NIMONIC alloy 115 is a nickel/chromium/cobalt based alloy developed as a vacuum processed creep resisting alloy for service at temperatures up to about 1010 C (1850 F) as a turbine blade material for aircraft turbines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on heat treating. Filing Code: Ni-104. Producer or source: INCO Alloys Limited. Originally published as Nimonic 115, August 1965, revised November 1991.

aircraft turbines, chemical composition, creep resistance, elasticity, heat treatability, NIMONIC ALLOY 115, physical properties, tensile properties, turbine blades
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Copyright © ASM International® 1996
1996
ASM International
Topics
Aircraft turbines Nickel-chromium alloys Chemical composition Heat treatability Creep resistance Elastic modulus Tensile properties Physical properties Thermal properties Turbine blades
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