Method for heat treating iron-nickel-chromium alloy
A method for heat treating an age-hardenable iron-nickel-chromium alloy to obtain a bimodal distribution of gamma prime phase within a network of dislocations, the alloy consisting essentially of about 25% to 45% nickel, 10% to 16% chromium, 1.5% to 3% of an element selected from the group consisting of molybdenum and niobium, about 2% titanium, about 3% aluminum, and the remainder substantially all iron. To obtain optimum results, the alloy is heated to a temperature of 1025.degree. C. to 1075.degree. C. for 2-5 minutes, cold-worked about 20% to 60%, aged at a temperature of about 775.degree. C. for 8 hours followed by an air-cool, and then heated to a temperature in the range of 650.degree. C. to 700.degree. C. for 2 hours followed by an air-cool.
- Research Organization:
- Hanford Engineering Development Lab., Richland, WA (United States)
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- EY-76-C-14-2170
- Assignee:
- The United States of America as represented by the United States Department of Energy (Washington, DC)
- Patent Number(s):
- 4,359,349
- Application Number:
- 06/137049
- OSTI ID:
- 864397
- 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
10
1025
1075
16
2-5
20
25
45
60
650
700
775
age-hardenable
age-hardenable iron-nickel-chromium
aged
air-cool
alloy
alloy consisting
aluminum
bimodal
chromium
chromium alloy
cold-worked
consisting
consisting essentially
degree
dislocations
distribution
element
element selected
essentially
followed
gamma
gamma prime
heat
heat treating
heated
hours
iron
iron-nickel-chromium
iron-nickel-chromium alloy
method
minutes
molybdenum
network
nickel
niobium
obtain
optimum
phase
prime
prime phase
range
remainder
results
selected
substantially
temperature
titanium
treating
treating iron-nickel-chromium