REM-CRU A-70 is the grade of unalloyed titanium used where higher strength is required. It is specified for many moderately stressed aircraft parts. (Formerly known as RC-70.) This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-16. Producer or source: Rem-Cru Titanium Inc..

aircraft components, bearing strength, chemical composition, compressive strength, corrosion-resistant alloys, creep properties, elasticity, fracture toughness, heat treatability, high-temperature alloys, joinability, low-temperature alloys, machinability, physical properties, REM-CRU A-70, shear strength, tensile properties, workability
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Copyright © ASM International® 1996
1996
ASM International
Topics
Aircraft components Corrosion-resistant alloys High-temperature alloys Commercially pure titanium Chemical composition Heat treatability Joinability Machinability Workability Compressive strength Creep properties Elastic modulus Fracture toughness Shear strength Tensile properties Physical properties Thermal properties
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