19/03; C22C19/05; C22C19/051; C22C19/055; Y; Y10; Y10S; Y10S166/00; Y10S166/902

Claims Analysis

Total Claims: 23
Claim 1
Independent Claim 110 words
A cold-worked and age strengthened nickel and/or cobalt, chromium, molybdenum superalloy having less than 1 At% phosphorus in its grain boundaries, a tensile strength ranging from 150 to about 250 ksi and a resistance to hydrogen embrittlement such that when a steel anode is galvanically coupled to a test specimen of said superalloy and said test specimen is exposed to an aqueous test solution saturated with hydrogen sulfide containing 5% NaCl and 0.5% acetic acid, by weight, at room temperature and at atmospheric pressure, the test specimen resists hydrogen embrittlement or cracking for more than 25 days when it is stressed to 100% of the transverse 0.2% offset yield strength.
Claim 2
Dependent Claim 110 words
A cold-worked and age strengthened nickel and/or cobalt, chromium, molybdenum superalloy having less than 1 At% phosphorus in its grain boundaries, a tensile strength ranging from 150 to about 250 ksi and a resistance to hydrogen embrittlement such that when a steel anode is galvanically coupled to a test specimen of said superalloy and said test specimen is exposed to an aqueous test solution saturated with hydrogen sulfide containing 5% NaCl and 0.5% acetic acid, by weight, at room temperature and at atmospheric pressure, the test specimen resists hydrogen embrittlement or cracking for more than 25 days when it is stressed to 100% of the transverse 0.2% offset yield strength.
Claim 3
Dependent Claim 45 words
The cold-worked and age strengthened superalloy of claim 1 wherein said superalloy contains 12 to 25 wt. % chromium, from 10 to about 20 wt. % molybdenum, up to 10 wt. % iron, up to about 50 wt. % cobalt and the balance essentially nickel.
Claim 4
Dependent Claim 32 words
The superalloy of claim 2 wherein the superalloy is further characterized as containing less than 0.003 wt. % phosphorus, less than 0.02 wt. % carbon and less than 0.08 wt. % silicon.
Claim 5
Dependent Claim 54 words
The superalloy of claim 1 wherein said superalloy has the following chamical composition in weight percent: ______________________________________ Phosphorus <0.002 Chromium 14-17 Molybdenum 14-16 Iron 0-7 Cobalt 0-2.5 Aluminum 0-0.25 Columbium 0-4 Titanium, Zirconium or Hafnium 0-0.75 Tungsten 0-4 Manganese 0-1 Vanadium or Tantalum 0-0.4 Carbon 0-0.01 Silicon 0-0.03 Nickel and Incidental Impurities Balance ______________________________________
Claim 6
Dependent Claim 117 words
A cold-worked and age strengthened nickel and/or cobalt, chormium, molybdenum superalloy characterized by having less than 1 At% phosphorus in its grain boundaries, a high tensile strength and an improved resistance to hydrogen embrittlement when subjected to an oxygen-free hydrogen sulfide saturated, aqueous solution containing 5% NaCl and 0.5% acetic acid, by weight, at room temperature and at atmospheric pressure, said superalloy comprising 12 to 25 wt. % chromium, from about 10 to about 20 wt. % molybdenum, up to 10 wt. % iron, up to about 50 wt. % cobalt and the balance essentially nickel, and wherein the phosphorus content in said superalloy is maintained and controlled at a level of less than 0.003 wt. %.
Claim 7
Dependent Claim 117 words
A cold-worked and age strengthened nickel and/or cobalt, chormium, molybdenum superalloy characterized by having less than 1 At% phosphorus in its grain boundaries, a high tensile strength and an improved resistance to hydrogen embrittlement when subjected to an oxygen-free hydrogen sulfide saturated, aqueous solution containing 5% NaCl and 0.5% acetic acid, by weight, at room temperature and at atmospheric pressure, said superalloy comprising 12 to 25 wt. % chromium, from about 10 to about 20 wt. % molybdenum, up to 10 wt. % iron, up to about 50 wt. % cobalt and the balance essentially nickel, and wherein the phosphorus content in said superalloy is maintained and controlled at a level of less than 0.003 wt. %.
Claim 8
Dependent Claim 56 words
A cold-worked and age strengthened superalloy in accordance with claim 5 having the following composition in weight percent: ______________________________________ Phosphorus <0.003 Chromium 12-15 Molybdenum 10-20 Iron 0-10 Cobalt 0-50 Aluminum 0-0.5 Columbium 0-4 Titanium, Zirconium or Hafnium 0-3 Tungsten 0-7 Manganese 0-1 Vanadium or Tantalum 0-0.75 Carbon 0-0.02 Silicon 0-0.08 Nickel and Incidental Impurities Balance ______________________________________
Claim 9
Dependent Claim 56 words
A cold-worked and age strengthened superalloy in accordance with claim 5 having the following composition in weight percent: ______________________________________ Phosphorus <0.002 Chromium 14-17 Molybdenum 14-16 Iron 0-7 Cobalt 0-2.5 Aluminum 0-0.5 Columbium 0-4 Titanium, Zirconium or Hafnium 0-0.75 Tungsten 0-4 Manganese 0-1 Vanadium or Tantalum 0-0.4 Carbon 0-0.01 Silicon 0-0.03 Nickel and Incidental Impurities Balance ______________________________________
Claim 10
Dependent Claim 49 words
A cold-worked and age strengthened superalloy in accordance with claim 5 having the following composition in weight percent: ______________________________________ Phosphorus <0.001 Chromium 14-16 Molybdenum 15-17 Iron 4-7 Cobalt 0-2.5 Aluminum 0-0.2 Titanium 0-0.5 Tungsten 3-4.5 Manganese 0-1 Vanadium 0-0.4 Carbon 0-0.01 Silicon 0-0.03 Nickel 52-56 Incidental Impurities Balance ______________________________________
Claim 11
Dependent Claim 23 words
The superalloy of claim 5 wherein the superalloy has been cold-worked within the range from about 15% to about 90% reduction in area.
Claim 12
Dependent Claim 23 words
The superalloy of claim 6 wherein the superalloy has been cold-worked within the range from about 25% to about 75% reduction in area.
Claim 13
Dependent Claim 23 words
The superalloy of claim 7 wherein the superalloy has been cold-worked within the range from about 35% to about 65% reduction in area.
Claim 14
Dependent Claim 23 words
The superalloy of claim 8 wherein the superalloy has been cold-worked within the range from about 35% to about 65% reduction in area.
Claim 15
Dependent Claim 27 words
The superalloy of claim 5 which is further characterized as having been strengthened by aging at a temperature ranging from about 800° F. to about 1200° F.
Claim 16
Dependent Claim 12 words
The superalloy of claim 5 in the form of a tubular conduit.
Claim 17
Dependent Claim 135 words
A process for producing a superalloy characterized as having a high tensile stength and an improved resistance to hydrogen embrittlement when subjected to an oxygen-free hydrogen sulfide saturated aqueous solution containing 5% NaCl and 0.5% acetic acid, by weight, at room temperature and at atmospheric pressure, which comprises treating an alloy of the following chemical composition in weight percent: ______________________________________ Phosphorus <0.003 Chromium 12-25 Molybdenum 10-20 Iron 0-10 Cobalt 0-50 Aluminum 0-0.5 Columbium 0-4 Titanium, Zirconium or Hafnium 0-3 Tungsten 0-7 Manganese 0-1 Vanadium or Tantalum 0-0.75 Carbon 0-0.02 Silicon 0-0.08 Nickel and Incidental Impurities Balance ______________________________________ by the steps: (a) cold-working said alloy within the range from about 15% to about 90% reduction in area, and (b) age strengthening the cold-worked alloy at a temperature ranging from about 300° F. to about 1100° F.
Claim 18
Dependent Claim 135 words
A process for producing a superalloy characterized as having a high tensile stength and an improved resistance to hydrogen embrittlement when subjected to an oxygen-free hydrogen sulfide saturated aqueous solution containing 5% NaCl and 0.5% acetic acid, by weight, at room temperature and at atmospheric pressure, which comprises treating an alloy of the following chemical composition in weight percent: ______________________________________ Phosphorus <0.003 Chromium 12-25 Molybdenum 10-20 Iron 0-10 Cobalt 0-50 Aluminum 0-0.5 Columbium 0-4 Titanium, Zirconium or Hafnium 0-3 Tungsten 0-7 Manganese 0-1 Vanadium or Tantalum 0-0.75 Carbon 0-0.02 Silicon 0-0.08 Nickel and Incidental Impurities Balance ______________________________________ by the steps: (a) cold-working said alloy within the range from about 15% to about 90% reduction in area, and (b) age strengthening the cold-worked alloy at a temperature ranging from about 300° F. to about 1100° F.
Claim 19
Dependent Claim 148 words
A process for recovering oil and/or gas from subterranean surfaces under conditions of high stress and hydrogen sulfide environments which comprises using a tubular conduit for transporting said oil and/or gas from subterranean surfaces, wherein said tubular conduit comprises a cold-worked and age strengthened nickel and/or cobalt, chromium, molybdenum superalloy having less than 1 At% phosphorus in its grain boundaries, a tensile strength ranging from 150 to about 250 ksi and a resistance to hydrogen embrittlement such that when a steel anode is galvanically coupled to a test C-ring of said superalloy and said C-ring is exposed to an aqueous test solution saturated with hydrogen sulfide containing 5% NaCl and 0.5% acetic acid, by weight, at room temperature and at atmospheric pressure, the test C-ring resists hydrogen embrittlement or cracking for more than 25 days when it is stressed to 100% of the transverse 0.2% offset yield strength.
Claim 20
Dependent Claim 148 words
A process for recovering oil and/or gas from subterranean surfaces under conditions of high stress and hydrogen sulfide environments which comprises using a tubular conduit for transporting said oil and/or gas from subterranean surfaces, wherein said tubular conduit comprises a cold-worked and age strengthened nickel and/or cobalt, chromium, molybdenum superalloy having less than 1 At% phosphorus in its grain boundaries, a tensile strength ranging from 150 to about 250 ksi and a resistance to hydrogen embrittlement such that when a steel anode is galvanically coupled to a test C-ring of said superalloy and said C-ring is exposed to an aqueous test solution saturated with hydrogen sulfide containing 5% NaCl and 0.5% acetic acid, by weight, at room temperature and at atmospheric pressure, the test C-ring resists hydrogen embrittlement or cracking for more than 25 days when it is stressed to 100% of the transverse 0.2% offset yield strength.
Claim 21
Dependent Claim 41 words
The process of claim 16 wherein said superalloy contains 12 to 25 wt. % chromium, from 10 to about 20 wt. % molybdenum, up to 10 wt. % iron, up to about 50 wt. % cobalt and the balance essentially nickel.
Claim 22
Dependent Claim 32 words
The process of claim 17 wherein the superalloy is further characterized as containing less than 0.003 wt. % phosphorus, less than 0.02 wt. % carbon and less than 0.08 wt. % silicon.
Claim 23
Dependent Claim 54 words
The process of claim 16 wherein said superalloy has the following chemical composition in weight percent: ______________________________________ Phosphorus <0.002 Chromium 14-17 Molybdenum 14-16 Iron 0-7 Cobalt 0-2.5 Aluminum 0-0.5 Columbium 0-4 Titanium, Zirconium or Hafnium 0-0.75 Tungsten 0-4 Manganese 0-1 Vanadium or Tantalum 0-0.4 Carbon 0-0.01 Silicon 0-0.03 Nickel and Incidental Impurities Balance ______________________________________

References Cited (Backward Citations)

US3356542A Cited
US3767385A Cited
US4080201A Cited
US4099992A Cited
US4129464A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-01-20 1984-07-21 1985-01-20 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-01-20 1988-07-21 1989-01-20 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-01-20 1992-07-21 1993-01-20 $7700.00 Window Closed / Lapsed

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