Alloy 80 (Nimonic 80A)
Alias
Nickel Alloy 80A
NC20TA (Fr)
BS HR 1, HR 201, HR 601
WL 2.4631 (De)
NiCr20TiAl (EU)
ASTM B637 N07080
Bs3076NA20
2.4952 (De)
ASME SB637 N0780
Chemistry
Element | Min | Max |
---|---|---|
Ti (Titanium) | 1.8 | 2.7 |
Al (Aluminium) | 1.0 | 1.8 |
Co (Cobalt) | 2% | |
Ni (Nickel) | BAL | |
C (Carbon) | 0.10% | |
Cr (Chromium) | 18 | 21% |
Si (Silicon) | 0.10% | |
Cu (Copper) | 0.2% | |
Fe (Iron) | 3.0% | |
Mn (Manganese) | 1.0% | |
B (Boron) | 0.008% | |
Zr(Ziciumon) | 0.15% | |
S (Sulphur) | 0.015% |
Mechanical Property | Min | Max |
---|---|---|
Ultimate Tensile Strength (ksi) | 145 | |
Yield Strength (ksi) | 90 | |
Elongation on 4D | 20 | |
Hardness (HV) | 300 |
Uses
Commonly used for Gas turbine components
Fasteners and components within the Nuclear Energy (Turbo Exhaust Systems), Motor Sport and aerospace Industry’s.
Properties
Good Mechanical Properties at Elevated Temperatures
Oxidation Resistant
Precipitation Hardenable
Creep Resistance
Disclaimer:
Information is given for illustrative purposes only. Tachart accepts no responsibility for the accuracy of the data contained within or the use of the data by any other party.
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