SAE AMS5668B
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings, 72Ni 15.5Cr 7.0Fe 2.5Ti 1.0(Cb + Ta) 0.70Al, 2100°F (1149°C) Solution and Precipitation Heat Treated.
Standard:
AKA:
- AMS5668
- Revision: B
- 1950-06-01
- Historical. Access the latest revision: AMS5668J
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts, such as bolts, turbine blades, and turbine seals, requiring oxidation resistance and high strength at 1250 to 1500 degrees F (675 to 816 degrees C), but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5668J | 2007-05-15 | Latest | |
| AMS5668H | 1993-04-01 | Historical | |
| AMS5668G | 1991-10-01 | Historical | |
| AMS5668F | 1981-01-01 | Historical | |
| AMS5668E | 1972-11-01 | Historical | |
| AMS5668D | 1953-12-01 | Historical | |
| AMS5668C | 1951-06-01 | Historical | |
| AMS5668B | 1950-06-01 | Historical | |
| AMS5668A | 1949-03-01 | Historical | |
| AMS5668 | 1947-12-01 | Historical |
- SAE AMS 5668
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties