Method for heat treating iron-nickel-chromium alloy
- Richland, WA
A method for heat treating an age-hardenable iron-nickel-chromium alloy to obtain a morphology of the gamma-double prime phase enveloping the gamma-prime phase, the alloy consisting essentially of about 40 to 50% nickel, 7.5 to 14% chromium, 1.5 to 4% niobium, 0.3 to 0.75% silicon, 1 to 3% titanium, 0.1 to 0.5% aluminum, 0.02 to 1% carbon, 0.002 to 0.0015% boron and the remain substantially all iron. To obtain optimal results, the alloy is cold-worked 20 to 60% followed by heating at 1050.degree. C. for 1/2 hour with an air-cool plus heating at 800.degree. C. for 2 hours with a furnace cool to 625.degree. C. The alloy is then held at 625.degree. C. for 12 hours, followed by an air-cool.
- Research Organization:
- Pacific Northwest National Laboratory (PNNL), Richland, WA (United States)
- DOE Contract Number:
- E(45-1)-2170
- Assignee:
- United States of America as represented by United States (Washington, DC)
- Patent Number(s):
- US 4225363
- OSTI ID:
- 863663
- Country of Publication:
- United States
- Language:
- English
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Method for heat treating iron-nickel-chromium alloy
Method for heat treating iron-nickel-chromium alloy
Related Subjects
0015
002
02
1050
12
14
20
40
50
60
625
75
800
age-hardenable
age-hardenable iron-nickel-chromium
air-cool
alloy
alloy consisting
aluminum
boron
carbon
chromium
chromium alloy
cold-worked
consisting
consisting essentially
cool
degree
enveloping
essentially
followed
furnace
gamma-double
gamma-double prime
gamma-prime
gamma-prime phase
heat
heat treating
heating
held
hour
hours
iron
iron-nickel-chromium
iron-nickel-chromium alloy
method
morphology
nickel
niobium
obtain
optimal
phase
phase enveloping
plus
prime
prime phase
remain
remain substantially
results
silicon
substantially
titanium
treating
treating iron-nickel-chromium