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Elmet Technologies

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Titanium Ti-6Al-2Sn-2Zr-2Mo-2Cr-.25Si Alpha-Beta Processed + Aged
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy

Material Notes: Annealed 8 hr at 950°C followed by 8 hr age at 540°C. High strength and fracture toughness. Lower density, deep-hardenable. Welding is not recommended.

Applications: Aerospace - thick-section components

Forms typically available: Billet, bar and plate

3 other heat treatments of this alloy are in MatWeb.

Key Words: Ti-6-22-22-S
Vendors: Visit metalmen for your metals needs. Products include special chemistry, tight tolerances, custom tempers, odd dimensions/forms, and small quantities. Phone 1-800-767-9494.

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Physical PropertiesOriginal ValueComments
Density 4.65 g/cc
 
Mechanical PropertiesOriginal ValueComments
Tensile Strength, Ultimate 1120 MPa
Tensile Strength, Yield 1010 MPa
Elongation at Break 14 %
Tensile Modulus 108 GPa
Compressive Yield Strength 1050 MPa
Poissons Ratio 0.33
Fatigue Strength 280 MPa
@# of Cycles 1.00e+7
Kt (stress concentration factor) = 3.0
 480 MPa
@# of Cycles 1.00e+7
Unnotched
Shear Modulus 46.0 GPa
Shear Strength 720 MPaUltimate shear strength
Charpy Impact 20.0 JV-notch
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.000160 ohm-cm
 
Thermal PropertiesOriginal ValueComments
CTE, linear 9.20 µm/m-°C
@Temperature 20.0 - 315 °C
average; annealed
 9.40 µm/m-°C
@Temperature 20.0 - 93.0 °C
Specific Heat Capacity 0.500 J/g-°CEstimated from similar materials
Thermal Conductivity 7.80 W/m-K
Melting Point <= 1650 °CEstimated from similar materials
Liquidus 1650 °CEstimated from similar materials
Beta Transus 960 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 6.0 %
Carbon, C <= 0.040 %
Chromium, Cr 2.0 %
Iron, Fe <= 0.25 %
Molybdenum, Mo 2.0 %
Nitrogen, N <= 0.030 %
Oxygen, O <= 0.14 %
Silicon, Si 0.25 %
Tin, Sn 2.0 %
Titanium, Ti 86 %
Zirconium, Zr 2.0 %

References for this datasheet.

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MTP225 / 14232

Ensinger PEI

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