Journal
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING
Volume 859, Issue -, Pages -Publisher
ELSEVIER SCIENCE SA
DOI: 10.1016/j.msea.2022.144232
Keywords
Additive manufacturing; Selective laser melting (SLM); Fatigue behaviour; Titanium alloys; Microstructural characterization
Categories
Funding
- Science Foundation Ireland (SFI)
- Stryker
- SFI Research Centre for Advanced Manufacturing
- Advanced Metallic Systems Centre for Doctorial Training (AMS - CDT)
Ask authors/readers for more resources
This study evaluated the fatigue behavior of additively manufactured Ti-6Al-4V via Laser Powder Bed Fusion in three different conditions: as-built, heat-treated, and hot isostatically pressed (HIP'ed). The results indicate that fatigue failure in as-built and heat-treated conditions was mainly driven by early-stage crack growth, while crack initiation was the main controlling factor for fatigue deformation of HIP'ed samples. Furthermore, a strong correlation between impact energy and fatigue limit was observed. The findings were based on detailed microstructural and crystallographic characterization, as well as mechanical testing. The as-built and heat-treated conditions exhibited poor fatigue response compared to HIP'ed, which can be attributed to lower levels of porosity.
The fatigue behaviour of additively manufactured Ti-6Al-4V via Laser Powder Bed Fusion (L-PBF) was evaluated in three different conditions, as-built, heat-treated and hot isostatically pressed (HIP'ed). Fractography analysis interpreted together with the S-N curves indicates that fatigue failure in as-built and heat-treated conditions where <0.2% porosity was present, was mainly driven by early-stage crack growth. However, crack initiation was determined to be the main controlling factor for fatigue deformation of HIP'ed samples. Moreover, a strong correlation between the impact energy and fatigue limit was found. The findings were based on detailed microstructural and crystallographic characterization, as well as mechanical testing. The as-built and heat-treated conditions exhibited poor fatigue response in comparison to HIP'ed which is largely attributed to the lower levels of porosity identified. Even though similar levels of porosity are present in as-built and heat-treated samples, improvement in fatigue limit was determined in the heat-treated condition due to phase transformation and microstructural coarsening leading to reduction in micro-strain.
Authors
I am an author on this paper
Click your name to claim this paper and add it to your profile.
Reviews
Recommended
No Data Available