ATI Allvac® 3-2.5 Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal

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ATI Allvac® 3-2.5 Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal
Categories:	Metal; Nonferrous Metal; Titanium Alloy; Alpha/Near Alpha Titanium Alloy
Material Notes:	Data provided by Allvac. Applications: Excellent cold formability, 20-50% higher tensile properties than CP titanium grades. Primarily used in aircraft hydraulic systems.
Key Words:	UNS R56320; AMS 4943, 4944; MIL-T-9046, -9047. ASTM B 265, 337, 338, 348, 381, Ti-3Al-2.5V; Half 6-4; Ti-3-2.5; Allvac, an Allegheny Teledyne Company
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Physical Properties	Metric	English	Comments

Density	4.48 g/cc	0.162 lb/in³

Mechanical Properties	Metric	English	Comments
Hardness, Brinell	256	256	Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop	278	278	Estimated from Rockwell C value.
Hardness, Rockwell C	24	24
Hardness, Vickers	269	269	Estimated from Rockwell C value.
Tensile Strength, Ultimate	690 MPa	100000 psi
Tensile Strength, Yield	586 MPa @Strain 0.2 %	85000 psi @Strain 0.2 %
Elongation at Break	15 %	15 %
Reduction of Area	25 %	25 %

Component Elements Properties	Metric	English	Comments
Aluminum, Al	3.0 %	3.0 %
Carbon, C	<= 0.050 %	<= 0.050 %
Hydrogen, H	<= 0.015 %	<= 0.015 %
Iron, Fe	0.13 %	0.13 %
Nitrogen, N	0.010 %	0.010 %
Oxygen, O	0.10 %	0.10 %
Titanium, Ti	94 %	94 %	as balance
Vanadium, V	2.5 %	2.5 %

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