Selective laser melting of Ti6Al4V alloy: Effect of post-processing on fatigue life, residual stress, microstructure, microhardness and surface roughness


Önder S., Saklakoğlu N., Sever A.

MATERIALS CHARACTERIZATION, cilt.196, ss.1-12, 2023 (SCI-Expanded)

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 196
  • Basım Tarihi: 2023
  • Doi Numarası: 10.1016/j.matchar.2022.112571
  • Dergi Adı: MATERIALS CHARACTERIZATION
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, PASCAL, Aerospace Database, Chemical Abstracts Core, Chimica, Communication Abstracts, Compendex, INSPEC, Metadex, Civil Engineering Abstracts
  • Sayfa Sayıları: ss.1-12
  • Dokuz Eylül Üniversitesi Adresli: Hayır

Özet

In this study; turning, milling, heat treatment and shot peening (SP) post-process operations alone or in different

combinations were performed on Ti6Al4V specimens which were produced by selective laser melting (SLM); then

the effects of these operations on the fatigue life, residual stress, microstructure, microhardness and surface

roughness were investigated. SP processes were carried out in two different types, traditional and multiple, and it

was observed that the multiple SP process, which was carried out with the same almen intensity as traditional,

with a smaller ball diameter, was effective in reducing the surface roughness. As a result of the heat treatment, α

+ β transformation was observed in the microstructure. α phase was seen in both lamellar and globular forms.

Traditional SP and multiple SP processes provided a significant increase in microhardness values in the 0–250 μm

depth range. A significant decrease in the microhardness values of the heat-treated specimens was observed due

to the α + β transformation in the microstructure. Traditional SP and multiple SP processes enabled the residual

stress type to become compressive type in both the x-axis and the y-axis in the 0–150 μm depth which is a very

critical region for fatigue cracks despite the x-axis direction surface unmachined. Fatigue test were performed on

machined, multiple shot-peened and machined after heat-treated specimens. The best results in terms of fatigue

strength were obtained in the specimens that were heat-treated. It was observed that the most important cause of

fatigue crack initiation in multiple shot-peened specimens was an internal defect located deeper than 250 μm.

Fisheye formation was observed on fracture surfaces of some multiple shot-peened fatigue specimens.