Haynes alloy 75 is an 80 nickel-20 chromium alloy with both good oxidation resistance and good mechanical properties at high temperatures. It is amenable to all forms of fabrication and welding. A typical application for sheet metal is fabrications in gas turbine engines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming and heat treating. Filing Code: Ni-557. Producer or source: Haynes International Inc.

chemical composition, creep properties, elasticity, gas turbine engines, HAYNES ALLOY 75, heat treatability, high-temperature alloys, oxidation resistance, physical properties, tensile properties, workability, thermal properties
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Copyright © ASM International® 1999
1999
ASM International
Topics
Gas turbines High-temperature alloys Nickel-chromium alloys Chemical composition Oxidation resistance Heat treatability Workability Creep properties Elastic modulus Tensile properties Physical properties Thermal properties
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