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UNS N06625 high temperature alloy steel

UNS N06625 high temperature alloy steel has the characteristics of uniform structure, low density, high thermal conductivity and low thermal expansion coefficient. Therefore, it is widely used to manufacture various aircraft engine parts, turbine impellers, compressor rotor blades and other components; it can also be used to manufacture steam turbine rotors and gas turbine rotor blades.

UNS N06625 steel is a new type of high-temperature alloy. This material is mainly used in aerospace engines and is characterized by high strength and good high-temperature resistance.

UNS N06625 belongs to the nickel-based alloy (Ni-C) series of high-temperature alloys. It is strengthened by adding copper or silicon to the nickel-based iron-chromium aluminum alloy; the density of this material is only 7.24g/cm3. It is much lighter than ordinary high-temperature structural steel; at the same time, its tensile strength is about 930-1200MPa, and its torsional strength reaches more than 1000MPa.

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