Special Metals NIMONIC® Alloy 115

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Special Metals NIMONIC® Alloy 115
Categories:	Metal; Nonferrous Metal; Nickel Alloy; Superalloy
Material Notes:	A precipitation-hardenable nickel-chromium-cobalt alloy with an addition of molybdenum for solid-solution strengthening. It is similar to NIMONIC alloy 105 but has higher levels of aluminum and titanium for increased strengthening by precipitation hardening. The alloy has high strength and creep resistance at temperatures to about 1850°F (1010°C). Used for turbine blades in aircraft gas turbines. The standard product forms are round and extruded section. Data provided by the manufacturer, Special Metals.
Key Words:	BS HR4; Werkstoff Nr. 2.4636; AFNOR NCK 15 ATD; AECMA Pr EN 2196, 2197, Nickel-Chromium Alloy
Vendors:

Available Properties

Density
Tensile Strength, Ultimate, Precipitation Hardened prior to test
Tensile Strength, Ultimate
Tensile Strength, Yield, Precipitation Hardened. Value at room temperature
Tensile Strength, Yield, Precipitation Hardened prior to test
Elongation at Break, Precipitation Hardened
Elongation at Break, Precipitation Hardened prior to test.
Electrical Resistivity
CTE, linear
Specific Heat Capacity
Thermal Conductivity
Melting Point
Solidus
Liquidus
Aluminum, Al
Boron, B
Carbon, C
Chromium, Cr
Cobalt, Co
Copper, Cu
Iron, Fe
Manganese, Mn
Molybdenum, Mo
Nickel, Ni, As remainder
Silicon, Si
Sulfur, S
Titanium, Ti
Zirconium, Zr

Property Data

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Manufacturer Notes:
Special Metals (includes the former Inco Alloys International Inc.)

Category Notes
none

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