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ATI Allvac® 6-6-2 Titanium Alloy, Heat Treatment: 718°C (1325°F) Anneal

Category Metal , Nonferrous Metal , Titanium Alloy , Alpha/Beta Titanium Alloy
Manufacturer ATI Allvac
Trade Name
Port Ningbo port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF ATI Allvac® 6-6-2 Titanium Alloy, Heat Treatment: 718°C (1325°F) Anneal.pdf
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Material Notes:
Data provided by Allvac.Applications: Airframes, jet engines, rocket engine cases, nuclear reactor components, ordnance components.
Physical Properties Metric English Comments
Density 4.54 g/cc
0.164 lb/in³
Mechanical Properties Metric English Comments
Hardness, Brinell 326
326
Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop 354
354
Estimated from Rockwell C value.
Hardness, Rockwell C 35
35
Hardness, Vickers 341
341
Estimated from Rockwell C value.
Tensile Strength, Ultimate 966 MPa
140000 psi
Tensile Strength, Yield 897 MPa
130000 psi
0.2% Offset
Elongation at Break 15 %
15 %
Reduction of Area 35 %
35 %
Component Elements Properties Metric English Comments
Aluminum, Al 5.5 %
5.5 %
Carbon, C 0.050 %
0.050 %
Copper, Cu 0.50 %
0.50 %
Hydrogen, H <= 0.015 %
<= 0.015 %
Iron, Fe 0.50 %
0.50 %
Nitrogen, N 0.020 %
0.020 %
Oxygen, O 0.20 %
0.20 %
Tin, Sn 2.0 %
2.0 %
Titanium, Ti 86 %
86 %
as balance
Vanadium, V 5.5 %
5.5 %
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