NIMONIC 75
NIMONIC 75
List of Features
Nimonic 75
NIMONIC®alloy 75 (UNS N06075/W.Nr. 2.4951 &2.4630) is an 80/20 nickel-chromium alloy withcontrolled additions of titanium and carbon. Firstintroduced in the 1940s for turbine blades in theprototype Whittle jet engines, it is now mostly used forsheet applications calling for oxidation and scalingresistance coupled with medium strength at highoperating temperatures. It is still used in gas turbineengineering and also for industrial thermal processing,furnace components and heat-treatment equipment.
%Chemical Composition
| Ti | Mn | Si | Fe | Cu | Cr | C | Ni |
| 0.6 - 0.2 | (max) 1 | (max) 1 | (max) 5 | (max) 0.5 | 21 - 18 | 0.15 - 0.8 | Balance |
Density & Melting Rang
| Melting Range (Celsius) | Density |
| 1380 - 1340 | (g/cm) 8.37 |
Mechanical Properties
| Modulus of Elasticity (GPa) | % Elongation | Yield Strength (MPa) | Tensile Strength (MPa) |
| 206 | 42 | 275 | 750 |
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