2021
DOI: 10.1016/j.ijfatigue.2020.105945
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Variable amplitude loading of additively manufactured Ti6Al4V subjected to surface post processes

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Cited by 15 publications
(10 citation statements)
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“…Post-processing applied on additive manufactured Ti-6Al-4V components show enormous potential in improvement of the alloy’s quality, e.g., by HIP process which leads to a homogenous microstructure and can reduce the porosity of titanium alloy parts produced by selective laser melting (SLM) [ 89 ]. In addition to internal defects and inhomogeneous microstructure, alloys fabricated by AM processes like laser powder bed fusion (L-PBF) and electron beam powder bed fusion (EB-PBF) can present a rough surface, where surface features can act as stress concentration factors that are responsible for strong reduction of fatigue strength with respect to conventionally manufactured materials [ 90 ]. Then, this aspect often requires additional surface post-processing stages on additive manufactured components, like surface machining, electropolishing, chemical polishing, and shot peening.…”
Section: Aircraft Engines and Crmsmentioning
confidence: 99%
See 1 more Smart Citation
“…Post-processing applied on additive manufactured Ti-6Al-4V components show enormous potential in improvement of the alloy’s quality, e.g., by HIP process which leads to a homogenous microstructure and can reduce the porosity of titanium alloy parts produced by selective laser melting (SLM) [ 89 ]. In addition to internal defects and inhomogeneous microstructure, alloys fabricated by AM processes like laser powder bed fusion (L-PBF) and electron beam powder bed fusion (EB-PBF) can present a rough surface, where surface features can act as stress concentration factors that are responsible for strong reduction of fatigue strength with respect to conventionally manufactured materials [ 90 ]. Then, this aspect often requires additional surface post-processing stages on additive manufactured components, like surface machining, electropolishing, chemical polishing, and shot peening.…”
Section: Aircraft Engines and Crmsmentioning
confidence: 99%
“…Then, this aspect often requires additional surface post-processing stages on additive manufactured components, like surface machining, electropolishing, chemical polishing, and shot peening. Different surface post-processing methods on L-PBF and EB-PBF Ti-6Al-4V alloys have been analyzed in a recent work by Kahlin et al [ 90 ] in order to reduce surface roughness and control the residual stresses in the material, so to increase the fatigue life of the alloy. A specific paragraph dedicated to laser shot peening (LSP) on Ti-based alloys is reported later.…”
Section: Aircraft Engines and Crmsmentioning
confidence: 99%
“…Consequently, it is widely adopted in aerospace and biomedical applications which predominantly are geometrically complex shapes. This material is responsible for higher tool wear and worse machined surface integrity [1][2][3]. Many cutting tool materials are in fact chemically reactive to the titanium alloys, which makes it difficult to machine using traditional methods.…”
Section: Introductionmentioning
confidence: 99%
“…The independent variables include the post-processing technique, the built orientation during fabrication, and the stress intensity factor. These three parameters significantly influence the FCGR and are independent of each other [3,11,[30][31][32][33]. Given these three independent variables, the ML models are used to estimate the FCGR of Ti-64 alloy.…”
Section: Introductionmentioning
confidence: 99%
“…They include geometrical defects, difficulty to control dimensional and form tolerances (Denti and Sola [23]); rough surfaces, thermal-induced distortion, shrinkage cavity, balling, stair-case effects, and dimensional inaccuracy (Kumar [24], Hamidi et al [25], Maleki et al [26], Tian et al [27]); metallurgical defects such as microcrack, thermal-induced microstructural change, grain size variation, preferred grain texture, porosity, and anisotropic mechanical properties (Teng et al [28], Maskery et al [29]); detrimental residual stress (Jawade et al [30]). Tiny defects can play a decisive role in the mechanical behavior of AM material, especially on the relationship between fatigue behavior and surface finishing (Azarniya et al [31], Kahlin et al [32]). Most of these limitations are primarily related to the process nature, which is very complex in terms of the thermo-mechanical phenomenon and limited available knowledge (Yadroitsev and Smurov [33], Zinovieva et al [34]).…”
Section: Introductionmentioning
confidence: 99%