High strength nickel-chromium-iron austenitic alloy
Abstract
A solid solution strengthened Ni-Cr-Fe alloy capable of retaining its strength at high temperatures and consisting essentially of 42 to 48% nickel, 11 to 13% chromium, 2.6 to 3.4% niobium, 0.2 to 1.2% silicon, 0.5 to 1.5% vanadium, 2.6 to 3.4% molybdenum, 0.1 to 0.3% aluminum, 0.1 to 0.3% titanium, 0.02 to 0.05% carbon, 0.002 to 0.015% boron, up to 0.06 zirconium, and the balance iron. After solution annealing at 1038.degree. C. for one hour, the alloy, when heated to a temperature of 650.degree. C., has a 2% yield strength of 307 MPa, an ultimate tensile strength of 513 MPa and a rupture strength of as high as 400 MPa after 100 hours.
- Inventors:
-
- Ringwood, NJ
- Richland, WA
- Issue Date:
- Research Org.:
- Pacific Northwest National Laboratory (PNNL), Richland, WA (United States)
- OSTI Identifier:
- 863664
- Patent Number(s):
- 4225364
- Assignee:
- United States of America as represented by United States (Washington, DC)
- Patent Classifications (CPCs):
-
C - CHEMISTRY C22 - METALLURGY C22C - ALLOYS
Y - NEW / CROSS SECTIONAL TECHNOLOGIES Y10 - TECHNICAL SUBJECTS COVERED BY FORMER USPC Y10S - TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- DOE Contract Number:
- E(45-1)-2170
- Resource Type:
- Patent
- Country of Publication:
- United States
- Language:
- English
- Subject:
- strength; nickel-chromium-iron; austenitic; alloy; solid; solution; strengthened; ni-cr-fe; capable; retaining; temperatures; consisting; essentially; 42; 48; nickel; 11; 13; chromium; niobium; silicon; vanadium; molybdenum; aluminum; titanium; 02; 05; carbon; 002; 015; boron; 06; zirconium; balance; iron; annealing; 1038; degree; hour; heated; temperature; 650; yield; 307; mpa; ultimate; tensile; 513; rupture; 400; 100; hours; austenitic alloy; ultimate tensile; balance iron; consisting essentially; solid solution; tensile strength; yield strength; solution strengthened; alloy capable; /148/376/
Citation Formats
Gibson, Robert C, and Korenko, Michael K. High strength nickel-chromium-iron austenitic alloy. United States: N. p., 1980.
Web.
Gibson, Robert C, & Korenko, Michael K. High strength nickel-chromium-iron austenitic alloy. United States.
Gibson, Robert C, and Korenko, Michael K. Tue .
"High strength nickel-chromium-iron austenitic alloy". United States. https://www.osti.gov/servlets/purl/863664.
@article{osti_863664,
title = {High strength nickel-chromium-iron austenitic alloy},
author = {Gibson, Robert C and Korenko, Michael K},
abstractNote = {A solid solution strengthened Ni-Cr-Fe alloy capable of retaining its strength at high temperatures and consisting essentially of 42 to 48% nickel, 11 to 13% chromium, 2.6 to 3.4% niobium, 0.2 to 1.2% silicon, 0.5 to 1.5% vanadium, 2.6 to 3.4% molybdenum, 0.1 to 0.3% aluminum, 0.1 to 0.3% titanium, 0.02 to 0.05% carbon, 0.002 to 0.015% boron, up to 0.06 zirconium, and the balance iron. After solution annealing at 1038.degree. C. for one hour, the alloy, when heated to a temperature of 650.degree. C., has a 2% yield strength of 307 MPa, an ultimate tensile strength of 513 MPa and a rupture strength of as high as 400 MPa after 100 hours.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Jan 01 00:00:00 EST 1980},
month = {Tue Jan 01 00:00:00 EST 1980}
}