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UNS N09901/Incoloy 901/2.4462/2.4975/Nimonic901/1.4898 Bar Ideal For High-Stress Applications In Sulphide Environments With Longevity And Durability
UNS N09901 (Incoloy 901) is a nickel-iron-chromium alloy known for its high strength, excellent corrosion resistance, and outstanding performance at elevated temperatures. Enhanced with titanium and aluminum, it provides superior creep and oxidation resistance, making it ideal for aerospace, gas turbines, and power generation applications. It maintains high tensile strength and fatigue resistance under extreme thermal conditions. Equivalent grades include 2.4462, 2.4975, Nimonic 901, and 1.4898. Typically supplied as bars, rods, and forgings, it is used in jet engine components, turbine discs, and structural applications. This alloy is also recognized for its good machinability and weldability, ensuring ease of fabrication in demanding environments.
Chemical Composition Wt.% | % | Ni | Cr | Fe | C | Mn | Si | Mo | Al | Ti | B |
Min | |||||||||||
Max | Bal | 12.5 | 34 | 0.05 | 0.24 | 0.12 | 6 | 0.15 | 2.7 | 0.015 |
Physical Constants | Density(g/cm³) | 8.14 | |||||
Melting Range(℃) | 1343–1400°C |
Minimum mechanical properties of alloy at room temperature | Typical mechanical properties | Tensile strength Rm N/mm² | Yield strength RP 0.2 N/mm² | Elongation A5 % | ||||
Solution treatment | 896 | 585 | 15 |
UNS N09901 (Incoloy 901) / 2.4462 / 2.4975 / Nimonic 901 / 1.4898 Bar – Key Features
Precipitation-hardened nickel-iron-chromium alloy with titanium and aluminum additions.
Excellent mechanical properties at elevated temperatures (up to ~650°C / 1200°F).
Outstanding creep strength under long-term stress conditions.
High resistance to thermal fatigue and stress rupture.
Excellent oxidation resistance at high temperatures.
Good corrosion resistance in harsh environments, including oxidation and sulfidation.
Can be formed, machined, and welded using conventional methods.
Requires appropriate heat treatment for optimal performance.
UNS N09901 (Incoloy 901) is a nickel-iron-chromium-based superalloy known for its high strength, corrosion resistance, and excellent oxidation resistance at elevated temperatures. It is commonly used in high-performance applications that require both strength and resistance to extreme conditions.
This alloy’s combination of strength, corrosion resistance, and high-temperature stability makes it ideal for demanding engineering applications, especially in aerospace and power generation. Let me know if you need specific details on mechanical properties or heat treatment processes!