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Rulon Bearings

TIMET TIMETAL® 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Aged Billet/Bar per ASTM 4984
Categories: Metal; Nonferrous Metal; Titanium Alloy; Beta Titanium Alloy

Material Notes: High-Strength Forging Alloy. Mechanical property data reported per ASTM 4984 after solution treatment and aging 900°-950°F (482°-510°C) then air cool.

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, actuators, flap tracks, and rotor heads.

Typical heat treatment for this alloy: Solution heat treat: 28-56°C below beta transus for a minimum for 30 mins, then water quench. Age then air cool.

Data provided by TIMET.

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Physical PropertiesMetricEnglishComments
Density 4.65 g/cc0.168 lb/in³Typical
 
Mechanical PropertiesMetricEnglishComments
Tensile Strength, Ultimate 1260 MPa183000 psiTypical
Tensile Strength, Yield 1170 MPa
@Strain 0.2 %
170000 psi
@Strain 0.2 %
Typical
Elongation at Break 10 %10 %Typical
Modulus of Elasticity 107 GPa15500 ksiTypical
Tensile Modulus 109.6 GPa15900 ksi
 95.0 GPa
@Temperature 316 °C
13800 ksi
@Temperature 601 °F
Compressive Yield Strength >= 1145 MPa>= 166100 psi
Compressive Modulus 112.3 GPa16290 ksi
Ultimate Bearing Strength >= 1613 MPa>= 233900 psie/D = 1.5
 >= 1958 MPa>= 284000 psie/D = 2.0
Bearing Yield Strength >= 1565 MPa>= 227000 psie/D = 1.5
 >= 1800 MPa>= 261000 psie/D = 2.0
Poissons Ratio 0.320.32
Fatigue Strength 945 MPa137000 psiLimit; 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-in½ST then Aged 8 hrs
Shear Modulus 42.1 GPa6110 ksi
Shear Strength >= 669 MPa>= 97000 psi
 
Thermal PropertiesMetricEnglishComments
CTE, linear 9.70 µm/m-°C
@Temperature 20.0 °C
5.39 µin/in-°F
@Temperature 68.0 °F
Beta Transus 800 °C1470 °F
 
Component Elements PropertiesMetricEnglishComments
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 %
Other, each <= 0.10 %<= 0.10 %
Other, total <= 0.13 %<= 0.13 %
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 %

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to view all the property values for this datasheet as they were originally entered into MatWeb.

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NTIME1023 / 19279

Master Bond adhesives

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