Method for heat treating iron-nickel-chromium alloy
Patent
·
OSTI ID:863663
- 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
Similar Records
Method for heat treating iron-nickel-chromium alloy
Method for heat treating iron-nickel-chromium alloy
Method for heat treating iron-nickel-chromium alloy
Patent
·
Tue Sep 30 00:00:00 EDT 1980
·
OSTI ID:863663
Method for heat treating iron-nickel-chromium alloy
Patent
·
Fri Jan 01 00:00:00 EST 1982
·
OSTI ID:863663
Method for heat treating iron-nickel-chromium alloy
Patent
·
Thu Apr 03 00:00:00 EST 1980
·
OSTI ID:863663
Related Subjects
method
heat
treating
iron-nickel-chromium
alloy
age-hardenable
obtain
morphology
gamma-double
prime
phase
enveloping
gamma-prime
consisting
essentially
40
50
nickel
14
chromium
niobium
75
silicon
titanium
aluminum
02
carbon
002
0015
boron
remain
substantially
iron
optimal
results
cold-worked
20
60
followed
heating
1050
degree
hour
air-cool
plus
800
hours
furnace
cool
625
held
12
iron-nickel-chromium alloy
consisting essentially
heat treating
remain substantially
gamma-double prime
alloy consisting
prime phase
chromium alloy
phase enveloping
treating iron-nickel-chromium
gamma-prime phase
age-hardenable iron-nickel-chromium
/148/
heat
treating
iron-nickel-chromium
alloy
age-hardenable
obtain
morphology
gamma-double
prime
phase
enveloping
gamma-prime
consisting
essentially
40
50
nickel
14
chromium
niobium
75
silicon
titanium
aluminum
02
carbon
002
0015
boron
remain
substantially
iron
optimal
results
cold-worked
20
60
followed
heating
1050
degree
hour
air-cool
plus
800
hours
furnace
cool
625
held
12
iron-nickel-chromium alloy
consisting essentially
heat treating
remain substantially
gamma-double prime
alloy consisting
prime phase
chromium alloy
phase enveloping
treating iron-nickel-chromium
gamma-prime phase
age-hardenable iron-nickel-chromium
/148/