Comparison between mechanical properties of specimens and tear down of representative airframe Ti-6Al-4V L-PBF part
Laser Power Bed Fusion (L-PBF) is one of the AM processes having the highest potential for aeronautic application of metallic end-use parts.
This work presents the mechanical properties and microstructural evaluation of Ti-6Al-4V parts by L-PBF process. It gives a detailed view on design for AM, topology optimization, manufacturing and testing specimens, and also the tear-down of a representative demonstrator part.
Test specimens and demonstrators’ evaluation was performed by tensile and fatigue tests, as well as microstructural characterization. In addition, non-destructive CT-scan was carried out.
For both specimens and demonstrators, following manufacturing sequence was applied: 3D printing of the specimens/parts by L-PBF, stress relief heat treatment, HIP, and milling of specimens and tear-down.
Lamelar microstructure was identified in the “as L-PBF” condition, whilst columnar microstructure was pictured after the heat treatment in this α + β titanium alloy.
The specimens were manufactured in three different building orientations: 0°, 45° and 90°. Regarding tensile tests, specimens fabricated at 45° presented higher values of tensile strength in comparison to specimens manufactured horizontal or vertical. Furthermore, fatigue test results showed that specimens manufactured at 45° exhibited slightly higher fatigue strength when compared to specimens manufactured at 90° and 0°.
Regarding the tear-down of the demonstrator, the tensile and fatigue tests results presented equivalent values to the L-PBF specimens.