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TIMET 8-1-1 Titanium Alloy (Ti-8Al-1Mo-1V); Annealed Sheet

Category Metal , Nonferrous Metal , Titanium Alloy , Alpha/Near Alpha Titanium Alloy
Manufacturer TIMET
Trade Name
Port Ningbo port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF TIMET 8-1-1 Titanium Alloy (Ti-8Al-1Mo-1V); Annealed Sheet.pdf
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Material Notes:
Industry Specifications: USA Aerospace: AMS 4915,4916. France: T-A8DV. Features: Designed for creep resistance up to 450°C, used primarily in engine applications such as forged compressor blades and disks. This alloy has a relatively high tensile modulus to density ratio compared to most commercial titanium alloys.Data provided by TIMET.
Physical Properties Metric English Comments
Density 4.36 g/cc
0.158 lb/in³
Typical
Mechanical Properties Metric English Comments
Tensile Strength, Ultimate 1020 MPa
148000 psi
Typical
Tensile Strength, Yield 930 MPa

@Strain 0.200 %
135000 psi

@Strain 0.200 %
Typical
Elongation at Break 13 %
13 %
Typical
Modulus of Elasticity 125 GPa
18100 ksi
Typical
Fatigue Strength 460 MPa
66700 psi
Limit; test specifics not reported
Bend Radius, Minimum 4.5 t

@Thickness 2.00 mm
4.5 t

@Thickness 0.0787 in
Typical; sheet
Thermal Properties Metric English Comments
Beta Transus 1040 °C
1900 °F
Component Elements Properties Metric English Comments
Aluminum, Al 8.0 %
8.0 %
Molybdenum, Mo 1.0 %
1.0 %
Titanium, Ti 90 %
90 %
Calculated as remainder
Vanadium, V 1.0 %
1.0 %
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