Eklemeli Üretim ile Üretilen Ti6Al4V Parçaların Mekanik Özellikler Perspektifinden Deneysel Araştırması

This study aims to generate research data on basis of engineering evidences in terms validation tests for Additively Manufactured (AM) Ti4Al4V parts. It is known that Ti6Al4V alloy broadly used highly-engineered air vehicles and compliance with the aviation-grade specifications. For validation, test parts have been manufactured using EOSM290 DMLS (Direct Metal Laser Solidification) machine under argon inert gas. The raw powder has inspected before manufacturing process "better size brand" particle evaluation machine. composition determined as 90% Ti, 5,48% Al, 4,22% V, 0,369% C, 0,112% Fe, 0,0625% Sn, 0,00386% Nb, 0,0099% Cr accordance ASTM F1472 ATFM 2924 standards average diameter evaluated 30 µm. Since elongation, yield-strength tensile strength values are key indicators mechanical features stress-strain analysis was performed Analysis results indicate construction direction, heat treatment, turning finishing operations such sandblasting directly affect properties