Ti-6Al-2Sn-2Zr-2Mo-0.05Si alloy is used as heavy section forgings that require high strength, fracture toughness, and high modulus. It is used as forgings and sheet for air frames. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as fracture toughness and creep. It also includes information on high temperature performance as well as joining. Filing Code: TI-119. Producer or source: RMI Company.

air frames, bend strength, chemical composition, creep properties, elasticity, forgings, fracture toughness, high-temperature alloys, joinability, physical properties, sheets, tensile properties, titanium-aluminum-tin-zirconium-molybdenum-silicon alloys, thermal properties
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2001
ASM International
Topics
Air and spacecraft High-temperature alloys Forgings Sheets and strips Alpha-beta titanium alloys Chemical composition Joinability Bend strength Creep properties Elastic modulus Fracture toughness Tensile properties Physical properties Thermal properties
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