Nimonic75 Material introduction
Nimonic75(UNS N06075\W.Nr2.4951\2.4630) The control of titanium and carbon is improved on the basis of Cr20Ni80 nickel chromium alloy. It was first applied to the turbine blade of the prototype Whittle jet engine in 1940s, and now it is mainly used for high-temperature parts with oxidation resistance but little load. It is used in gas turbine engineering and industrial heat treatment furnace components and heat treatment equipment. The alloy has good cold stamping and welding process properties.
Nimonic75 Chemical composition of alloy
Ni | Cr | Fe | Mn | C | Si | Ti |
more than | 18.0-21.0 | ≤5.0 | ≤1.0 | 0.08-0.15 | ≤1.0 | 0.2-0.6 |
Nimonic75 Physical and mechanical properties
density | melting point |
8.37g/cm³ | 1340-1380℃ |