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Nimonic 115/2.4636 Sheet/Bar/Pipe
Nimonic115 nickel-based alloy with high strength and high temperature is widely used in aviation, aerospace and industry. Its excellent oxidation resistance and high temperature strength characteristics are suitable for high temperature components. Good weldability, mechanical and physical properties make it an ideal material for high temperature applications.
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Product Details

Super alloys can be strengthened by precipitation hardening, solid-solution hardening and work hardening methods. These alloys can function under high mechanical stress and high temperatures and also in places that require high surface stability.Nimonic 115 is a nickel-chromium-cobalt-molybdenum alloy that can be precipitation-hardened. It has and suitable for oxidation resistance and high temperature strength.


Equivalent Grades

Alloy NameTrade NameUNS No.British SpecsAmerican SpecsGerman SpecsFrench Specs
Alloy 115Nimonic 115
BS HR4
WS 2.4636AFNOR NCK 15ATD

Nimonic 115 chemical composition

ElementContent (%)
Nickel, Ni54
Chromium, Cr14.0-16.0
Cobalt, Co13.0-15.5
Aluminum, Al4.50-5.50
Molybdenum, Mo3.0-5.0
Titanium, Ti3.50-4.50
Iron, Fe1.0
Manganese, Mn1.0
Silicon, Si1.0
Copper, Cu0.20
Zirconium, Zr0.15
Carbon, C0.12-0.20
Sulfur, S0.015
Boron, B0.010-0.025

Nimonic 115 physical properties

PropertiesMetricImperial
Density7.85 g/cm³0.284 lb/in³
Melting point1304°C2380°F

Nimonic 115 mechanical properties

PropertiesMetricImperial
Tensile strength (precipitation hardened, value at room temperature)1300 MPa189000 psi
Yield strength (precipitation hardened, value at room temperature, @strain 0.200%)850 MPa123000 psi
Elongation at break (precipitation hardened)25.00%25.00%


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