2022
DOI: 10.1016/j.ijfatigue.2022.106862
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Interior initiation and early growth of very high cycle fatigue crack in an additively manufactured Ti-alloy

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Cited by 28 publications
(9 citation statements)
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“…In addition, the selection of stress amplitude and load period of variable amplitude fatigue test is also based on the relevant literature (Chi et al, 2022).…”
Section: Materials and Experimental Proceduresmentioning
confidence: 99%
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“…In addition, the selection of stress amplitude and load period of variable amplitude fatigue test is also based on the relevant literature (Chi et al, 2022).…”
Section: Materials and Experimental Proceduresmentioning
confidence: 99%
“…Most of the AM parts have gas pore and lack of fusion defects (Yang et al, 2020;Liu et al, 2020;Chi et al, 2022), which have an important influence on the fatigue performance of the material. Gas pore and lack of fusion defects can also be seen in this study, as shown in Figures 2 and 3.…”
Section: Microstructure and Defect Characteristicsmentioning
confidence: 99%
“…For the fatigue failure caused by interior inclusions, the matrix structure diagram around the inclusion cluster before cyclic loading is drawn, Figure 8b. Secondly, under the combined action of cyclic normal stress, surface residual stress and the mismatch of elastic modulus between inclusions and matrix, grain refinement occurs around the inclusion cluster due to local stress concentration [41]. Subsequently, under the cyclic loading of variable amplitude loading, the grain begins to slip and dislocation accumulation around the inclusion cluster, which makes the grain rearrange to the new grain boundary and further forms a fine grain layer composed of sub grains.…”
Section: Analysis Of Failure Mechanism For Interior Fatigue Failurementioning
confidence: 99%
“…Sun et al 10 identified that surface or internal microstructural defects dominate the failure of SLM Ti-6Al-4V in VHCF regime and observed fish-eye pattern (FiE) and fine granular area (FGA) features surrounding the crack source, with crack growth rates of about 10 À13 -10 À11 m/ cycle inside FGA. 11 Electron backscatter diffraction was adopted to observe the characteristics of the FGA. The FGA SIF amplitude ΔK FGA was calculated with the help of the above mentioned ffiffiffiffiffiffiffiffiffi area p parameter estimation model and found to correspond to the crack growth threshold of conventionally processed (CP) Ti-6Al-4V alloy in ultra-high vacuum environment.…”
Section: Effect Of Internal Defectsmentioning
confidence: 99%
“…Sun et al 10 identified that surface or internal microstructural defects dominate the failure of SLM Ti‐6Al‐4V in VHCF regime and observed fish‐eye pattern (FiE) and fine granular area (FGA) features surrounding the crack source, with crack growth rates of about 10 −13 –10 −11 m/cycle inside FGA 11 . Electron backscatter diffraction was adopted to observe the characteristics of the FGA.…”
Section: Fatigue Characteristics Of Am Metalsmentioning
confidence: 99%