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
Price	EMAIL US sales@lookpolymers.com

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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