Maraging superalloys and heat treatment processes
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:
-
- Wexford, PA
- W. Richland, WA
- Richland, WA
- Issue Date:
- Research Org.:
- Hanford Engineering Development Lab., Richland, WA (United States)
- OSTI Identifier:
- 865775
- Patent Number(s):
- 4572738
- Assignee:
- United States of America as represented by United States (Washington, DC)
- Patent Classifications (CPCs):
-
C - CHEMISTRY C22 - METALLURGY C22C - ALLOYS
- DOE Contract Number:
- EY-76-C-14-2170
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- maraging; superalloys; heat; treatment; processes; described; nickel-chromium-iron; gamma; prime; strengthened; containing; 18; 25; weight; percent; nickel; chromium; forming; elements; aluminum; titanium; solid; solution; strengthening; element; molybdenum; ausaging; microstructure; phase; decomposed; fe-ni-cr; type; martensite; produced; gamma prime; alloys containing; weight percent; heat treatment; solid solution; treatment process; alloys contain; percent nickel; structure containing; prime phase; percent chromium; treatment processes; forming element; /420/148/
Citation Formats
Korenko, Michael K, Gelles, David S, and Thomas, Larry E. Maraging superalloys and heat treatment processes. United States: N. p., 1986.
Web.
Korenko, Michael K, Gelles, David S, & Thomas, Larry E. Maraging superalloys and heat treatment processes. United States.
Korenko, Michael K, Gelles, David S, and Thomas, Larry E. Wed .
"Maraging superalloys and heat treatment processes". United States. https://www.osti.gov/servlets/purl/865775.
@article{osti_865775,
title = {Maraging superalloys and heat treatment processes},
author = {Korenko, Michael K and Gelles, David S and Thomas, Larry E},
abstractNote = {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.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Wed Jan 01 00:00:00 EST 1986},
month = {Wed Jan 01 00:00:00 EST 1986}
}
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