EOS Titanium Ti64 Processed by DMSL on EOSINT M 270 and EOSINT M 280

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EOS Titanium Ti64 Processed by DMSL on EOSINT M 270 and EOSINT M 280
Categories:	Metal; 3D Printing/Additive Manufacturing Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy
Material Notes:	Description: Parts built in EOS Titanium Ti64 have a chemical composition corresponding to ISO 5832-3, ASTM F1472 and ASTM B348. This well-known light alloy is characterized by having excellent mechanical properties and corrosion resistance combined with low specific weight and biocompatibility. This material is ideal for many high-performance engineering applications, for example in aerospace and motor racing, and also for the production of biomedical implants (note: subject to fulfillment of statutory validation requirements where appropriate). Due to the layerwise building method, the parts have a certain anisotropy, which can be reduced or removed by appropriate heat treatment - see Technical Data for examples. Heat treated at 800 °C (1470 °F) for 4 hours Information provided by Proto3000
Key Words:	Direct Metal Laser Sintering, Ti-6-4; UNS R56400; ASTM Grade 5 titanium; Ti6Al4V; Titanium Ti-6Al-4V
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Physical Properties	Original Value	Comments

Density	4.41 g/cc

Mechanical Properties	Original Value	Comments
Hardness, Vickers	308 - 332	EN ISO 6507-1
Tensile Strength	980 - 1020 MPa	in vertical direction (Z), Heat treated; ISO 6892-1:2009 (B) Annex D
	1030 - 1070 MPa	in horizontal direction (XY), Heat treated; ISO 6892-1:2009 (B) Annex D
	1020 - 1120 MPa	in vertical direction (Z), As built; ISO 6892-1:2009 (B) Annex D
	1180 - 1280 MPa	in horizontal direction (XY), As built; ISO 6892-1:2009 (B) Annex D
Tensile Strength, Yield	980 - 1020 MPa @Strain 0.2 %	in horizontal direction (XY), Heat treated; ISO 6892-1:2009 (B) Annex D
	980 - 1020 MPa @Strain 0.2 %	in vertical direction (Z), Heat treated; ISO 6892-1:2009 (B) Annex D
	1010 - 1110 MPa @Strain 0.2 %	in horizontal direction (XY), As built; ISO 6892-1:2009 (B) Annex D
	1020 - 1120 MPa @Strain 0.2 %	in vertical direction (Z), As built; ISO 6892-1:2009 (B) Annex D
Elongation at Break	8.00 - 12.0 %	in horizontal direction (XY), As built; ISO 6892-1:2009 (B) Annex D
	8.00 - 14.0 %	in vertical direction (Z), As built; ISO 6892-1:2009 (B) Annex D
	13.0 - 15.0 %	in horizontal direction (XY), Heat treated; ISO 6892-1:2009 (B) Annex D
	14.0 - 16.0 %	in vertical direction (Z), Heat treated; ISO 6892-1:2009 (B) Annex D
Modulus of Elasticity	100 - 120 GPa	in horizontal direction (XY), As built; ISO 6892-1:2009 (B) Annex D
	100 - 120 GPa	in vertical direction (Z), As built; ISO 6892-1:2009 (B) Annex D
	104 - 124 GPa	in vertical direction (Z), Heat treated; ISO 6892-1:2009 (B) Annex D
	106 - 126 GPa	in horizontal direction (XY), Heat treated; ISO 6892-1:2009 (B) Annex D

Thermal Properties	Original Value	Comments
Maximum Service Temperature, Air	350 °C

Component Elements Properties	Original Value	Comments
Aluminum, Al	5.50 - 6.75 %
Titanium, Ti	88.75 - 91.0 %	Balance
Vanadium, V	3.50 - 4.50 %

Descriptive Properties
Material composition	< 2000 ppm	O
	<150 ppm	H
	<3000 ppm	Fe
	<500 ppm	N
	<800 ppm	C

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