ATI Allvac® 6-4 Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal

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ATI Allvac® 6-4 Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal
Categories:	Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy
Material Notes:	Data provided by Allvac. Applications: Blades, discs, rings, airframe, fasteners, components. Vessels, cases, hubs, forgings. Standard, rotor/premium grades.
Key Words:	UNS R56400; AMS 4906, 4920, 4928, 4965, 4967; MIL-T-9047, -81556, Ti-6Al-4V; Ti-6-4; ASTM B 348, B 381, F 1472; Allvac, an Allegheny Teledyne Company
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Physical Properties	Original Value	Comments

Density	4.43 g/cc

Mechanical Properties	Original Value	Comments
Hardness, Brinell	304	Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop	330	Estimated from Rockwell C value.
Hardness, Rockwell C	32
Hardness, Vickers	318	Estimated from Rockwell C value.
Tensile Strength, Ultimate	931 MPa
Tensile Strength, Yield	862 MPa @Strain 0.2 %
Elongation at Break	15 %
Reduction of Area	30 %

Component Elements Properties	Original Value	Comments
Aluminum, Al	6.0 %
Carbon, C	<= 0.10 %
Hydrogen, H	<= 0.015 %
Iron, Fe	0.20 %
Nitrogen, N	0.030 %
Oxygen, O	<= 0.20 %
Titanium, Ti	89 %	as balance
Vanadium, V	4.0 %

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