Ti-8A1-1Mo-1V is a titanium alloy having excellent creep resistance and stress-rupture life. It is recommended for jet engine components operating up to 900 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness and creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ti-32. Producer or source: Titanium Metals Corporation of America.

chemical composition, creep resistance, elasticity, fracture toughness, heat treatability, high-temperature alloys, jet engine components, joinability, machinability, physical properties, shear strength, stress rupture, tensile properties, titanium-Aluminum-molybdenum-vanadium alloys, workability
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Copyright © ASM International® 1996
1996
ASM International
Topics
Creep fracture High-temperature alloys Alpha and near alpha titanium alloys Chemical composition Heat treatability Joinability Machinability Workability Creep resistance Elastic modulus Fracture toughness Shear strength Tensile properties Physical properties Thermal properties Aircraft turbine engine components
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