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Superalloy Nimonic 80A is the alloy from series NIMONIC nickel-base superalloys that contain 20% of chromium . It is intended for use at elevated and high temperatures at which the creep process occurs significantly. Alloy 80A has good corrosion and oxidation resistance and high tensile and creep-rupture properties at temperatures to 815ºC (1500ºF). Vacuum refined versions are also available.
Superalloy Nimonic 80A Availability
Typical applications of Alloy 80A are for highly stressed components such as aircraft or marine gas based turbine rotors and as well exhaust valves and diesel engine combustion chambers
Alloy 80A Basic Chemical Composition
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Alloy 80A Basic Chemical Composition |
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|
Weight % |
Ni |
Cr |
Ti |
Al |
C |
Si |
Cu |
Fe |
Mn |
Co |
B |
Zr |
S |
|
Alloy 80A |
Bal |
18.0-21.0 |
1.8-2.7 |
1.0-1.8 |
0.10 max |
1.0 max |
0.2 max |
3.0 max |
1.0 max |
2.0 max |
0.008 max |
0.15 max |
0.015 max |
Superalloy Nimonic 80A Mechanical Properties
Material |
Condition |
Ultimate Tensile Strength ksi |
Yield Strength ksi |
Elongation on 4D (min) |
Hardness min |
|
Alloy 80A |
Solution Annealed & Precipatation Treated (aged) |
145 |
90 |
20 |
300 HV |
The key features of Alloy 80A make it perfect for use in across a variety of markets, including Aerospace, Oil and Gas and Motorsport. For more information on this alloy, or to get a quote fill in our online quote form or send email [email protected], we will reply you as soon as possible!
TEL : 0086-18317160019
E-mail : [email protected]
Address : No.230,1st Floor,Building No.1,No.221 Of Huashen Road,Free Trade Area Of Pudong New District,Shanghai China
