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TIMET 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Aged Billet/Bar per ASTM 4984

Category Metal , Nonferrous Metal , Titanium Alloy , Beta Titanium Alloy
Manufacturer TIMET
Trade Name
Port Shanghai port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF TIMET 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Aged Billet/Bar per ASTM 4984.pdf
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Material Notes:
High-Strength Forging Alloy.Industry Specifications: USA Aerospace: AMS 4984.Features: A readily forgeable alloy that offers excellent combinations of strength, ductility, fracture toughness and high cycle fatigue strength. Typically used for critical aircraft structures, such as landing gear.Typical heat treatment for this alloy: Solution heat treat: 28-56°C below beta transus for a minimum for 30 mins, then water quench. Aging heat treatment: 482-593°C for 8 hrs, air cool.Data provided by TIMET.
Physical Properties Metric English Comments
Density 4.65 g/cc
0.168 lb/in³
Typical
Mechanical Properties Metric English Comments
Tensile Strength, Ultimate 1260 MPa
183000 psi
Typical
Tensile Strength, Yield 1170 MPa

@Strain 0.200 %
170000 psi

@Strain 0.200 %
Typical
Elongation at Break 10 %
10 %
Typical
Modulus of Elasticity 107 GPa
15500 ksi
Typical
Compressive Yield Strength >= 1145 MPa
>= 166100 psi
Ultimate Bearing Strength >= 1613 MPa
>= 233900 psi
e/D = 1.5
>= 1958 MPa
>= 284000 psi
e/D = 2.0
Bearing Yield Strength >= 1565 MPa
>= 227000 psi
e/D = 1.5
>= 1800 MPa
>= 261000 psi
e/D = 2.0
Poissons Ratio 0.32
0.32
Fatigue Strength 945 MPa
137000 psi
Limit; test specifics not reported
490 MPa

@# of Cycles 1.00e+7
71100 psi

@# of Cycles 1.00e+7
Notched (Kt = 3); Stress Ratio = 0.1; Axial Loading;
910 MPa

@# of Cycles 1.00e+7
132000 psi

@# of Cycles 1.00e+7
Smooth (Kt = 1); Stress Ratio = 0.1; Axial Loading
Fracture Toughness >= 44.0 MPa-m½
>= 40.0 ksi-in½
ST then Aged 8 hrs
Shear Modulus 42.1 GPa
6110 ksi
Shear Strength >= 669 MPa
>= 97000 psi
Thermal Properties Metric English Comments
CTE, linear 9.70 µm/m-°C

@Temperature 20.0 °C
5.39 µin/in-°F

@Temperature 68.0 °F
Beta Transus 800 °C
1470 °F
Component Elements Properties Metric English Comments
Aluminum, Al 2.6 - 3.4 %
2.6 - 3.4 %
Carbon, C <= 0.050 %
<= 0.050 %
Hydrogen, H <= 0.015 %
<= 0.015 %
Iron, Fe 1.6 - 2.2 %
1.6 - 2.2 %
Nitrogen, N <= 0.050 %
<= 0.050 %
Oxygen, O <= 0.13 %
<= 0.13 %
Titanium, Ti 83 - 86.8 %
83 - 86.8 %
Calculated as remainder
Vanadium, V 9.0 - 11 %
9.0 - 11 %
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