2020
DOI: 10.1016/j.ijfatigue.2020.105610
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Residual stress formation and stability in bearing steels due to fatigue induced retained austenite transformation

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Cited by 21 publications
(13 citation statements)
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“…Conversely, RA that is not adequately stable will undergo the martensitic transformation prematurely, and the maximum benefit is not achieved 24 . This was previously observed for torsional fatigue of AISI 8620 carburized steel 25 . Much of the RA had undergone the phase transformation within the first cycle of fatigue and did not cause significant change in the material condition.…”
Section: Resultssupporting
confidence: 72%
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“…Conversely, RA that is not adequately stable will undergo the martensitic transformation prematurely, and the maximum benefit is not achieved 24 . This was previously observed for torsional fatigue of AISI 8620 carburized steel 25 . Much of the RA had undergone the phase transformation within the first cycle of fatigue and did not cause significant change in the material condition.…”
Section: Resultssupporting
confidence: 72%
“…24 This was previously observed for torsional fatigue of AISI 8620 carburized steel. 25 Much of the RA had undergone the phase transformation within the first cycle of fatigue and did not cause significant change in The high RA specimens had a significant amount of RA within the microstructure; however, the RA remained stable throughout the entire test and the RCF performance was worse compared to the lower RA specimens. There is a trade-off between retaining austenite in the matrix and producing a fine martensitic microstructure.…”
Section: Resultsmentioning
confidence: 97%
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“…It has already been reported that the presence of WL can lead to early microcracking [ 14 ] and premature failures of components [ 15 ]. The presence of retained austenite [ 16 ] and a very steep stress and microstructure gradient [ 17 ] should also be considered as the main sources of near-surface failures.…”
Section: Introductionmentioning
confidence: 99%
“…。 この残留 γ は,疲労過程においても変態することが知ら れており,これまで低サイクル疲労域 [9][10][11] や高サイクル疲 労域 [12][13][14][15] を対象として幅広い研究が行われてきた。その結 果,残留 γ は,疲労負荷の 1 サイクル目でその多くが変態 し,2 サイクル目以降では変態量が少なく比較的安定にな ること 10,11,14) ,残留 γ の変態により試験片表面の圧縮残留 応力が増加すること [13][14][15]…”
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