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ATI Allvac® 6-2-4-2 Titanium Alloy, Heat Treatment: 982°C (1800°F) + Age

Category Metal , Nonferrous Metal , Titanium Alloy , Alpha/Near Alpha Titanium Alloy
Manufacturer ATI Allvac
Trade Name
Port Shanghai port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF ATI Allvac® 6-2-4-2 Titanium Alloy, Heat Treatment: 982°C (1800°F) + Age.pdf
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Material Notes:
Data provided by Allvac.Applications: High-temp jet engines. Blades, discs, spacers, seals. High performance automotive valves. Standard, rotor/premium grades.
Physical Properties Metric English Comments
Density 4.54 g/cc
0.164 lb/in³
Mechanical Properties Metric English Comments
Hardness, Brinell 318
318
Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop 346
346
Estimated from Rockwell C value.
Hardness, Rockwell C 34
34
Hardness, Vickers 333
333
Estimated from Rockwell C value.
Tensile Strength, Ultimate 1035 MPa
150100 psi
Tensile Strength, Yield 966 MPa

@Strain 0.200 %
140000 psi

@Strain 0.200 %
Elongation at Break 15 %
15 %
Reduction of Area 30 %
30 %
Component Elements Properties Metric English Comments
Aluminum, Al 6.0 %
6.0 %
Carbon, C <= 0.10 %
<= 0.10 %
Hydrogen, H <= 0.015 %
<= 0.015 %
Iron, Fe 0.050 %
0.050 %
Molybdenum, Mo 2.0 %
2.0 %
Nitrogen, N 0.040 %
0.040 %
Oxygen, O 0.20 %
0.20 %
Tin, Sn 2.0 %
2.0 %
Titanium, Ti 86 %
86 %
as balance
Zirconium, Zr 4.0 %
4.0 %
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