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US4572738A Expired / Lapsed US ⏱️ 0.0 years remaining

Maraging superalloys and heat treatment processes

Assignee: United States Department of Energy
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Filing: 1982-04-21
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Granted: 1986-02-25
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Expires: 2002-04-21
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Abstract

Abstract Described herein are nickel-chromium-iron maraging, gamma prime strengthened superalloys containing about 18 to 25 weight percent nickel, about 4 to 8 weight percent chromium, gamma prime forming elements such as aluminum and/or titanium, and a solid solution strengthening element, such as molybdenum. After heat treatment, which includes at least one ausaging treatment and at least one maraging treatment, a microstructure containing gamma prime phase and decomposed Fe-Ni-Cr type martensite is produced.

Inventors

  • 👤 Michael K. Korenko
  • 👤 David S. Gelles
  • 👤 Larry E. Thomas

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 03:55
CPC Classifications
C; C22; C22C; C22C38/00; C22C38/18; C22C38/40; C22C38/50

Claims Analysis

Total Claims: 28
Claim 1
Independent Claim 92 words
An iron base composition maraging superalloy characterized by a gamma prime strengthened microstructure, wherein beta prime precipitates, and gamma prime precipitates are dispersed in a ferritic matrix; and said maraging superalloy consisting essentially of the following elements: approximately 18 to 25 weight percent Ni; approximately 4 to 8 weight percent Cr; approximately 0.5 to 1.5 weight percent of Mo, a solid solution strengthening agent; approximately 1.5 to 3.5 weight percent Ti; approximately 0.4 to 2.5 weight percent Al; and with Fe forming essentially the balance of said iron base composition maraging superalloy.
Claim 2
Dependent Claim 92 words
An iron base composition maraging superalloy characterized by a gamma prime strengthened microstructure, wherein beta prime precipitates, and gamma prime precipitates are dispersed in a ferritic matrix; and said maraging superalloy consisting essentially of the following elements: approximately 18 to 25 weight percent Ni; approximately 4 to 8 weight percent Cr; approximately 0.5 to 1.5 weight percent of Mo, a solid solution strengthening agent; approximately 1.5 to 3.5 weight percent Ti; approximately 0.4 to 2.5 weight percent Al; and with Fe forming essentially the balance of said iron base composition maraging superalloy.
Claim 3
Dependent Claim 19 words
The alloy according to claim 1 wherein the Mo is present at a level of about 1 weight percent.
Claim 4
Dependent Claim 34 words
The alloy according to claim 1 or 2 further consisting essentially of: up to about 0.4 weight percent Si; about 0.01 to 0.1 weight percent C; and about 0.005 to 0.11 weight percent Zr.
Claim 5
Dependent Claim 17 words
The alloy according to claim 1 further consisting essentially of about 0.1 to 0.5 weight percent Mn.
Claim 6
Dependent Claim 17 words
The alloy according to claim 3 further consisting essentially of about 0.1 to 0.5 weight percent Mn.
Claim 7
Dependent Claim 74 words
An iron base maraging superalloy consisting essentially of: about 18 to 25 weight percent nickel; about 4 to 8 weight percent chromium; a gamma prime forming agent selected from the group consisting of Al and Ti, alone or in combination with each other; about 0.5 to 1.5 weight percent molybdenum, a solid solution strengthening agent; with iron forming essentially the balance of said alloy; and a microstructure containing gamma prime phase dispersed in ferrite.
Claim 8
Dependent Claim 74 words
An iron base maraging superalloy consisting essentially of: about 18 to 25 weight percent nickel; about 4 to 8 weight percent chromium; a gamma prime forming agent selected from the group consisting of Al and Ti, alone or in combination with each other; about 0.5 to 1.5 weight percent molybdenum, a solid solution strengthening agent; with iron forming essentially the balance of said alloy; and a microstructure containing gamma prime phase dispersed in ferrite.
Claim 9
Dependent Claim 16 words
The alloy according to claim 6 wherein said microstructure further comprises an Fe-Ni-Cr type martensite phase.
Claim 10
Dependent Claim 16 words
The alloy according to claim 6 or 7 wherein said microstructure further comprises an austenite phase.
Claim 11
Dependent Claim 19 words
The alloy according to claim 6 wherein said microstructure further comprises a beta prime phase dispersed in said ferrite.
Claim 12
Dependent Claim 69 words
The maraging superalloy according to claim 1 consisting essentially of the following nominal composition: about 25 weight percent Ni; about 5.5 weight percent Cr; about 1.0 weight percent Mo; about 0.3 weight percent Si; about 0.2 weight percent Mn; about 0.05 weight percent Zr; about 3.3 weight percent Ti; about 1.7 weight percent Al; about 0.05 weight percent C; and with the balance being essentially iron except for impurities.
Claim 13
Dependent Claim 69 words
The maraging superalloy according to claim 1 consisting essentially of the following nominal composition: about 20 weight percent Ni; about 7.5 weight percent Cr; about 1.0 weight percent Mo; about 0.3 weight percent Si; about 0.2 weight percent Mn; about 0.05 weight percent Zr; about 3.3 weight percent Ti; about 1.7 weight percent Al; about 0.05 weight percent C; and with the balance being essentially iron except for impurities.
Claim 14
Dependent Claim 69 words
The maraging superalloy according to claim 1 consisting essentially of the following nominal composition: about 20 weight percent Ni; about 5.5 weight percent Cr; about 1.0 weight percent Mo; about 0.3 weight percent Si; about 0.2 weight percent Mn; about 0.05 weight percent Zr; about 3.3 weight percent Ti; about 1.7 weight percent Al; about 0.05 weight percent C; and with the balance being essentially iron except for impurities.
Claim 15
Dependent Claim 69 words
The maraging superalloy according to claim 1 consisting essentially of the following nominal composition: about 20 weight percent Ni; about 7.5 weight percent Cr; about 1.0 weight percent Mo; about 0.3 weight percent Si; about 0.2 weight percent Mn; about 0.05 weight percent Zr; about 3.3 weight percent Ti; about 1.7 weight percent Al; about 0.05 weight percent C; and with the balance being essentially iron except for impurities.
Claim 16
Dependent Claim 52 words
A maraging superalloy according to claim 1, 2, 6 or 7, heat treated in accordance with the following process, which comprises the steps of: austenitizing said alloy; ausaging said alloy; cooling said alloy below the M s temperature; ausaging and maraging said alloy simultaneously; cooling said alloy below the M s temperature.
Claim 17
Dependent Claim 23 words
The alloy treated in accordance with claim 14 wherein said ausaging steps comprise forming gamma prime phase in the austenite of said alloy.
Claim 18
Independent Claim 42 words
A method of heat treating an iron-nickel-chromium type maraging superalloy comprising the steps of: austenitizing said superalloy; ausaging said alloy; cooling said alloy below the M s temperature; ausaging and maraging said alloy simultaneously; cooling said alloy below the M s temperature.
Claim 19
Independent Claim 42 words
A method of heat treating an iron-nickel-chromium type maraging superalloy comprising the steps of: austenitizing said superalloy; ausaging said alloy; cooling said alloy below the M s temperature; ausaging and maraging said alloy simultaneously; cooling said alloy below the M s temperature.
Claim 20
Dependent Claim 32 words
The method according to claim 16 further comprising, after the second cooling step, the following steps: ausaging and maraging said alloy simultaneously; and then cooling said alloy below the M s temperature.
Claim 21
Dependent Claim 20 words
The method according to claim 16 wherein said cooling steps comprise cooling said alloy to a temperature below 0° C.
Claim 22
Dependent Claim 18 words
The method according to claim 17 wherein said cooling steps comprise cooling said alloy to approximately room temperature.
Claim 23
Independent Claim 24 words
The method according to claims 16 or 17 wherein said ausaging steps comprise forming a gamma prime phase in the austenite of said alloy.
Claim 24
Dependent Claim 21 words
The method according to claim 20 wherein said ausaging and said maraging steps are performed between about 650° and 800° C.
Claim 25
Dependent Claim 21 words
The method according to claim 16 or 17 wherein said initial ausaging step is performed between about 750° and 850° C.
Claim 26
Dependent Claim 20 words
The method according to claim 16 or 17 wherein said maraging steps are performed between about 650° and 800° C.
Claim 27
Dependent Claim 19 words
The method according to claim 23 wherein said initial ausaging step is performed between about 750° and 850° C.
Claim 28
Dependent Claim 18 words
The method according to claim 16 wherein said austenitizing step is performed at about 900° to 1200° C.

References Cited (Backward Citations)

US3199978A Cited
GB1104932A Cited
US4125260A Cited
US4049431A Cited
US4129462A Cited
US4172742A Cited
US4259126A Cited
US4359349A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-02-24 1989-08-26 1990-02-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-02-24 1993-08-26 1994-02-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-02-24 1997-08-26 1998-02-25 $7700.00 Window Closed / Lapsed

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